Text

Vol I,Rev 0 to Cchvac Concern Resolution Task - Duct Evaluation of 4316 Sys Series
	ML20210E320
Person / Time
Site:	Fermi
Issue date:	06/11/1996
From:	Chiou C, Yu H; WISCONSIN PUBLIC SERVICE CORP.
To:	;
Shared Package
ML20134M106	List: ML20210E320;
References
	DC-5773, DC-5773-R, DC-5773-R00, NUDOCS 9611250099
	Download: ML20210E320 (125)
	v • d • e

{{#Wiki_filter:_ _ _ _ _ ' to 3 NRC 96 0127 Page! ENCLOSURE 4 DC 5773 Vol i Rev 0 Systems 43161,4316-6 & 4316-7 Duct Evaluation (includes Attachnents A F) '9611250099 961100 PDR ADOCK 05000341 P PDR

m mmiurasaw 4 DBim CALCt'LAllON COVER SilEET et.os 60 me%.wg w+A PageI ofary 3 - ~ lk'thb:l;NL PA R T I: DESIGN C4!.CUl.4 T10N !DENTIf!C1 T10N Al Design Calculassun Number "I DC-5773 I iG f ,i C) Res nion D) I'15 Sumber l E) QA Lesel ,Y O T4102 l l l Non O MI 111M O ASME Code Classification p(NA G) Certification Required ()Yes [ N No [ !!) Lead Disciphne Hochanical/ Civil lI) incorporation Code p. K J) Title CCHVAC Concern P.esolution Task - Duct Evaluation of mA Myat.ca 5cr_ica __ K) Design Change Documents Incorpormied INumber and Resisioni y Hone M fM

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Design Calculationis Super *.eded eNurnber and Hesisioni y Hone 2 @L 4

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? 40% '*4~, M w.G j ;-f ~ M) Restsion Summary m.$. Original inuuc. x. 20$'LJ..' Effective section property calculations and evaluation of 5'J. overall duct stressen in duct / support systemn for stringn 4316-1, 4316-2, 4316-3, 4316-6 and 4316-7 are performed. Modification to one vyc fitting is required and implemented. $h This calculation in part of the basis for EDP-28147. j i{ hd PART.': PREPARA T10N. ret 1EH*. AND APPROl'AL A) Prepared us C H uA/C+- YI CHION I ib [1l 6 4' N - I'

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Duct Evaluation of 4310 an *16230.502 ?' tusJtCT _Syst ern S e r i e s s J.,;., i ^ 1

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3 Y'- {c,. IABLE OE.COMrFMT.S i i + n Sheet I? s Y J. 1 { Design Calcuhtion Cover Sheet n .2. ( - Table of Contents o ' +. D Purpose e t b Scope ,,e m ~7 Y Methcdology c II h Results and Conclusions A. t $b, '} 12-Refenners 91 >,y

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~ 4 m SN..P Calculations 4f ![:,N; l (A) Effecttive Section Properties for Rectangular Ducts 13 '9 yd (ii) Overall Duct Stress Evaluations for Hectangular Docts 38 ft ~ (C) Evaluation of ACME leek 1.ongitudinal Seams for Round Ducts 71t 4 en..M u o@ M kg Atuchments ~^ { fg'. Summary of incam Element leads for System 43141 9 1. s Attachment A: 12c !$ 1: Summary of Ikam Element leads for System 43162 8 j W 1 E [' Attachment C: Summary of iteam Element Loads for System 43163 5 ' _,2 e n' ; s?w ij Attachment D: Summary of Ikam Element lads for System 43166 l 4j y % ;,36 ' t._ Attachment E Summary Of 11eam Element Loads for System 43167 21 ) m T 3 N(hk, h[ Attachment F: Duct Database 3 9 I $m< ,m. g .m. 'h g a

t s..swi. 4+n c.=ca.Atm ut *o s,av cran, e, casco my 5, Ni COM T ON QQ e = 0 n SHEET b$/6 $ 4 .t f PMo>tCT, DECO E ERfq,,J - c[Jp'/g_ ___ f Duct Evaluation of 4319 FM 3 (* ll pig mig 1 i Sut.ftC1 Systern Series Jo 76230.507 I% p HIRPOSE 2 ,f a j' [ Fermi 2 Control Center lleating, Ventilation and Air Conditioning (CCIIVAC), and other affected safety related seismic category I duct, duct supports and anchorages were revalidated to demonstrate their structural adequacy under the effects of applicable loads and their combinations in accordance with the requirements and acceptance criteria contained in Design Criteria No: Fermi DC 762301, 'CCllVAC Duct and Duct Support Qualification *, (Ref.1). This revalidation effort is a result of the commitments made by DECO to the USNRC staff, to provide resolution of all the issues on the CCilVAC structural upects identified by the staff it, their letter, dated December 7,1995 (Ref. 2) and during subsequent rnectings held on February 7,1996 and March 1,1996 in 11cthesda, hfD. The overall revalidation program, referred to as the *CCllVAC Concem Resolution Task" is an l integrated effort which includes recalculation of system operating (Po) and masimum (P ) pressures for duct evaluations; determination of pertinent seismic re>ponse on duct, duct supports and anchorages; structural adequacy evaluation of duct and duct transition segments (Tees, Wyes, elbows, etc.); evaluation of support and anchorage structural adequacy; and documentation of the structural ^ adequacy in calculations and, where required, the identification of hardware modifications, which Duet and duct are issued for implementation in Engineering Design Package (EDP) No. 28147. ) support systems shown to require modification (s) are reevaluated with the mcdified configurations to demonstrate structural adequacy of the modified system. Pressure calculations are contained in calculations DC 5714 and DC 5758, (Ref. 3 & 4). De results 4 of structural evaluation of duct, supports and anchorages are summarized in a series of calculations as listed telow. Generally the results of duct and duct support system evaluations are arranged based o on the drawing series where they appear, to facilitate correlation. a }h.

NON RlGID DUCT AND DUCI' SUPPORT _SYSTDIS; h(

y a 7 ,w. )I I STRING ANALYSES, SUPPORT AND ANCli.QRAGE EVALUATIONS ( .A AA DC 5762 Generic Evaluations '2 DC 5763 2268 System Series R ,x 02 DC 5764 2848 System Series a b DC 5765 2S49 and 4126 System Series y 4 fb DC 2766 2850 System Series C 'c DC-S767 4316 System Series Mk 56 i M Q EFFECTIVE SECTION CALCULATIONS AND DUCT EVALUATIONS 4 My A o , _ Q1 h: Doct Skin Stress Evaluations Under internal Pressure t W :' DC 5768 i J.W DC 5770 2268 and 2848 System Series Q a _p, t Q&

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C 'a" <W 0 SHEET WM i i x th0MCrJLC,n,,,,f[ M,_j - CQg } L "M. E, f* I part oatt Duct I'valuatson of 4330 3c,,,,,7 6 D o. 5 02 ? $UBJrCr Sybtem Series T;n ~ i .w ,s #j4 p= l dy> WQEE q y f j 'nds calculation contains the pr<xess, methodology and results of rectangular duct i calculations ad the duct structural evaluations for duct (rectangular and round) in s system series. Duct strings of 4316 system f.eries consist of string analysis s 43163,43166, and 43147. String analysis systems referred to above correspond t ) r-and seismic dynamic tesponse analysis strings documented in Calculation DC 5767 } structural adequacy of round duct has been established in Calculation DC 5768 (Ref. qualificat}on of AChf E Icd longitudinal scatm for rouno duct is provided in this l Duct string system 43166 has one (1) round duct site of 17.50' diameters as we f b rectangular duct sire 16*x16*. Round duct wenion propedies are included in C (Ref. 6), and the structural adequacy of round duct has b l evaluations of rectangular duct (including the calculations of effectu e sect;on pro (Ref. 5). in this calculation bawd on the string analysis results contained in Attachment D o There are two (2) wyc sections (Q-344 and Q-348) in string analysis system 431 ) t configuration of wyc section Q344 was utilized in duct panel stress evaluation internal pressure of 14' v.ater gage. The efore, the acceptability nf wyc section 4 m the as built configuration.

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Duct string system 43147 has Iwo ( ) round duct sites (17.50* and 18.00* diameters k (1) rectangular duct site 16*x16*. Round duct section properties are included 5767 (Ref. 6). The structural adequacy of round duct has evaluations of rectangular duct (including the calculations of effective section prop (Ref. 5). in this calculation based on the string analysis results contained in Attachment E of .n .G y Ea ]^ Duct string systems 4316-1,4316 2 and 43143 have re W ~ i of effective section properties and overall stress evaluations for rectangular duct based analysis results contained in Attachments A through C of this calculation. There j sections (Q318 and Q 309) in string analysis system 43161. Evaluation results of ' 318 st.bject to a maximum intemal pressure of 14' water gage have concluded t ili f tion Q318 is based _ adding stiffener)is required (Ref,5). Therefore, the acceptab ty o wye sec ( n M . on the modified configuration. y n p y^ +;dl M p p g M j.n n, pup-3 jy a_

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S t, L m.u vm 0 SHEET g f X ') sWutCf ffCo FEQil, ? - CR VAC 'g Duct Evaluatten or m c y g.) o8 Da p tC1 Systorn Sarles so 76230.502 oi,. ?' 1hc duct stress calculations performed in this calculation establish the state of longitudiant stresses due to internal pressure, dead load, and seismic loads (global and local panel vibration). The calculated longitudinal stresses are compared to stress allowables per design criteria (Ref.1) for acceptability, in addition, the ct!culated longitudinal stresses are also compared to the longitudinal stress margins calculated in Calculation DC 5768 (Ref. 5) for acceptability. f Mg e,

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0 Naiwe'F***n of e 7 4 'S GENERAL. [f/C COMPUT ATION WW '.444 n=a 0 it O W %% - w > SHEET X AGRC1.EF:Co FTIZ W _CL'!W U 7 N t,an o4u P Duct Evaluaticn of.; ) 1 t. Jo 7(,230.50? System Serles _ m.- l t.usstCT 7 ? P MrruoDolitGy Duet strings of 4316 system series include five (5 n design criteria (Ref.1) and documented in this calculation: Feview duct attributes such as duct size and duct configuration. 1. Update duct database for string analysis system to include duct s duct configurations. Duct database is included in Attachment F of this c 2. Calculate effective !.ection properties for each rectangular duct sire utiliain FORTRAN program ' DUCT 24'. The output of DUCT 24 program is inte 3. formatted as regular hand calculation sheets for checking purpose. Effective section properties for OBE and SSE caws are calculated per i The duct orientation is shown in Fig, 3.4 3 and Fig. 3.4-4. ) For each duct size, the following inputs are required for DUCT 24 to comp g_ D.7 effective section properties: Width of duct (W) y lleight of duct (11) e p Gy Duct sheet bare metal thickness (t) ,; ) g

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Effective length factors (Ky and Kr) y ^" x J;: Duct lengths (Ly and L ), i.e. spans between supports Ky, Ly, Kz and Lz values used in EQ (3.4.17) are deter RU l ( of string analysis model. directions and for duct elbows or duct segme P unection, Maximum Ly and Lz lengths are determined for each duct sire, ,I Calculate duct longitudinal stresses due to: ) x c f, ~. Internal pressure per EQ (3.6.1 1) and EQ. (3.6.12) 4. ", t s- -) p li. g4 he masimum (accid:nt) pressure considered for duct in -string analysis W systems of 43161,43166,4316 7 and a small straight portion.of 6 =e g -11 .sq 26

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ll oate part Duct Evaluaticri of 4316 r.utut C t System Serleta Jo 76730.507 h k g g 1 1 14' water gege, and the operating (normal) pretrure is r.egligible (Ref. 3 & 4). nerefore, only SSE load case is evaluated when comparing the calculated e longitudinal stresses to longitudinal stress margins. The maximum and operating pressures considered for duct in string analysis system 43163 and the remaining large portion of 4316 2 are 6.5* w2ter gage, llowever, a operating pressure of 2.5" water gage is used to specifically evaluate the structural adequacy of one (1) wye section Q300 in string analysis system 43162. Since the SSE load case have higher stress allowables than OllE load case and same order of magnitude of stress levels as OBE load case, only OllE load case is evaluated when comparing the calculated longitudinal stresses to longitudinal stress margins. h,h Table 3.6.1 1 is used for correlation factors Cl and C2. To compare with the - F longitudinal stress margins, correlation factors for elbows are used for duct tecs to facilitate the process. When various duct configurations occurs for same duct sire, envelope values of C1 and C2 are used conservatively for all ) duct configurations to simplify calculations. [ local panel vibration per EQ, (3.6.13) and EQ. (3.6.1-4) ~ U l.5 x maximum peak g values (envelope of 3 carthquale directions and 3 building floor elevations) at 4% and 7% damping response spectra curves are used for ODE and SSE, respectively. \\ Unit weight of duct panel is calculated to include the weight of duct metal and (* weight of insulation. He weight of duct metal is conservatively calculated i based on a steel density of 0.2906 lb/cu.in (larger than 0.2835 lb/cu.in) and the coated metal thickness per Part 6 of AISC manual (Ref. 8). The weight l of insulation is calculated based on a density of 6.0 lb/cu.ft and a thickness of 1.5*, per Deco Specification 307132, " Insulation of Piping and Mechanical Equipment" (Ref. 7). j;g i g 1 w M a' Dead load and global seismic load obtained from string analysis. g h he maximum and minimum beam element loads (forces) at Beam Ends A and . B for dead load, OBE and SSE are determined by STARMAP computer program by enveloping beam elements with same bearn properties. ( lb- -) a .," M V h;w' W 4 w i Mp$, 4 P R

O. w w.en U 9. I-W GENERAL W 9 i $4 COMPUTATION ' ~.t = 0 i l b/g);(, b [ SHEET y ,) Pneutet DECO FER M.' - CCHVAC 9 " 77 o.n o.n i l Duct Evaluation of 431s-~~ ~ exc, systern series so 76?30.507 e a The following forces are used in stress calculations and are dettnnined by enveloping the maximum and minimum forces at Beam Ends A and D: l i Axial Force (Fx) .l Shear 2 Force (Fy) y f Shear 3 Force (Fr) ty . y, ,a. Torque (61x) } l hfoment2 (hly) i l l .%, t hioment3 (hiz) m. j j in the enveloping process for dead load, absolute values are used. l y' l .. ' J 5. Calculate duct suess allowables per Section 3.5.4. i ( '[' Shear stress allowables are computed per EQ. (3.5 1) and EQ. (3.5 2) for rectangular i and round duct longitedinal seam evaluations. t Yield strength of 33 Lsi for duct sheet metal is used to calculate axial and bending allowables. .: s 6. Calculate total duct longitudinal stresses per load combinations. Evaluate duct structural adequacy based on total duct longitudinal stresses. 7. i, Duct is considered to behase as a beam globally. j .~ l :- Calculate in plane shear stress due to dead load + global seismic load. 8. y

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^;o Evaluate duct in-plane shear stress vs shear stress allowables for longitudinal seams 9. and identify cases, if any, wherethat the calculated shear stress is greater than 1.0 ksi.

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[ Update duct database to include duct internal pressure, longtudinal stresses and she 4 l 10. stresses for cach duct sire. Verify that total duct longitudinal stresses are less than the longitudinal stress margins i-11. determined in Calculation DC 5768 (Ref. 5). Specifically, the total duct longitudinal stress in compression is compared to the sum of longitudinal stress margin for The total duct y compression and calculated longitudinal stress per EQ. (3.6.12). 7 1 4.

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+ ,i i. b, ~, longitudinal stress in tension is compared to the sum of longitudinal s y? ~ tension and calculated longitudinal stresses per EQ. (3.6.1 1). For thot.e cases with shear stress from dead load + global seismic load gre l.0 ksi, longitudinal stress margins are either re calculated or jusitified in t calculation. i 'e E l c hJ 12. Document results. 9 '. f h# l 'l ', l A LOTUS 123 program *DUCSTitS* is developed and used to accomp!!sh the wor ltem Nos. 4 through 9 and 11. The output of DUCSTitS h intentionally formatted as regu ,I> l l :. calculation sheets for checking purpse. (. v. I p +'., l l,- i p. i il t {b i V.. i.., L ,,) y N ^;. L i [ ". y 4 'j (f d;, at -- ?.[ - e ,e ~ 1 j i s 4 1 $4 if.,+ i 96 n.. by ? -;j t

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,, y Duct Evaluation of 4316 Jo 76230.502 Systern Series SvaJECT v RESULTS AND CONCLUSIONS !,( Calculation (A) contains the effective section properties calculations for rectangular duct in duct ) strings of 4316 system series. Rese effective section properties are used in the corresponding strin analyr.s contained in Calculation DC 5767. ' Calculation (B) contains the overall duct stress evaluations for rectangular duct in duct strings of 4316 system series. Rased on the results. it is concluded that the duct are structurally adequate meet the requirements and acceptance criteria el Design Criteria No. Fermi DC-762301. In addition, Attachment F contains the calculated longitudinal stresses at duct corners (LSc and LSt) membrane stresses per EQ and corresponding LSMc and LSMt (lengitudinal stress margins + It is nn'ed that all straight duct segment stresses are within the stress. (3.6.1 1) & EQ (3.6.12)). margins. One wye (Q318) required a modification as shown in EDP 28147 and calculation DC- $768. L A Calculation (C) contains the structural adequacy evaluation of the ACME Icek longitudinal seams for ~~ -) round duct. De calculated OBE shear stress is 403.9 psi which is less than the ODE shear stress allowable of 5775.9 psi. u e a4 r, (a -

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i 5'* " O- ., 7 Duct Evaluatten at 4];t 8 oars oan I SU6 JECT System Serios 40 76?30.502 7 i ]} [ RffERLNCES / 1 1. CCl!VAC Duct and Duct Support Qualification, Fermi Design Criteria No FERMI DC-762301, Revision 0, Dated 3/15/96. L* 2. NRC letter dated Decemtier 7,1995, ' Fermi 2 Control Center ifcating, Ventilation and Air Conditioning (CCllVAC) System, including Safety Evaluation on the Same Subject *, 6 3. DECO Calculation DC 5744. Revision 0. n 4 DECO Calculation DC 5758, Revision 0. i l' I' 5. DECO Calculation DC 5768. Revision 0. u. (f 6. DECO Calculation DC 5767, Revision 0. 3, I 7. DECO Specification 3071 32,

Insulation of Piping and Mechanical Equipment', Revision li, Dated 12/13/95.

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l we, .., w e we 0 e i4 fpe WEET 1 enoster Deco FFRMI.2 '(IHVAC "" N" N's DA's l Duct Evaluattin of 4316 ~ Jn 76230.502 I sussect _S.ys t em Se r i e s li j. j i A. Effective Section Properties Calculations for l l W..A9 --4 . Rectangular Ducts 3. J A.01 String Analysin No. 4316 - 1 4. i 1 DUCT NODE NODE LENGTH Ky KZ SIZE I J Ly LZ 14X14 300 285 3'-11' 3'-11' 2.0 2.0 i' p' 285 280 28-2" 28-2" 2.0 2.0 7 200 260 8'-0" 8'-0" 2.0 2.0 260 250 6'-6" 6'-6" 1.0 1.0 I 250 240 8'-6" 88-6" 1.0 1.0 )' ) 240 230 o'-6" 6'-6" 1.0 1.0 B ' .r - 230 220 5'-5" 5'-5" 1.0 2.0 }lS 220 210 3'-7" '3'-7" ~ 1. 0 * * ' 2. 0 ~ >$ -O 4 210 200 l'-0" 7'-5" 1.0 1.0 1. ib* 200 190 6'-5" 7'-5" 1.0 1.0 / 190 175 7'-0" 8'-4" 1.0 1.0 i 175 170 1'-4" B'-4" 1.0 1.0 170 150 8'-0" a'-0" 1.0 1.0 a 63 150 140 7'-0" 7'-0" 1.0 1.0 j. to 140 135 l'-5" l'-5" 1.0 2.0 i 13b 120 5'-7" 5'-7" 1.0 2.0 l 9 120 100 9'-2" 9'-2" 1.0 1.0 i f 200 335 6'-5" 4'-6" 1.0 2.0 i 4 j [ 335 320 6'-5" 3'-3" 1.0 2.0 ) J 320 310 7'-0" J'-10" 1.0 2.0 g P 310 175 7'-0" 4'-6" 1.0 2.0 l - 1 hu Uso Ly = 96" Ky = 2.0 i 96" KZ = 2.0 LZ G: -- q j = y fry ( y y.4.. Ry ,y INPUT FILE = DUCIN.009 t p/ iN ~# c OUTPUT FILE = DUCOUT.009 1 W.. l' i N '.u s t js ' 9 5". g

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w '~ --~ U GENfhAL. C[5 3 7,.. y " O *""' coMPuiATioN gjg 0 a's I /Th 4 b .,.#As 4-SHEET x enostc? DECO. FERMI 2 .g2QC M " O cars para Duct Evaluaticn of 4314 Suss(Cf System Series so 76230.502 m EFFECT. PROPERTIES FOR DUCT SIZE W(IN)XH(IN) : 14.0X14.0 DUCT SHEET BARE METAL TilICKNESS = .0478 IN TULL SECTION AREA, Aq = 2*(W+11)*T = 2.6768 IN**2 FULL SECTION MOMENT OF INERTIA ABOUT Y - AXIS Iyy = TXH**3/6 + TXWXH**2/2 = 87.4421 IN**4 FULL SECTION MOMENT OF INERTI A ABOUT Z - AXIS: Izz = TXW**3/6 + TXilXW**2/2 = 87.4421 IN**4 FULL SECTION RADIUS OF GYRATION ABOUT Y - AXIS (Iyy/Ag)**0.5 = 5.7155 IN Ryy =SECTION RADIUS OF GYRATION ABOUT Z - AXIS FULL Rzz = (Izz/Ag)**0.5 = S.7155 IN 1 YIELDING STRESS = .3300E+02 KSI MODULUS OF E!ASTICITY = .2900E405 KSI 1 ALPHAc PER EQ. (3.4.1-2c) FOR llEIGitT(!!) OF DUCT: ALPHAc = 0. 2's6 + 0.328X(ll/T)X(Fy/E)**0.5 = 3.4966 DETAc PER EQ. (3.4.1-2c) FOR WIDTil(W) OF DUCT 6 DETAc = 0.256 + 0.328X(W/T)X(Fy/E)**0.5 = 3.4966 y (A) CALCULATE Ag FOR AXIAL TENSION ODE & SSE 3-FULL SECTION AREA, Ag=2X(W+11)XT= 2.6768 IN**2 e (B) CALCUIATE Acx FOR AXI AL COMPRESSION 4 - 2.0000 EFFECTIVE LENGT!! FACTOR (Y) = 96.0000 IN 3-UNDRACED LENGTH DETWEEN SUPTS (Y) = pJ. KL/Ry = 33.5930 2.0000 EFFECTIVE LENGTil FACTOR (Z) = m 96.0000 IN UNBRACED LENGTil BETkEEN SUPTS (Z) = .KQ KL/Rz = 33.5930 33.5930 k,f KL/Rmax = MAX (KL/Ry,KL/Rz) = Fe = TT**2XE/(KL/Rmax)**2 = 253.6293 KSI

s.i Fe.GT.Fy/2, Fn=FyX(1.0-Fy/(4.XFe))=

31.9266 KSI - OddYdh* 1:ib N-Fa = Fn/1.92 = 16.6284 ALPHAi=1.052/SQRT(4.0)X(H/T)X(Fa/E)**0.5= 3.6890 BETAi =1. 052 / SQRT ( 4. 0) X (W/T) X (Fa / E) *

0. 5=

3.6890 ALPHA 1.GT.ALPHAc, RH0i=(0.41+0.59X(Fy/Fa)**0.5-0.22/ ALPHA 1)/ALPHAi .3203 = v He = RJioiXH = 4.4839 IN o B ETA i.CT. B ETAc. M RHoi=(0.41+0.59X(Ty/Fa)**0.5-0.22/DETAi)/BETAi ,f = .3203 -t" .s ( I-c w@ ] (* ( mlp. ', n. t e h. h)h; se:-

~~_ m cou* e coyoos

s. = wo e. n.,

wcur.ca w40 Y DC~5

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' con [A$on ~"" m o e 6D t l* * * " * * * * " ' SHEET 4 6 x ~ E -o* u o* rs nostc7. Deco TERMI 2 - q_CU~V Ac ~ t> Duct Evaluation ot 4316 76230.502 eo usstcf_ System Series t; !.+

We a RilOiXW =

4.4839 IN [., .8573 IN642 y. EFFECTIVE AREA, Acx_OBE = f ~ SSE CASE [ 24.9426 4.5181 Fa = 1.5X(ra/1.92) = ALPHAl=1. 05 2 /SQRT 4. 0) X (H/T)X (Ta / 4.5181 P ) RilOi= ( 0. 414 0. 59X ( Ty/ Ta) *

0. 5-0. 2 2 / ALPilAi) / ALPIIAi ALPilA1.GT. ALPHAc, K

.2302 = 3.2224 IN lio = RitolXil = Ril0i= (0. 41 + 0. 59X ( Ty/ Ta) *

0. 5-0. 2 2 / DETAi) / BETAi BETAi.GT.BETAc,

.2302 = 3.2224 IN We = PJIOiXW = e .6161 IN**2 p EFFECTIVE AREA, Aox_SSE = M. EFTECTIVE AXIAL AREA FOR ANALYSIS:1.6465 IN**2 Ac ANALYSIS = .114 3 E-01 Pr*

2 M.

~ = g,( CALCULATE Iey, FOR BENDIND MOMENT Hy (C) ~ OBE CASE 'x; m 19.8000 1.6434 ALPilAi=1. 052 / SQRT ( 2 4. 0) X (ll/T) X ( ra / E) *

4.0255 Pa = 0.6*Fy =

b BETAi =1.052/SQRT(

0. 67 3.GT. ALPilA1. LE. ALPilAc,(1.358 - 0.461/ALPilAi)/ALPHAl

,,P Ril0i = .6556 4.5895 IN O = 0.511oy = 0.5 X Ritoi X 11 = WY> R110i= ( 0. 41+ 0. 59X ( Ty/ Pa) *

0. 5-0. 2 2 / DETA1) / DETA1 DETA1.GT.BETAc, k

.2775 1.9424 IN = 0.5Wey = 0.5 X Ril01 X W = ? 39.1661 IN**4 R FOR Hy, Iey'OBE = 5.5952 IN**3 x, Sey ODE = -i c4 %a. ' J ;6 - SSE CASE T O-29.7000 2.0127 Q*' Fa = 0.9XTy = QRT(24.0)X(ll/T)X Fa/E)**0.5= 4.9302 ~! O ALPilAi=1.052/S

4. 0) X (W/T) X Fa / E) *

0. 5=

if BETAi =1.052/SQRT( ~ 0.673.GT. ALPilA1.LE. ALPilAc, p 1U101 = (1. 358 - 0.461/ ALPilA1) / ALPHAi + R-O .5609 O = 2 F. .9 .g. wr ~ 7 m,p + = .1 s u;. b

I au j J r acuuro, m.o >==w.,,,. oc.5;73 U[C M o N h,k.*1,y' GENEHAL 0 e ' 3Sy09 boost m 7 QK z. m COMPUTATION _wi on 4 omw .3 m %~.+ SHEET x ~6Iii" YI- ~ oatt M ~~~ 5'* " 2 - ccwAc enoxct Eco FERMIEvaluation of go s 76230 502 4316 Duct CututCy ptem Series 3.9263 IN p 0.5 X R1101 X 11 = TA1) /BETAi O. 51 toy =T. DETAc, Ritol=(0.41+0.59X(Ty/Fa)**0.5-0.22/BE BETA 1.G l' .2003 1.4018 IN 0.5Woy = 0.5 X R1101 X W = = 33.1428 IN**4 FOR My, Iey'SSE 4.7347 IH**3 = Soy ~SSE 28.1714 IN**4 = loy~AN ALYSIS = .1359E-02 FT**4 = FOR DENDIND MOMENT Mz CALCUI. ATE 102 K (D) W - OBE CASE 4.0255 r 19.80004.0)X(ll/T)X(Fa/E)**0,5= 1.6434 Fa = 0. 6

Fy =/ SQRT (

/E)**0.5= ALPilAl=1.052BETAi =1. 052 / SQRT( 24. 0) X (W /T) X (F NAi)/ALPNAi i ALPilAi.GT. ALPNAc,Rlloi=(0.41+0 59X(Fy/Fa)**0.5-0.22/ ALP .2775 1.9424 IN

0. 5 X RJfo i X 11

= 0. 5110 2

0. 67 3 07 BFTAi.LE.DETAc,Ritol = (1.358 - 0.461/DETA1)/B l

65$6 4.5895 IN ' (i r

0. 5Wo z = 0. 5 X Ritoi X W = 661 IN *

4

= if 39.1 TOR Mz, 10 2'OBE = 5.5952 IN**3 Soz OBE = - SSE CASE 4 4.9302 29.7000 2.0127 Fa = 0.9XFy =/ SQRT( 4.0) X(ll/T) X(Fa/E) *

0. 5=)**0.5=

i ALPilAi=1.052BRTAi =1 052/SQRT(24.0)X(W ?: ALPilAi.GT. ALPilAc,Ritoi=(0.4140.59X(Fy/Fa)**0.5-0.22 A 4 .2003 1 4018 IN h O. 5110 z = 0. 5 X Rlloi X 11 = = 0.673.GT.BINA1.LE.DETAc, Ai) /BETAi Ritoi = (1.358 - 0.461/DET .5609 3.9263 IN 0.5Woz = 0.5 X Ritoi X W = 33.1428 IN**4 = FOR Hz, Ioz SSE 4.7347 INa*3 = ,s, Soz'SSE 28 1714 IN**4

- - 4ALYSIS =

.1359E-02 FT**4 fj ' a = m <4 102 =

1 DE & SSE CALCULATE Ay FOR Y-DIRECTION SilEAR O u

'N ' 1.3384 IN**2 y, (E) SilEAR AREA, Ay = 2XWXT = .9294E-02 FT**2 '? r = , g'aqi. =q , gs .fjM' n. xM'Q h '}lfih -y

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veo o a r 4fp W SHEET x PROJECT _ DECO. U,M1 2 - CCHV AC "" $7 C# 1 ^) - cart oats t Duct Evatuation of 4 J I t> sveatc, System Series ao 76230.502 5 f fm '_I \\ g q. (F) CALCULATE At FOR Z-DIRECTION SHEAR OBE & SSL v. n SHEAR AREA, Az = 2XHXT = 1,,3384 IN**2 .9294E-02 FT**2 = x

s..

(G) CALCULATE Ixx FOR TORSIONAL M0HENT Mx OBE & SSE FOR Mx, Ixx ANALYSIS = 131.1632 IN**4 .6325E-02 FT**4 ~ = .h?< z. j 2 g e 1 4lp 4 ?

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C + i&[ ..Y~ fJ 6' j g J ' " "q, Effective Section Properties Calculations for A. Rectangular Ducts (Con't) E R"IR,t$. ;W@sth.: o ,f A.02 String Analysis No. 4316 - 2 DUCT NODE NODE LENGTH Ky KZ g SIZE I J Ly L2 t 19X19 200 220 9'-2" 9'-2" 1.0 10 's 220 235 7'-9" 7'-9" 1.0 2.0 235 250 3'-4" 38-4" 1.0 2.0 k 250 260 7'-0"

/'-0" 1.0 1.0 260 270 8'-0" 8'-0" 1.0 1.0 270 280 8'-4" 88-4"

.0

1. 0 280 295 7'-5" 7'-5" 1.0 1.0 295 300 l'-1" l'-1" 1.0 2.0 I4 N.

300 310 3'-4" 3'-4" 1.0 2.0 ~ 310 330 6'-6" 6'-6" 1.0 1.0 330 340 6'-8" 6'-8" 2.0 3.0 340 350 6'-10" 2'-4" 2.0 1.0 F 350 360 6'-10" 4'-6" 2.0 1.0 360 370 6'-10" 4'-6" 2.0 1.3 D h-_ 350 385 6'-10" 4'-6" 2.0 1.0 185 400 6'-10" 4'-G" 2.0 1.0 W> ~ .L. g 'p %y:. 7 N fy. Uso Ly = 82" Ky = 2.0 fbf. ' 93" Ka = 2.0 4 L: v_ w, . l{g ,n. 6 -x", ve: DUCIN.006 'M .c INPUT FILE = wi OUTPUT FILE = DUCOUT.006

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19.0X19.0 PROPERTIES FOR DUCT SIZE W(IN)XH(IN) w%

EFFECT. .0478 IN DUCT SHEET BARE METAL THICKNESS = 3.6320 IN**2 FULL SECTION AREA, Ag = 2*(W+H)*T = FULL SECTION MOMENT OF INERTIA ABOUT Y - AXIS: 218.5735 IN**4 TXH**3/6 + TXWXH**2/2 = Iyy =SECTION MOMENT OF INERTI A ABOUT Z - AXIS: i FULL 218.5735 IN**4 l Izz = TXW**3/6 + TXHXW**2/2 = FULL SECTION KADIUS OF GYRATION ADOUT Y - AXIS: 1.7S67 IN i Ryy = (Iyy/Ag)**0.5 = FULL SECTION RADIUS OF GYRATION ABOUT Z - AXIS: 1 ' s 7.7567 IN Rzz = (Iz z / Aq) * *0. 5 = YIELDING STRESS = .3300E+02 KSI i .2900E+05 XSI y MODULUS OF ELASTICITY = x i o, e (3.4.1-2c) FOR HEIGHT (H) OF DUCT: [ ALPHAc PER EQ. 4.6540 0.256 + 0.328X(H/T) X(Fy/E) * *0. 5 = ALPHAc = BETAc PER EQ. (3.4.1-2c) FOR WIDTH (W) OF DUCT: 4.6540 N 0.328X(W/T)X(Fy/E)**0.5 = .x BETAc = 0.256 4 L . l[ l l en. Y OBE & SSE ~ ~ CALCULATE Ag FOR AXI AL TENSION pp (A) lR FULL SECTION AREA, Aga2X(W+H)XT= 3.632B IN**2 C. j ....,p' f-d CALCULATE Acx FOR AXIAL COMPRESSION ,d (B) 2.0000 b EFFEC" RIVE LENGTH FACTOR (Y) = B2.0000 IN j UNBRACED LENGTH BETWEEN SUPTS (Y) = 21.1430 KL/Ry =VE LENGTH FACTOR (Z) 2.0000 9 1 EFFECTI (Z) = 93.0000 IN f[$je UNBRACED LENGTH BETWEEN SUPTS = .a r, ? KL/Rz = 23.9792 i , j;h ! 7 23.9792 KL/Rmax = MAX (KL/Ry,KL/R2) 497.7681 FCI i = 7; " Fe = TT**2XE/(KL/Rmax)**2 = 32.4531 KSI W Q: l h Fe.GT.Fy/2, Fn= FyX ( 1. 0-Fy/ (4. XFe) ) = r hJ -1: Ef@i 3 i - OBE CASE fY S 6 0@h g% Fa = Fn/1.92 = 16.9026 5.0477 5 ALPHAi=1.052/SQRT(4.0)X(H/T)X(Fa/E)**0,5= S.0477 v i_ i M'th BETAi =1.052/SQRT(4.0)X(W/T)X(Fa/E)**0.5= m ALPHAi.GT ALPHAc, Y RHOi= ( 0. 41+ 0. 59X ( Fy / Fa) *

0. 5-0. 22 / ALPilAi) / ALP 11A1

,7' 6 ,2359 .M = hw He = RHOiXH = 4.4823 IN t ; a4 BETAi.GT.BETAc, Qg r_ g dr. 'RH0i=(0.41+0.59X(Fy/Fa)**0.5-0.22/ BETA 1)/BETAi Q y% f My .2359 N j = y .9 v. p h;fj ? k 4 ng h h h &w 1

gg ttg p a

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x 0.

W"'" SHEET ~ Pnodct Deco FER E 2 _Q,qljyAC N Duct Evaluation of 4316 E" c*tt oatt SusstCT System Serie.5 Jo 76230: 502 1 4 4 ,1.. J - P We = RlloiXW = 4.4823 IN 1 E EFFECTIVE AREA, Aex_OBE = .8570 IN**2 g SSE CASE (, r 25.3540 Fa = 1.5X(Fn/1.92) = 6.1821 ALPHAi=1. 052 / SQRT ( 4. 0) X (H /T) X( Fa / E) *

0. 5=

4 BETAi =1. 052 / SQRT(4. 0) X (W/T) X ( Fa/ E) *

0. 5=

6.1821 ALPHA 1.GT.ALPHAc, RilOi= (0. 41+ 0. 59X ( Fy/ Fa) <

0. 5-0. 2 2 / ALPHAi) / ALPilAi

= .1644 lie = RilOiXII = 3.2195 IN BETAl.GT.BETAc, Ritoi = ( 0. 41+ 0. 59X ( Ty/ Fa) *

0,5-0. 2 2 / BETA l ) / BETAi K

.1694 = We = P.110iXW = 3.2195 IN ?._ EFFECTIVE AREA, Aex_SSE = .6156 IN**2 g 6 EFFECTIVE AXI AL AREA FOR AN* LYSIS: ^ D Ao ANALYSIS = 2.1242 IN**2 7

%y-

.1475E-01 FT**2 = f[ (C) CALCULATE Iey FOR BENDIND MOMENT My (., OBE CASE ) 1 Fa = 0.6*Fy = 19.8000 W ALPilAi=1. 052 / SQRT(24. 0) X (H/T) X ( Fa / E) *

0,5=

2.2303 BETAi =1.052/SQRT( 4.0)X(W/T)X(Fa/E)**0.5u 5.4632 0 673.GT.ALPilAi.LE.ALPl!Ac, RIIO L = ( 1. 3 58 - 0. 4 61/ ALPHAi) / ALPHAi L.? a, .5162

0. 511ey = 0. 5 X Ritoi X 11 =

4.9039 IN Q W; u i 97, y, BETAi.GT.BETAc, it ?S 1 SF-Bitola ( 0. 41+ 0. 59X ( Fy/ Fa) *

0. 5-0. 22 /BETAi) /BETAi Cl-y?,,

0.5Wey = 0.5 X RI:01 X W = 1.9674 IN .2071 i l.f., = M ~ ~ FOR My, Iey~ ODE = 82.4054 IN**4 1 m @2 Sey OBE = 8.6743 IN**3 m .) SSE CASE Q y Fa = 0.9XFy =' 29.7000 2.7316 b AI.PRAi=1. 052 / SQRT( 2 4. 0) X (ll/T) X ( Fa/ E) *

0. 5=

BETAl'=1.052/SQRT( 4.0)X(W/T)X(Fa/E)**0.5= 6.6910 c 0.673.GT.ALPRA1.LE.ALPRAC, 10 A M RHOi- = (1. 358 - 0,461/ ALPHAi) /ALPHAi A '%0 t- - .4354 T lQf o = < v %,. h

%s w,

< l &y:n up "+w pgk _.m

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X. i 2 moxct DECO FERMI !" - CCHVAC' " D " oart o*n ~ Duct Evaluatier, of 4316 4 Re/tCT System Series Jo 76230,502 7 E, r ) Q k" 0.5 Hey a 0.5 X RHOi X H = 4.1360 IN' I BETAi.GT.BETAc, E Ritoi= ( 0. 41+0. 59X ( Py/ Fa) *

0. 5-0. 22 / BETAi ) / BETAi

.1493 = i e j I 0.5Wey = 0.5 X RHOi X W = 1.4184 IN t 69.2832 IN**4 i l FOR My, Icy SSE = 7.2930 IN**3 SSE = l ~ Sey ANALYSId 58.8908 IN**4 f ', ' Iey- = .2840E-02 FT**4 = g %4 (D) CALCULATE Iez FOR DENDIND NOMENT Mz

n

- OBE CASE E Fa = 0.6*Fy = 19.8000 NU. ALPilAi= 1. 05 2 / SQRT ( 4. 0) X(H/T) X ( Fa / E) *

0. 5=

5.4632 h BETAi =1. 052 /SQRT( 2 4. 0) X (W/T) X ( Fa / E) *

0. 5=

2.2303 4.. ALPHA 1.GT.ALPHAc, 9,A RHOi=(0.41+0.59X(Fy/Fa)**0.5-0.22/ ALPHA 1)/ALPHAi .2071 = s' QP,. 0.5Hez = 0.5 X RHOi X H = 1.9674 IN 1 O.673.GT.BETAi.LE.BETAc, RHOi = (1.358 - 0.461/BETAi)/BETAi 5162 i D = 1 - N 0.5Wez = 0.5 X Rlloi X W = 4.9039 IN 4, FOR Mz, Iez OBE = 82.4054 IN**4 l Sez OBE = 8.6743 IN**3

n t ;

u., SSE CASF 3 y i Fa = 0.9XFy = 29.7000 ) h@,;,f ALPHAi=1.052/SQRT( 4.0)X(H/T)X(Fa/E)**0.5= 6.6910 W BETAi =1.052/SQRT(24.0)X(W/T)X(Fa/E)**0.5= 2.7316 (jg ALPHAi.GT.ALPHAc, 4 l RHOi=(0.41+0.59X(Fy/Fa)**0.5-0.22/ALPHAi)/ALPHAi 9 ~+L .1493 i = O. Silez = 0. 5 X RIIOi X H = 1.4184 IN I u 0.673.GT.BETAi.LE.BETAc, 4 Jg Rl!Oi = (1.358 - 0.461/BETAi)/BETAi ] .4354 s c n v. = D,7 0.5Wez = 0.5 X RHOi X W = 4.1360 IN f-I 69.2832 IN**4 , EU h FOR Mz, Iez SSE i = 7.2930 IN**3 I2 Soz~SSE p;T ' J.t = pg Iez ANALYSIS = 58.G908-IN**4 4 .284(E-02 FT**4 ^W l l j.y 2 = %q[ , ;.5 Sf3db .(E) CALCULATE Ay FOR Y-DIRECTION SHEAR OBE & SSE ?j x,:; my, ~ jp. SHEAR AREA, Ay = 2XWXT = 1.0164 IN**2 .1261E-01 FT**2

y fa

= $pMM' f-hki I h 'I u # 4 m> ) 12 9';4v(6 n i 1 MM M $$5~, (* j QRy_ _ _ _ _ _

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+y p

i 3 CALCULATE Az FOR Z-DIRECTICH SHEAR OBE & SSE t, N' (F) SHEAR AREA, Az = 2XHXT = 1.8164 IN**2 w + .1261E-01 Pr**2 = i ~i CALCULATE Ixx TOR TORSIONAL MOMENT Mx ODE & SSE (G) FOR Mx, Ixx ANALYSIS = 327.8602 IH**4 e .1581E-01 FT**4 @l j = i l1. o Y. -. k., u., "- !f 4 97 !n.. a-1- ' fj:g ,(p . w..< .sp ; $t l 3: ae .a ; NA: - $.5 y*, i-' + ln 6 i s

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'm ae 0 ' $'[. a n7 /kh n x Pn0 JECT _ Deco FERMI 2 - CCH$/Ac + " I' U # omit onrs Duct Evaluation of 4316 Sua>ECT System Series ao 76230.502 4 ic h f 'i'(: A. Effective Section Properties Calculations for {(l-Rectangular Ducts (Con't) y [ A.03 String Analysis No. 4316 -3 3 g L i' DUCT NODE NODE LENGTH Ky Kz SIZE I J Ly LZ y

I 10X10 370 358 5'-4" 5'-4" 1.0 1.0 f

358 ELBOW O'-11" O'-11" 1.0 2.0 Ll ELDOW 332 4'-3" 4'-3" 1.0 2.0 )*) 332 320 7'-0" 7'-0" 1.0 1.0 320 300 6'-10" 6'-10" 1.0 1.0 M' use Ly = 84.0" Ky = 1.0 Lz = 51.0" Kz = 2.0 ,i ; m DUCIN.005 p'. INPUT FILE = g OUTPUT FILE = DUCOUT.005 3,. s s g,(.. 'E5 s E "' e w L JV l'. h,, ~ i

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10.0X10.0 N

EFFECT. PROPERTIES FOR DUCT SIZE W(IN)XH(IN) W. DUCT SHEET BARE METAL THICKNESS = .0478 IN FULL SECTION AREA, Ag = 2 * (W+H) *T = 1.9120 IN**2 FULL SECTION MOMENT of INERTI A ABOUT Y - AXIS: Iyy = TXHa*3/6 + TXWXH**2/2 = 31.8667 IN**4 -FULL SECTION MOMENT OF INERTIA ABOUT Z - AXIS: Izz = TXW**3/6 + TXHXW**2/2 = 31.8667 IN**4 FULL SECTION RADIUS OF GYRATION ABOUT Y - AXIS: i Ryy = (Iyy/Ag)**0.5 = 4.0825 IN L FULL SECTION RADIUS OF GYRATION ABOUT Z - AXIS:

o Rzz = (Izz/Ag)**0.5 =

4.0825 IN YIELDING STRESS = .3300E+02 KSI MODULUS OF ELASTICITY = .2900E+05 KSI j +. A y' @ ? *- ALPHAc PER EQ. (3.4.1-2c) FOR HEIGHT (H) OF DUCT: N ALPHAc = 0.256 + 0. 323X (H/T) X (Fy/ E) *

0. 5 =

2.5707 BETAc PER EQ. (3.4.1-2c) FOR WIDTH (W) OF DUCT: i BETAc

0.256 + 0.328X(W/T)X(Fy/E)**0.5

2.5707 l: o : iO T (A) CALCULATE Ag FOR AXIAL TENSION OBE & SSE i i ' d' "b FULL SECTION AREA, Aga2X(W+H)XT= 1.9120 IN**2 (B) CALCULATE Acx FOR AXIAL COMPRESSION ,r = 1.0000 EFFECTIVE LENGTH FACTOR (Y) ($T UNBRACED LENGTH BETWEEN SUPTS (Y) 84.0000 IN = ~ KL/Ry = 20.5757 2.0000 EFFECTIVE LENGTH FACTOR (Z) = 51.0000 IN UNBRACED LENGTH BETWEEN SUPTS (2) = , ya 4 24.9848 W KL/RZ = 24.'9848 1 P* KL/Rmax = MAX (KL/Ry,KL/Rz) = Fe = TT *

2 XE/ (KL/ Rmax) *
2 = -

458.5064 KSI ? Fe.GT.Fy/2, Fn=FyX(1.0-Fy/(4.XFe))= 32.4062 KSI 'i w ,j M - CBE CASE U$th; c~ Fa = Fn/1.92 = 16.8782 $g~' ALPHAi= 1. 052 /SQRT ( 4. 0) X (H/T) X ( Fa / E) *

0. 5=

2.6547 1~~ ~ g BL'rAl =1.052/SQRT(4.0)X(W/T) X(Fa/E) **0.5= 2.6547 gu ALPHAi.GT.ALPHAc, g-RHOi=(0.41+0.59X(Py/Fa)**0.5-0.22/ ALPHA 1)/ALPHAi rw b [d 0 He = RHOiXH 4.3398 IN ,l4 ( 1 BETA 1. GT. B ETAc, RHOi=(0.41+0.59X(Fy/Fa)**0.5-0.22/BETAl)/BETAi i 9.D {d 'J3 = .4340 g x $th OM) M lj$r$ fMY P. 4 g Ay Nfh? w,y 1 1 er mw r: f .h f(h a hy; Ibb n O S .pq - po, - ; ye

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Duct Evaluaticn of 4316 Jo 76230.502 System Series sus)(Cy }[j[ We = RHOiXW = 4.3398 IN EFFECTIVE AREA, Aex_OBE = .8298 IHa*2 e js s . m - SSE CASE g. 25.3174 E Fa = 1.5X(Fn/1.92) = [ ALPHAi=1. 052 / SQRT ( 4. 0) X (ll/T) X ( Fa / E) *

0,5=

3.2514 BETAi =1.05?/SQRT(4.0)X(W/T)X(Fa/E.)**0.5= 3.2514 ALPHAi.GT.ALPHAc, Rlloi=(0.41+0.59X(Fy/Fa)**0.5-0.22/ ALPHA 1)/ALPHAi y .3125 = i A= He = RHOiX11 = 3.1246 IN BETA 1.GT.BETAc, f RHOi=(0.4.+0.59X(Py/Fa)**0.5-0.22/BETAi)/BETAi ( .3125 = We = RilOiXW = 3.1246 IN s %D EFFECTIVE AREA, Aex SSE = .5974 IN**2 p EFFECTIVE AXIAL AREA FOR ANALYSIS: L Ae ANALYSIS = 1.2547 IN**2 z .8713E-02 FT**2 ~ = ((^~ A.; CALCULATE Iey,FOR BENDIND MOMENT My R. (C) o W i - OBE CASE Tep, m aa Fa = 0.6*Fy = 19.8000 l' ALPilAi= 1. 052 / SQRT ( 24. 0 ) X (H /T) X ( F a / E) *

0. 5r 1.1739 BETAi =1.052/SQRT( 4.0)X(W/T)X(Fa/E)**0.5=

2.8754 [ pc 0.673.GT.ALPHAi.LE.ALPHAc, 6f' Ritoi = (1.358 - 0.461/ALPHAi)/ALPHAi .8223 = thh3 0.5 Hey = 0.5 X RilOi X ll = 4.1116 IN BETA 1.GT.BETAc, RIIOi= ( 0. 41+ 0. 59X ( Fy/ Fa ) *

0. 5-0. 2 2 / BETAi) / BETAi F

d'gh'g .3809 = O.5Wey = 0.5 X RHOi X W = 1.9044 IN {' FOR My, Iey 0 ' = 17.0251 IH**4 N@f 3.4050 IN**3 J Epf Sey O /. = o< hE-W- ~ ' 1 kE - SSE CASE Q~ Wn Fa = 0.9XFy = 29.7000 7' ALPHAi=1.052/SQRT(24.0)X(H/T)X(Fa/E)**0.5= 1.4377 BETAi =1.052/SQRT( 4.0)X(W/T)X(Fa/E)**0.5= 3.5216 li 0.673.GT. ALPHA 1.LE.ALPHAc, Rlloi = (1.358 - 0.461/ALPHAi)/ALPHAi t h([/,.

n. Q

.7215 = f 9,' .ah - QQ ${O h\\; dy %U-h2hkb j de ?g f fp M* gJ '- % n +> =- s s Ikhhbi4-; i:_ .QQ_de

wn w i. a n> I GENERAL [g([(y 0 ';g s 7"' COMPUTATION <e o og SHEET YZ41$h y PROJECT ~ Deco FERMI 2 ~CCHVAC 5""' N " ll oati~ onw ~ Duct Evaluation o:' 4 316 7 System Series ao 76230.502 I sutuccf k V' ra u i 0.5 Hey = 0.5 X R}{0i X H = 3.6077 IN 4 .,ic BETA 1.GT.BETAc, ($f"$ Ritoi=(0.41+0.59X(Fy/Fa)**0.5-0.22/ BETA 1)/BETAi i, ; D s,. ++- .2753 = i\\ 0.5Wey = 0.5 X RilOi X W = 1.3764 IN 14.3740 IN**4 u FOR My, Iey SSE = 2.8748 IN**3 o Sey SSE = Iey~ ANALYSIS = 12.2179 IN**4 3 .5892E-03 FT**4 = / (D) CALCULATE Iez FOR BENDIND MOMENT Mz y QJ - OBE CASE { 4 i, y Fa = 0.6*Fy = 19.8000 4 ALPHAi=1.052/SQRT(

4. 0) X (il/T) X ( Fa / E) *

0. 5=

2.8754 1.1739 BETAi =1.052 / SQRT( 2 4.0) X (W/T) X (Fa / E) *

0. 5=

( ALPHA 1.GT.ALPHAc, Ritol= ( 0. 41 + 0. 59X (Fy/ Fa) *

0,5-0. 2 2 /ALPHAi) / ALPHAi t

.3809 IA = il 0.5Het = 0.5 X RHOi X H = 1.9044 IN O.673.GT. BETA 1.LE.BETAc, &(. Ritoi = (1. 358 - 0. 4 61/ BETA 1) /BETAi p 8223 =

.7 0.5Wez = 0.5 X RHOi X W =

4.1116 IN FOR Hz, Iez OBE = 17.0251 IN**4 h Sez OBE = 3.4050 INa*3 v

e

1

- SSE CASE Fa = 0.9XFy = 29.7000 pr;. K ALPilAi=1.052/SQRT( 4.0)X(H/T)X(Fa/E)**0.5= 3.5216 BETAi =1.052/SQRT(24.0)X(W/T)X(Fa/E)**0.5= 1.4377 ALPHA 1.CT.ALPHAc, O, RHOi=(0.41+0.59X(Fy/Fa)**0.5-0.22/ ALPHA 1)/ALPilAi .2753 = 0.5Hez = 0.5 X RilOi X H = 1.3764 IN g-q e -O.673.GT. BETA 1.LE.BETAc, m 77 0-- Riioi = (1.358 - 0.461/DETAI)/BETAL n: a.. .7215 = [ 0.5Wez = 0.5 X RH0i X W = 3.6077 IN @M, FOR Ma, Iez_SSE 2.8748 IN**3 14.3740 IN**4 SSE = r = Sea-kg Iez ANALYSIS = 12.2179 IN**4 W ~ = .5892E-03 FT**4

Og

'M w. hN:i (E) CALCULATE Ay FOR Y-DIRECTION SHEAR OBE & SSE c:r T1 W n/ SiiEAR - AREA, Ay = 2XWXT = .9560 IN**2 .6639E-02 FT**2 = l c.e w e y ai v Lf X WiM y< >% Q. g y:- ll: W C.. bi@hM,W m & l

"'""."-"-'_v- -m__ _ _ I !, t . ~....u GENERAL .(l((/ WM COMPUTATION '^ o o o, ? Q^ ^- SHEET I/L9_8 8 Y4 x ( PRCutCT Deco FERR ? 1 CCH'JAC " M* cm om Duct Evaluat ion of AJ:6 I SututCT System Serir.s Jo _ 7 62 3 0. 502 F i's j CALCULATE Az FOR Z-DIRECTION SHF.AR OBE & SSE g p ( '* J P )! 2XHXT = .9560 IN**2 [ SHEAR AREA, A2 a . 66 3 9 E-0 2 FT**2 = CALCULATE Ixx FOR TORSIONAL HOMENT Mx OBE & SSE 1,f (G) l' FOR Mx, Ixx ANALYSIS = 47.8000 IN**4 .2305E-02 Fr**4 ~ = a t g N. l s .l p

p 6

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my wA J W g

Rectangular Ducts (Con't) /} A.04 String Analysis No. 4316 - 6 DUCT NODE NODE LENGTil Ky KZ SIZE I J Ly L2 6 ( 16X16 7~20 775 4'-9" 4'-3" 2.0 1.0 100 775 6'-5" 38-7" 2.0 1.0 J 775 120 6'-5" 2'-11" 2.0 1.0 120 1014 l'-8" l'-8" 2.0 1.0 '014 135 48-0" 4'-0" 1.0 2.0 135 1013 2'-4" 2'-4" 1.0 2.0 1013 150 l'-2" 6*-2" 1.0 1.0 150 175 5'-0" 6'-2" 1.0 1.0 't 205 220 4'-8" 5'-0" 1.0 1.0 J 220 1011 0'-4" 5'-0" 1.0 1.0 A 2011 245 7'-0" 7'-0" 2.0 2.0 8 150 355 5'-0" 5'-0" 1.0 2.0 ~ Il 355 375 2'-2" 2'-2" 1.0 2.0 FEp 6405 415 18-7" l'-7" 1.0 2.0 415 220 5'-0" 5'-0" 1.0 2.0 H m g3 p Use Ly = 84.0" Ky = 2.0 M:: i 35' bz = 84.0" Kz w 2.0 s.m.. g, e t '} \\, y

e DUCIN.007

"1 INPUT FILE

= ,. y [E.l OUTT'.'T FILE = DUCOUT. 007 n. ri, h. h .;j n-yLQ ?- u o ^ . {g 4 Jg mp-dt-.h - '^ [ Nhf ^ h@a.n 'y).. Q *%, J d v $:p;Ie' ~ e m<. M 4 t 4,. @x pyf 1 ~ a .i hW j.3 p -f Agq G- .. ;, se p:i, Ci s ..,d@ b-J 'g Q. 4 ya . y,, >p 4,

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't d.

in t, 2 - r EFFECT. PROPERTIES FOR DUCT SI7E W(IN)XH(IN) : 16.0X16.0 l P* - . DUCT SilEET DARE METAL THICKNESS. = .0478 IN / yt; FULL SECTION AREA, Ag~= 2*(W+H)*T = 3~0592 IN**2 FULL SECTION MOMENT OF INERTIA ABOUT Y - AXIS 1, Iyy a TXH**3/6 + TXWX11**2/2 = 130.5259 IN**4 l FULL SECTION MOMENT OF INERTIA ABOUT Z - AXIS: Izz a TXWa*3/6 + TXHXW**2/2 = 130.5259 IN**4 l-FULL SECTION RADIUS OF GYRATION ABOUT Y - AXIS: Ryy = (Tyy/Ag)**0.5 = 6.5320 IN j' FULL SECTION RADIUS OF GYRATION ABOUT Z - AXIS: Rzz = (Izz/Ag)**0,5 = 6.5320 IN YIELDING STRESS = .3300E+02 KSI MODULUS OF EIASTICITY = .2900E+05 KSI iF k A7 PHAC PER EQ. (3.4.1-2c) FOR HEIGl!T(ll) OF DUCT: g D ALPHAc = 0.256 + 0.328X(H/T)X(Fy/E)**0.5 = 3.9596 l' 1 BETAc PER EQ. (3.4.1-2c) FOR WIDTH (W) OF DUCT: ) [ BETAc

0.256 + 0.328X(W/T)X(Fy/E)**0.5

3.9596 i-a i M( F' (A) CALCULATE Ag FOR AXIAL TENSION OBE & SSE if FULL SECTION 'AkEA, Ag=2X(W+H)XT= 3.0592 IN**2 e< ~ (B) CALCUIATE Aex FOR AXIAL COMPRESSION EFFECTIVE LENGTH FACTOR (Y) 2.0000 = 84.0000 IN I UNBRACED LENGTH BETWEEN SUPTS (Y) = KL/Ry = 25.7196 = 2.0000 EFFECTIVE LENGTH FACTOR (Z) n-84.0000 IN t p UNDRACED LENGTH BETdEEN SUPTS (Z) = d.- KL/Rz = 25.7196 25.7196 KL/Rmax = HAX (KL/Ry,KL/Rz) = 432.6004 KSI Fe = TT**2XE/(KL/Rmax)**2 = C Fe.GT.Fy/2, Fn=FyX (1. 0-Fy/ ( 4. XFe) ) = 32.3708 KSI t - OBE CASE 4 My ?:9 Fa = Fn/1.92 = 16.8598 h, y

a =

ALPHAi=1.052/SQRT(4.0)X(H/T)X(Fa/E)**0.5= 4.2453 ~- BETAi =1.052/SQRT(4.0)X(W/T)X(Fa/E)**0.5= 4.2453 4/L ,1 ALPHA 1.GT.ALPHAc, 76 R110i= ( 0. 41+ 0. 59 X (Fy/ Fa) *

0. 5-0. 2 2 / ALPHAi) / ALPHAi

.2788 n, fM = 4 He = RHO 1XH = 4.4609 IN i 41 4;Wx. BETA 1.GT.BETAc, 7 M(b. .2788 M {y'i,. RHOi=(0.41+0.59X(Fy/Fa)**0.5-0.22/BETAi)/BETAi n-sa fa ci; M i; }l b& &p; .A % f + c C { h. u~ wn &p, -_ m o* m. s' iMcp !%-

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t SHEET / PROJECT DFCO F FRM I _.? - CCHVAC "" %& 77 ~ oars oars f Duct Evaluation of 4316 Jo 76230.502 ) sua;tcf Systein Series u. t Y y We = RHOiXW = 4.4609 IN j l [ f.. EFFECTIVE AREA, Acx_ ODE = .8529 I N '.

2 s.

l L I; [ - SSE CASE 25.2897 I Fa = 1.5X'Fn/1.92) = ALPilA i= 1. 052 /SQRT( 4. 0) X (ll/T) X ( Fa / E) *

0. 5=

5.1994 j BETAi =1.052/SQRT(4.0)X(W/T)X(Fa/E)**0.5= 5.1994 ALPIIA1.GT. ALPHAc, i j RII0i= ( 0. 41 + 0. 59 X ( Fy/ Fa) *

0. 5-0. 2 2 / AI.PHAi) / ALPilAi

.2003 = f 1 He = RilOiXII = 3.2055 IN BETAl.GT.BETAc, ( Rifoi= ( 0. 41+ 0. 59X ( Fy/ Fa) *

0. 5-0. 2 2 / DETAi) / BETAi g

.2003 = ? We = RHOiXW = 3.2055 IN / s ( s , ( O EFFECTIVE AREA, Anx SSE = .6129 IN**2 + EFFECTIVE AXIAL ARPA FOR ANALYSIS: j Ae ANALYSIS = 1.8360 IN**2 = .1275E-01 FT**2 .3 t y (C) CALCULATE Iey, FOR BENDIND MOMENT My i - OBE CASE N 'T Fa = 0.6*Fy = 19.8000 ALPl!A i= 1. 052 / SQRT ( 24. 0 ) X (ll/ T) X ( Fa / E) *

0, 5 =

1.8782 ( f BETAi =1.052/SQRT(

4. 0) X(W/T) X( Fa/ E) * *0. 5=

4.6006 O. 673.GT. ALPilA1. LE. ALPHAc, i t (1.358 - 0.461/ALPilAi)/ALPHAi iL i RilOi = .5924 = t; f O. Siley = 0. 5 X R}loi X H = 4.7389 IN t BETAl.GT.DETAc, .i RilOi=(0.41+0.59X(Fy/Fa)**0.5-0.22/BETAi)/BETAi y .2443 = i l; [ 0.5Wey = 0.5 X RIIOi X W = 1.9543 IN

t. * ;

S O FOR My, Iey OBE = 54.3355 IN**4 4 ) lE Scy ODE a 6.7919 IH**3 .y: W% , N; WJO i h19* - SSE CASE - v ;v; D i[ f ALPilA i=1. 052 / SQRT ( 2 4. 0) X (H/T) X (Fa / E) *

0. 5=

2.3003 Fa = 0.3XFy =- 29.7000 BETAi =1.052/SQRT( 4.0)X(W/T)X(Fa/E)**0.5= 5.6345 4

0. 6 7 3. GT. ALP!IA i. LE. ALPHAc,

-m Rlloi = (1.358 - 0.461/ ALPHA 1)/ALPHAi

J j

y .5032 'n, r - = (n

1. Q

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v.= w a,. m ^# d.h M[M GENERAL ~ 0 COMPUTATION _**4 *' ww 0 on ,jj. - ^ 4 SHEET 7/#/O 7/3 x n 5""' 31 " ll cytVAc monct _ DECO FEREL2 can om Duct Evaluation of 4316 so 76230.502 J SuaXCT System Series 1 3 f 4.0259 IN 0.511ey = 0.5 X RitOi X li = BETAi.GT.BETAc, Ri!Oi= ( 0. 41+0. 59 X ( Py / Fa ) *

0. 5-0. 2 2 / BETA 1) / BETA 1 I

.1762 = 1.4097 IN 4-0.5Wey = 0.5 X 10101 X W = p 45.8814 IN**4 Iey SSE = FOR Hy, Sey ANALYSIS =5.7352 IH**3 SSE = 38.9992 IN**4 Iey~ ,1881E-02 FT**4 = +- CALCULATE Ioz FOR DENDIND MOMENT Mz (D) Q b - OBE CASE Fa = 0.6*Fy = 9.8000 4.6006 4.0)X(H/T)X(Fa/E)**0.5= ALPitA i= 1. 052 / SQRY ' 1.8782 i DETAi = 1. 052 / SQRT(2 4. 0) X (h/T) X ( Fa / E) *

0. 5=

ALPHAi.GT.ALPHAc, RilOl = ( 0. 41 t 0. 59X ( Fy/ Fa) *

0. 5-0. 2 2 / ALPilAi) / ALPilAi 2

.2443 4 = 1.9543 IN L

0. 51iez = 0. 5 X R}{Oi X H =

U 0.673.GT.BETAi.LE.BETAc, 0,7 ( Ritoi = (1.358 - 0. 4 61/BETAl) /DETAl .5924 = G

0. 5Wez = 0.5 i R}iOi X W =

4.7389 IN $9 FOR Hz, Icz OBE = 54.3355 IN**4 IA.. Sez[OBE = 6.7919 IN**3 bi - SSE CASE R Fa = 0.9XFy = 29.7000 5.6345 $h ALPHAl=1. 052 /SQRT(

4. 0) X (ll/T) X ( Fa/ E) *

0. 5=

2.3003 f BETAi =1.052/SQRT(24.0)X(W/T)X(Fa/E)**0.5= i-m b ALPilA1.GT.ALPHAc, 7; Ritoi= ( 0. 41+0. 59X (Fy/ Fa) *

0. 5-0. 2 2 / ALPilA1) / ALPHAi

~ .1762 = 0.5Hez = 0.5 X RitOi XH= 1.4097 IN Q 0.673.GT.BETAi.LE.DETAc, RIIOi = (1.358 - 0.461/BETAi)/DETAi W% .5032 = c 4.0259 IN f[ 0.5Woz = 0.5 X Rlloi X W = 45.8814 INa*4 FOR Mz, Iez SSE = 5.7352 IH**3 b Sez[SSE 38.9992 IN**4 t = Ie ANALYSIS = + .1881E-02 FT**4 ~~ = (( l SSE CALCULATE Ay FOR Y-DIRECTION SHEAR OBE & k (E) SilEAR AREA, Ay = 2XWXT = 1.5296 IN**2 .1062E-01 FT**2 VO 4 = 4 ' "l k . I? f5 v km.I n u a } <. hs h &m

-w w,r.-.. + v, cat (u aft.JPeSti M) 84V CC4A*, Cf C*O #f _ = = - - - [2h bM S tare CO AP A ON 'a oo o e SHEET +3o- !4 PaoJtCT Ofco FERMI 2 - CCHVAc qq W, oart oarg l Duct Evaluation of 4316 l" $UBKCT System Series so 76230.502 a. E l, (' (F) CALCULATE Az FOR Z-DIRECTION S!! EAR OBE & SSE .r. '3 - SHEAR AREA, Az - 2XHXT = 1.5296 IN**2 .1062E-01 FT**2 ( [ = (G) rALCULATE Ixx FOR TORSIONAL MOMENT Mx OBE & SSE FOR Mx, Ixx ANALYSIS = 195.7888 INa*4 .9442E-02 FT**4 = s y 9 1 l r ? >;9 i W I i D.o,r. 5 A, s i ,,J I g A, ) a a ' g j. {Iw F D 2: ,f it. T} ?:Y ,;y ? y -y 91: .W* p folt ,<..g j. + v <} 't.' 1,- 3 3 l Q)t; .~ pk: r a /L,< ) % L. '_'**4* p'_f *,.,. c, ..q c u1' t -Q /. f 'T:: b-Q

~

?; : r y

' * (,,

5 t[ $) p - n y *ll? 1 +, < 4,, '): I'-(ke

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p..

f, " e Effective Section Properties Calculations for g io A. Rectangular. Ducts (Con't) s: r~ 3 A.05 String Analysis No. 4316 - 7 M DUCT NODE NODE LENGTH Ky Xz W SIZE I J Ly LZ m.$ 1 J, 16X16 720 715 6.00' 7.58' 1.0 1.0 v-W(. 715 710 1.58' 7.58' 1.0 1.0 g@** 710 705 1.42' 1.42' 1.0 2.0 705 701 4.0' 4.08 1.0 2.0 c 715 725 4.0' 4.0' 1.0 2.0 d Use Ly = 72" Ky = 1.0 48" Kz = 2.0 4.: tev,, e LZ =

b... _

.'t, + DUCIN.010 INPUT FILE = r *- OUTPUT FILE = DUCOUT.010 '( ) - 6 .g. ly{6' e _h ( h Q, i.&.. g t w. '.,g ( 3 ', h ' J; y, r fj;hb y p y@q. ..g i mh

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n N

yl < ~$ kI p h EFFECT. PROPERTIES FOR DUCT SIZE W(IN)XH(IH) : 16.0X16.0 DUCT SilEET BARE METAL THICKNESS = .0478 IN -FULL SECTION AREA, Aq = 2*(W+11)*T = 3.0592 IN**2 FULL SECTION MOMENT OF INERTIA ABOUT Y - AXIS: Iyy = TX11**3/', + TXWXHa*2/2 = 130.5259 IN**4 FULL SECTION r.OMENT OF INERTIA ABOUT Z - AXIS: J Izz = TXW**3/6 + TX11XW**2/2 = 130.5259 IN**4 FULL SECTION RADIUS OF GYRATION ABOUT Y - AXIS: (Iyy/Ag)**0,5 = 6.5320 IN Ryy = FULL SECTION RADIUS OF GYRATION ABOUT Z - AXIS: Rzz = (Izz/Ag)**0.5 = 6.5320 IN YIELDING STRESS = .3300E+02 KSI MODULUS OF ELASTICITY = .2900E+05 KSI ALPilAc PER EQ. (3.4.1-2c) FOR HEIGHT (ll) OF DUCT: ALPliAc = 0.256 + 0.328X(H/T)X(Fy/E)**0.5 = 3.9596 BETAc PER EO. (3.4.1-2c) FOR WIDTH (W) OF LUCT: 0.328X(W/T)X(Py/E)**0.5 = 3.9596 BETAc = 0.256 + E. J' (A) CALCULATE Ag FOR AXIAL TENSION OBE 6 SSE w 3: ) FULL SECTION* AREA, Ag=2 X (W +11) XT= 3.0592 IN**2 1 (B) CALCULATE Acx FOR AXIAL COMPRESSION n EFFECTIVE LENGTil FACTOR (Y) 1.0000 = 72,0000 IN UNBRACED LENGTH BETWEEN SUPTS (Y) = i KL/Ry = 11.0227 2.0000 EFFECTIVE LENGTil FACTOR (Z) = 48.0000 IN a UNBRACID LENGTil BETWEEN SUPTS (Z) = n 7' KL/Rz = 14.6969 14.6969 KL/Rmax = MAX (KL/Ry,KL/Rz) p = g Fe = TF*

2XE/ (KL/Rmax) * *2 =

1325.0830 KSI !y Fe.GT.Fy/2, Fn=FyX ( 1. 0-Fy/ ( 4. XFe ) ) = 32.7945 KSI ,[ ? [ - OBE CASE Fa = Fn/1.92 = 17.0805 ALPilAi= 1. 052 / SQRT ( 4. 0) X (ll/T) X ( Fa / E) *

0. 5=

4.2730 4.2730 i BETAl = 1. 052 / SQRT ( 4. 0) X (W/T) X ( Fa / E) *

0. 5=

ALPilA1.GT. ALPilAc, 4;t Rlb)i= ( 0. 41+ 0. 59X ( Fy/ Fa) *

0. 5-0. 2 2 / ALPliAi) / ALPIIAi

.2758 = g E lic = RitoiXil = 4.4132 IN 2 BETA 1.GT.BETAC, Ritoi=(0.41+0.59X(Fy/Fa)**0.5-0.22/BETAi)/BETAl i [L . 2 5.iS r ax: = 4. 'di B. ? w& n; w l Ey r) % y h". - x g. i y. m lL Mi[ Mi

+ ... ~.. ~. atv ccue cv Cw3 eV cA cm a tos f,t1 a<., g

* ~ " ' '

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o 76230.502
f We = RiiOiXW =

4.4132 IN ),; y n JJ EFFECTIVE AREA, Aex_OBE = .8438 IH**2 y n.- - SSE CASE N C" Fa = 1.5X(Fn/1.92) 25.6207 = ALPilA i= 1. 052 / SQRT ( 4. 0) X (II/ T) X ( Fa / E) *

0. 5=

5.2333 t BETAi =1.052/SQRT(4.0)X(W/T)X(Pa/E)**0.5= 5.2333 / ALPilA1.GT.ALPHAc, RitOi= ( 0. 414 0. 59X ( Fy/ Fa) *

0. 5-0. 2 2 / ALPilAi) / ALPilAi i[

= .1983 f J He = ElloiXil = 3.1722 IN B ETA i. CT. B ETAc, RilOi= ( 0. 41 + 0. 59 X ( Fy/ Fa) *

0. 5-0. 2 2 / BETA i) / BETAi g

.1983 = g We = RilOiXW = 3.1722 IN EFFECTIVE AREA, Aex,,SSE = .6065 IN**2 h- ~ EFFECTIVE AXIAL AREA FOR ANALYSIS: Ao ANALYSIS = 1.8329 IN**2 .1273E-01 FT**2 ~ a = l (C) CALCULATE Icy FOR BENDIND MOMENT My - OBE CASE { Fa = 0.G*Fy = 19.8000 J ALPilAi= 1. 052 / SQRT ( 2 4. 0) X (ll/T) X ( Pa / E) *

0. 5=

1.8782 i BETAi =1.052/SQRT( 4.0)X(W/T)X(Fa/E)**0.5= 4.6006

0. 67 3.CT. ALPilAi. LE. ALPi!Ac, I-Ritoi = (1.358 - O.461/ALPl!Ai)/ALPHAi

.5924 3 = O.51{ey = 0.5 X RilOi X H = 4.7389 IN BETAi.GT.BETAc, Ritol=(0.41+0.59X(Fy/Fa)**0.5-0.22/DETAi)/ BETA 1 t .2443 .s? N = /e-0.5Wey = 0.5 X RH01 X W = 1.9543 IN } S' FOR My, Iey OBE = 54.3355 IN**4 }+. Scy[OBE = 6.7919 IN**3 l 'm ( 28 - SSE CASE 'l ^ .s> Fa = 0.9XFy = 29.7000 p ALPflAi= 1. 052 / SQRT ( 2 4. 0) X (ll/T) X ( Fa / E) *

0. 5=

2.3003 p BETAi =1.0.2/SQRT( 4. 0) X (W/T) X (Fa/ E) *

0,5=

5.6345 O. 6 7 3. GT. ALPilA1. LE. ALPitAc, t RHOi = (1.358 - 0.461/ALPilAi)/ALPHAi .5032 f ( = ^ "_ y 3 n L% %=

},

a E f h $ ;g '9' \\ Es . ;?g ' fi 9.3 \\ y, +. , y 6 1_

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92 "

oart 04r1 Duct Evaluation of 4316 Jo 76230.502 SufutCT System Series 4.0259 IN 0.5 Hey = 0.5 X Ritoi X H = BETA 1.GT.BETAc, R110i= (0. 41+ 0. 59X ( Fy/ Fa) *

0. 5-0. 2 2 /BETAi) / DETAi

.1762 = 1.4097 IN r 0.5Wey = 0.5 X RHOi X W = ? 45.8814 IH**4 FOR My, Iey~SSE 5.7352 IN**3 = SSE = Sey~ ANALYSIS = 38.9992 IN**4 Iey- .1881E-02 FT**4 = c-- j k (D) CALCULATE Icz FOR BENDIND MOMENT Mz s. hl: - CBE CACE R m Fa = 0.6*Fy u 19.8000 4.6006 ALPllAi=1.052/SQRT( 4.0) X(!!/T) X(Fa/E) * *0. 5= 1.8782 BETAi =1. 052 / SQRT(24.0)X(W/T) X(Fa/ E) * *0. 5= g ALPHA 1.GT.ALPHAc, RilOi= ( 0. 41 + 0. 59 X ( Fy/ Fa) *

0. 5-0. 2 2 / ALPHA 1) / ALPilAi E

I .2443 =

0. 511ez = 0. 5 X RH0i X 11 =

1.9543 IN L C 0.673.GT. BETA 1.LE BETAc, i( Ritoi = (1.358 - 0.461/ BETA 1) / BETA 1 M ' .,5924 = 0.5Woz = 0.5 X Ritoi X W = 4.7389 IN s. T k* FOR Mz, Iez OBE = 54.3355 IN**4 6.7919 IN**3 Soz_OBE = i s. - SSE CASE ift$* ( g Fa = 0.9XFy = 29.7000

4. 0) X (il/T) X ( Fa / E) *

0. 5=

5.6345 ALPHAi=1.052/SQRT( 2.3003 BETAi =1.052 / SQRT(24. 0) X (W/T) X ( Fa/ E) *

0. 5=

ALPHAi.GT.ALPHAc, RllOi= ( 0. 41 + 0. 59X ( Fy / Fa ) *

0. 5-0. 2 2 / ALPHA L ) / ALPilA i J'II"

.1762 ? = (f 0.5Hez = 0.5 X RHoi X H = 1.4097 IN A h 0.673.GT. BETA 1.LE.BETAc, Rlloi = (1. 3 58 - 0. 4 61/ BETAi) / BETAi ,.6 r' .5032 F 0.5Wez = 0.5 X Ritoi X W = 4.0259 IN g%~ 45.8814 IN**4 FOR Mz, Iez SSE W = Uf Sez SSE 5.7352 IN**3 = 8f~ Icz ANALYSIS = 38.9992 IN**4 Y ?* ~ = .1881E-02 FT**4 CALCULATE Ay FOR Y-DIRECTION SHEAR OBE & SSE KL ' (E) f [ SHEAR AREA, Ay = 2XWXT = 1.5296 IN**2 7

t v

.1062E-01 FT**2 y = akG W .1

*i I;.

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ao 76230.502

'. v !V S 1 'j sk i y. CALCULATE Az FOR Z-DIRECTION SHEAR OBE & SSE k 9i. (F) 1.5296 IN**2 S!! EAR AREA, Az = 2XHXT = .1062E-01 FT**2 26 = + CALCULATE Ixx FOR TORSIONAL MOMENT Mx OBE & SSE ~ " " (G) FOR Mx, Ixx ANALYSIS = 195.7888 INa*4 .9442E-02 FT**4 = ,4 INPUT TO STRING ANALYSIS (STARDYNE FORMAT): Izz Az/A Ay/A j .1273E-01 .9442E-02 .1881E-02 1881E-02 .8345E+00 .8345E+00 { q.- A Ixx Iyy t c ~ l$? ' ' k +.l $.s P [:! hk. . g. k k-a .3-a r 3, s. - p; _ <p. f, ' fl ( h '.t ~ bh{ l ~ 4 1 u+.

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arv cowe av o s o ev i== wot v. # m cAc aro 916 [ Clh jM l I COMPUTAllON 0 o*1 3 SHEET $11/4b yg" x N"D - oare oat i' enoJECT _ Deco FERMI 2__ - CC H'/ AL Duct Evaluation of 43:T so 76230.502 p& system Series wester I ,t O M,6.$ 1 w ' z..- q g.i Overall Stress Evaluations for Rectangular Ducts .p :[ r ff B. s 4316 - 1 ... c (( B.01 Duct String Analysis No. 14 W (in) = x Duct Size: 14 u H (in) = L 0.0516 <=== Enter Value { 0.0478 t (in) = Bare Metal Thickness: = Daro Metal + Coating: Q Section Properties (based on bare metal thickness): ~.-. } 7 1.6768 Arg (in'2) = Gross areat Effect. area (OBE): Axco (in*2) = 0.857324 ~ F Effect. area (SSE): Axes (in*2) = 0.616123 Effect, moment Iyyo (in*4) = 39.16619 s 39.16619 of inertia (ODE): Izzo (in'4) S = e 33.14285 Effect, moment Iyys (in'4) = fr of inertia (SSE): Izza (in'4) = 33.14285 1.3384 Effect, shear area: Any (in*2) = 1.3384 Anz (in*2) = , b-ft(?' Torsional moment Ixx (in*4) = 131.1632 H of inertia: Torsional section* 18.7376 Sxx (in*3) / = modulus: 30 4 Stiffener or C.A. spacing:1 (in) = 192 Effect. length: KLy (in) = 192 KLz (in) = R Radius of gyration: ry (in) = 5.715476 rz (in) = 5.71547 6 = 33.59300 7 Maximum of KL/r: (KL/r) max .g; _ Material Properties (une coated metal thickness for weight): o s, h, ' 29000 E (ksi) = -Modulus of elasticity:Py (ksi) 33 (ASTM A526/A527) y = J-45 (ASTM A526/A527) Yield strength: U^ Ultimate strength: Fu (ksi) = (lb/ft*2) = 2.909274 w Unit weight: r nsh I.oad Data: 8 <=== Enter Value h' Inter, prost.ure : Po(in of v.g.) <=== Enter value = 14 Inter pressure: Ps(in of w.g.) <=== Enter Value = 0.84 i C1 = p Correlation factors: 1.27 <=== Enter Value ^ C2 = s-; 677', 659' & 643'):- Panel vibration input (enveloped El. C.v. using maximum of 3 directions . g:

p. v. -

OBE (4% damping) l A %g. n.

g n' s.

ym Ef 1 rn .g-- - -

...w GENERAL 04b [ COMPUTATION %.c ^t N'" m o paq 4 *' SHEET A ZAMb 0 I k y CCH'/AC I' PROJECT DECO FERMI 2 1 DaTE oaTE Duct Evaluation c1 4316 SUtutCT System Series Jo 76230.502 + 1.9 ACCons (in g's) = + 1.86 rm! ~ ACCoev (in g's) = 2.1 ACCovt (in g's) = y, ACComax (in g's) 2.1 = gg SSE (7% damping) using maximum of 3 directions: 1.52 ACCsns (in g's) = 1.52 ACCsev (in q's) = 1.27 ACCsvt (in g's) = 1.52 ACComax (in g's) = Element Forces from String Analysis No. 4316 - 1 (enveloped & in element coordinates) Dead load: 192 <=== Enter Value Fxd (1bs) = 32 <=== Enter Value 0 Fyd (1bs) = E(' 164.3 <=== Enter Value Fzd (lbs) = 122.9 <=== Enter Value Mxd (1b-ft) = 306.8 <=== Enter value Hyd (1b-ft) = 130.6 <=== Enter Value Mzd (1b-ft) = b; Global seismic loads: 586 <=== Enter Value OBE: Fxo (lbs) h" Fyo (1bs) = 574.9 <=== Enter Value = 155.4 <=== Enter value

y Fzo (1bs)

= 594 <=== Enter Value_- Mxo (Ib-ft) = 594 <=== Enter Value-Myo (1b-ft) =

1^

Mzo (lb-ft) 1617.6 <=== Enter Value = E 731.8 <=== Enter Value M SSE: Fxs (lbs) = 711.3 <=== Enter value-7' Fys (1bs) = 225.9 <=== Enter Value Pzs (lbs) = 861.9 <=== Enter Value pt Mxs (lb-ft) 4 = ( 861.9 <=== Enter Value j,L, Mys (lb-ft) = 2000.9 <=== Enter Value Mzs (lb-ft) = ,t. a o A) Internal pressute stress: 1 Q Longitudinal tensile stress in duct plate 4.162136 e per EQ. (3.6.1-1): fxpts (kni) = 2.866097 fxpto (ksi) = @(d-Longitudinal compressive stress at duct corner 6.292754 g' - per EQ. (3.6.1-2): fxpcs (ksi) = 4.33326G fxpco (ksi) = o Ny# ~ 'Ei 'a B) Panel vibration stress: j ,e + Ek q_. 3' QM x w;h k a.

..=w... 4 m YY I GENERAL., d O *** COMPUTATION mn" voo o 1htin 9. b o % g- ',. SHEET A x PAOJECT DECO FERMI 2 - CCHVAC 5"ni 4O& 77 out ces [ Duct Evaluation of 4316 so 76230.502 System Series 5' SusJECT ] 4 7 [L OBE CASE: Longitudinal tensile stress in duct plate f-per EQ. (3.6.1-3): fxsto (ksi) =1.045423 Longitudinal compressive stress at duct corner per EQ. (3.6.1-4): fxsco (ksi) =1.580580 h SSE CASE:

i Longitudinal tensile stress in duct plate per EQ. (3.6.1-3):

fxsts (ksi) =0.842768 L Longitudinal compressive stress at duct corner f per EQ. (3.6.1-4): fxscs (ksi) =1.274186 shall be combined The stresses calculated under B)ia SRSS Note: with those calculated under D) v i Dlate stresses due to dead load when combined w th H C) (' OBE Axial tons, stress: fxdto (ksi) = 0.071<27 Axial comp. stress: fxdco (ksi) = 0.223952 f bzdo ( ksi) = 0.280098 Dending stress: fbydo(ksi)= 0.657996 Shearing stresses: 1 'O' Y-dir. ftydo+fvydo (ksi) = 0.102617 Z-dir. ftzdo+fvzdo (ksi) = 0.201466 i El SSE: Axial tons. stress; fxdts (ksi) = 0.071727 S ' -- Axial comp stress: fxdes (ksi) = 0.311625 fbzds(ksi)= 0.331003 Bending stress: fbyds(ksi)= 0.777579 Shearing stresses: A Y-dir. ftyds+fvyds (ksi) = 0.102617 Z-dir. ftzds+fvzds (ksi) = 0.201466 y(y 1 D) Plate stresses due to global seismic loads t OBE: Axial tens. stress: fxgto (ksi) =0.218918 ~ ((,h' Axial comp. stress: fxqco (ksi) =0.683522 Dending stress: fbzgo(ksi)= 3.469277 ^- f bygo (ksi) = 1.273955 ,e wD' 't ?'b Shearing stresses: Y-dir. f tygo+fvygo (ksi) =0.809954 f Z-dir. ftzgo+fvzgo (ksi) =0.496520 J[ fxgts (ksi) =0.273386 IE Axial comp. stress: fxges (ksi) =1.187748 ^ .[ k SSE: Axial tens. stress: ~V f bzgs (ksi) = 5.071246 Bending stress: 'l ^ - pt a ys .j. u "q A i ("I .m y, e kW

~ n i Rtv Coup 81 C>arO #7 y tem Wor 3%. Am CA Cwaf(Pe WTPs0 ' " ^ 25 GENERAL DC-$773 O/f'b OkN' i~*f?**'* " " COMPUTATION 0 h ~~ SHEET Y1.4{Gb-i "" bl " M oatt oatt PaostCT Deco FEPJ41 2 - 00HV Aq_ Duct Evaluation or 4316 so 76230.502 c, System series yg 7' suastc1 9 -y; e;- j f bygs (ksi) = 2.184470 .i. if Shearing stresses: Y-dir, ftygs+fvygs (ksi) =1.083436 s 5 % p4 u_ ,~ '2-dir,' f tzgs+f vzgs. (ksi)._ =0.7 20764 ---s-.-.m_ y c,0 W E) Overall stress evaluation: E.1) Combined axial tension & bending stresses fto=fxpto+(fxdto+fbydo+fbzdo)+((fxgto+fbygo+ I OBE: ksi f bzgo) "2 +f xsto"2)

0.5= 8.947000 o:

l ' Fto (Allowable) = 0.6*Fy = 19.8 ksi Fto >= fto, OK <=== fts-fxpts+(fxdts+fbyds+fbzds)+((fxgts+fbygs+ SSE: fbzgs)'2+fxsts"2)'O.5= 12.91857 ksi Fts (Allowable) = 0.9*Fy = 29.7 ksi Ftn >= fts, OK <=== $3, 3 1

.3%

E.2) Combined axial compression & bending stresses fxdco&fxgco CBE: fxco(per EQ. (3.4.1-3)) = l4 0.907474 ksi = Fac = 16.62842 ksi Fao (Allowable) = 19.8 ksi Fno (0.6*Fy) = s,? For fxco/Fao <= 0.15: U Fbyo = Fbzo = 19.8 ksi ( 4 A For fxco/Fao > 0.15: i Feyo = 132.3285 kai e

l:

Fezo = 132.3285 ksi U-fxgo(using full area)= ( Axco/ Axq)

f xco 0.290645 ksi

= 9. Fbyo = 19.75651 ksi 4, Fbzo = 19.75651 kai i -;j#p. ? For this case, fxco/Fao = 0.054573 <= 0.15 P USE Fbyo = 19.8 ksi 'b +. Fbzo = 19.8 kai dE g x Vf{ Overall interaction coefficient (IC): m u p. IC=(fxdco/Fao+fbydo/Fbyo+fbzdo/Fbzo)+(fxpco/Tmo)+ f,. 4 M ((fxgco/Fao+fbygo/Fbyo+fbzgo/Fbzo)~2+ 0.571492 <= 1.0 (fxsco/Fmo)'2) 0.5 = y OK <=== $r [; " ~ fco-fxpco+(fxdco+fbydo+fbzdo)+((fxgco+fbygo+ M. f bzgo)

2 +f xsco'2)
0. 5= 11.14756 ksi y,4 n

p[*. SSE: fxes(per EQ. (3.4.1-3)) = fxdcs+fxges i 1.499374 kai , :p = -Fas(Allowable)= 1.5*Fao = 24.94264 ksi +,, @a = 1.g z .x 8, i [k [f

f;;

?{% 9 9 m. pp? ,s, --- +

___.__.-.,__._m_______

r,, - .s, 1 ' V * %i! Ma $ 4) 7

GENFRAL

'w re W*** COMPUTATION e SHEET vm o ,d Hei h_ H x _7 I PHOJECT Deco FEFlij.2 - CCityAC "" bb " Y ~ ~ ~ g# gyp @ Duct Evaluatton of 43 6 oats oart GusJtci Systen Series so 76230.502 a p Fms (0.9*Fy) = 29.7 kai 7 For fxco/ Fan <= 0.15: i= Tbyn = Fbzs = 29.7 kni E' For fxen/ Fan > 0.15: Feys = 198.4928 kai Foza = 198.4928 kai fxgs(uning full area)= (Axes /Axg)*fxen = 0.345113 kai Tbya = 29.64836 kai 1 Tbzu = 29.64836 kai for this caso, fxes/ Fan = 0.060112 <= 0.15 USE Fbya = 29.7 kni Tb3s = 29.7 kni n> overall interaction confficient (IC): b, IC= ( f xdcs/ Fan + f byda/ Fbyn+ f bzda/ Fbza) + ( f xpen/ Fms) + R-- ( f xacn/ Fmo)

2 ) ygs/ Fbys + f bzgn/ Fbzo)
2 +

((fxges/ Fan +fb 0.556752 <= 1.0 0.5 = OK <=== f csa f xpcs+ ( f xdes+ f bydn + f bzds) + ( ( f xqco + f bygs+ y( fbzgn)'2+fxscs'2)*0.5= 16.25203 kai f av - ff F. 3 ) Combined in-plano chear stress J+ 4g OBE f* Allowable shear otrons for ducts with Pittsburgh lock longitudinal scamn (por EQ.3.5-1): a ~ Tvyo (kni) 2.704437 =

jet, Fva.o (kni) 2.704437 u

F: Maximum chcar allowable (0.4*Fy): 4 Fvmo (kni) 13.2 = 7 Use shoar allowable: M 3F Fvyo (ksi) 2.704437 M = &Q;y Fvzo (kai) y' ' 41 - 2.704437 _? = y Combined chcar utrossen in Y-direction: F fyyo (kai) =(fyydo+ftydo)+(fvygo+ftygo) 0.912571 = ,p fvyo <= Fvyo,ox <=== hR. Combined shear strenson in Z-direction: k fvzo (kni) =(fvzdo+ftzdo)+(fvzgo+ftzgo) WE h. 0.697986 ww = '??? T~ tygo <= Pvzo ox <=== f Maximum in-plano chear streno ='O.912571 kok g{ d+* SSE: M

L. !-l

?;

$ NT w Allowable ahear stress for ducts with Pittaburgh lock u_.h _ L nQ a lh L f,y nqJ w L p;;@. \\y y .a M4 ~^ p_ (-, < lg _% * / rr 33 ; -t

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- U O& 77 cats part Duct Evaluatien of 4316 SututCT System Series Jo 76230.502 P

A vr ^ longitudinal seams (per EQ.3.5-3): 3.940012 A Fvys (ksi) = 3.940012 Fvzs (ksi) = Maximum shear allowable (0.52*Fy): 4 17.16 U Fvas (ksi) = Use shear allowable: 3.940012 Fvys (ksi) = 3.940012 Fvzs (ksi) = s ? Combined shear stresses in Y-direction: fyys (ksi) =(fyyds+ftyds)+(fvygs+ftygs) 1.186053 = fvys <= Fvys,OK <=== Combined shear stresses in Z-direction: fvts (ksi) =(fv:ds+f t:ds) +(fvzgs+f tzgs) 0.922231 = ~ fvzs <= Fvzs[OK <=== 1.186053 ks ? Maximum in-plane shear stress = -.,Q '?:: *' .:r Q: a dr w. jh.~ ( 4

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0^ t3 0^'E 'j, Duct Ev tuation of 4316 ao 76230.502 l System Series sueJECT ,1 m, + += + p:> \\ 2 q_ n: Qg Overall Stress Evaluations for Rectangular Ducts (Con't) { ! hh d = .B. W. c B.02 Duct String Analysis No. 4316 - 2 ~ ! 19 x, Duct Size: W (in) = 19 H (in) = ~ i 0.0470 Bare Metal Thickness: t (in) = 0.0516 <=== Enter Value Bare Metal + Coating: = ~, ~

i Section Properties (based on bare metal thickness)

v a y-p 3.6328 Gross area: Axg (in*2) = Effect. area (OBE): Axco (in*2) = 0.857022 Effect, area (SSE): Axes (in*2) = 0.615559 h, Effect. moment Iyyo (in*4) = 82.40558 4 of inertia (OBE)

Izzo (in~4) = 82.40558 Effect. moment Iyys (in'4) = 69.28337 of inertia (SSE):

Izzs (in~4) = 69.28337 1.8164 Effect. shear area: Asy (in~2) = 1.8164 7" Asz (in*2) = j f!j Tor:lional moment I Q.. of inertia: Ixx (in*4) = 327.8602 Torsional section

N ri-34.5116

{ dM modulus: Sxx (in'3) = Stiffener or C.A. spacing:1 (in) 30 = h* Effect. length: KLy (in) = 164 186 'E. KLz (in) = gg, Ra'dius of gyration: ry (in) = 7.756717 t 3u rz (in) = 7.756717 o/ T@ Maximum of KL/r: (KL/r) max = 23.97921 gp . ~ - Material Properties (use coated metal thickness for weight): h 6, w 'I p Modulus of elasticity: E (ksi) 29000 PR = 33 (ASTM A526/A527) Yield strength: Fy (ksi) = 45 (ASTM A526/A527) N Ultimate strength: 7u (ksi) = 0 .g g Unit weight: w (lb/ft*2) = 2.909274 q,k. %$[ Load Data: pw 6.5 <=== Enter Value' "I i Inter. pressure: Po(in of w.g.) j MP = 6.5 <=== Enter Value Q = 47 Inter.. pressure: Ps(in of v.g.) Correlation factors: C1 = 0.34 <=== Enter Value - W p; e C2 = .1.27 <=== Enter Value M (1 af SM w ~k 1 Panel vibration input (enveloped El. 677', 659' & 643'):

q py,;

OBE (41 damping) using maximum of 3 directions: M II. 1 ,^ y - Ql1

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~

V ACCovt in gs) = 2.1 ACComax in g s) = ( ssE (7% damping) using maximum of 3 directions: i,j 1.52 J I ACCons (in g's) e = 1.52 ACCnev (in g's) = 1.27 ACCovt (in g's) = 1.52 f [: ACCucax (in g's) = 4316 - 2 ~ Element Forces from String Analysis No. k (enveloped & in element coordinates) ' de s 9;, Dead loads 309.3 <=== Enter Value t Fxd (1bs) = 80.3 <=== Enter Value f D.) Pyd (1bs) 159.3 <=== Enter Value a = c Fzd (lbs) = 102 <=== Enttr Value Mxd (Ib-ft) i = 343.9 <=== Enter Value ,f. Hyd (lb-ft) = 122.9 <=== Enter Value Mzd (lb-(t) = ~ v, y T' Global seismic loads: 715.7 <=== Enter Valuo t r ODE:' Fxo (lbs) = Fyo (lbs) = 443.3 <=== Enter Value 145.3 <=== Enter Valus '/ e Fzo (Ibs) = 449.7 <=== Enter Valuo '1' Mxo (1b-ft) = 556.6 <=== Enter Value Myo (lb-ft) = 873 <=== Enter Valuo Mzo (lb-ft) = g 1005.9 <=== Enter Value SSE: Fxs (lbs) = l Fyn (lbs) 621.3 <=== Enter Valuo = 207.7 <=== Enter Value L. Fzs (lbs) = 610.4 <=== Enter Value y Mxs (1b-ft) = 6 Mys (lb-ft) 782.2 <=== Enter Value' = d 1207.3 <=== Enter Valuo Mzs (1b-ft) = 4,; V s. g: e; A Internal pressure stress: h)umrMkmew[EdIEa~19ensilofutresseingduqt plate m _. 'd m r Long a j ( por EQ. (3.6,1-1): fxpts (ksi)~ s 27495590*d"*uiMWsd%mpq ? fxpto (kni) = 2.495590 0-Longitudinal compressivo stress at duct corner ( por EQ. (3.6.1-2): fxpcs (ksi) = 3.773094 fxpco (ksi) = 3.773094 r .g. D) Panel vibration stress: n (. ,,,4 4 g a 7 ? N

):,

l;

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no cmo w c.uovo. ut m mv uw e; g" U /g ^ ~ COMPUT ATION "*^6 vm 0 %j'*t.' p I SHEET 4 i 9 x. em0 JECT _D, Eco _ FQt:LL-CC)W AC "" %

D catt oars Duct f. valuation of 4316 so 76230.S02

^ SundCf System Series ? N"o OBE CASE: Longitudinal tensito stress in duct plate 7 per EQ. (3.6.1-3): fxato (ksi) =1.045423 Longitudinal compressive stress at duct corner por EQ. (3.6.1-4): fxsco (kni) ='.580580 i SSE CASE: Longitudinal tensile stress in duct plate s .e,. T per EQ. (3.6.1-3): f xsts (kni) =0.842768 Longitudinal compressive stress at duct corner i '.~ per EQ. (3.6.1-4): fxsca (ksi) =1.274186 shall be combined The stresses calculated under B)ia SRSS lhte with thoso calculated under D) v Plate stresses due to dead load when combined with g l -{ C) OBE Axial tenu, stress fxdto (ksi) = 0.015140 t: Axial comp. stress fxdco (ksi) = 0.360900 W( y1 Honding stress: tbrdo(ksi)= 0.170020 3S (bydo(kai)= 0.475751 h Shearing stresses Y-dir. ttvdo+fyydo (ksi) = 0.079674 K 7, Z-dir, ftzdo+fvzdo (ksi) = 0.123167-g.- SSE: Axial tens. stress fxdts (ksi) = 0.08$140 w ( Axial comp. stress: fxdcs (kai) = 0.502469 .'4 Dending stress: tbzds(ksi)= 0.202221 tbyds(ksi)= 0.565850 ? Shearing stresses: ?. Y-dir, ftyda+fvyds (ksi) = 0.079674 Z-dir. Itr.ds+fvzda.(ksi) = 0.123167 'N }g Plate stresses due to global seismic loads D) a f-ODE: Axial tens. stress: f xgto (ksi) =0.197010 hi '6xial comp. stress fxgco (ksi) =0.835101 yo l Dending stress: tbzgo(kai)= 1.207709 s fbygo(ksi)= 0.770001 4+, Y-dir. ftygo+fvygo (kni) =0.400418 '., if Shearing stresses E"' [y... fxqts (ksi). =0.276893 Z-dir. L'tzgo+fvzgc (ksi) =0.236358 4 y% SSE: Axial tens. strosci Axial comp, streus fxges (ksi) =1.634123 3 a* i t. Bending stress fbzgs(kni)= 1.986511 - a Qt i Q;].-

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^" GENERAL 03 5773 O ,,0 [,/ 1 COMPUTATION "" I ' **' 0 I "i I. g { Juat W" SHEET ~~~ ~ El emostcf,,9170 FEPMI 2 - CCHVAC Duc IEvaluation of 4316 - W care o tu so 76230.5n2 / Svaltcr System Series pl -e 1. d. 1 ~ fbygs(ksi)= 1.287044 ?(3 Y Shearing stresses Y-dir. f tygs+ f vygs (ksi) =0.554291 Z-dir. f tzgs+fvzgs (ksi) =0.326588 r [ [ E) Overall strous evaluation: I J E.1) Combined axial tension & bending strouses I) ' O OBE: fto=fxpto+jfxdto+fbydo+fbzdo)+((fxgto+fbygo+ tbzgo) 2+fxnto*2)*0.5= 5.639451 k s., 19.8 ksi j i ' in Fto (Allowable) = 0.6*Fy = Pto >= fto, OK <=== l f. fts=fxpts+{fxdts+fbyds+fbzds)+((fxgts+fbygs+ i SSE: l tbzgs) 2 + f xsts

2)
0. 5= 6. 997 914 ksl Fts (Allowable) = 0.9ery = Pts >= fts, OK 29.7 ksi

<=== l A (. i E E.2) Combined axial compression & bending stresses i lL. OBE: 1xco(per EQ. (3.4.1-3)) = fxdco+fxgco 1.196001 ksi = 4-Fac = 16.90263 kai $ I Foo (Allowable) = 19.8 kai i ? Fmo (0.6*Fy) = For fxco/Fao <= 0.15: li L Tbyo a Tbzo = 19.8 kai l 0 For fxco/Fao > 0.15: Feyo = 334.0561 kai Fezo = 259.7055 ksi l ; f fxgo(using full area)= (Axeu/Axg)*fxco i dj 1 0.282151 ksi c. e = _k$ Pbyo = 19.78327 ksi 4 Fbzo = 19.77848 kai n po: $N For this case, fxco/Fao = 0.070758 <= 0.15 N USE Tbyo = 19.8 kai 6;- Pbzo = 19.8 kai i g overall interaction coefficient (IC): + IC=(fxdco/Fao+fbydo/Fbyo+fbado/Fbzo)+(fxpco/rmo)+ h l {! ((fxgco/Fao+fbygo/Fbyo+fbzgo/Fbzo)*2+ s 0.413820 <= 1.0 4 ( f xsco/ Fmo) ' *t ) 0.5 = 7[ + %- OK <=== } fco=fxpco+jfxdco+fbydo+fbzdo)+((fxgco+fbygo+- 7 y{a ~ j fbzgo) 2&fxsco*2)*0.5= 8.006242 ksi n 1 ; Q SSE: fxes(por EQ. (3.4.1-3)) = fxdes+fxges ",J 2.136593 kai = J Wf j; Fas ( Ali.owable) = 1. 5

Fao = 25.35395 ksi

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o 76230.502 Systen Series SunJtct 1

0 29.7 kai U{ Fms (0.9*Fy) = For fxes/ Fan <= 0.15: Tbys = Fbzs = 29.7 ksi 1 For fxes/ Fan > 0.15: f' Feys = 501.0841 koi / Fats = 389.5583 ksi fxgs(using full area)= (Axes /Axg)*fxcs 0.362034 kai = Tbys = 29.67854 kai Tbts = 29.67239 ksi )'S k For this case, fxes/Fas = 0.084270 <= 0.15 USE Thys = 29.7 kai L Fbzs = 29.7 ksi overall interaction coefficient (IC): 6 ~ 1C= ( f xden/ Fas+ f byds / Fbys+f b2ds / Fbas) + ( f xpcs/ Fan)'?~*"", n;p u newm % m%.,.._. ((fxges/Fas+fbygs/Fbys+fbrys/Fbzs)*2+ 0.352584 <= 1.0 O. (fxacs/Fes)*2) 0.5 = OK <=== (; fes=fxpcs+(fxdes+fbyds+fbrds)+((fxqca+fbygs+ kai tbzgs)*2+fxscs*2)'O.5= 10.11403 ,,( E.3) Combined in-plane shear stress OBE: Allowabic chear stress for ducts with Pittsburgh lock I longitudinal seams (per EO.3.5-1): 2.316954 Fvyo (ksi) t = ?L Fvzo (ksi) = 2,316954 'g,*qi - Hax4. mum shear allowable (0.4*Fy); 3 13.2 0 Fvmo (ksi) = Use shear allowable L 2.316954 9 Fvyo (ksi) = 2.316954 k Tvro (ksi) = / _,.h' Combined shear stresses in Y-directions fvyo (ksi) =(fvydo+ftydo)+(fvygo+ftygo) 0.480093

(

fyyo <a Fvyo,0K <=== 't- = $3 Co7bined shear stresses in Z-direction: rh ' fvzo (kni) =(fvzdo+ftzdo)+(fvzgo+ftzgo) 9; 0.359525 p ', _ + .' t- = i r.- fvzo <= Fvzo OK <=e= 0.480093 kuk t hq Haximum in-plane shear stress = 1 f.4 w q $$ F. 3 s:@o:. tj t 7 E Allowable shear stress for ducts with Pittsburgh lock </M Tj: N Q, Q; k N' q ;g Y $$ Kf* w y [h

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^ P%TCt ~ DECO FEM ' / - Egg /;AC 1 cars cars S""' ~ Duct f.vah.stion of 4316 ao 76230.502 Sua>fCf System Series te A longitudinal seams (per EQ.3.5-1):.1.475431 ryys (ksi) R = 3.475431 rvzs (ksi) = Haximum shear allowable (0.52*ry) s 17.16 0' ryms (ksi) = 000 shear allowablet /. Tvys (ksi 3.475431 Tvzs (ksi)== ) ) 3.475431 Combined shear stresses in Y-direction =(fvyda+ftyda)+(fvygs+ftygo) e f vya (ksi) 0.633966 b i fyys <= Fvyn,0K <=== = e Combined chear stresses in Z-directions =(fv2dn+ftzdo)+(fvzgs+ft29s) ( fvts (ksi) 0,449756 OX <=== L = fvts <= TVZo1 0.633966 kn ~ g_ 1:l Maximum in-plane shear strero = u {. p? 4 E i s 'e u~ f 1 w,c ) y lj i j N. %d 3e. N l

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x i' rnon ct _ DECO __[f2V)))_L - CCH V A C "" J O " l1 catt oars ~~ Duct Evaluation of 4316 System Serien jo 76230.50? SunACf 1 D. Overall Streun D.aluations for Hectangular Ducts (Con't) [ D.02 Duct String Analysis No. 4316 - 2 (Con't) 19 k Duct Size: W (in) = 19 H (in) = 6 Daro Hotal Thickness: t (in) 0.0478 = 0.0516 <=== Enter Value 3 Dare Metal + Coating: = d Section Proportien (based on bare inctal thick ess): 3.6328 E Group area: Axg (in~2) = Effoct. area (OBE): Axco (in*2) = 0.857022 l Effect. area (SSE); Axes (in"2) = 0.615559 r' in*4) = 82.40558 (in*4) = 82.40558 Effect. moment lyyo N}}. (in*4) of inertia (ODE) : Izzo 69.28337 ( f Effect. moment Iyys = 69.28337 y' of inertia (SSE): Izzn (in*4) = 1.8164 l7 Effect. shoal area: Any (in*2) = 1.8164 Asz (in~2) = i Torsional moment 327.8602 lL' g of inertia: Ixx (in*4) = i-Torsional nection, 34.5116 K! modulus: Sxx (in*3) = 30 Stiffener or C.A. spacing:1 (in) = 164 4 Effect. length: KLy (in) = 186 KLz (in) r M '.' 7.756717 [ Radius of gyration: ry (in) a 7.756717 rz (in) = n 23.97921 l${ Haximum of KL/r (KL/r) max = M ? Haterial Propertien (use coated metal thicknens for weight): 29000 Modulun of clasticity: E (ksi) = 33 (ASTM A526/A527) Yield strength: Fy (ksi) = = 45 (ASTH A526/A527) Ultimate strength: Tu (kni) 2.909274 Unit weight: w (Ib/ft 2) = Load Data: e.- = 8 <=== Enter Value gi Inter, prensure: Po(in of v.g.) 14 <=== Enter Value 7 Inter, pressure: Pn(in of w.g.) = Correlation factora: C1 = 0.84 <=== Enter Value. C2 = 0.47 <=== Enter Value; g. ' 4 +g .[ h Panel vibration input (enveloped El. 677', 659' & 643'); ue i ODE (4% damping) using maximum of 3 directions: ,,'1, m; - ll- %, v x y .2 c

a kk{

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ihv

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- MI Duct Evaluation of 4316 Jo 76230.502 System Series 7

susJCCT -

141,

+ ACCons (in g's) = 1.9 ,3 ACCoeV in q'sh = 1.86 2.1 ACCovt in gsD = M ACComax in g sj = 2.1 Q-- using maximum of 3 directions: u SSE (7% damping) { 1.52 ACCans (in g's) = 1.52 ACCsev (in g's) = 1 1.27 ACCsvt (in g's) = 1.52 b' ACCamax (in g's) = g; from String Analysis No. 4336 - 2 x,; Element Forces in element coordinates) 4 (enveloped & 6-309.'s <=== Enter Value Dead load: Fxd (lbs) = 80.3 <=== Enter Value [s ~ Fyd (lbs) 159.3 <=== Enter Value = Pzd (lbs) 102 <=== Enter Value = e Mxd (1b-ft) 343.9 <=== Enter Value = lE Hyd (1b-ft) = 122.9 <=== Enter Value > tEr Mzd (Ib-ft) = [1 Global seismic loads: 715.7 <=== Enter Value K> OBE:* Fxo (1bs) = Enter Value 443.3 <e== Fyo (1bs) = 145.3 ;=== Enter Value-Y- Fzo (lbs) 449.7 <=== Enter Value = Mxo (lb-ft) = 556.6 a== Enter value Hyo (Ib-ft) = 873 *.'=== Enter Value 1, Mzo (lb-ft) = f 1005.9 <=== Enter Value ,9 SSE: Fxa (1bs) 621.3 <=== Enter Value = W Fys (1bs) = 207.7 <=== Enter Value [' Fra (lbs) <=== Enter Value = 610.4 v. Mxs (Ib-ft) 782.2 <=== Enter Value, = Mys (1b-ft) 1207.3 <=== Enter Value_. y = Mza (Ib-ft) = e I Elll [ A) Internal pressure stress: 1,ongitudinal tensile stress in duct plate = 4.162136 $N i per EQ. (3.6.1-1): fxptu (ksi) fxpto (ksi) = 2.866097 g L 1.ongitudinal compressive stress at duct corner por EQ. (3.6.1-2): fxpcs (ksi) = 2.328814 T s

?w fxpco (ksi) = 1.603649

-a ~ 3,g 3 y Panel vibratjon stress: .y g. B) a.,{k E" g g. .-g .hg -[; \\ps I .l% e j .:. w I x_-

c

=< w s...,. o GENERAL h

f g -' y.;'," SHEET O COMPUTATION mnw vc=o 0 x PROJECT,pEco FERMI ? -J CHVAc e "" O " ~ 0*ft 0411 _~ Duct Evaluation of 4316 so 7G230.502 i l ta;eatet Systen Series 4 y. m c f, q OBE CASE: 'l Longitudinal tensile stress in duct platef xsto (ksi) =1.045423 l,' per EQ. (3.6.1-3): 3 Longitudinal compressive stress at duct corner ( per EQ. (3.6.1-4): fxsco (ksi) =0.584939 SSE CAS,': y Longitudinal tensile stress in duct plate per EQ. (3.6.1-3): fxsts (ksi) =0.842768 C 7 Longitudinal compressive stress at duct corner per EQ. (3.6.1-4): fxsca (ksi) =0.471549 shall be combined l_ The stresses calculated under B)ia SRSS. Note: with those calculated under D) v t plate stresses due to dead load when combined with C) OBE: Axial tons. stress: fxdto (ksi) = 0.085140 ,i Axial comp, stress fxdco (ksi) = 0.360900 l tbzdo(ksi)= 0.170020 w' Dending stress: tbydo(ksi)= 0.475751 Shearing stresses: Y-dir, f tydo+f vydo (ksi) = 0.079674 [j Z-dir. ftzdo+fvzdo (ksi) = 0.123167 i i SSE: Axial tons. stress: fxdts (ksi) = 0.085140 I{ Axial comp. stress: fxdco (ksi) = 0.502469 fbzds(kai)= 0.202221 Bending stress: fbyds(ksi)= 0.565858 A I i ff Shearing stresses: r p. Y-dir. f tyds+fvyds (ksi) = 0.079674 p, 2-dir. f tzds+f vzds (ksi) = 0.123167 d D) plate stresses due to global seismic loads sz s M f E. OBE: Axial tons. s.ieers: fxgta (ksi) =0.197010 e Axial comp. stress: fxgco (ksi) =0.835101 fbzgo(ksi)= 1.207709 y E Bending stress: tbygo(ksi)= 0.770001 4 m., q M Shearing stresses Y-dir. f tygo+fvygo (ksi) =0.400418 V 1H ,j Z-dir. f tzgo+fvzgo (ksi) =0.236358 T% 7 N SSE: Axial tons, stress fxgts (ksi) =0.276893 b {E. Axial comp stress: fxges (ksi) =1.63412'l ,.. M s fbzgs(ksi)= 1.986511 Bending stress g, :; g f y@J ee l

M: n i

h, u: l-c. q~f: 4

e,= w r %. a. WU. '^ GENERAL M WOh" COMPUTATION F 0 SHEET 4/f$ hI I_ 'au .. ~. ee4 .~ x PROJECT DECO FERMI ? - CCMVAC "" 9 !!. 17 - oats oats Duct Evaluation of 4316 so 76230.53 t.va>(C f System Ser!es I tbygs (ksi) = 1.287044 [L Shearing stresses: Y-dir. ftygs+fvygs (ksi) =0.554291 J-Z-dir. ftzgs+fvzgs (ksi) =0.326588 E) Overall stress evaluation: E.1) Combined axial tension & bonding stresses fto=fxpto+(fxdto+fbydo+fbzdo)+((fxgto&fbygo+ ksi OBE: fbzgo)*2+fxsto*E)*0.5= 6.009959 kai 19.8 y: Fto (Allowable) = 0.6*Fy = Fto >= fto, OK <=== p f xdts+ f byds+ f bzds) + ( ( f xgts+f bygs+ fts=fxpts+l2+fxnts*2)*0,5= 8.664460 ksl F3E: (bzgs) 29.7 kai Fts (Allowable) = 0.9*Fy = Fts >=-fts, OK <=== Coobined axial compression & bending stressos f' E.2) OBE: fxco(per EQ. (3.4.1-3)) = fxdco+fxgco 1.196001 ksi f, = Fac = 16.90263 k91 Fao (Allowable) = 19.8 kai

.H '

Fmo (0.6*Fy) = p for fxco/fao <= 0.15: 19.8 kai Pbyo = Fbzo = th For fxco/Fao > 0.15: ?; Feyo = 334.0561 kai Fezo = 259.7055 kai fxgo(using full area)= (Axeo/Arg)*fxco 0.282151 kai s = Fbyo = 19.78317 kni [k'r Fbzo = 19.77840 kai [ \\ For this case, fxco/Fao = 0.070758 <= 0.15 s fiw USE Fbyo = 19.8 kai Fbzo = 19.8 kai 9 overall interaction coefficient (IC): t m 1 N IC=(fxdco/Fao+fbydo/Fbyo+fbzdo/Fbro)+(fxpco/Pmo)+ ((fxgco/Fao+fbygo/Fbyotfbzgo/Fbzo)*2+

p,c (fxsco/Fmo)*2) 0.5 0.287144

<= 1.0 = IR . OK <=== 's 1 '. v fco-fxpco+(fxdco+fbydo+fbzdo)+((fx co+fbygo+ u kai f$. fbzgo)~2+fxsco*2)*0.5= 5.48331

)c 1

Ds SSE: fxes(per EQ. (3.4.1-3)) = fxdcs+fxgcs y 2.136593 kai = 25.35395 kai 1" Fas(Allowable)= 1.5*Fao = a w$ -;Q w A y %? -3 *,; gy[ c 0;g

r ku Y

x _ _ _ -y,}{. - -@

e,= 5xig. 4.n ex oratc u t 4: mv ccw cv o,* o se M f RN %.a' 70 COMPUTATION O 4!witk SHEET ,N x s l paoxct Deco FERMI 2 - ccHVAc "" b#1 " ~I 1 ~ pit pra ~ Duct Evaluation of 4316 so 76230.502 System Series tk SUGXC f Y< h Fan (0.9*Fy) = 29.7 kai For fxcs/Fas <= 0.15: 29.7 kai n'P Tbys = Fbzs = For fxcs/Fas > 0.15: A Feys = 501.0841 kai Fezs = 389.5583 kai

q fxqs(using full area)= (Axes /Axg)*fxcs 0.362034 kai

= Tbys = 29.67854 kbi Fbzs = 29.67239 kal 'I rS For this case, fxcs/ Fan = 0.084270 <= 0.15 USE Fbys = 29.7 kai Fbzs = 29.7 kai j i overall interaction coefficient (IC): i IC= ( f xdes / Fas+ f byds/ Fbys+ f br ds / Fbz s) + ( f xpcs/ Fms) + et ((fxges/Fas+fbygs/Fbys+fbzgs/Fbzs)"2+ 4 0.299483 <= 1.0 (fxscs/Fms)*2) 0.5 = OK <=== M. f es= f xpcs+ ( f xdes + f byds+ f bzds) + ( ( f xges+ f bygs+ ksi fbzgs)"2+fxacs*2)*0.5= 8.529645 + b E.3) Combined in-plane shear stress g% OUE' Allowable shear stress for d' cts with Pittsburgh lock s f1 longitudinal seams (per EQ.3.5-3): 2.294724 Fvyo (ksi) 5 = 2.294724 Fvzo (ksi) = ,c,6 Maximum shear allowable (0.4*Fy): W 13.2 3 y Fvmo (ksi) '1' = gei Use shear allowable 2.294724 F[h/ Fvyo (ksi) P = 2.294724 ':> : W' d(- Fvzo (ksi) = ifs

f '

Combined shear stresses in Y-direction: fvyo (ksi) -(fvydo+ftydo)+(fvygo+ftygo) p;t 0.4 BOO 93 <=== = fvyo <= Fvyo,OK 4: s' if' Combined shear stresses in Z-direction: h, fvro (ksi) =(fvzdo+ftzdo)+(fvzgo+ftzgo) 7' 0.359525 S s fvzo <= Fvzo OK <=== = kok ,:n a*8 + 0.480093 !?.* Maxitium in-plane shear stress = I' .g gA$ .A h, p.1 + SSE: z{.,+ Allowable shear stress for ducts wit.h<Pittsburgh lock d,,.l,[ 4 .s .t iL ? + p. m m. [&,- b..; ~y G,l r

%N.

n i a:r

gW -

y!

== w,1.s 4ta bl '

i GENERAL o filb. COMPUTATION O ~ ~ ~ o an h:kt; sneer 4h4/# d x ( 5 5_ f 7l oatt ous PAO,stCT Deco FERMT ? - CCHVAC 9a rt Duct Evaluat.icn c: 4319 so 76230.502 System Series { '7 4 SututCT va, longitudinal seams (per EQ.3.5-1): 2 3.325442 Fvyn (ksi) = e,, 3.325442 y Fvzu (ksi) = g Maximum shear allowable (0.52*ry): 17.16 2 y Fyms (ksi) = Uno shear allovables g 3.325442 L Fvys (ksi) s = 3.325442 Fvzs (ksi) = C ?, Combined shear stresses in Y-directions t fyys (ksi) =(fyyds+ftyds)+(fvygo+ftygs) = 0.633966 K fyys <= Fvys,0K <=== Combined shear stresses in Z-directiont >U Ivra (ksi) =(fvads+ftzds)+(fvzgs+ftzgs) 0.449756 = fvzs <= Fvza,0K <=== s 0.633966 ksi Maximum fn-plane shear stress = a.f . l_ ?' i a 4 , o !;y '4 ile I-[gL 4 h, K,* .f e 4s n .D 3* i e? 4 y;> q[e 3.. 1, .r e k[ p. b y fE5 i.

.yQ a r.

w R;m;p ab.:. .v M 'yg ' - ',' f y tg /kc y\\ 4 m[j I(, f,3& y '5 G f.Q z, .yp -gs Jp-f,,.... . m\\ ' %\\,f ,u I1_M [ <a -W 'o ( q.:.y[ Y ,? .IEi Ils k' ay+ v,

!:C % &

N} M M('; b wp:r c

yl FSy&

M 0

+

qid m. Wl% fj f 4 4 ag O t 3, B ~ ;;r ,$m{ ( $4 X :a,g9-(G l w

ac

%$ (f g.i t A m_ 7 ' ',* 'r*. z_'> kk h ug -

5. plvn y;l(

kj? m k 2 pp, y 1

lE l pygrv=yrgyJ2Ty l l .,.w.....a_,._._.-._._. W GENERAL

,;c. 5 7 71 f.

i r 'o"f. i 4"* " C*'"** COMPUTATION ^ o 7j he .4 SHEFT i t enOXCT DECO FERMI __2 - C ';H'k -

qq D

D l Duct Evaluation of 43:6 so N230.502 b Gus#C f Systen Series I 7 4 s-s_ y. f Overall Strecs Evaluations for Rectangular Ducts (Con't) f D. 3 5 E D.03 Duct String Analysis No. 4316 - 3 4-- r 10 W (in) = y i Duct Size: 10 H (in) = 3 L Bare Metal Thickness: t (in) = 0.0478 0.0516 <=== Enter Value l-(, Bare Metal + Coating: = P-5 Section Properties (based on bare metal thicknesu): s LI 1.912 j-O' Gross area: Axg (in*2) = E Effect. area (OBE) : Axeo (in'2) = 0.829775 N Effect. area (SSE): Axes (in'2) = 0.597476 17.02515 Effect, moment lyyo (in*4) = hr[-- 17.02515 of inertia (OBE): Izzo (in*4) = 0 Effect. moment Iyys (in'4) = 14.37405 14.37405 ![i-of inertia (SSE) : Izzs (in~4) = 0.956 Effect, shear area: Any (in'2) = 0.956 Asz (in*2) = j-P- N' Torsional moment k 47.8 of inertia: Ixx (in*4) [4-I Torsional section = i fe 9.56 c-medulus: Sxx (in'3) = = 60 L Stiffener or C.A. spacing:1 (in) 84 W Effect. length: KLy (in) a 4 102 ifa KLs (in) = [-- f) Radius of gyration: ry (in) = 4.082482 p U rt (in) = 4.082482 i-- p Maximum of KL/r: (KL/r) max = 24.98479 l-__ V H Material Properties (use coated metal thickness for weight): r-L b y Modulus of elasticity: E (ksi) = 29000 3.3 (ASTM A526/A527) i. S Yield strength: Fy (ksi) = 45 (ASTM A52G/A527) i a Ultimate strength: Fu (ksi) = 2.909274 Unit weight: w (1b/ft"2) = 17 h[- N-Load Data: N 6.5 <=== Enter Valuo C- - is Inter, pressure: Po(in of v.g.) = 6.5 <=== Enter Value !?- Inter. prensure: Ps(in of v.g.) = 0.84 <=== Enter Value " Correlation factors: C1 = e C2 = 1.27 <=== Enter Value 3 w" P-Panel vibration input (enveloped El. 677', 659' & 643'); x 4 -- 1 OBE (4% damping) using maximum of 3 directions: e-- q.. S N.. ) y'.- ([. ](f h.. h-- W. O Q g3 C, t F b-e ,6 , i.i., m

~~ > arv ' coue e, e,.co e, cu e w <.= so ao -t f=.L'2".t*?l* DC-5773 r,KK GENERAt- .co o COMPUTATION 94 9y p_- ~~

r w e, SHEET x

ll~- W oars ~~ ? " C ".$02 C.CJHVAC t. 40JCC7 ~ DECO FERM} L a ~ u Duct Evaluation of 431A 4, Pf 76230 1 Y ty_ Systen Series is ' Sva/C1 L.h 1 : /k, 19 'N $A a ACCons in gs) = 1.86 W = k ACConv in g's 2.1 = ACCovt in g s 2.1 ACComax in q's = SSE (7% da:eping) using maximum of 3 directionst t,N 1-1 52 6 ACCans in q's) = 1.52 ACCsev in q's) = 1.27 ACCsvt in gs) 1 52 = M ACCsmax in g s) = s; 4316 - 3 Element Forces from String Ar.alysis No. f, in element coordinates) TP [h (enveloped t. s i 15.2 <=== Enter Value 6t, Dead load: fxd (lbs) 14.3 <=== Enter Value = t ad Fyd (lbs) 52.2 <=== Enter Value- = N Fzd (lbs) Enter Value = 0 <wa= f Mxd (lb-ft) <=== Enter Value = 65.2 e Myd (1b-ft) 15 7 <=== Enter Value = I Mad (lb-ft) = 7 p-., Global soismic loads: 620.1 <=== Enter Value 49 ODE: fxo lbs) 644.8 <=== Enter value = Fy-; lbs) 134.3 <=== Enter Value e- = f Fzo lbs) = 557.6 <=== Enter Value-y Mxo (lb-ft) = 283 <=== Enter Value K. Myo (1b-ft) 1315.3 <=== Enter value = Mzo (1b-ft) = 593.6 <=== Enter Value o, ti, Fxs (lbs) 617 <=== Enter Value; = %s4 SSE: <=== Enter Value 4 "' Fys (Ibs) = 130.4 Fzs (lbn) 578.1 <=== Enter Value ~ = h Mxa (lb-ft) 278.2 <=== Enter Value = 3-Myu (lb-ft) = 1322.1 <=== Enter Valup Mza (lb-ft) = {t 1+ .l, e j;W Internal pressure stress: 7,M iA) Longitudinal tensile stress in duct plato fxpts kai = 3.961502 y a fxpto kai = 3.961502 (3.6.1-1):

J.

per EQ. Longitudinal compressive stress at duct corner y fxpcs (ksi) = 5.989414 A -; {d per EQ. (3.6.1-2): fxpco (ksi) = 5.989414 + -a p4 j 4; f 7-p ~ , j LB) Panel vibration stress: Qg 3;[Q U4 -t 3& y; * - q 4! b l } ;? s R q TWEg.t

~ - _ _ _. _ _._ auemmer- } ,,,~..u. _ j,,,, MN GENEPAL DC-5773 [g {ff5 8h *

C*"""*

COMPUTATION SHEET 44 /fff[ 8 su av. sa X -f D"' ~ 10 ~ l so 76230.502 .r suastCT SYSE*" 0011"S ODE CASE: s f 1,ongltudinal tensile stress in duct plate per EQ. (3.6.1-3): fxsto (ks') =1.659506 ~ tongitudinal compressive stress at duct corner per EQ. (3.6.1-4): f xsco (ksi) =2.509015 SSE CASE: Longitudinal tensile stress in duct plate per EQ. (3.6.1-3): f xsts (kni) =1.337812 i 1 Longitudinal ccepressive stress at duct corner per EQ. (3.6.1-4): fxscs (ksi) =2.022644 Note: The stresses calculated under B) shall be combined )' with those calculated under D) via SRSS plate stresses due to dead load when combined with i C) OBE: Axial tens. stress; fxdto (ksi) = 0.007949 - t Axial comp. stress: fxdco (ksi) = 0.018318 Bending stress: fbzdo(ksi)= 0.055329 fbydo(ksi)= 0.229777 c Shearing streasus: Y-dir, ftydo+fvydo (ksi) = 0.014958 Z-dir, f tzdo+fvzdo (ksi) = 0.054602 L e o', SSE: Axial tens. stress: f xdts (ksi) = 0.007949 0.025442 Axial comp, stress: fxdes (ksi) = Bending stress: fbzds(ksi)= 0.065534 fbyds(ksi)= 0.272156 g-Shearing stresses: Y-dir. f tyds+f vyds (ksi) 0.014958 = ('i, Z-dir. ftzds+fvzds (ksi) = 0.054602 ee g. D) Plate stresses duo to global seismic loads b OBE: Axial tens. stress: fxgto (ksi) =0.324320 Axial co.ap. stress: fxgco (ksi) =0.747310 g Dending stress: fbzgo(ksi)= 4.635376 y. fbygo(ksi)= 0.997347 p Shearing stresses: Y-dir, f tygo+ fvygo (ksi) =1.374393 e l 0 Z-dir. ftzgo+fvzgo (ksi) =0.840397 i ( 3E, ( SSE: Axial tens. stress: fxgts (ksi) =0.310460 {- Axial comp. stress: fxges (ksi) =0.993594 e Bending stress: (bzgs(ksi)= 5.518692 3 8+ l 2; \\ W, ' Q[ ~* Q p

c4(ctutoe u r

o Mv cw' se oy3fv t=m w,r A.

4n, y GENERAL O, i i COMPUTATION O j-7- p ,g sNur M " ll- ~ o*1t Pncutcf. DECO FEPMI 2 - CCHVAC oatt + Duct Evaluation of 4316 ao 76230.502 tMutet,5ystem Series ,1 + 4 fbygn(ks1)= 1.161258 is R Shearing stresses: 7; Y-dir. ftyqu+fyygs (ksi) =1.371046 p Z-dir. f tzgn+fvzgs (ksi) =0.862050 f i: fp 45)*Overall stress evaluations Combined axial tension & bending strences 1 E.1) fto=fxpto+jfxdto+fbydo+fbzdo)+(3843(fxgto+fbygo+ o kal OBE f bzgo) - 2 + f xsto* 2 )

0. 5= 10. 4 19.8 kai Fto (Allowable) = 0.6*Fy = Fto >= fto, OK

<=== fts-fxpts+(fxdts+fbydn+fbzds)+((fxgts+fbygs+ kol SSE: f bzgs)

2 + f xsts
2 ) '9. 5= 11. 4 24 41 29.7 koi 1

Fts (Allowable) = 0.9*Fy = Fts >= ftu, OK <=== If .b t Combined axial compression & bending stresses E.2) OBE: fxco(por EQ. (3.4.1-3)) = fxdco+fxgco 0.765628 kai 4 = Fac = 16.87824 kai .( Fao (Allowable) = 19.8 kai [<; ~ Pno (0.6*Fy) = For fxco/fao <= 0.15: 19.8 kai im Pbyo = Fbzo = E/ For fxco/Fao > 0.15 Feyo = 352.7291 kai Fezc = 239.2211 koi p' "', fxgo(using full area)= (Axco/Axq)*fxco 0.332269 koi = t,. Tbyo = 19.70134 koi ., f. - Fbzo = 19.77249 kai A,. 0.045361 <= 0.15 ^ t-( For this case, fxco/Fao = y- ~ USE Fbyo = 19.8 koi [@R ' Fbzo = 19.8 koi }lj t n;. overall interaction coefficient (IC): gi{s IC=(fxdco/Fao+fbydo/Fbyo+fbzdo/Fbro)+jfxpco/Feo)+ 'f n 2+ ((fxgco/Fao+fbygo/Fbyo+fbzgo/Fbzo) 5-0.670314 <= 1.0 (fxsco/Fmo)*2) 0.5 = OK <=== i g; d fco=fxpco+jfxdco+fbydo+fbado)+((fxqco+fbygo+ tbzgo) 2+fxsco*2) 0.5= 13.14849 kal + +n 41 SSE: fxes(per EQ. (3.4.1-3)) = fxdes+fxges 'l Q{-? 1.019036 kai = 25.31736 kai Fas(A11ovable)= 1.5*Fao = N; ? '21... E. 1 y rdy $p a we

p

.E ){hf w+

~ "' s.. uor.a. 9 cAcuto. to no awv cosa et coerp er (2/b I ~ s ""um=== a c==*a=*-* CO AT ON sm m 0 3 b,Oi t SHEET g ii Paoxcf _D. Eco FFly41 2 - gg WAC t ~ OAtt cast Duct Evaluation of 4316 so 76230.502 System Series SUSXCT Fas (0.9*Fy) = 29.7 ksl + For fxcs/ Fan <= 0.15: 29.7 kai. Tbys = Fbas = o For fxes/Fas > 0.15: Foys = 529.0936 kai d' Fezs = 358.8317 kai fxgs(using full area)= (Axes /Axg)*fxes i 0.318410 kai = Tbys = 29.68212 kai Tbzs = 29.67364 kai !f; 0.040250 <= 0.15 n For this case, fxes/ Fan = 29.7 kai USE Tbys = Fbts = 29.7 kai Overall interaction coefficient (IC) IC=(fxdes/Fas+fbyds/Fbys+fbzds/Fbza)+(fxpcs/Fas)4 ( ( f xges / Fas + f bygs / Fbys+ f bzqs/ Fbza)

2+

0.486836 <= 1.0 {(, (fxsco/Fms)*2) 0.5 = OK <=== fcnafxpco+jfxdcs+fbyda+fbrds)+((fxges+fbygs+ fbzgs) 2+fxsce*2)*0.5= 14.28818 kai n ~ (. [* E.3) Cotabined in-plano, 4 hear strono c .l P ODE Allowable shear stress for ducts with Pittsburgh lock longitudinal coams (por EQ.J.5-1):3.45)260 Fvyo (kai) l = 3.499260 E Fvzo (ksi) = Haximum shear allcwable (O.4*Fy): 9 13.2 D Fvmo (ksi) = p 000 shear allowables ~ 3.499260 ..ji - p,6 Fvyo (ksi) = sis Fvzo (ksi) = 3.499260 y Combined shear stresr.os in Y-directions 3 f vyo (ksi) =(fvydo+f tydo)+(f vygo+f tygo) "i' 1.389351 h_ = f yyo <= Fvyo,0K <===

s.,

{d. Combined shear stressos in 2-direction: N fvzo (ksi) =(fvzdo+ftzdo)+(fvzgo+ftzgo) 0.895 W. fvzo <= Fvzo OK <=== 12 = 1.389351 kol vS Haximum in-plane shear stress = Sh k: ye 4 SSE A11owabio snear stress for ducts vita rittsburgn rock 7 ...m m*j fj.g~ 9e 1 w 4 ng b g; ,? jo ..,Q r;:~ 4 k '*~k5 l jf h_ - + S ~ .n

u.u.,en + u t o sar v ccua e' cm o

e... w in..

. o i I GENERAL DC-5773 bb I -~ 'j - COMPUTATION gucer gg; 9,y nc~ ~~ m o t x b1 11 ~ 0*tt Dart PROJECT _ DECO T EPMI 1 - CQJiV AC / Duct Evaluation of 4316 y so 76210.502 r,un;t e t System Series e longitudinal seams (per EQ.3.5-1): 5.248890 Tvys kni) I o = 5.248890 Fvro kai) = i Maximum orcar allovable (0.52*ry): 17.16 Tvss (ksi) = Use shear allovablet 5.248890 rvys (ksi) = 5.248890 Tvra (kni) = Combined shear strouses in Y-directiont lt. fvyn (kni) = ( f vyds+ f tyds) + ( f vygs+ f tygs) 1.386004 = fvys <= Fvyn,0K <=== Combined shear stresses in 2-directiont i; tvzs (ksi) =(f vzdu+ f tzds)+ (f vzgs+ f tzgs) a 0.916652 = v fvzs <= fvzo,0K <=== Maximum in-plano shear stress = 1.386004 kni i i I i.h k,',b k. I 4 - l.. j; y I V: E /y 'N fg p 6 ( hi e g e I E c 3 r, , j l f.f l t-j. ( I J. t If

u 3

z. y lli. f. h* > a. C .\\d* 4 .6' 1 3 3 f o r w;,. 3 'd s e 2 +-,

ema. a = w, # %.. s a cucu.arde sti eso wy - cos av oerg my ^ DC-5773 g g' ^ ~ f FAT agheese a conserwet. 6'y sWWs \\ ][4-g ~" s~ee' enoJtCT. Deco FERM1 2 - CCHVAC ~ D'it. C# Daft Duct Evalu5 tion of 4316 e Jo 76230.502 SUBJECf System Series l l. j b l Y Overal!, Stress Evaluations for Rectangular Ducts (Con't) t D. [ D.04 Duct String Analysis No. 4316 - 6 Duct Size W in) = 16 16 H in) = 0.0478 Barc Metal Thickness t in) o = 0.0516 <=== Enter Value Bare Metal + Coatings = Section Propertion (based on bare metal thickness): } Gross area Axg (in*2) = 3.0592 Effect, area (OBE) : Axco (in*2) = 0.852928 Effect. area (SSE): Axes (in*2) = 0.612886 Effect. moment Iyyo (in*4) = 54.33562 i of inertia (OEE): Izzo (in*4) = 54.33562 in*4) = 45.88151 b Effect. moment Iyys (in*4) = 45.88151 4 Izza (in*2) = of inertia (SSE): 1.5295 Asy (in*2) Effect, shear area: 1.5296 Anz ( = Torsional moment %'( [ of inertia: 1xx (in*4) = 195.7888 i f Torsional section F' modulus: Sxx (in*3) = 24.4736 A Stiffener or C.A. spacing 1 (in) = 30 168 Effect. length KLy (in) = [i i 168 KLz (in) = [J. Radius of gyration ry (in) = 6.531972 rz (in) = 6.531972 l 4 l Ly Maximum of KL/r: (KL/r) max = 25.71964 t 1 - p Material Properties (use coated metal thickness for weight): f, Modulus of elasticity: E (ksi 29000 = 33 (ASTM A526/A527). ksi Yield strength: Fy (ksi = i 45 (ASTM A526/A527) ru ( Ultimate strength: = i < l Unit weight: w (1b/ft"2) = 2.909274 i Load Data; y \\ A<, <2 8 <=== Enter Value= 'S l W~ Inter, pressure: Po(in of W.g.) = k Inter. pressure: Ps(in of w.g.) = 14 <=== Enter Value. 7 p Correlation factors: C1 = 0.92 <=== Enter Value C2 = 1.27 <=== Enter Value Q t; %e pMs ll panel vibration input (enveloped 4 El. 6778, 659L 0 643J):.: y{ M. OBE (4% damping) using maximum of 3 directions: W M h (. hk . ;s. x g, 7 'sh Cm p 15 p g e u. ~- ~h:

hh

&&m t _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ __ _j

l 1 tw= sou a.. m, mcuamme to seo mv ct w ev oeroey $h W O C*'"*****" COIM)UTATION y mw s e.s vr.mo 0 i-SHECT X enOJtCt,prto t'f P'ilj ,qpgQq 94u (O rs M __ p,, - Duct Evaluatten of 4316 40 76230.502 SveLAct Systen Series -i ACCons (in g'sh = 1.9 ACCoeW f in qs3= 1.86 2.1 ACCovt fin g s) = 2.1 ACComax din n's) = SSE (74 damping) using maximum of 3 directionst ACCann in q's) = 1.52 1.52 ACCnew in g' = 1.27 ACCnyt in g' = 1.52 ACCsmax in g' = 'e i 4316 - 6 Element Forces from String Analysin No. + h (enveloped & in element coordinates) S: Dead loads 243.1 <=== Enter Value rxd (1bu) = 0.7 <=== Enter value ryd (15s) 267.3 <=== Enter Value = Tzd (1bs3 = 77.5 <=== Enter Value Mxd (1b-ft) = 697.7 <=== Enter Value Hyd (1b-ft) = 19.8 <=== Enter Value 1 Mtd (1b-ft) = N( Global noismic loads: r, ODE: Txo (1bs3 = 531.9 <=== Enter Value 418.3 <=== Enter Value h ryo (1bs) = 195.1 <=== Enter Value 9-rzo (Ibs) = 238.6 <=== Enter Value Mxo (1b-ft) = 734.2 <=== Enter Value f Hyo (1b-ft) = 1011.7 <=== Enter Value Hao (1b-ft) = 1009.8 <=== Enter Value hi SSE: Txo (1bs = 638.8 <=== Enter Valua Fys (1bs = E. 312.6 <=== Enter Value ti Tzs (Iba = 384.3 <=== Enter Value Mxa (1b-ft) 1177.9 <=== Enter Value = p Mys (Ib-ft) 1623.3 <=== Enter Value. = Hza (Ib-ft) = 'O hit [? x. n; pp. h, A) Internal pressure stress: N Longitudinal tennile strean in duct plate "i as g4 L; per EQ. (3.6.1-1): fxpts (kni) = 4.558530 fxpto (kai) = 3.139059 Longitudinal compressive stress at duct corner l '*2 por EQ. (3.6.1-2): f xpcs (kni) = 6.292754 fxpco (kni) = 4.333266 .f m m. B) Panel vibration stress: Q:& y; 'p @ ;O a f ry. .3 h DQ uri fl[

ggj-; n

= ._.n > 8th CCasp CV O ey ...-~...a CACUL.Aficpd MT esp 5 M ~ 'COMPUT AllON 0 h$,g SHEET a'k X u enoxcf _ Deco FEPH] 2 - CCHVAC ' * * ' ' b#1 " "I 'I- ~ m n Duct Evaluation of 4316 so 76:30.502

}

Systen Serios svaxcf L. 3 .1a s -i y 8~ ODE CASE fL 1,ongitudinal tensile stress in duct plate =1.144987 per EQ. (3.6.1-3): f xsto (ksi) l 1,ongitudinal compressive stress at duct corner fxnco (kni) ~1.580580 por EQ. (3.6.1-4): e SSE CASE @p+ <. A t,ongitudinal tensile stress in duct plate t + a. per EQ. (3.6.1-3): f xsts (kni) a0.923032 i.ongitudinal compressive stress at duct corner por EQ. (3.6.1-4): f xscs (ksi) =1.274186 h-shall be combined The stresses calculated under B)via SRSS. With those calculated under D) ? Note: Plate stressou due to dead load when combined with C) OBE Axial tons. stress fxdto (kai) = 0.079465 j p (, Axial comp, stress fxdco (ksi) = 0.285017 tbzdo(kci)= 0.0349c2 j Dending stress: fbydo(ksi)= 1 232693 r Shearing stresses:ftydo+fvydo (ksi) = 0.038457 Y-dir, 9 Z-dir. ftzdo+fvzdo (ksi) = 0.212751 y fxdts (ksi) = 0.079465 SSE: Axial tens. stress fxdcs (kni) = 0.396647 Axial comp. stress: fbzds(ksi)= 0.041428 p{1 Bending stress: t byds (ka i) = 1.459829 1 7 Shearing stresces: 0.038457

/f Y-dir.

f tyds+f vyds (ksi) = 18 Z-dir. ftzds+fvzds (ksi) = 0.212751 g + y D) Plate stresses due to global seismic loads fxgto (ksi) =0.173868 ,p W ODEt Axial tons, stress fxgco (ksi) =0.623616 Axial comp. stress fbzgolksi)* 1.787468 {;ls* : Dending stress: fbygo(ksi)= 1.297182 d Shearing stresses:f tygo+f yygo (ksi) =0.390461 J r Y-dir, =0.244541 Z-dir. f tzgo+f vzgo (kai) c (fh ;;' 1 h. rde fxqts (ksi) =0.330086 ~T SSE Axial tens. stress: f xqcs (ksi) =1.647613 Axial comp. stress: Ibzgs(kni)= 3.396505 J.,,i Bending stress: O)'. g, % g i V.i 7. ik ' a e: dy; 'i g;

~~= fto, OK~~

<=== SSEt f tsa rxpts+ (f xdts+ f byds+ f brds) + ( ( f xgts+ f bygs+ + fbzgs)'2+fxsts*2)*0,5= 12.39884 kal Fts (Allowable) = 0.9aFy = 29.7 kai Fts >= fts, OK <=== ,? E.2) combined axlal enmpression & bending stresses fxdco+fxqco E OBEt fxco(per EQ. (3.4.1-3)) = 0.908634 kul = Fac = 16.85978 kai Y4 Foo ( Allowable) = 19.8 kai Fmo (0.6*Fy) = G For fxco/Fao <= 0.15: h;l Fbyo = Tbzo = 19.8 kai 4 For fxco/Fao > 0.15: l' Feyo = 225.7466 kol Fezo = 225.7466 kai I: fxgo(using full area)= ( Axeo/ Axg)
~~f xco N~~
0.253334 kai = Fbyo = 19.77778 kai @0 Fbzo = 19.77778 kni ,l .g [. For this case, fxco/Fao = 0.053893 <= 0.15 USE Pbyo = 19.8 kas i 'k t. Fbzo = 19.8 kai M:,. overall interaction coefficient (Ic)t g, Ic=(fxdco/Fao+fbydo/Fbyo+fbzdo/Fbzo)+{2+fxpco/Fmo)+ ((fxgco/Fao+fbygo/Fbyo+fbzgo/Fbro) 0.508434 <= 1.0 g (fxsco/Fmo)*2) 0.5 = l ,y > OK <=== I f co= f xpco+ j f xdco+ f bydo+ f bzdo) + ( ( f xqco + f bygo+ fbzgo) 2+fxsco*2)*0.5= 9.917025 kai -4 g ? SSEt fxes(por EQ. (3.4.1-3)) = f xdes+f xges Js: 4 2.044260 kai p0 + = Fas(Allowable)= 1.5*Fao = 25.28967 kai M M b.1 /-
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we 0 l SHEET k h x i e40;tcf.EEco T rPfi 2 - 02WF; S'* " N2_ C# oave - cain s Duct Eva luat i::n of 4J 6 a M 2 3 0. 502 ,c W suaxCT. System Serlos ~ ~ ^ ^ Fan (0.9*Fy) = 29.7 kai v, 6' For fxes/ Fan <= 0.15: 29.7 kai Tbyn = Tbzs = for fxcn/Fas > 0.153 Feys = 338.6199 kai Fors = 338.6199 kai fxqs(using full area)= (Axes /Axq)*fxco 0.409551 ksi = Tbys = 29.66407 kai Tbts = 29.66407 kai b-For this case, fxes/Fas = 0.080833 <= 0.15 h USE Fbys = 29.7 kai p Fbts = 29.7 kai y; overall interaction coefficient (IC): IC=(fxdes/Fas+fbyds/Fbys+fbzds/Fbzs)+jfxpcs/Fms)+ h ~ 2+ (fxacs/Fms)'2)ygs/Fbys+fbzgs/Fbzs) (fxges/Fas+fb 0.544084 <= 1.0 ( 0.5 = k-OK <=== { p ten = f xpco+ ( f xdes+ f byds + f bzds) + ( ( f xqcs+ f bygst e kai N. ibzgs)'2+fxsco'2)'0.5= 15.80669 ifi I" E.3) Combined in-plane shear stress V ODES Allowabic shear stress for ducts with Pittsburgh lock [ longitudinal seams (por EQ. 3.5-1) : 2.477965 Fvyo (ksi) = 2.477965 Fvzo (ksi) = 4 Maximum shear allowable (O.4*Fy): h+ Fvmo (ksi) = 13.2 Use shear allowablat L Fvyo (ksi) 2.477965 = r* '. c Fvro (ksi) = 2.477965 6% 'T N Combined shear stressen in Y-direction: f fvyo (ksi) =(fvydo+ftydo)+(fvygo+ftygo) y-0.428919 =
~~gh.~~
fvyo <= Fvyo,OM <=== r M Combined shear stresses in Z-directiont fvzo (kni) =(fvado+ftzdo)+(fvzgo+ftzgo) 0.457292 f. ,k = pm fvzo <= Fvzo OK <=== ,= 0.457292 ks1 J!' Maximum in-plano ahear stress = Q ,h[ w SSE 4 Nk/,,- Allowable shoor stress for ducts with Pittsburgh lock i,. 3
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3.589195 ) = k-4 Maximum shear allowablo (0.52*Fy): t'.v 17.16 i Fvas (ksi) = ? Uno shear allowables 3.589195 ksi Fvys (kni) = 3.589195 Fvzs ( ) = Combined shear stresses in Y-direction 1 p l-y fyys (ksi) =(fyyds+ftyds)+(fvygn+ftygs) 0.644514 G, fvys <= Fvyn,OK <=== = 4 S* Combined shear stresses in Z-directiont I. fvru (ksi) =(fvzdu+ftzds)+(fvzgs+ftzgs) 0.605550 i = p fvts <= Fvzak OK <=== Irl. Maximum In-plano ahear stress = 0.644514 ka e. ) [ f, i }& us U...a ' 2 r a 0 b% I a s M-4 i : m.. iy y i, i W "; = y., . v4 - t M 3 g pp. k (1 $m\\. < i 2: i es;,Y y ~~E ' g g - u. t. o'y cm 3-p, -,c'. f_n.[A .~., ~.: e 4 h, 4 Nh l 4 Q 4: K fT Ja . ; ;1 - a c. ?O y - Yh J.. f*ji O .-y p g. ^ w M r f
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c4cueroe r4t so mv ccw at cHro et j, Q C 'M.n, ~ COMPUTATION mt= ww 0 p . t."4 " SHEET 4/27/46 x PRO >tCT Deco TERMI 2 - CcHVAC [9 ts 17 s>< t t p,,, 3,,, Duct Evaluation of 4316 Jo 76230.502 SututCT ' System Ser ies .4. H. Overall Stress Evaluations for Rectangular Ducts (Con't) D.05 Duct String Analysis No. 4316 - 7 16 Duct Size W (in) = 16 H (in) = 0.0478 Bare Metal Thickness: t (in) = 0.0516 <=== Enter Value Bare Metal + Coating: = Section Propertion (based on bare metal thickness); i. 3.0592 Cross area: Axg in'2) = Effect, area (OBE): Axco in*2) = 0.843810 Effect, area (SSE): Axes in*2) = 0.606520 54.33562 Effect. moment lyyo (in*4) = 54.33562 of inertia (OBE) : Izzo (in*4) = Effect, moment Iyys (in*4) = 45.88151 3 45.88151 of inertia (SSE): Izzo (in*4) = 1.5296 Effect. shear area: Asy (in*2) = 1.5296 Anz (in*2) = .( Torsional moment of inertia: Ixx (in'4) = 195.7888 Torsional section* ,v 24.4736 i modulus Sxx (in~3) = 30 ? Stiffener or C.A. spacing 1 (in) = 72 Effect. length KLy (in) = 96 KLz (in) = Radlus of gyration: ry (in) = 6.531972 i rz (in) = 6.531972 / Maximum of KL/r: (KL/r) max = 14.69693 p,. Y Material Properties (use coated metal thickness for weight): p 29000 E (kni Fy (ksi)) h Modulus of elasticity: s, = 33 (ASTM A526/A527) = P2 Yield strength 45 (ASTM A526/A527) f Ultimate strength: Tu (ksi) = (1b/ft"2) = 2.909274 ? Unit weights v J _; Load Data 3 g_ i ' 8 <=== Enter Value' 1 Inter. pressure: Po(in of v.g.) = 14 <=== Enter Valuo; O. Inter. pressure: Ps(in of W.g.) = Correlation factors: C1 = 0.92 <=== Enter,Value1 C2 = 1.27 <=== Enter Value 4 f Panel vibration input (enveloped El. 677', 659' & 643'): OBE (4% damping) using maximum of 3 directions: s di {N, 1 e '5 N r g 1p Uj, 'M t.<j: c I -!f e - I t
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X Pn0XCT DE('o FERMI 2 - CCHVAC b$C# 97 ~ oats oars Duct Evaluation of 4316 so 76239,.502 System series suturct W i ~}' ACCons (in g's3 = 1.9 Y* ACCoew f in gs) 1.06 = 2.1 ACCovt f in g s) = i ACComax din g'sj = 2.1 2 (7% damping) using maximum of 3 directionst i SSE O 1.52 ACCsns (in g's = 1.52 9 ACCsev (in g's = 1.27 ACCavt (in g's = 1.52 ACCsu x (in g's) = 4316 - 7 1 Element Forces from String Analysis No. t-6 (enveloped & in element coordinates) Dead load: 243.1 <=== Enter Value /- Fxd (1bs) = 0.7 <=== Enter Value k Fyd (1bs) 267.3 <=== Enter Value = p Pzd (1bs) = 77.5 <=== Enter Value Mxd Ib-ft) = 697.7 <=== Enter Value- ,.l' Myd Ib-ft) = 19.8 <=== Enter Value. ?- O Mzd Ib-ft) = L, bl Global seismic loadst
~~y 531.9 <=== Enter Value, p~~
OBEt Fxo (Ibs) = 418.3 <=== Enter Value 2; Fyo (1bs) = 195.1 <=== Enter Value W Fzo (1bs) = 238.6 <=== Enter Value fE Mxo (1b-ft) = 734.2 <=== Enter value Myo (Ib-ft) = 1011.7 <=== Enter Value Mzo (1b-ft) = 1009.8 <=== Enter Value b.' SSE: Fxs 1bs) = 638.8 <=== Enter Value Fys Ibs) = 312.6 <=== Enter Value. 7 Pzs 1bs) = 384.3 <=== Enter Value X. Mxs 1b-ft) = 1177.9 <=== Enter Value <ly f Mys Ib-ft) = 1623.3 <=== Enter Value $ ~ Mza lb-ft) L.$ = 07 p4 IY [ t. 6. M 's " A) Internal pressure stresst 41 3 - Longitudinal tensile stress in duct plate a 4.558530 -ll .) ;, per EQ. (3.6.1-1): fxpts (kni) = fxpto (ksi) = 3.139059 M Longitudinal compressive stress at duct corner per EQ. (3.6.1-2): fxpcs (ksi) = 6.292754 J fxpco (ksi) = 4.333266 4 ,.s -. Pi n yJ* j D) Panel vibration stress: f r. D h. L:A ~ jf%. f ~, , [ [a +( ~ m7 . y -s .g . - _,(4M kW
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0 = x PaostCT DECO FEPM! ? - CCHYM Duct Evaluation of 4i16 "" D" E oatt omit Sus >tC; _ System Series Jo 76230.502 a t; 1 '; OBE CASE: ae 1~ a; wo Longitudinal tensile stress in duct plate por EQ. (3.6.1-3): fxsto (kni) =1.144987 Longitudinal comp)ressive stress at duct corner per EQ. (3.6.1-4 : fxsco (ksi) =1.580580 SSE CASE: s l~ Longitudinal tenslie stress in duct plate por EQ. (3.6.1-3): fxsts (ksi) =0.923032 Longitudinal compressive stress at duct corner per EQ. (3.6.1-4): fxscs (ksi) =1.274186 f Notet The stresses calculated under D) shall be combined {; with those calculated under D) via SRSS t. E C) plato stresses due to dead load when combined with fxdto (ksi = 0.079465 N~; OBE: Axial tons. stress: fxdco (ksi)) = 0.288098 Axial comp. stress Dending stress: fbzdo(ksi)= 0.034982 fbydo(ksi)= 1.232693 Shearing stresses w Y-dir. f tydo+fvi-jo (ksi) = 0.038457 Z-dir. ftzdo+fvzdo (ksi) = 0.212751 k SSE: Axial tens. stress fxdts (ksi) = 0.079465 7 Axial comp. stress fxdes (ksi) = 0.400810 Dending stress: fbzds(ksi)= 0.041428 [C i. fbyds(ksi)= 1.459829 R Shearing stresses: ^ Y-dir. ftyds+fvyds (ksi) = 0.038457 a Z-dir. f tzds+fvzda (ksi) = 0.212751 f .N (y 2t .gg D) plate stresses due to global seismic loads I[ly ODE: Axial tens. stress fxgto (ksi) =0.173868 s, r, Axial comp. stress fxgco (ksi) =0.630355 5 ' 'J 1; Dending stresst fbzgo(ksi)= 1.787468 6j-fbygo(ksi)= 1.297182 y' Shearing stresses: ~ ~ Y-dir. ftygo+fvygo (ksi) =0.390461 g' Z-dir, ftzgo+fvzgo (ksi) =0.244541 3 h,6 SSE: Axial. tens, stress fxgts (ksi) =0.330086 [y Axial comp, stress: fxges (ksi) =1.664906 ~ Dending stress: tbzgs(ksi)= 3.396505 d } M(f . h QQ w u 34[. kt b h $.h[/ M
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tbygs(kni)= 2.464574 4' Shearing stresses: 4 Y-dir. ftygs+fvygs (ksi) =0.606057 Z-dir. ftzgs+fvzgs (ksi) =0.J92798 a: E) Overall stress evaluation: E.1) Combined axial tenslor t bending stresses l 1 f to=f xpto+ j f xdto+ f bydo+ f bzdo) + ( (f xgto+f bygo+ ODE: tbzgo) 2+fxsto"2)*0.5= 7.940031 kal 19.8 kai / Fto (Allowabic) = 0.6*Fy = Fto >= fto, OK <=== j fts-fxpts+(fxdts+fbyds+fbzds)+((fxgts+fbygs+ ksl SSE: tbzgs)*2+fxsts*2)*0.5= 12.39884 Fts (Allowable) = 0.9*Fy = 29.7 koi Fts >= fts, OK <=== Combined axial compression & bending stresses a,5 E.2) ODE: fxco(per EQ. (3.4.1-3)) = fxdco+fxgco 0.918453 kai = Fac = 17.08049 kai J*L( Tao (Allowable) = 19.8 kai . Fmo (0.6*Fy) = For fxco/Fao <= 0.15: 19.8 kai Tbyo = Tbzo = For fxco/Fao > 0.15: Feyo = 1229.065 kai Fezo = 691.3491 kai 2 t fxgo(using full area)= (Axeo/Axq)*f::co 0.253334 kai i 6: Tbyo = 19.79591 kai f' ~- = ?, Tbzo = 19.79274 ksi [$:g 6:: - For this case, fxco/Fao = 0.053772 <= 0.15 USE Tbyo = 19.8 kai t 4 S Fbzo = 19.8 kai J ,,4 I" D Overall interaction coefficient (IC): 'S d' f.. IC=(fxdco/Fao+fbydo/Fbyo+fbzdo/Fbzo)+(fxpco/Fmo)+ + ((fxgco/Fao+fbygo/Fbyo+fbzgo/Fbzo)*2+ 0.508318 <= 1.0 4' (fxsco/Fmo)*2) 0.5 = OK <=wa fco=fxpco+(fxdco+fbydo+fbzdo)+((fxqco+fbygo+ kai f fbzgo)*2+fxsco*2)*0.5= 9.926305 <.g ,f. ~ . b' SSE: fxcs(per EQ. (3.4.1-3)) = fxdcs+fxges W 2.065716 kai L Mb' = 25.62073 ksi Fas(Allowable)= 1.5*Fao = $ '. fig Q.. 'k)
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~~oatv, Duct Evaluation of 4J16 jo 76230.502 g~~
System Series SututCT ,j~(() Pas (0.9ery) = 29.7 kai N ja For fxcs/ Fan <= 0.153 29.7 kai t Tbys = Tbts = b For fxes/Fas > 0.15 Foys = 1843.597 kai Feza = 1037.023 kai fxgs(using full area)= (Axes /Axg)*fxcs 0.409551 kai = Fbys = 29.69340 ksi [ Tbzs = 29.68827 ksi For this case, fxes/ Fan = 0.080626 <= 0.15 USE Thys = 29.7 kai 1 t i Tbzs = 29.7 kai 'l 1- ' 1 overall interaction coefficient (IC): 1 IC= ( f xdes/ Fas+ f byds/ Fbys+ f bzds/ Fbza) + ( f xpcs/ Fas) + 1 (fxscs/Fms)'2)ygs/Fbys+fbzqs/Fbza)"2+
~~'t (fxges/Fas+fb 0.543879~~
<= 1.0 0.5 = ( ox <=== f xdes + f byds+ f bzds) + ( ( f xges+f bygs+ a fes=fxpca+{2+fxscs*2)'O.5= 15.82791 kai t tbrgs) r ,( V l l E.3) Combined in-planc shear stress { .r, OBE: ~ [ Allowable shear stress for ducts Vith Pittsburgh lock r O longitudinal seams (per EQ.J.5-1): 2.477965 r Fvyo (ksi) = 2.477965 Fvzo (ksi) = m 4 Maximum shear allowable (0.4*Fy): }7h Fvmo (ksi) 13.2 = O Use shear allowable: 2.477965 e si. Fvyo (ksi) = 9 N.6 Pvzo (ksi) 2.477965 i. c, = Y" 4 l, vv. l [% Combined shear stresses in Y-directiont f yyo (kui) =(fyydo+ftydo)+(fvygo+ftygo) 0.428919 y y = fvyo <= Fvyo,0K <=== ain O Combined shear stresses in Z-direction: fvzo (ksi) =(fvzdo+ftzdo)+(fvzgo+ftzgo) ta 0.457292 c = OK <=== 9#* fvzo <= Fvzok 0.457292 ks .y l' Maximum in-plane shear stress = w c y
~~Q., 06~~

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SHEET x P80JEc7 DECO FERMI 2 - CCHVAC _ MU ') 1- ' oart onre r ' Duct-Evaluation of 4316 74230.502 I n I SUBJECT _ System Series , -R W v$ ,e-j ($'? ( l M longitudinal seaan (per EQ.3.5-1):).589195 K t t: Fvys (ksi) 3.589195 = y e h Fvzs (Kni) = Maximum shear allowablo (0.52*Fy): 4 i i Fvms (ksi) = 17.16 ~ W 1 } ph Use shnar allowable:Fvyn (ksi) 3.589195 = S' 3.589195 Fvzu (ksi) w = Combined shear stresses in Y-direction:= ( f vyds+ f tyds) + ( f yygs+ 3 g Q-fvys (ksi) 0.644514 i'. <=== y [, fyys <= Fvys,0K = Combined shear stresses in Z-direction:=(fvads+ftzds)+(fvzgs+ftzgs) h . y~, fvzs (ksi) 0.605550 fvas <= Fvzs OK <=== f -: A' = ksi r 0.644514 jy $pN Maximum in-plane shear stress = WL, g,3.., 'Y '; ll{ /y.. k, 3 1 e fQ ,wr ( ~p gw m h.w!:w, + 3, y 4.h !, %Gl $'{ e nhd h' n k %] f g W
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FLl 1/R.,MIVlr.lN L A SET I nr e) = gp' 7 ~ "C# S RE4 W 5 - c w m.ww tuy heess Engineers & GENERAL 72%Q g PREUM. FtNAL VOto -o Constnictors COMPUTATION SHEET k X fNf FERMI 2 - CClWAC ~ SEEI W OATE DATE uvur t.vALv,u= Ion ur m 1 80-76230.502 suaxcl CV& TEM-GEREG o / The data contained in this attachment are generated using - the f STARMAP is a companion program of STARMAP post processing feature. STAROYNE vhich is used to perform the system string analyses, Q-.i k The purpose of the tabulated data is to present the forces and the ductvork by each duct size for DL, OBE and SSE moments in Maximum and ninimum values for each duct size are also conditions. presented. M. Based on the commands issued by the preparer, STARMAP accesses the-h working files saved by STARDYNE during the string analysis runs andThe data ar in tabular form. prints the data against the string analysis outputs by the checker, S N The string analysis outputs are contained in the following o ,s calculations: m g; CCHVAC Concern Resolution Task E DC-5763 Duct String Analysis and Support Evaluation of [ 2268 System Series it ( J CCINAC Concern Resolution Task k DC-5764 Duc.t String Analysis and Support Evaluation of p 2848 System Series a E CClWAC Concern Resolution Task M DC-5765 Duct String Analysis and Support Evaluation of %' _c 2849 and 4126 System Series 4 if + CCHVAC Concern Resolution Task h' -. ' DC-5766 g' t + Duct String Analysis and Support Evaluation of 4 4 2850 System Series
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a ' ATTACHMENT W,M$M i t [i ww#. 8& 8A DtCO ttuv&O STsttu 4316 1.2.3 T'-R 1 OF 9 DC*SIO [ - $1AmmAP veralon 4.41 iet Apr 12 14:37:31 19 % eeport : Etenant E ; - Nedet 4 [ Ferent 1 $1AaDiet Der / Beam Element - 4 h' *4 ' l title : Peor 1 14*x14+ M output Set 1
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') 9,* 8i&M LLtMEu! L0A05 C* Ax1At tutAs swtA8 tcasicW BEucluG 8tel#C 8 TAM P v2 v3 M1 M2 M3 1 JA 0.0 1.476710t+0 5.80%31t 1 8.393562D1 1.064550D1 1.744179D 2 1.470957b 0 stAMG e' JS 100.0 1.476710D 0 5.80%31t 1 8.393562t*1 1.084550D1 3.522116t*1 1.854904 0 2 e 2 JA 0.0 1.476710D 0 5.809631t 1 *1.787671t*1 1.084550t*1 3.52211M *1 1.854904b 2 atAMG \\ JS 100.0 1.47671M
~~0 5.8096314 1 1.T87671t*1 1.084550t+1 9.183669t*1 1.821361t*0 3 JA 0.0 1.4 7671M +0 5.80%3ff 1 4.308971t*1 1.08455M +1 9.183669t+1 1.821361t+0 stAMG~~
~~.ts 100.0 1.476710D 0 5.8c 4 31t 1 4.308971E~~
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JA 0.0 1.4767100 0 5.80 % 311 1 6.68%69D1 1.08455M + 1 1.642970D1 2.838047D0 6tAMG JS 100.0 1.476710t+0 5.809631t 1 6.685469D 1 1.064550t+1 1.005 Mob 2 3.854732D0 5 JA 0.0 1.476710t+0 1.4 M19% 0 7.947839D 1 1.084550D 1 1.005660t*2 3.854732D 0 SEAMG A. JB 100.0 1.476710D 0 1.4 M 19M *0 7.947139D 1 1.084550t+1 6.082681t+1 3.11713M+0 3-6- JA 0.0 1.4767100 0 1.4 75199t + 0 4.066%0t+1 1.co4550t+1 6.082681t*1 3.1171330 0 stAMG Je 100.0
~~1. 47671M~~
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[ 7 JA S0 1.476710t+0 1.4751NDO 6.149856E v 1.084550D1 2.049999t+1 1.667350 6 1 stAMC J8 V: 0 1.4767100 0 1.4 M19960 6.149856( 4 1.06M50t*1 3.946000t*1 4.381303t*0 8 JA 0.0 1.475200 0 0 1.476711t+0 6.808514t+1 3.9 W Act*1 *1.0845450 1 4.38130M *0 stat. J8 100.0 1.475200l+0 -1.4767110 0 6.8085146 1 3.946000D 1 -8.543119D1 2,28880M *0 5 9 JA 0.0 1.4M200bo 3.4410578 1 3.9e1229D 1 3.M60000 1 8.563119t+1 2.258803t+0 stAMG U 46 10'3.0 1.+ 7520000 3,441c578 l 3.96122W et 3.9460000 1 1.007210D1 1.457444f + 0 10 JA 0.0 1.4M200D0 3.4410571 1 -6.796244b o 3.946000D 1 1.00721061 1.457444b0 8tAMG J5 100.0 1.4 5200b 0 3,4410571 1 6.7962440 0 3.9460000 1 2.649862D1 6.257402t 1 J 11 JA 0.0 1.475200t*0 3.4410571 1 4.45487!b t 3,946000t*1 2.649862t+1 6.2574021 1 stAMG J8 100.0 1.4 M 200D 0 3.4410571 1 4.4548Mt+1 3.9460000 1 2.174768t
~~1 2.530737t 1 12 JA 0.0 1.4 520000 3.4410571 1 5.926267t+1 3.946000t+1 2.1747686 1 2.530737t 1 stAMG c~~
JS 100,0 1.475200f *0 3.4410571 1 5.926267D 1 3.946000D 1 8.598641b1 1.199368t 1 p$ (. 13 JA 0.0 -1.4752006 0 7.6D0%t 2 5.383398b t 3.946000t+1 8.598841b 1 1.197368 0 1 6tAMG 1 JS 100.0 1.475200 0 0 7.673034t 2 5.383398t*1 3.M6000t+1 6.20550M*1 3.309453 0 1 lf 14 JA 0.0
~~1. 4 75200t +0 7.6730%t 2 5.9985136 0 3.946000D 1 6.205503t*1 3.3094534 1 atAMG b~~
JB 100.0 1.4 52006 0 7.673034t 2 5.9985130 0 3.946000D 1 5.0058000 1 4.844060E 1 15 JA 0.0 1.4 5200t*0 7.6730%E 2 3.937813b t 3.M4000D 1 5.005300D1 -4.844060t 1 atAMG J8 100.0 1.475200 0 0 7.67*,0%f 2 3.937813D1 3.94600001 -6.476862D1 7.081517t 1 16 J4 0.0 1.4752000 0 7.673034t 2 8.901883D 1 3,946000t+1 6.4768621 1 7.081517t 1 atAMG JS 100.0 1.4 M200E 0 7.6730 KI 2 8.9018a31 1 3.946000D ? 9.441189D 1 7.337029b1 3 17 JA 0.0 1.4M20060 3.643754t 1 1.236859t+2 3,9460000 1 9.441189t+1 7.337029b 1 stAMG Je 100.0 1.4 M 200D 0 3.6437548 1 1.23M59D 2 3.9460000 1 7.046138t+1 1.21M15t +0 (' 18 JA 0.0 1.915790t+0 8.027965t 2 -1.T30116t+1 1.421460t+1 8.215705t+0 4.863944t 1 s(AMG JB 100.0 1.9157W60 8.027965t 2 1.730116t+1 1.421460D 1 6.15725M*1 7.339769b t 19 JA 0.0 1.915790D 0 8.027965t 2 2.457950D 1 1.4214606 1 6.157256b t 7.3397691-1 stAMG p* Ja 100.0 1.9157906 0 8.0279651 2 2.457950D 1 1.421460t+1 1.423063D 1 9.815593t 1 Q 20 JA 0.0 1.915790(+0 8.027965t 2 9.21M9301 1.421460t+1 1.423063D 1 9.8155930 1 atAMG y Je 100.0 1.915790C+0 8.027965t 2 9.217593t+1 1.421460t+1 9.101317t+1 1.048432t+0 4 W 21 JA 0.0 1.915790D 0 6.5260071 1 4.682442b 1 1.421460t+1 9.101317bt 1.0484320 0 stm 4 J8 100.0 1.915790t+0 6.5260071 1 4.682442t+1 1.421460D 1 2.6356M b 0 2.567691E 1 22 JA - 0.0 1.9157904 0 6.5260071 1 9.3%67600 1.421460D 1 2.635673 6 0 2.567691b 1 stAMG Je 100.0 1.915790D 0 6.5260071 1 9.33467M +0 1.421460D 1 -1.798462D1 1.698364t+0 23 JA 0.0 1.915790D i 6.3260071 1 3.93260M+1 1.421460E*1 1.798462t*1 1.698364t+0 stAMG E Ja 100.0 1.915790b'1 6.5260071 1 3.932608t*1 1.421460D 1 1.048166t+2 3.139306t+0 v 24 JA 0.0 1.475200t+0 1,391091t+0 1.643284E+2 9.032750t+0 1.135837t+2 5.1542231 0 stAMG Je 100.0 1.475200t +0 1.39109190 1.643284b2 9.032750D 0 2.779120t*2 6.547314t+0 ' JA. 0.0 -1.475200t+0 1.661740t+0 8.2ST258bt -9.032750 0 0 2.779120t*2 6.54 5140 0 stAMG .t. g 25 Je 100.0 1.475200D0 -1.M1740bo 8.287258t + 1 9.032750 0 0 -1.294044b 2 3.56M 75t+0 M 26 JA = 0.0 -1.4M200t+0 1.661740t+0 3.097081t+1 9.032750D 0 1.294044E+2 3.f 6947500 SEAMG 7+ Ja 100.0 1.475200t +0 -1.661740s 0 3.097081bt 9.0327506 0 7.39ue4bt -5.9495986 1 N 27 JA 0.0 1.661740D 0 1.4M199t+0 1.146315b1 7.3966609 1 9.032747t+0 5.9495988-1 stAMG ^e R JS 100.0 1.661740D 0 -1.4M 19990 1.1463159 1 7.396660D1 -2.144M401 2.192600E+0 7" 28 J4 0.0 1.661740D 0 1.4 M 1990 0 3.846953D1 T.396M0t + 1 2.144734t +1 -2.192600D0 SEAMG J8 100.0 1.661740D0 -1.4M199DO . 8469530 1 7.196660D 1 6.353184D 1 5.451314E+0 29 JA 0.0 -1,661740t+0 1.4751996 0 6.789734t* I.396660t+1 -6.353184t+1 5.451314t+0 stAMG t ?, Ja 100.0 1.661740 0 0 *1.4751991+0 6.789736i. 7.396660t+1 2.078137t+2 8.586111t+0 30 JA 0.0 -1.661740t+0 3.06099990 7.000432b. -7.396660D 1 2.078137D2 -8.586111t+0 SEAM $Q' 1 J8 100.0 1.661740D0 3.060999t*0 F.000432D 1 7.396660D 1 6.780510t+1 2.464114 b 0 ^* 31 JA 0.0 -1.6617400 0 3.060999D0 4.2844346 1 7.396660t+1 -6.780510D 1 2.464114DO BEAMG Y $$wm asyg . Agqv . ;g p&s q r M W,: < ,s n yrp$MMit MM
l ATTACHMENNA@ l %M6 9 Y - Of to CCWAC $111tM 43161.2.3 SHEET OF 9 ~ ~ m MOD pri Apr 12 14:37:35 1994 $1AasuP versten 4.41 Report s Element p, Model 1 Fernet t $1AA0 fat Sar/ seam Element -- R Title PecP 1 14+I14+ Pi tutput set 1
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~~AdlAt intAA snot ites10s ttupluG MuDinG P v2 V3 af M2 M3 4 }il Js 100.0 1.M1740D0 3.060999t*0 4.284434D) 7.39666M *)~~
~~1.788358O 1 3.6578 m +0 StAM 1~~
~~. 32 /4 0.0 1.661740t 0 3.06099W+0 2.864317D1 7.3946M*1 1.788358O1 3.65T88M*0 SumG JS 100.0 1.661740t+0 3.060999DO 2.864317D1 7.36660t*1 1.792038O 1 7.48413tt+0 33 JA 0.0 1.M1740t~~
0 3.060999D 0 +4.56t816t*1 T.39666M

1 l.792038t*1 7.484131E o stAMG J8 100.0 1.M17&OD O 3.06099% + 0 4.561416DI 7.396660D 1 7.494308t*1 *1.131038t+1 34 JA 0.0
1. M17604 + 0 9.123543D0

5. 53049t + 1 7.356660t*1 7.49430M*1 1.131038D 1 LEAMG J8 100.0 1.6617400 0 e.123% 3D 0

5. 53049t+1 T.396660D 1 4.730921D1 3.069791t+1 35
'JA 0,0 1.661740D 0 9.123543DO 2.867301t+1 7.396660D1 4.730921E+1 3.069791U1 8tAMG J4 100.0 1.6417400 0 9.123%3D0 2.86001E*1 7.396660D 1 1.082394D2 5.008544t+1 34 JA 0.0 1.M17&Ot +0 9.123%3D0 2.77644TD1 7.396660D 1 1.082394D2 5.008544t*1 M AMG ss 100,0 1.6617400 0 9.1235&3D 0 2.776447t+1 T.396660(+1 4.923985t+1 6.947297E*1 31 JA 0.0 1.661740D 0 0.12354M
~~0 5.662195t+1 -T.396660t+1 4.923985D1 6.947297t+1 SUMG JS 100,0 1.661740D 0 9.1235431*0 5.662195D1 7.39M60t+1 7.108179D1 8.886049D 1 38 JA 0.0~~
-1,661740t+0 6.41390Tt+0 2.155455D 1 7.396660t+1 7.108179t+1 8.886049D 1 StAMG Ja 100.0 1.661740D 0 6.413907D 0 2,155455D1 7.396660D 1 3.605565D1 9.928309D 1 39 JA 0.0 1.661740t+0 e.613907D O -5.129330D1 7.396660D 1 3.605565t+1 9.928309D 1 stAMG JB 100.0 1.6617400 0 6.41390TD0 5.129330D 1 7.3966600 1 3.688917t + 1 1.097057t*2 40 JA 0.0 1,661740t+0 6.41390TD 0
~~T.200044D1 7.396660t+1 3.688917t+1 1.097057t+2 SEAMG Ja 100.0 1.661740D 0 6.413907t*0 7.700044D 1 T.39666M *1 1.538899t+2 1.201283D 2 E~~
41 JA 0.0 1.66tT404+0 6.413907t+0 9.406792t+1 7.396660t+1 1.538899t +2 1.201283D 2 StAMG JS 100.0 1.661740D 0 6.413907t+0 9.406792t+1 7.396660D1 3.067502D 2 1,305509D2 4 ^ 42 JA 0.0 1.661740D 0 1.586874D 1 1.333380D2 7.39460t+1 3.067502t+2 1.305509D 2 stAMG 2 JS 100.0 1.661740 D 0 -1.586874t+1 1.313380t
2 T.39666M *1 1.234105D 2 1.087314D Z 43 JA 0.0 1.661740D 0 1.5 M874t+1 1.146455D2 T.396460D1 1.23410$t+2 1,087314t+2 stAMG JB 100.0 1.661740D 0 1.586874D 1 1.146655D2 7.396660D 1 3.425451D1 8.69118M + 1 f
~~64 JA 0.0 -3.429050t+1 3.196190D 1 1.58474D1 1.137550 0 2 9.1905520 0 d.42%51D~~
stAMG JS 100.0 3.429050t*1 3.196190D 1 1.586874t*1 1.137550D2 2.540346D 1 1.03931M*2 45 JA 0.0 1.339180D 1 1.1010021 1 t.586874D1 1.137140D 2 2.55880 m 1 1.039318D 2 StAMG JS 100.0 1.339180D 1 1.101002t+1 1.586874D1 1.13T1406 2 6.014843D1 1.279104t*2 to JA 0.0 1,661740D 0 1.58687&t+1 5.5945334+1 1.2289000 2 1.279104D 2 3.803615E+1 atAMG Je 100.0 1.661740D 0 1.584874D1 5.594533#*1 1.228900D 2 6.5090371+0 3.600092t+0 47 JA 0.0 1.586870D 1 1.661T&ct+0 8.539354D 1 6.509040D 0 1.2289000 2 3.600992D0 stAMG JS 100.0 1.586870D 1 1,661740D0 8.5393% D1 6.509M OD O 6.215735t+1 1.3111731 13 48 JA 0.0 1.596350D 2 1.586874t*1 1.661740D 0 2.9309900 14 6.519037t +0 6.215785D1 atAMG J8 100.0 4 596350D 2 1.586874t*1 1.461740D0 2.930990014 2.630535D 0 2.512021E+1 49 JA 0.0 1.919720t+2 1.586874D1 1.o6174cD0 3.164140014 2.63053$t+0 2.512021E+1 SUMG iX J8 100.0 1.91072M

2 1.586874D1 1.M174000 3.1641400 14 2.828293b l4 3.441691E 14 N
/ 50 JA 0.0 1.124690t 1 1.1050060 1 3.934771t+1 6.185730E+1 2.618264D'1 7.330209t 1 SuMG Ja 100.0 5.124690t-1 1.10500eO i 3.934771t+1 6.185D0D1 1.142962t+2 4.855650E 1 0 51 JA 0.0 5.1240000 1 1.106242t 1 3.47434M*1 6.192940E*1 1.142592f+2 4.8556500 1 St.ueG C; Ja 100.0 5.126000E 1 -1.108242t.1 3.474343D1 6.192940E+1 3.645447D1 2.373845b 1 b' 1 52 J4 0.0 4.405960t 1 2.840958t 1 6.013398t+1 1.799160t*1 6.957341E*1 2.3738450 1 atAMG Ja 100.0 4.405960t 1 2.840958E 1 6.01339eD 1 1.799160E*1 2.062737t*1 6.6352821 1 53 JA 0.0 4.605960t 1 2.840958D I 8.051076D1 -1.799160E+1 2.062737t+1 6.6352820 1 suMG Ja 100.0 4.405960t 1 2.840958D 1 8.051076D 1 1.799160E+1 1.414740t+2 1.089956t+0 54 JA 0.3 4.4059600 1 2.840958D 1 *1.373586D2 1.799160t+1 1.414740D 2 1.089956t+0 suMG JS 100.b 4.405960t 1 2.840958e 1 1.373586t+2 1.799160D 1 2.558937D2 1.326608t+0 55 JA 0.0 4.405960E 1 T.384903t 1 9.72TT29t+1 1.799160t+1 2.558937t*2 1.3266080 0 suMG 0** JS 100.0 4.405960t 1 7.3849030 1 9.72T729D1 1.799160t+1 6.133917t+1 1.503728t 1 F 56 JA 0.0 4.405960t 1 7.38490 M 1 8.086587t+1 -1.799160D 1 6.133917t+1 1.503728U 1 stAMG JS 100.0 4.6059606 1 7.38 903t 1 8.086587t+1 1.799 40E*1 2.7i1810E*1 4.5832336 1 57 JA 0.0 4.4059600 1 7.384903e 5 5.053837t+1 1.7999001 2.)o1810D 1 4.583233D 1 BUMG J Ja 100.0 4.405960t 1 T.3849030 1 5.053837D 1 1.799160t+1 -1.443036t+1 1.0734860 0 i* 58 JA 0.0 8.3380606 1 2.1037980 1 2.947674t+ 1 -2.475540D 0 2.296190t+1 1.073486t*0 stAMG h Ja 100.0 -8.3380604 1 2.103798D 1 2.967674D1 2.475540E*0 8.942020D 1 1.544612t+0 $9 JA 0.0 8.336730E 1 2.109063t 1 -4.433441D1 2.532010t+0 S.941862D 1 1.544612t+0 stAMG W Je 100.0 8.3367300 1 2.1090610 1 4.433441D1 2.532010D 0 9.864172t+0 2.014917t+0 - M 5 ~ Title 1 P1 top 1 14=x14= -/ W , OJtpJt Set 1
~~OtAD (CAD (OL) set 10 value~~
~~<fM N ' t Set ' MAX / Mis saamary table seem tal A Aztet forte Minimum 1 44 34.2905 p&m @4 nm-NM~~
~~u. w Rw Vej hbf~~
~ p \\((uM %
I 'k .ATTACHlylEN!g$=. be ~ OF O - ^ 9 k DECD CCmVAC $f$1tm 45161,},] 3H s o c.- r n 3 s 8 el Apr 12 14:37:39 1996 stammAP version 4.41 esport : Element +' 4 M( meest i y = 1 $1AR0 Tut Ser/Sean Element 1% Forent -( 7[^ + Title : Peop 1 14*I14= 4 masium 1 49 191.9T2 ~' / output Set 1
~~DEAD LOAD (DL)~~
~~T Seen End A theer2 f orce minimus 1 48~~
~~15.6687 maaiaum 1~~
~~44 31.9619 hf ** 4 Seem (M A Sheer) f orce nintam 1 54~~
~~137.359 x~~
maa lmas 1 24 144.328 &~ ulniman 1 46 122.89 ) M, - team EM A forcpe maala m 1 1 10.6455 ei Seem (M A moment 2 minimm 1 42 +306.75 - W 1 ) ) 1 5 O maximm 1 25 277.912 , y aN... minisus 1 45 +103.932 T 4 Seas (M A moment 3 maalma 1 42 130.551 [l = ~ Deam EM 8 Aalet f orce minious 1 49
~~191.972 m~~
~~menimm 1 44 34.2905~~
P
%9, team trus 8 sheer 2 force minimm 1 44 +31.9619 I maa t sum 1 48 15.8687 h 1 minimue 1 24 -164.328 Seen EM S Sheer 3 Force maa t am 1 54 137.359 minimm 1 1 10.6455 1 )) seen K M 8 Torma maalam 1 46 122.89 minimm 1 24 277.912 AJO Seem E M 8 mesent2 manium 1 41 306.75 minimm 1 41 130.551 K;, team (M e nament3 m stam 1 45 127.91 g$ , TJ g .4 e .titte t P90P 1 14*I14' i pT4 f ; tht}ut Set 2
~~Ost BtAm ILEaEw1 L0A05 D ij ".~~
AILAL SutAt $NEAR 10lt$lCN 8 M INE SENDING ~~ @% * ~ ttAM P v2 V3 mi t '. M3 1 JA 0.0 5.859480D 2 2.267689D2 2.01482001 2.893955t+0 4.1f2046D1 5.782528E+2 SEAMG Mh, R'- JB 100.0 5.859480f+2 2.267689D 2 2.014820(+1 2.89396CE+0 8.453264t+0 2.551645D1 b 2 JA 0.0 5.839530(*2 2.251692D2 4.306672D0 2.893955t+0 8.453264t+0 2.551645D1 stAMG Ja 100.0 5.839530D 2 2.2516t2t*2 4.3066721 0 2.893960D 0 2.20690D1 7.027229D2 3 JA 0.0 5.8214900 2 2.223042D 2 1.0.54778D 1 2.893955D0 2.206983t+1 7.027229D2 stAnc O Ja 100.0 5.821490D 2 2.223042t+2 1.034778D1 2.893960(+0 4.317021t+0 1.091560D 3 4 JA 0.0 5.8 %610D 2 2.219255D 2 1.604911D 1 2.893955D 0 4.317021D0 1.091560D3 stAMG Je 100.0 5.814610D 2 2.219255D2 1.604911D1 2.893960 D 0 2.425290D1 1.479697D3 0 5 JA 0.0 5.783890(+2 5.630072D 2 1.9+3a2501 2.893955 D o 2.425290D 1 1.479697t+3 BEAMG 6a Je 100.0 5.713890D 2 5.6300721*2 1.943825f+1 2.893960D0 1.460757D 1 1.1964406 3 Di 6 JA 0.0 5.774900E.2 5.593217D 2 1.044623D I 2.893955Dv 1.460757D 1 1.*a9644003 stAMG Je 100.0 5.774900D 2 5.593217t+ 2 1.044623D 1 2.893960D 0 8.51019eD0 9.510515D1 7 JA 0.0 5.766870(+2. 5.4W764t*2 3.978296(+0 2.893955t+0 8.510196D 0 9.510515D1 EtAMG yn Ja 100.0 5.766870E+' 5.499764t+2 3.97829M *0 2.893960D 0 2.063278D1 1.617552E+3 h~ lo-8 Ja 0.0 5.107750(*2 5.749308D 2 1.677003t+1 2.063278O 1. 2.893955t+0 1.617552t+3 stAMG JS 100.0 5.107750D 2 5.749308E*2 1.677003t+ 1 2.00270(+ 1 2.095247t+1 8.261139D2 9 JA 0.0 4,622OOD 2 1.415456D 2 9.55462M*0 2.ta3278t+1 2.0952471+1 8.241139E*2 8(AMG Je 100.0 4.622 00E+2 1.4186560 2 9.55462M*0 2.063270t+1 3.000904t+0 4.909908E*2 6 10 JA 0.0 4.4496706 2 1.440095f+2 1.893236D 0 2.063278t +1 3.000904D 0 4.909908E+2 atAMG p JE 100.0 4.449670D2 1.440093D Z 1.8932.36D 0 2.063270(+1 6.383470E+0 1.773263t+2 11 JA 0.0 4.1789300 2 1.474139D 2 1.073591t+1 2.063278t*1 6.383470t+0 1.T73263(+2 stAMG e ? JS 100.0 4.1789100 2 1.474139D 2 1.073591t+1 2.063270D 1 5.459250E+0 1.233036D2 M 12 JA 0.0 4.1014500 2 1.484158D 2 1.425654t+1 2.00278E+1 5.459250D0 1.Z33036E*2 SEAMG b Ja 100.0 4.101450E+2 1.484158E+2 1.425654 D 1 2.00270E+1 2.080766E+1 2.237343E+2 13 JA - 0.0 3.6971506 2 5.0123M
~~1 1.300664(+1 2.0632786 1 2.080766D 1 2.237343t*2 stAMC C~~
JS 100.0 3.697150D 2 5.8312360 1 1.300664D 1 2.0632706 1 1.4 W 95t+1 1.314344t+2 14 JA 0.0 3.3850600 2 4.91182SD1 2.042484t+0 2.063278t+1 1.4 W 95D 1 1.314344E+2 stAmc A. JS 100.0 3.385060(+2 4.91182SE*1 2.042484t+0 2.00270E.1 1.278068t+1 1.325097D 2 15 JA 0.0 3.211790E+2 4.44WOD1 9.557304D O 2.063278E+1 1.278068D1 1.325097D 2 BEAMG JB 100.0 3.211790(+2 4.44 WOE +1 9.557304D0 2.00270D1 1.771669t +1 2.033796E+2 u i' to JA 0.0 2.955320(*2 4.0025229 1
2. t 41172t + 1 2.00278D1 1.771669E+1 2.033796E+2 DEAMC Je 100.0 2.955320D 2 4.0025221 1 2.1411729 1 2.043270E+1 2.436924D 1 2.105262t+2 17 JA 0.0 2.58798cD 2 6.653263D 1 2.97420?t+1 2.063278t+1 2.436924t+1 2.105262t+2 stAMC JS 100.0 2.587980C+2 6.6532 0(+1 2.974202f+1 2.06327DD 1 1.890944t+1 2.502673E+2
~~( 18 JA 0.9 9.405320E+1 2.880196E+1 1.28&39M~~
~~1 2.845726D 1 3.481194D1 1.105105t+2 EEAMc J5 100.0 9.405320(+1 2.880196(*1 1.286396t+1 2.M5720D1 1.507225t+1 9.115167D1~~
~~,d - N$dQs 7 h[Mh y' W h% e 9 4 k~~
~~f % &;nh~~~
d'
ATTACHMENT WR C SHEET 1 0F[ 9 OtCO CCNVAt 5Y51tm 43161.2.3 D t frl Apr 12 14:37:43 1996 h $1AamAP versten 4.41 teport : Element I: T6 meda) format : 51 AA01st ter/seem itemmt -. + 4 %q p@ ' title rear 1-14+ 14= $(Aa t4tMtuT LOAD $ 4 ,AJ* F Owsut set 2 + cas i 5 ' AX1AL let At SmEAA TCall0g H21sG MaltG P y2 y} mi M2 H3 4,
~
19 JA 0.0 9.354890D1 3.717734tv 1.353978D1 2.84572M+1 1.507225D1 9.115167t+ 1 SEANG '( MAN E JS 100.0 9.354890t*1 3.11TT34D1 1.3539?st*1 2.8457?M +1 4.054360t+1 1.478620D 2 20 JA 0.0 1.03905M*2 4.655540D1 2.530514D 1 2.84572M *1 4.054360t+1 1.4786200 2 SumG Ja 100.0 1.0390%D 2 4.6555400 1 2.530574t +1 2.84572M *1 5.51450 D 1 1.771647D 2 21 JA 0.0 1.293300D 2
~~1. W 613D 2 3.480859t+1 2.84572M+1 5.51450 D 1 1.T718471+2 MneG Je 100.0 1.2933000 2 1.364613D 2 3.480859D 1 2.845720D 1 1.574147t+1 1.25850M*2 22 JA 0.0.~~
~~1.5245700 2 1.145246 0 2 3.224640D1 2.84572M +1 1.574147t+1 1.258506t+2 HANG' ~ Ja 100.0 1.52457M~~
~~2 1.34524M*2 3.224640D1 2.M 572M + 1~~
~~8. MOM 4t + 1 4.120172t*2~~
~~+ 23 JA 0.0 1.658140t+2 1.33799M*2 3.30243M~~
~~1 2.845726t*1 8.M 0644t+1 4.1201T2t+2 stAmG s~~
JB 100.0 1.658140D 2 1.337993D2 3.302433D I 2.84572M *1 1.58015M+2 7.0540 1D 2 24 JA 0.0 2.419910D 2 2.160C75D2 4.917165D 1 6.43614M +1 1.971328t*2 1.235118t+3 SEAMG Je 100.0 2.419910D 2 2.160075D2 4.917165E+1 6.0614M+1 2.341854t+2 1.42475M+3 25 JA 0.0 2.849970D2 4.642364D2 4.500065D1 6.43614M *1 2.341854t+2 1.42475M *3 etAmG Je 100.0 2.849970D ? 4.642 W t+2 4.500065t+1 6.436140t+1 2.865845t*2 8.9601860 2 26 JA 0.0 3.117470D 2 4.500317D2 3.9195 T3D 1 6.43614M
1 2.845845t+2 8.96018M *2 SumG Jo 100.0 3.119470D2 4.50031?t+2 3.919573D 1 6.436140D 1 3.51543M

2 8.94T74M+2 27 JA 0.0 4.4 *80D 2 3.221110D2 3.850187t+1 3.5154321+2 6.436143D1 8.94774M+ 2 SumG JS 100.0 4.4104800 2 3.22t110D2 3.850187D1 3.515440D 2 2.62585t*1 5.974472t+2 28 JA 0.0 4.179580D 2 3.445319e2 4.212741D1 3.515432t+2 2.62585D1 5.974472t+2 SumG i
Je 100.0 4.177580E*2 3.445319D2 4.212741t+1 3.5154400 2 6.M391?t*1 5.00722O2 h 29 JA 0.0 4.042380D 2 3.519815D 2 4.550242t+1 3.515432t+2 6.843917t*1 5.00722t+2 stAmc JS 100.0 4.042380D 2 3.51985D2 4.55024?t+1 3.515440D 2 1.640228D2 1.12168M+3 30 JA 0.0 3.40350E
~~2 1.318960D 2 3.011794 U 1 3.515432D2 1.640228D 2 1.12168603 MAMG Je 100.0 3.40350E+2 1.318960D 2 3.011794D 1 3.515440t+2 1.076072D 2 8.7070780 2 31 JA 0.0 3.25490D2~~
!.326731D2 2.T3217tt+1 3.515432t*2 1.076072O 2 8.7070780 2 MAMG bf Je 100.0 3.275490D 2 1.326731t +2 2.732171D1 3.515440E+2 5.601180t+1 6.367321t*2 3 32 JA 0.0 2.936110D 2 1 W755D2 2.726011t+1 3.515432t+2 5.601180t+1 6.347321t+2 atAMG R Je 100.0 2.936110D 2 1.366785D 2 2.72601161 3.515440D 2 2.350584D1 5.15639M+2 33 JA 0.0 2.8552900 2 1.3778 W 2 2.873913t+1 3.515432 O 2 2.350584t+1 5.150 960 2 SumG JS 100.0 2.855290D 2 1.3T7858t+2 2.873913D1 0.515440D2 2.130507t+1 4.026340t+2 34 JA 0.0 2.449960E
2
~~4. 839685D 1 1.621537D 1 3.515432t+2 2.130507F *1 4.026340D 2 SumG J4 100.0 2.449960D 2 4.889M5D 1 1,621537D 1 3.51544M *2 2.910193t*1 3.77451M+2 4~~
35 JA 0.0 2.31172M + 2 4.299664D1 1.086891D 1 3.51543292 2.91019M*1 3.774516D2 MAnc JS 100.0 2.31172M +2 4.299664D1 1.086891D 1 3.515440D 2 5.111869E*1 3.648125D2 S 36 JA 0.0 2.0403900 2 3.187470D1 1.054574D I 3.515432D 2 5.111249D1
~~3. M8125 D 2 MAMG JB 100.0 2.040390E*2 3.187470D 1 1.054574t + 1 3.515440E +2 6.208335t+1 3.48399M*2 5~~
37 JA 0.0 1.901260D 2 2.893442t+1 1.582160t +1 3.5154321+2 6.208335t+1 3.48399M*2 sum /. JS 100.0 1,901260D 2 2.893442t + 1 1.582160D 1 3.515440E 2 7.96977M *1 3.3241ME+2 9 38 JA 0.0 1.320250D 2 4.290475D) 8.510741D1 3.515432t+2 7.969T7661 3.324164t+2 SumG t JS 100.0 1.320250(+ 2 4.2904 5t+1 8.510741E +1 3.5154406 2 6.09330M*1 2.94295M+2 39 JA 0.0 1.214160D 2 3.832235D1 8.468345D 1 3.515432t+2 6.0933080 1 2.9429580 2 tumG 4'~ JS 100.0 1.214160E*2 3.&l223M +1 8.4683454 1 3.515440D2 1.980736D2 2.63198M +2 40 JA 0.0 8.TZ3960E*1 3.209675D1 8.5tS642t+1 3.515432D 2 1.980736D2 2.63196M*2 tuMG 9 Ja 100.0 8.723960E+1 3.209675D1 8.515642E+1 3.515440t+2 3.35395M+2 2.3059200 2 41 JA 0.0 7.681020E+1 3.304495D1 8.607797t+1 3.515432t+2 3.353953D 2 2.305920D 2 sumG g JS 100.0 7.6810200 1 3.304495t*1 8.607797t+1 3.51544M+2 4.740760D 2 2.0558ett+2 42 JA - 0.0 4.510760D 1 8.908400D 1 t.075775D2 3.515432D 2 4.740760E*2 2.055881t+2 MAMG g J8 100.0 4.510760D 1 8.9084000 1 1.07577'D2 3.51544M+2 4.038383D 2 1.436422t+2 p +, 43 JA 0.0 4.76353001 7.893653D 1 1.058563D 2 3.515432E+2 4.0383&3D 2 1.436422t+2 suMG Jo 100.0 4,763530t+1 7.895653D 1 1.05856M+2 3.5154409 2 3.727844t+2 1.605509D 2 g 44 JA 0.0 1.121260t+2 5.156705D1 4.515302D 1 2.132209D 2 3.182383t+ 2 3.T27844t+2 sumG a' C J8 100.0 1.121260E*2 5.156705D I 4.515502E*1 2.132210E*2 3.762347D 2 3.646350t+2 L 45 JA O.0 1.2086300 2 4.378149D 1 3.sc4M eE+1 2.127400D 2 3.765041D 2 3.M6350t+2 SEAmG Ja 100.0 1.208630t*2 4.378'49D1 3.80604tt+1 2.127400D2 4.062564D 2 3.8665336 2 46 JA 0.0 1.059480D2 4.218365t+1 9.910458D 1 4.16T204t+2 3.866533E+2 2.2888 4D 2 SOMG .? J8 100.0 1,059480t+2 4.218365D1 9.910458D 1 4.16T200t+2 5.940352t+2 2.557386t+2 [ 47 JA 0.0 5.657870t
~~1 1.180t30E+2 1.037170D 2 5.940352t+2 4.1672036 2 2.557366t*2 stAmG -~~
~~~' Je 100,0 5.657820t *1 1.180150D 2 1.037170D 2 5.940350D 2 4.199651D 2 3 01T204t 12 (.- 48 JA 0.0 1.08755M~~
~~2 1.031521Di 1.491515D 2 8.818701E 13 5.940352t+2 4.198651E 2 Sumc N'~~
Ja 100.0 1.087550D 2 1.031521D 2 1.491515E+2 1.818700D 13 2.459896D 2 1.782104t+2 49 JA 0.0 1.117430D 2 1.125776t +2 1.553946t+ 2 1.218661D13 2.45Va9M+2 1.782104(+2 SumG y%. W@ c 4 ~ f pLk W . s gg Q;s idy 4 QN &, m .+ w, gn%, ,n c , # wph t% ~ @Yh
EIN lu N ATTACHMENT M.D ? A L 4,m%a MU b OF _ 9 ~ m Mto etwne svstin 4316 1.2.3 W DN'N pri ser 12 14:37:47 1996 SinamAP version 4,41 Report t it ement madel t M. forest 2 STA40 Tut Sar/Seem tienent e q 7 u 3
title 1 Pe0P 1 14*S14*
~~M@3 v ~ mf,1 gn - ~ -Q'"?M-d J Qutyest set 1~~
004 8EAa iLtu(u7 L0&D1 AX1A4 SutAt tutAa 10ntica t(401ec NuelmG

Y' N'
~~P V2 V3 MT N2 R3 M4 e e Je 100.0 1.11743CE~~
~~2 1.12577M *2 1.553946(+2 1.21866M 13 1.1535734 12 2.897665t 12 QM' KAN '~~
~~? 10 JA 0.0 2.162660t+2 1.192414t*2 1.587066(+1 2.T77559t~~
~~1 3.799458E*1 2.200160(*2 stmG b~~
~~J8 100.0 2.162660(+ 2 1.192414t 2 1.587066t*1 2.T77560(*1 2.906015t*1 7.954992t+1 i 4 St JA 0.0 1.977%M + 2 9.543075t + 1 1.561370f~~
1 2.77898M *1 2.9046521*1 7.9549921+1 SEAMG 48 100.0 1.977940t + 2 9.503075t+1 1.561370t + 1 2.778980(*1 2.228911t+1 2.5M261t*2 52 JA 0.0 1.948490(+2 8.204323t+1 f.98504M*1 3.12645M +1 1.707724t*1 2.590261t*2 stAMG Jr. 100.0 1.94549C(+7 8.2%323t.1 1.985049t*1 3,126460f*1 1.&55341t + 1 1.638580f*2 51 Ja 0.0
1. 6732Kt + 2 S.41987M *1

2. 378127t+ 1 3.126458t+1 1.885341t+1 1.638580t+2 stAmG JS 100.0 1.473280t
2 8.4 n879t

1
2. 378127t + 1 3.12460t *1 5.158508t*1 1.324090E*2 54 JA 0.0 1.0802M + 2 8.8391cas.1 3.5875664+1 3.12645M *1 5.158508E+1 1.324090t*2 atAmG JS 100.0 1.69802Ct+2 8.55910N +1 3.587566(+1 3.126460t*1 7.954031t+1 1.666386t*2 2
~~55 JA 0.0 1.53951M~~
~~2 1.007431t + 2 2.34388E +1 3.126458t+1 7.954031E*1 1,6663864*2 stAmG c.~~
~~tJ JS 100.0 1.539510t+2 1.007431t + 2 2.343888t~~
1 3.126460t+1 4.879939E*1 1.0541422*2 56 JA 0.0 1.518120(+2 9.980013t*1 1,950680t+1 3.146458t+1 4.879939t*1 1.056142t+2 NAMG Js 100.0 1.518120(+2 9.980015t+1 1.950680t+1 3.12644M *1 4.620006(+1 1.3363621*2 4
~~+ 57 JA 0.0 1.490370t+2 9.8216711 1 1.225367t+1 3.126458t +1 4.620006t*1 1.336344t+2 stAMG Js 100,0 1.490370t+2 9,82t971t+1~~
1. 225367t+ 1 3.126460(+1 4.440907t + 1 2.0264464*2 58 Ja 0.0 1.444860t+2 1.c2143M.2 7.308734t+0 5.317071t+1 1.104884t+1 2.026446(*2 stAmG as 100.0 1.444860t+2 1.02t43M +2 7.308734t +0 5.317070t+1 2.249874t+1 3.766711t+2 59 JA 0.0 1,562030t+2 9.055772(+ 1 1.07779ef *1 5.3167041 1 2.250727t+1 3.764711t*2 stheG p-j h
~~J8 100.0 't. 562030( +2 9.055T72t +1 1.077798t + 1 5.316710(*1 5.616553(+0 5.441864t*2 Title P40P 1 14'1114 i e .Cutput Set 2~~
~~CH set 10 Value~~
$'c Set-MX/ MIN Sunnery f ebte minim m 2 42 45.1076 Seen Erd A Axlet f orce maa taus 2 1 585.948 'a minlaus 2 18 28.802 i ( seem Erd A th44r2 force ,p man teus 2 8 574.931 '"^ M miniaun 2 10 1.89324 e it' team Erd A theer3 force ^ maalma 2 49 155.395 ..2 Minium 2 49 1.21866(-13 A Sean Erd A f orge { manieus 2 47 594.035 minieum 2 8 2.89396 team Erd A masent2 g mes taus 2 48 594.035 minieue 2 2 25.5165 maa l =/= 2 8 1617.55 g" 4 'Q.. Seen trd A wt3 @g % Minimm 2 42 45.1076 TQ Am J. ~ - team End 8 Atlet force Masiam 2 1 585.948 %p minimum 2 18 28.802 N . seem Erd S theer2 force b, e& y Manimm 2 8 574.931 y hMMh ch e M,.M. ulniaam 2 to 1.89324 W -- 5 Saum taf 8 sheer 3 force mealam 2 49 155.395 'f i N.Ms 1 'sL Minlaus 2 49 1.21866( 13 ^, ' Seem Erd 8 forgae maalam 2 47 594.035 r PP, Minisue 2 49 1.15357E 12 5een tre 5 mcument2 ? O]p @M neatum 2 46 594.035 ,.6 _ Minlam 2 49 2.89767E*12 %, l 7 Some Erd 8 nament: Naaf am 2 7 1617.55 .?
~~L;g W.1~~
~~r. -~~
4 14**14" y f;g { Y 4titte'=t PROP 1 C cM ~Uutput Set 6 = 15E stAn tLtMt4i LCAD$ m. A. i AXIAL SutAA SWEAR TOR $1CDI 3DeluG SEM018G r@ P V2 V3 NT M2 M3 N#I k '! 'N. ~ htAM i 7.317540t+2 2.807119t+2 1.679365E*1 2.668617t+0 3.494551E*1 7.176914t+2 BEAMG JB 100.0 - 7.317540t+2 2.807119E*2 1.679365E+1 2.668620E+0 7.044581t+0 4.110779t+1 1 JA 0.0 Et : ( 2' JA 0.0 7.276230t+2 2.783555t+2 3.604884(+0 2.668617t +0 7.044531t*0 4.110779t+1 MAMG
~
Je 100.0 7.276230t+2 2.7&l555(+2 3.604854(+0 2.668620t+0 1.841992t+1 8.6758621*2 3 JA 0.0 7.240550t+2 2.743449t+2 8.629581t+0 2.468617t+0 1 841992E+1 8.6788621*2 atAMG f (( Je 00.0 7.240550f*2 2.743449t+2 8.629581t+0 2.668620E+0 3.939185t+0 1.347439t+3 / 4 JA 0.0 7.227340t+2 2.73922M 2 1.337837t+1 2.468617t+0 3.939185t+0 1.3474395 3 stmG.... 7 MLc Q if ,sp vn.c .g g/h t V_ lj 's 4
~~1g+DdQ fy 7~~
n u 8 l ' $.h y g49 g@My)ff -t' @@k h jh,N [ ~n v 4c 3j pj,h aj r
J A L i ACHMENT~5#.+ g =~ 1 g Of c0 ccavn smta 43 4 1.2.3 SHEET 7 we a nh, ;.MA OF 9 gf*/D ^, e i staamAp version 4.41 fri Apr 12 14:37M N Report t itement ] Modet : (- forset 51A80fut Sar/$ema fleswN
~~,. 4,t.~~
~~?,Qf [ ,11tle 1 P90P 1 14.I14* 4 i' - Outpet Set 6 * $14 , f % g: 9 _ _ $ TAN tLtMtuI LOADS ,y6 AXIAL pus SatAs TOR 1ICW 8tuoleG 8tW0l#G y-7;, -.' BEAM P V2 V3 "I "I "3 2 i 1 Je 100.0 7,N7340D 2~~
2. TD22914 1.137837t +1

2. M4620D 0 2.032852t+1 1.826081D3 5 JA 0.0 7.170580D 2 6.956290t 4 1.655291t*1 2.668617D0 2.032852t+1 1.826081t+3 SuMG i
~~46 100.0 7.17058M 4 6.95629ct q 1.0 5291t*1 2.666620(+0 1.218254t*1 1.478734D 3 ') 6 JA 0.0 7,15458M~~
2 6.910412t d 9.M5M2t

0 2.668617t+0 1 J18254D1 1.47873 4 *3 HAMC Je 100.0 7.154580( d 6.9104124 4 9.345682t*0 2.6686?ot+0 9.49e583D 0 1.227675D2 7
~~JA 0,0 7.140890D 2~~
~~a. 79 3974t d 4.738419t+0 2.668617t+0 9.498583D 0 1.227675D2 8tAMG 1~~
~~Jo 100.0 7.1400 W 4 6.791974D2 4.738819D 0 2.668620D 0 2.40095M~~
1 2.000915t*3 8 JA 0,0 6.3040Mi d 7.112S671 4 1.438MID 1 2.40095M

1 2.Ma&2000 2.000915D3 stAMG Je 100.0 6.304060t 4 7.112M7I4 1.438667t*1 2.400950D 1 1.784 6 2t*1 1.0200 m *3 u
9 Ja 0.0 5.699700D 2 1.744954t d 8.00953M +0 2.40095M*1 1,784792t+1 1.0200134*3 SUMG 4 Je 100.0 5.6097000 2 1.744954D2 8.00953 e 4 2.400950D 1 2.967899D 0 6.100960t*2 I 10 Ja 0.0 5.4E860D 2 1.769825t 4 1.802840D 0 2.400956D 1 2.96789M
~~0 6.100960t d MAMC~~
~ Je 100.0 5.4k86cD 2 1.769825t d 1.80M40D0 2.400950t*1 5.34055t*0 2.307788D2 11 JA 0.0 5,149400D 2 1.41M21t d 8.989419D0 2.400956t +1 5.344055t*0 2.307784D 2 stAMG Je 100.0 5.149400D 2 1.512521t4 8.4094199 0 2.400950D 1
~~4. TTT797t+0 1.640510D 2 l '..~~
~~12 Ja 0.0 5.05 341C4 4 1.8263060 2 1.191281t+1 2.400956D 1~~
4. T77797D0 1.64051W e2 HAMG JR 100.0 5.CS341C( 4 1.82630AD 2 1.191281t*l 2.400950D 1 1.750649D 1 2.78W17t *2 13 JA 0.0 4.555670D 2 4.145665D I 1.092479D 1 2.400956D 1

1. MOM 991. 2.781917D 2 SOMG JS 100.0 4.555670D2 8.145M5++1 1.092479D1 2.400950D 1 1.25436M +1 1.655819D 2 14 JA 0.0 4.174200t*2 6.65495ap t 2.169227D0 2.40095M +1 1.254 M6D 1 1.655819D2 SDMG I
~~J8 100.0 4.174200D 2 6.654958D 1 2.14 9227E *0 2.400950D 1 1.13909tt*1 1.873184D2 15 JA 0.0 3.9635900 2 5.3%33D1~~
~~8. 074673t~~
~~0 2.400956D I 1.139091t*1 1.873184D2 stAMG Js 100.0 3.9635901 4 5.! W 33t+1 8.074673t+0 2.400950D 1 1.67521M + 1 2.913535D2 s~~
~~14 JA 0.0 3.65M10D2 5.145933D1 1.739253b t 2.400956D 1 1.675219t *1 2.913535t*2 atAMG Ja 100.0 3.6534101 4 5.145935t+1 1.739M 3D 1 2,400950D 1 2.19603M+1 2.999409D 2 Y;h 17 JA 0.0 3.2163600 2~~
8. 75692D I 2.430307D 1 2.40095M + 1 2.196037t+1 2.999409D 2 suMG 48 100.0 3.216360D 2 8,77569?D1 2.480307D1 2.400950D 1 1.742860C+1 3.446542D2 18 JA 0,0 1.247530D2 4.040.131D 1 1.554469D I 3.536571+1 4.337943D1 1.716439D2 SOMG Jo 100.0 1.2453044 4.080331t*1 1.55446W +1 3.53650D 1 1.280464D 1 1.259640D2 i
~~19 JA 0.0 1.24397tD 2 5.432415D1 1.595060 0 1 3.534757t*1 1.280444(*1 t.259640D 2 auMG~~
~~9 100.0 1.24397CD2 5.432415Dt 1.595060D1 3.534750D1 5.028071D1 1.920706D 2 i~~
~~' 20 JA 0.0 1.371910( 4~~
~~6. 94 5405 t~~
~~1 2.393501D 1 3.536757D1 5.028071D1 1.920706D 2 8tAMG S~~
~~JC 100.0 1.37!910D 2 6.94540$ D1 2.393501t*1 3.536750t+1 6.549630D 1 2.346835D 2 4 1~~
~~r 4~~
21 Ja 0.0 1.685980D 2 1.T72626D 2 4.1716950 1 3.53675M + 1 6.549630t+1 2.346835D 2 atAMG E JS 100.0 1.6859806 2 1.772626tQ 4.171695D1 3.534750t +1 1.872571t*1 1.687235t+2 L - 22 JA 0.0 1.974060t4 1.746 720( 4 3.9Y9447D 1 3.534757t+1 1.872571t *1 1.68T235t*2 stAMG Q Ja 100.0 1.974060tQ
~~1. 746T20D2 3.9W487t+1 3.536750t +1 1,026909(4 5.3699390 2 y~~
~~. 23 JA 0.0 2.14000D 2 1.73876/1 4 4.022267t+1 3.53475 71 + 1 1.066909t+2 5.369939D 2 suMG D J8 100.0 2.14083cD 2~~
~~1. 734 7671 4 4.022267D1 3.534750D 1 1.9474234 4 9.175867D2 g~~
' 24 JA- 0.0 3.406040t d 2.757&22D2 4.923244t+1 8.02937M +1 2.429170D 2 1.442412t*3 8tAMG A J8 100.0 3.40604002 2.57822t +2 4.923244t*1 8.029370D 1 2.839232te2 n.877619t e3 25 JA 0.0 3.937900t*2 7.081358D2 5.0851434*1 8.02937M + 1 2.&39237t*2 1.87761?D3 8tAMG G JS 100.0 3.937900t+2 7.08a358t+2 5.ce5143D1 8.029370t+1 3.57000t*2 1.109708t+3 26 JA 0.0 4.2722404 4 6.SM32D2 4.178899D 1 8.0293 7M + 1 3.576100(+ 2 1.109708D 3 suMG Je 100.0 4.272240( 4 6.a66632t+2 4.772899D 1 8.029370D 1 4.400029t+2 1.36674M*3 C 27 JA 0.0 6.730460t d 4.39M52D 2 4.801213D 1 4.400027t*2 8.0293T3t+1 1.346747D3 SEAMG S-Je 100.0 6.730440t+2 4.3964521 4 4.801213D1 4.400010D 2 3.067406D 1 9.555999E*2 h[q , 28 JA - 0.0 6.3M 310E*2 4.68651M 4 5.156445t*1 4.400027t+2 3.06740M
~~1 9.555499t*2 SEAMG e~~
~~JS 100.0 6.350310t.2~~
~~6. 68651M Q 5.156445D1 4.400030t*2 8.434067t*1 6.668346t d l~~
29 ,JA 0.0 6.172010t + 2 4.787125( 4 5.396279D 1 4.4000271+2 8.438067t*1 6.668344t+2 SUMG JS 100.0 6.172070D 2 4.7371MD2 5.396279D1 4.400030E*2 1.963089E d 1.423144t+3 ~ 30 JA 0.0 5.201970 6 2 1.761343D 2 3.411854t*1 4.400027t*2 1.983089D2 1.423144t*3 suMG JS 100.0 5.201970t 4 1.761343D 2 3.411854t*1 4.400030D 2 1.324728D2 1.091033D 3 j. g ^.f. 31 JA 0.0 5.007020d 4
~~1. 763732t~~
~~2 3.255487t*1 4.400027t+2 1.324728D 2 1.091033D 3 suMG JS 100.0 5.007020D 2~~
~~1. 768732t~~
~~2 3.255487t+1 4.400030(*2 6.919681t+1 ' 7.927423D 2 g~~
7 32 JA 0.0 4.490820D 2 1.804270 0 2 1.28438M+1 4.40002M*2 6.919681t*1=1T.927423t*2 BOMG J8 100.0 4.49c820t d 1.8042700 2 3.284382t+1 4.400030D 2 2.927978t*1 6.424002D 2 i a_ 33 J4 0.0 4.367860t 4 1.8142634 4 3.375793D1 4.40002M +2 2.927978D 1 6.424002t*2. stAM4 V fL : JS 100.0 4.34786ct+2 1.814263D 2 3.375W3t+1 4,400030D 2 2.026591t+1 5.057627t*2 ~ $g (. s' 34 JA 0.0 3.M090Ct d 7.422492t*1 1.602450D 1 4.400027t+2 2.026591D 1. 5.057627D 2 suMG f JS 100.0 3.750900t
~~2 7.422492D 1 1.602450D 1 4.400030D 2 3.477638t+1. 4.809544D 2~~
~~-yg [_, p% b4 . L ' MWgi )ghM -hhhe mM~ -w a n?qfW A)Q; k M~~
~~y h&LWV ay 2Q kUS. ' w a~~
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= = - - - - - - - - - s ATTACMIENN> W' h h SHEET E OF 9 tt00 CDvat $1tftM 4316 1.2,3 4 tel Apr 12 14:31:55 1996 STAsnA# verstort 4.41 soport : Element DC.-$T O +-Ni nedst- : D Fernet : 51At0 Tut ser/Seem Element .M. I h6 .1 tte -s Peo* 1 14 M14" 6 Output Set 6
~~tst~~
,c stAe iLtutai LOA 05 e AIIA4 satat setA4 1CR$104 SEMDlhG stM0lBG P V2 v3 mr M2 M3 {j-1 35 JA 0.0 3.540360D 2 6.399215t+1 1.2426t2Dt 4.400027D 2 3.471638D1 4.809544t*2 - StAmc stM Je 100.0 3.540360D 2 6.399215D1 1.24261291 4.40003M
2 6.01121M *1 4.8026000 2 36 Ja 0.0 3.126950D2 4.428719D 1 1.201132t+1 4.400027t+2 6.0112T3D1 4.8026000 2 stAmc Je 100.0 3.12695M *2 4.428719D 1 1.20tt32D 1 4.400030D 2 7.889964t+1 4.708169t*2 31 JA 0.0 2.914&30D2 3.893066t+1 1.5'a312t+1 4.400027t +2 7.889964t+1 4.708169D 2 stueG Ja 100.0 2.916830D2 3 89306M*1 1.54A3 tit +1 4.400030D 2 1.013a29D 2 4.577022t+2 38 JA 0.0 2.028350D2 5.625090t+1 1.1027toD 2 4.400027D 2 1.013829t+2 4.5T7022D 2 stweG JB 100.0 LC2835cD2 5.625090t*1 1.102718D 2 4.40003002 7.91814M+ 1 4.164844t*2
- 39 JA 0.0 1.McM002 5.14M94D t 1.098173D 2 4.400027t+2 7.918146D 1 4.166844t+2 stAMG .M Je 100.0 1.86(340D 2 5.140494D 1 1.098173t+2 4,400030D2 2.571386t+2 3.812938D 2 0' 40 JA 0.0 1.%3/70D 2 4.891959D1 1.089813D 2 4.4000271+2 2.573386D 2 3.812938D 2 stAmG
~~i-Ja 100.0 1.343770D 2 4.891959D1 1.0898t3D 2 4.400030D 2 4.338385D 2 3.322004D 2~~
~ s 41 JA G0 1.1839 70t + 2 5.1428 MD I t.092248D2 4.400027D2 4.338385D 2 3.322004 D 2 StAmG Je 100.0 1.183970D 2 5.142879D 1 1.092248D2 4.400030D 2 '6.106570t*2 2.923246D 2 42 JA 0.0 6.165550D1 1.140377D 2 1.59254M +2 4.400027D 2 6.1065700 2 2.223244E+2 stAnc 4 :- Je 100.0 6.165550D 1
1. 640377D 2 1.592544D 2 4.400030t+2 5.05315tD 2 2.137900E*2 43 JA 0.0 6.296600D 1 1.022184D2 1.4 78157D2 4.400027D 2 5.053151D 2 2.11 M000 2 MAmG as 100.0 6.246600D 1 1.0221 M *2 1.5 7515 7t + 2 4.4000300 2 4.735971t*2 2.232150t 2 k,,
44 JA 0.0 1.60391CD 2 1.8295T2D 1 6.421501E*1 2.845123D 2 3.977837D2 %.735971t+2 t!Anc Ja 100.0 1.6039100 2 7.3295T2D1 6.421501Dt 2.845120E+2 6.723885E+2 4.929914t d 45 JA 0.0 1.T371000 2 6.4236c8D 1 5.68459D 1 2.839654D 2 4.727112t+2 4.92M14D2 stAMG Js 100.0 1.T371000 2 6.4236G8D 1 5.68%59t + 1 2.839650D2 5.205538D2 5.508M
2
~~= 46 JA 0.0 1.488490t * ?~~
~~6. 010325t~~
1 1.464384t+2 5.304093D 2 5.508299D 2 3.1k872t+2 stAMG JB 100.0 1.4854900 2 6.0103251et 1.66438&D 2 5.3M090D2 8.619048t*2 3.6410000 2 47 JA 0.0 1.583810D 1 1.6SO203D2 1.509442t+2 8.619047D2 5.3M092t*2 3.641000t+2 stAMG f
~~Ja 100.0 7.583810D1 1.680203D 2 1.509442t+2 8.619050D2 5.438542D 2 3.764144E 12 p- ~ 48 JA 0.0 1.53515M+2 1.341915D 2~~
~~2. te t 500D2 2.2541211 13 8.619M8D2 5.438542t+2 BEAnc Js 100.0 1.535150D 2 1.341915D2 2.1615000 2 2.25417N 13 3.5753T2t+2 2.307193t+2 h~~
~~49 JA 0.0 1.5502100 2 1.457482D T 2.258604D 2 1.113091t 13 3.5753T2t*2 2.307193D 2 stAMG 48 100.0 1.5502106 2 1.457482t~~
~~2 2.2586M D 2 1.713090D 13 1.782864D12 3.6957218 12 1~~
~~50 JA. 0.0 2.T96710D2 1.515854D 2 1.781135D1 3.148720f +1 4.702217D1 2.935129t*2 stAMG~~
"a Je 100.0 2.796710t + 2 1.515854D 2 1.781135D 1 3.148720E +1 2.555Mit +1 1.188181D 2

51. JA 0.0 L et9320t+2 1.234530D 2 f.779958 0 1 3.149934t + 1 2.5535366 1 1.188181t+2 stAMG Ja 100.0 2.619320D 2 1.236530D 2 f.TM958D 1 3.14993M + 1 2.667219D 1 3.364121t+2 P
52 JA 0.0 2.538250D 2 1.124506D 2 2.062087t+1 3.So9857D 1 1.435391t+1 3.366121D 2 stAMG Je 100.0 2.588250D 2 1.124506D2 2.062087t+1 i.169860 D 1 2.30$N1t+1 2.063913t*2 ~. $3 JA 0.0 2.5tt7200 2 1 t618871+2 2.137118D ) 3.8698571+1 2.305791D1 2.063913D 2 stamG M: Js 100.J 2.511T20t+2 1.161887D 2 2.33717M
~~1 3.869660D 1 5.571932t*1 1.T3676'E*2 T~~
~~54 JA 0.0~~
~~2. 44500D 2 1.244375t + 2 3.239415D1 3.869857D 1 5.571932t+1 1.T36761D 2 stAMG Ja 100.0 2.344300D 2 1.244379D2 3.239415D 1 3.869860D 1 8.058423D 1 2.304374D 2~~
+ Y 55 JA 0.0 2.220GYD2 1.3056a3D2 1.960875D1 3.869857D 1 8.058423t+1 2.304374t*2 stAMG Je 100.0 2.2200000 2 1.305683D 2 1.96087!C+1 3.869860D1 5.874566t+1 1.3459t2DF - 56 JA 0.0 2.207660D2 1.291044D2 1.414317t +1 3.869657t+1 5.874566t+1 1.345962t+2 stAMG F' Je 100.0 2.207660D 2 1.291044D 2 t.634317D 1 3.869660D 1 5.674997D 1 1.670384t*2 57 JA 0.0 2.197880D 2 1.267158D 2 1.033599t*t 3,869857t+1 5.674997t*1 1.670364t+2 BEAMG JS 100.0 2.197880E+2 1.267158D2 1.C335999 1 3.869860D 1 5.475883t+1 2.525221t+2 58 JA O.0 2.0735900 2 1.450G52O 2 6.276858DO 6.589245D 1 1.242168t+1 2.525221D2 stAMG ,f f Je 100.0 2.073590t *2 1.450852 O 2 6.276858DO 6.589250D1 1.941569t*1 4.880791t*2 >y J [ p - 59 JA 0.0 2.221080t+2 1.373735D 2 9.12t873t+0 6.588806 D 1 1.943038t+1 4.880791t+2 stAMG Q f Js 100.0 2.221080D 2 1.373735D 2 9.121873DO 6.588800t+1 5.L8095t+0 7.459466t+2 4 J .Z DOM a title : Paw 1 14914* e J@ Wt . TM ' M . output set 6 - sst set 10 Value V g 4 Q Set,. mAXAalM Stannery f able mint uun 6 42 61.6555 mmoG /ce: Q. Seas Erd A Aalet Force
M;
~~~ maaloue 6 1 731.754~~
~~M l d%h}.~~
MJ 'Seem traf A Sheer 2 Force ulnimum 6 37 38.9307 Maslaum 6 8 711.287 WMd. %g_ g'. "- ' I 1. g} 'r. Dean truf A Sheer 3 Force Minisun 6 to 1.80284 - 1G man (sue 6 49 225.86 . Q.-[Q seem trus A Torque - Minimus 6 49 1.71309D13 mau(sum 6 47 861.905 gGme M. ,G mN g $ wx glyM'M ' %d[in,,y gw k R 3 yh}fQc auk
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$6-9 OF _ $ 0(C0 C mv4C St51ta 4316 1,2,3 SHEE.T MdN OC.-SW3 fri apr 12 14137:59 1996 -$1AAmAP Version 4.4% iepori (lement -* 1 ' Hodel. t format : STAA0ful ter/ team (leanent %c fitte PeCP 1 '14*M14 e NU k"; Cutput Set 6 * $$t s Seem tnd A nament! minimm 6 8 2.66842 f.1 .+ manimm 6 48 861.905 + g Seen tnd A w t3 ulnimm 6 2 41.10T4 3 .gi manian 6 8 2000.92 ~ Seen Erd 8 Amlet f orce minimm 6 42 61.6555 4 maa letse 6 1 731.754 ~_ ' Seem Erd a pear 2 f orce minim m 6 37 38.9347 3e. maelma 6 8 711.287 W. h-Seem trd 8 Seer) f orce mintam 6 10 1.00284 f man imm 6 49 225.86 e4 minimm 6 49 1.71349t 13 teen trd 8 foegd 47 861.505 uesim a e [/ been led 8 moment 2 minian 6 49 1.7828M 12 maa t am 6 46 861.W5 Seen Erd a moment 3 minina 6 49 3.695 T21 12 men tam 6 7 2000,92 e N' ti-Title Petr> 1 14*I14* set to value S. F irst >AX/ute sommery f acite Seen Erd A AAlet f orce minisue 1 44 +34.2905 7 me: E nm 6 1 731.754 Sees trd a peer 2 force minleus 1 48 15.8687 maalaue 6 8 711.287 Beam Erd A Deer) f orce minisue 1 54
~~137.339~~
~~+ ma a lam 6 49 225.86 o m 6 nimm 1 46 d22.89 .C Seem trd A f orge maa t am 6 47 &&1.905~~
~~g j~~
~~Seem Erd A moment 2 minisua f 42 306.75 maalaus 6 48 861.905 been Erd A moment 3 minimm 1 45 103.932 y iis gf - masimam 6 6 2000.92~~
~~s '~~
~~heen Erd 8 Aslet f orce minious 1 49 191.972 s v. men isun 6 1 T31.754 Seze Erd B n eer2 force ulnimm 1 44 a31.9619 L 9 maa tam 6 8~~
~~70. 287 Seem trd 8 Sheer 3 f orce minium 1~~
26 164.328 pgt manisue 6 49 225.84 mintam 1 1 10.8455 4 W g Sean Erd & Torgae mas isus 6 47 861.905 $^, * . Seem tnd 8 moment 2 minleus 1 24 277.912 s e, maafsue 6 46 861.905 gi %y 4een End a masent3 minim a 1 41 130.551 .4 mea tum 6 7 2000,92 -n.."yl ge Q /y, yfc \\n t f k.i I. n. n l 1] wg
~~wlM2!y1, r,slp?~~
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AlIACHMENT &.: i 3 ~. comi uer ra-ow
~~p l CALCULA SETE0 CDs CHKT10Y E/~~
moymeen Engineers & GENERAL. 2-i Constructors COMPUTATION o E pF SHEET PAEllM FIP4AL Voto g g l FERMI 2 - CCINAC X SHEET of OATE DATE CT uvu r.vaLuatic7r or GT J 0-76230.502 g LututCT SVGTEM-GERIEC g 4 Y4 The data contained in this attachment are generated using the STARMAP post proccasing f eature. STARMAp is a companion program of ST;RDYNE which is used to perf orm the system string analyses. L The purpose of the tabulated data is to present the forces and ductwork by each duct size for DL, OBE and SSE moments in the Maximum and minimum values for each duct si:e are also conditions. p"esented, g en Based on the commands issued by the preparer, STAR) TAP accesses the t working files saved by STARDYNE during the string analysis runs and y in tabular form. The data are then spot checked prints the data against the string analysis outputs by the checker. 7 7 The string analysis outputs are contained in the following 4 eg k., calculations: CCINAC Concern Resolution Task ~ DC-5763 Duct String Analysis and Support Evaluation of v[:j, 2268 System Series yp= CCINAC Concern Resolution Task W DC-5764 Duct String Analysis and Support Evaluation of 2848 System Series Ek CCINAC Concern Resolution Task N' DC-5765 Duct String Analysis and Support Evaluation of !?{E 2849 and 4126 System Series {0%,,,; CCINAC Concern Resolution Task ki DC-5766 5 Duct String Analysis and Support Evaluation of y {.7 $zw 2850 System Series
~~f Z((E L NL M' ",~~
~~DC-5767 CCINAC Concern Resolution Task Duct String Analysis and '.upport Evaluation of Q 4316 System Series B s M i, jff %>a au ih. { ' h-h h- ,ee w -j kb w /kU ~ t s +-7.y W, q 3 pr 1 ?f .$h: ~~~
~~It $NE~~
~~,.<{,m Z Q WQ( "( 3. i,Q5~~
~~_h9, 1$ s & ^~~
lt s ih U. : M_ k:f l k, ;j-A l w _w Ah,
-- ATTACHMENiew ' E OF O l $Le
~~tto 12reAt Sv51tu 4316 1,2.3 SHEET~~
~~'1 trl Apr 12 14:38:48 1994 + 11AmA# version 4.41 S ete t : Itenant I 'I, Model t-i 1 ma0m 4.y.. D-t 4w a L ifitte 1 Pew 2 19-319= 1 twegut tot 1 + NA0 toad (041~~
i4m t41ata1 4OAD8 YN T*
)
~~Ax1A4 tut A8 lutat frallow SteluG MeluG g, v2 V3 M1 m2 A3 60 JA 0.0 2.979980E 1 5.2946511 2 1.1007tM~~
2 1.020440D2 2.194436D2 6.901800D 1 HmG

~
~~J8 100.0 2.97v980D 1 5.2966518 2 1.1007?M~~
~~2 d.02044002 3.735589t+1 5.6455M 1 MM 61 J4 0.0 2.97v980t + % 294451t I t.724159D 1 1.02WOD 2 3.735589D 1 5.66655M 1 stA'eG Je 100.0 2.9 M 80D 1 5.2946511 2~~
~~1. 724759t~~
~~1 1.020440D 2 8.62101t+1 4.16658M 1 62 JA 0.0 2.979980D t 5.29 6510 2 6.472806D 1 1.02 m 00 2 4.621831E*1 4.16658M 1 timG f~~
Ja 100.0 2.979980E 1 5.2946518 2 -6.47250M +1 1.020440D2 4.33025M+1 3.1071240 1 63 JA 0.0 2.97998M 1 4.294651t 2 1.015975D2 1.02%40t+2 4.D02!3t *1 3.1071241 1 DEAMG Ja 100.0 2.979960t 1 5.2966518 2 1.015975t +2 1.02M4M *2 2.46497M
2 2.04819M 1 6*
~~JA 0.0 2.9799800 1~~
~~.kMuD2 1.407229D 2 1.020440D 2 2.4M97M + 2 2.048193t 1 EtAMG Je 100.0 2.979980E 1 4.M6440 2 1.407229D2 1.02M4062 3.480741t+1 1.11936M *1 65 JA 0.0 2.9799806 1~~
~~4. t* mud 2 1.m195D1 1.02m062 3.480741U1 1.119369D 1 atAMG JS 100.0 2.979980t 1 4.M M444-2 1,68419$t+1 1.02M40D2 1.0497100 2 8.16339M 2 M JA 0.0 2.979980t 1 4.M M44t 2 6.540688t~~
~~1 1.0?M40D 2 1.049710D2 8.1633 h D 2 stAW.~~
J4 100.0 2.9799800 1 4.MM64E 2 6.540688D 1 1.02M40D2 4.k817M+0 1.533286t 1 67 JA 0.0 -4.MM40D 2 2.97M78D1 9.11445M +1 4.048180D 0 1.02M45t+2 1.533286D1 StAMG Je 100.0 4.MM40D 2 2,979978D 1 9.114456t+1 4.k8180t+0 1.188625D1 5.25825M 1 h 68 JA 0.0 4.M6,4M 2 2.97997M 1 1.592976D 2 4.048180D 0 1.1884255*1 5.25425M 1 EEAMG Ja 100.0
,s.640s 2 2.97997M 1 1.5929 7M

2 4.M8180t *0 3.438625t+2 1.146853t+0 69 JA 0.0 4.MM40t 2 S.24178M 2 1.118M4t*2 4.048160D 0 3.438625D2 1.14645 M

0 SEAMG Je 100.0 4.MM40D 2 8.241780D 2 1,1tS664t+2 4.Ma184 0 1.480962t*2 1.002622D0 70 JA 0.0 4.MM40E 2 8.241780t 2 7.500617t+1 4.044180D 0 1.480962t+2 1.002622D 0 stAMG Je 100.0 4.646440t 2 8.241780D 2 7.500617D 1 4.048180D 0 2.066770D1 8.171819D 1 1
~~P 71 JA 0.0 4.MM40t 2 8.2417806 2 2.431659D 1 4,%8180D 0 2.066TTDE + 1 8.171819t*1 SEAMG C JS 100.0~~
~~4. MM40D 2 8.24118M 2 2,431659t*1 4.048160t+0 9.728035t+0 7.141597t = 1 s, 1.~~
~~72 JA 0.0 4.M6440t 2 8.24178M 2 5.196179t+1 4.k8160D0 9.72803M+0 7.141597E 1 SEAMG JB 100.0 4.64M4062 8.241780D 2 5.196179D1~~
4. k8180D 0 1.006612t*2 5.699235E 1 73 JA 0,0 4.46440D 2 2.8064318 1 7,9290W D1 4.ks180D0 1.006612t+2 5.699285 0 1 stAMG Je 100.0 4.M64401 2 2.80M31D 1 7.929099t + 1 4.044180D 0 3.476784t+1 9.059002D 2 74 JA 0.0
~~M644Ct 2 2.80M31D 1~~
~~4. 781232t~~
~~1 4.k8180D 0 3.476784t+1 9.0590020 2 8DMG.~~
Ja 100.0 4.M6440D 2 2.80643tD1 4.781232t+1 4.044180D 0 1.16431M*2 3.887485 0 1 l 75 44 0.0 4.64M400 2 2.806431D1 3.34939001 4.k8180D0 +1.164313D2 3.887485t 1 SEAMG J8 100.0 4.MM400 2 2.80M 31D1 3.349390D 1 4.044tS0D 0 4.247675D1 1.008409t+0 76 JA 0.0 4.MM40E -2 2.80M31D 1 7.572655t +1 4.048180t+0 4.247675f +1 1.008409D 0 stAMG e JB 100.0 4.MM400 2 2.80o431D 1 7.572655D1 4.k8180D0 1.373738D2 1.67493M +0 77 JA 0.0 4.M64400 2 1.uM24D2 1.100112D 2 4.k818M +0 1.373738D2 1.67493M +0 alAMG J8 100.0 4.MM4002 1.446424D 2 1.100112D 2 4.048130D 0 4.480244t+0 1.692409D 0 78 JA 0.0 4.64440D 2 1.444 24D 2 8.77476491 4.M8180D0 4.480244D0 -1.692409D 0 stAMG J8 100.0 4.4M40D 2 1.u 64241 2 8.774764D1 4.M8160t+0 1.015189D2 1.709882t+0 R 79 JA 0.0 4.M6440D 2 1.444424 0 2 1.772158D 1 4.048180D0 1.015189D2 1.709882t+0 SEAMG e Js 100.0 4.64440t 2 1 uo4248 2 1.772158t*1 4.048180D 0 4.908075D1 1.752681t+0 6 80 JA 0.0 -4.MM40t 2 1.4464241 2 7.225635D1 4.%8180D 0 4.908075D1 1.752681E+0 atAMG JB 100.0 4.6444062 1.u6424D2 7.225635t*1 4.048180D 0 1.647258D2 1.7954810 0 81 JA 0.0 4.4 44002 1.24131200 9.845376t+1 -4.M8180D 0 1.647258D2 1.7 t J8 100.0 4.64M40D 2 1.2413120 0 9.84537M+1 4.%8180D 0 9.7850400 1 1.515098t+0 W[ 82 JA - 0.0 4,64M40t
~~2 1.241312D 0 1.725217D1 4.048180D 0 9.785040tet 1.515098t+0 stAMG JS 100.0 4.64 M40D 2 1.241312t+0~~
~~1. 725217t +1 4.048180D 0 1.337867t+2 4.100751t+0 n~~
0 JA 0.0 4.MM40E 2 1.241312D 0 5.166573t + 1 4.k8180D0 1,337867t+2 4.100751t+0 stAMG JS 100.0 4.MM40Di 1.241312t*0 5.166573D1 4.M8180D0 4.486459D1 5.75666tt+0 2 i? k JA 0.0 4.64M400 2 1.241312f+0 7.624231t+1 4.048180D 0 6.486459D1 5.7566 tit *0 stAMG J8 100.0 4.MM400 2 1.241312t+0 -7.624231D1 4.044180D 0 3.676641t*1 7.411329D 0 E 85 JA 0.0 4.MM40D 2 8.608252t+0 2.922904D1 4.k S180t+0 3.676641t+1 7.4113290 0 SDMG N Ja 100.0 4.M6440E 2 8.608252t+0 2.922904t*1 4.M8180t +0 6.364109t+0 1.634391t+1 O q, 86 JA 0.0 8.608250t*0 4.M644402 7.739506D0 6.368210D 0 4.048176D 0 1.634391D 1 atMG Ja 100.0 8.6082500 0 4.44412 7.73950M+0 6.368210D 0 1.404762t+1 1.642394t+1 $7 JA 0.0 8.6082500 0 4.6464440 2 5.081144t*1 6.368210t+0 1.404762D1 1.642394t+1 StAMG JB 100.0 8.608250D 0 4.MM4402 5.08114*D 1 6.3682106 0 3.676355D1 1.647041t+1 t 88 JA 0.0 8.608250t+0 4.MM44E 2 6.924158D 1 6.368210D0 3.676383D 1 -1.647041D 1 b, JS 100.0 -8.608250t+0 -4.4 M440 2 6.9241586 1 6.3682106 0 1.060054D2 1.651687D 1 J N: 89 JA 0.0 8.608250D 0 3.167140D0 9.457244t+1 6.368210D 0 1.0600540 2 *1.651687t+1 SEAMG Ja 100.0 8.608250t*C 3.167140!*0 9.45T244t+1 6.368210D 0 -4.767482D 1 1.137027t+1 ~ ~ Vf 90 JA 0.0 8.608250D 0 3.167140D 0
~~2. 71934M + 1 6.364210t+0 4.76748291 1.137027t*1 luMG yQA~~
@y&R 6 Mg 'O' fN&'. %a NM 432n f&y ly {
l j[#m h hh I ATTACHMENf l" N M N Otto ttuvat Svitta 4316 1.2.3 3 Fel Apr 12 14:38:51 1994 Ob"b"II) l STMmAP version 4.41 eesort : ILement modoi 1 r.re.t i stAA0 m s.ri6. (i nt M,i b ~ Y W 3
~~-fitte Pew 2 19-n19e 1~~
~~+ Output let 1~~
~~MAD LCAD (Ot)~~
~~+ + etAe !Ltato1 10A0S mg AI14L tutAA latAs 10tt10m MuDinG MuefuG NAM - P V2 V3 m7 m2 m3~~
~~"p ',~~
~~JS 100.0 8.608250t+0 3.16 T14M~~
0
2. 71934M + 1 6.36821M +0 9.16641M + 1 6.2D6671*0 91 J4 0.0 8.60825Ct*0 3.16714M +0 3.239552t+1 6.36821M+0 9.186418t*1 -6.223667t+0 StAMG as 100.0

8. 60825M
C 3.16714M *C 3.239552t + l 6.368210t+0 + 3.92214M

1 1.077% 5t+0 h
~~92 Ja 0.0 8.608250t*0 3,16714M~~
~~0 6.2M449t*1 6.366210E+0 3.92214M +1 1.077065f+0 StAMG Je 160.0~~
~~8. 6C425M~~
0 3.167140t*0 6.234449t

1 6.368210E+0 6.20ec33f+1 4.069537t+0 93 Ja 0.0 8.60825M

0 9.377424t 1 6.4492671+1 6.368210t+0 6.206833t+1 4.069537t*0 stAMG Ja 100.0 8.608250t*0
9. 3 77424t. t 6.4492eTt+1 6.368210t+0 8,03114M *1 6.140073t+0 94 JA 0.0 8.608250(+0

9. 3 r7424t - 1 1.36*030(*1 6.36821M +0 8.03114M + 1 6,1400T3t+0 stamG JS 100.0 8.608250t
~~0 f.37*424t t t.364030tet 6.3M21Cf *0 5.018007t+1 8.211545t+0 95 JA 0.0 8.608250(*0 9.3 774244 1 5.434325t*1 6.36&210E+0 5.018007t+1 a.211545t+0 stAMG JB 100.0~~
-8.608250t+0 9.377424t 1 5.434325t*1 6.36821M *0 6.990902t+1 = 1.02820M +1 96 JA 0.0 9.618800t*1 8.608252teo 9.3774244 1 1.028210E*1 6.364209t+0 6.9809821*1 MAmG 9.3774248 1 1.02821M e l + 4.18045M +0 4.972677t+1
Ja.100.0 a 9.618890t + 1 _8.6082521 *0~ 5.172657t*1 ' ~ 2.101649t+0*3;652810t+0 **9.59 FIT 1t+0 w T.31992aE+ t watAMG4 4 97 JA 0.0 1.08784M +2 Je 100.0 1.087540t + 2 5.172657t.1 2.101649t*0 +3.652810t*0 6.624990E+0 4.686340E*2 98 Ja 0.0
~~1. 2 T2140(~~
2 7.01567tt+1 2.101649t *0 3.652810t+0 6.624990t+0 A.686340E 2 SEAmG JS 100.0 t,272140t*2 T.015671t*1 - 2. t 0 t %9t

0 3.652810t+0 3.652310t*0 9.916970t+1 99 JA 0.0 2,230060t*2 4.01*%ot 1 2.1018 9t*0 1.T30560t = 14 5.165853t*0 9.916970t+1 stAMG JS 100.0 2.230060t*2
~~. 01.5601 1 '2.101ket+0 1.73056ct 14 2.627061t*0 5.043211t+1 100 JA 0.0 3.0365 70t + ' 4.034569t + 1 2.10149t*0 1.3177005 14 2.627061t*0 -1.043211t*1 stAMG Ja 100.0 3.036570t+2~~
034569t*1 2,101649t*0 *1.317700E 14 7.699397t 14 1.8818284 14

~
101 JA 0.0 1.06710cter a.1826 MT + 1 3.039f91t*0 5.282670t+0.t.387937t+1 1.229261t*2 8tAMG d JS 100.0 1.06710ct + 2 6.1826771 1 3.039301t+0 5.2826TW*0 9.581019t*0 3.544979t*1 102 Ja 0.0 1.251400t*2 8.J2169ttet
~~3. 0.19391t~~
0 5.282670(*0 +9.581019t*0 3.548979t + 1 stAMG Je 100.0 1.251400E*2 8.02:00 t

1 3,039399t*0 5.282670t+0 5.232670t+0 7.801062t*1
~~[l 103 JA 0.0 2.236820t*2 - 3.173 744t~~
~~1 3.0393911 0. 4.10T&30(+ 15 F.470824t+0~~
?.801062t+1 8tAMG i J6 100.0 2.286820t+2 3.173744 t + 1 +3.039391t+0 4.107U C( 15 3.799239t*0 3.96?180t+1 104 Ja 0.0 3.093320t*2 3.173744t+1 3.019391t+0 1.337120E 14 3.799239t+0 3.96?180E+1 atAMG p Je 100.0 3.093320t*2 3.173744t*1 3.039391t*0 1.337120E 14 1.158?95t *14 4.813994t 15 Title : Pt0P 2 19*s19* chaput Set t
~~MAD LOAD t0L)~~
H gd Set. NAX/mit $6mmary table let 10 Value Y Seem Erd A Aalet force minim m 1 67 0.046464 masimm 1 104 309.332 f7 .J 8eam trup A Shear 2 f orce min 6 mm 1 99 40.3457 maaimm t 102 80.2569 41 Seem trus A theer3 perce minimm 1 64
~~140.TZ3~~
/ manimm 1 68 159.298 E h* minian 1 96 10.2821 Qf Beam Eful A Tortam masium 1 60 102.044 A M % Q j,, Seem tesi A hemmat2 minimm 1 83 -133.787* maaimm 1 69 343.863 qK4 .3ils M ( i s sj minimm 1 99 99.1692 n ,1
~~1.-~~
Seem truf A 3ecasnt3 maaisus 1 101 122.926 W ~, team trus 8 &aul f orce minium 1 104 -309.332 maaima 1 67 0.046464 'm Seem tres e sheer 2 Force minimm 1 102 80.2569 s s M maalam 1 99 40.3457 J' k NH Coen trus e shear 3 force minimm 1 68
~~159.296 maalam 1~~
~~64 140.723 kh 3 .m M Seen End 5 forsyn minim m 1 60~~
~~102.044 masisus 1~~
96 10.2321 C m Seem truf 5 Moment 2 minim a 1 68 343.863 . 4 T-D" w i. Sean End s momenti minim a 1 101 35.4a98 maaimm 1 82 133.T87 44 a, ,d f+C.}41 maaimm 1 98 99.1697 a: -4 c $$ c ;.. 2+ n ?& ~.. l QR p;nwO m m> n ,1 k
~~]%&~~
W i N:~ Mw swpq f:N. L q - + &o <%:f Q n ' %?
, w,.. ATTACHMENT i+4~ .. &., a ) 'a
~~os g# #.,~~
m 0 u - m M n 43,6 1.2.3 SHEET. b 0F b Title 1 PACP 2 19'I19= DCdTD t< ~ [ 1lhaput Set 2 + Cet F 9EAs ttIatut LOAD $ AI1AL sataa $kEAA ICRSION HelWG HelBG 7 P v2 v3 at K2 R3 M41 ? l-60 Ja 0.0 2.205390D2 6.41678M
~~1 2.641910D1 2.467699D1 5.26707M* 1 3.252691D2 StamG 2~~
~~t. e JS 100.0 2.205390D 2 6.4167S8D1 2.641910t*1 2.47700t +1 8.965429t+0 2.?M615E+2 61 Ja 0.0 2.108210t*2 6.270254D1 4.1498829 0~~
~~2. 47699D1 8.965429D 0 2.2%415D2 SEAMG 7~~
<t 100.0 2.108210t+2 6.270254t 1 4.1498820 0 2.4770001 2.070988t+1 1.907760(*2 62 JA 0.0 2.030490D2 5.971515D1 1.55374M*1 2.467699D1 2.070988D 1 1.90T760D 2 4 TANG f Ja 100.0 2.030490D2 5.971515D 1 1.55374M*1 2.4677000 1 1.0491121 1 2.499693D2 63 JA 0.0 1.9982500 2 5.8A217M + 1 2.438515t+1 2.47699t + 1 1.049112t+1 2.49969)(+2 M AmG + JD 100.0 1.998250D 2 5.832176D1 2.438515D 1 2.467700D 1 5.9193821 1 3.420009t+2 64 Ja 0.0 1.8961800 2 1.067916D 2 3.390029t*1 2.467699t*1 5.919382D 1 3.420009t*2 atAmG JS 100.0 1.896180D2 1.06791M
~~2 3.390029t+1 2.47700D1 9.193529D 0 1.362852D2 65 JA 0.0 1.8292200 2 9.638652t+1 4.972741D0 2.47699D1 9.193529D 0 1.342852t+2 StAmG as 100.0 1.82922002~~
~~9. tJ8e 5M~~
1 4.97274tD O 2.46T7000 1 2.979373t + 1 2.754254D2 s4 66 JA 0.0 1.??9060D 2 7.976849D 1 1.59658M

1 2.47699t + 1 2.9793S D 1 2.754254D2 StAMG Je 100.0 1.799060D 2 7.976849D 1 1.59+588D 1 2.4677%t + 1 2.04251?D 1 3.9579604 2 67 JA 0.0 7.430340D 1 1.79215802 2.20715M +1 2.042515D1 2.47696D1 3.957960D 2 DEAmG Je 100.0 7.43034001 1.792158D2 2.20715M+1 2.042510D1 2.9259371+0 2.914918D2 d.8 JA 0.0 6.257240t + 1 1.78165992 3.834800D1 2.04251591 2.925937D0 c.914918D 2 atAMG
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1. 21125M
2 9.0204100 1 6.1044200 2 6.81M37t + 1 4.67972M

2 SEAMG JS 100.0 5.93114 0D 2 1.211256D 2 9.0204100 1 6.1 442002 1.327871D 2 3.891651t+2 94 JA 0.0 6.068260D 2 9.230165t+1
~~8. 5272M~~
1 6.104420 0 2 1.3278716 2 3.891651D2 BtAMG JS 100.0 6.068264 2 9.230165D1 8.752n001 6.104420D2 3.2405799 2 3.965381E*2 95 JA 0.0 6.13950D2 7.349050t+1 8.720682D 1 6.104420 0 2 3.240579D 2 3.965341D 2 atAMG Ja 100.0 6.13950D 2 7.349050 0 1 8,no682t+1 6.104420 0 2 5.150395D 2 4.3789490 2 96 JA 0.0 8.873820D 1 6.21253M *2 5.486182t+1 4.378948D 2 6.104424t+2 5.15039BD 2 stAMG JS 100.0 8.87382C4 + 1 6.212538D2 5.486182D 1 4.378950 0 2 5.8815480 2 9.345911D2 97 JA 0.0 9.4244700 2
~~4. 762820t + 2 1.484172D2 3.4 71989D 2 7.821997t*2 5.027475E +2 8tAMG A~~
~~JB 100.0 9.424470 6 2 4.762820t4 1.4841Rt+2 3.4719900 2 5.732126D 2 1.759663 0 2 i 98 JA 0.0 9.445890t+2 4.?s3844D 2 1.604191D 2 3.471989t +2 5.732126D 2 1.759643t+2 stAMG 1 Ja 100.0 9.445890t=2~~
~~4. 743844D2 1.604191t+2 3.4719900 2 3.471987t+2 8.436039t+2 g~~
~~99 JA 0.0 1.00469Ct 3~~
~~3. 40tJL3 7t + 2 1.915871f*2 1.227085t 12 4.91013)t+2 8.436039t+2 stAMG~~
~~.2 Je 100.0 1.0046900 3 3.606837t+2 1.915871D 2 1.2270801 12 2.596586D 2 4.323148D 2 100 J4 0.0 1.0059CCD 3 3.4585184+2 2.CT7269t+2 5.228569D 13 2.596586D 2 4.3231480 2 stAMC Je 100.0 1.005900t*3~~
~~3. 45851M~~
2 2.077269 9 2 5.228570t 13 5.570 R9D 12 1.706110D 12 101 JA 0.0 8.64A640D2 4.313273D2 7.141M3E + 1 6.127850D 1 2.464975 t + 2 4.327040E+2 stAMG JS 100.0 8.648640D 2 4.313273D 2 7.141M3D1 6.1278500 1 1.460517t+2 1.825711D 2 102 JA 0.0 8.669720D 2. 29 115D 2 6.065508O 1 6.127850 0 1 1.460517D 2 1.825?11D 2 StAMG Ja 100.0 8.6697200 2 4.2M115D 2 6.06550M +1 6.127850D 1 6.127855t+1 7.867091t *2 103 JA 0.0 9.18011CD 2 3.1754130 2 4.006895D1 1.202658t 12 8.6660960 1 7.867091D 2 BEAMG Jo 100.0 9.180110D 2 3.175413D2 4.C06895D 1 1.202660D 12 3.853727t+1 4.033979t+2 104 JA 0.0 9.192890t*2 3.227183D 2 3.082981t+1 9.428237t 13 3.853727D 1 4.033979D 2 stAMG i
Ja 100.0 9.192890D 2 3.227183D 2 3.082981D 1 9.4282401 13 1.344886 0 12 1.340328D 12 Title : Peop 2 19=u19= 1 Out;nJt let 6 15E Set MI/ Min $4msnary table set 10 Vetue 9 Seen traf A AAlet forte minimm 6 69 75.0278 nea tma 6 100 1005.9 { Seam traf A Sheer 2 Force ulnimm 6 77 34.5317 j .a iam 6 96 621.254 Seen truj A Sheer 3 f orce minimm 6 61 L47249 9+ maalam 6 100 707.727 C Been EM A Tertpe minim a 6 100 5.22857D 13 h mes t am 6 86 610.442 'y Seem trvf A acment2 minimm a 68 2.53472 maximm 6 97 782.2 b{ s sees ind A Mcment3 minimm 6 98 175.964 i maa t am 6 86 1207.29 s, fel
'=
~~Sese Ert 0 Anlat force minimm 6 69 75.0278 1' f. keimm 6 100 1005.9 ' = Seen End 8 Shear 2 f orce m iaimm 6 77 36.5317~~
~~s :~~
maa imm 6 96 621.254 g Seen truj t sheer) force minimm 6 61 3.47249 g* men imm 6 100 207.727 seem End 5 forgae minimm 6 100 5.228571 13 n 's maa lam 6 86 410.442 k "I tema tras a Moment 2 minimm 6 104 1.34489D 12 P mea tma 6 85 610.442 3 Been truf a Monent3 minimm 6 104 1.340331 12 A men tam 6 85 1207.29 4 Title Pi& 2 19"X19* Fine 1 MX/ Min Summer 1> Tabte let 10 Veiue i ' g ;t Seen trui A Aalet Force minima 1 67 0.044464 man lam 6 100 1005.9 {y -n seem tnd A Sheer 2 force minimm 1 99 40.3457 s maalma 6 96 621.254 Been End A Shear 3 force minim m 1 64 -140.723 'O maalam 6 100 207.727 . ; Q[ me w Jc. _ ~ s@ czy, f*g e n.,.,,j 6.N hh.3 Q(' d qpum ~
.n j6r
~~s..,,.~~
ATTACHNgNTS ' j* ~ m 0 u. m., m m. m.1.2., SHEET d _OF....._ iri Apr 12 14:39:11 1996 gC,gg stumAP ve sten 4.41 44=r t stament modet i forest stuovat ser/se (leet O + Title : PeoP 2 19*319* U"r ' team trus & terem minf aus 1 96
~~10.2821 monimum 6~~
~~to 610.442 .s 'i _.~ Deem truf a moment 2 minimm 1 81~~
~~113.787 11/~~
maalaus 6 17 782.2 M team truf A moment 1 minisue 1 93 '99.169F maa t am 6 8d 1207.29 f, Seam truf 8 Aalet f orce ut n4mm i 104 +309.332 maa t sun 6 100 1005.9 Seam trus a sheer 2 f orce min 6 sue 1 102 +80.2569 mea tsus 6 96 621.254 team tid I LAeer3 Iorce minlaun 1 68 159.298 man tase 6 100 207.T27 Seem tid 6 tor pe m6nisue 1 60
~~102.044 maalaua 6~~
~~$6 610.442 Bese trad 8 moment 2 minisun 1 68 +343.843 mealsum 6 85 610.442 p lb72 6 iff pf~~
~~s n,~~
~~t.p $.,, _.,f 7 M g?l' r... Qf 4 p =r g 4 s N (* ( 1 7- - h. :;... 'a - , k' [ .r Y.$ y . p;f ' a ~,\\' d -s~~
~~J' A)ww.e g4.~~
~~) /he, Qyi[*$$$? m <'. t [?f0 mscP v%ey; s c;;g. -., +. x 9 b .,.-4, 'k. d; 'N - f i-a aD { e-~~
~~+ -~~
~~C+ k.,};$'.' ?${*,. la '~. ;}j .- a : * - qll%,"$ Q^ ., W b;ns A,Qrfiy,,k.f krf ' n:.s, x , y9. _- ~ b.f n [. cb, O k;? $'];^ .~, f - e, g uis u e. i. pY lce;_. h' ..g \\ v, Y, _ +~~
~~a4 r-.~~
~~.Jc ng " ~#h. $hhQ O, v;g;9 pp ge.r .+ xqv b., y;p y,, ,m s. .y,~~
~~@ w. m ;-~~
t ve,..gp - v%a w.
..-.h-...,,,,, wnu Al l ACHMENT c-uw < ~ c g# . - - - > ~.. - S .BY MM ,[ l* aytheen Engineers & GENERAL j o N I' Ih;O B Constructus COMPUTATION PA[UM. F ed AL CD SHEET J I I X FERMI 2 - CCHVAC 1 sHEU W DATE OME-( uuva z.vnvulus ut TM7 J 0-76230.502 h. N CE OV6TEH-GERIEC iv W attachment are generated using the y 0.g T' The dat'a contained in this STARMAp is a companion program of STARMAp post processing f eature. STARDYNE which is used to perform the system string analyses. The purpose of the tabulated data is to present the forces and the ductwork by each duct size for DL, OBE and SSE moments in Maximum and minimum values for each duct size are also conditions. I l presented. Based on the commands issued by the preparer, STARMAp accesses the b working files saved by STARDYNE during the string analysis runs and I prints the data in tabular form. The data are then spot checked against the string analysis outputs by the checker. The r,tring analysis outputs are contained in the following y calculations: CCHVAC Concern Resolution Task Duct String Analysis and Support Evaluation of DC-5763 h 2268 System Series VE CCm?AC Concern Resolution Task Duct String Analysis and Support Evaluation of D DC-5764 o M 2848 System Series i CCHVAC concern Resolution Task Duct String Analysis and Support Evaluation of e-DC-5765 J d [p+' 2849 and 4126 System Series .a 'i .? [ CCHVAC Concern Resolution Task DC-5766 Duct String Analysis and Support Evaluation of jk 4 _$r5; 2850 System Series Z. k*? %it @kV, CCHVAC Concern Resolution Task jS-DC-5767 Duct String Analysis and Support Evaluation of K, a M:, 4336 System Series .v Q $.,4 g', @y s - w.m a+
~~i :..wp S.~~
~~'h ^& w% ,.x, i, ;S:: $n Me+f .'; Ypi <. M2h '~~
~~n :p&z~~
. q" 4; p s 'q& [a [,~,, L ? a ..m M f QQ _. : w i & ar y g:9: 9 %h5 ~q" y"ny &-v.i?N d l Qv m mQ' Nl s w w., ~r I- (
Q YI'A h I/ ((gj d4 # IMAGE EVALUATION k//// [ $bf/ 4 1 TEST TARGET (MT-3) g 4 }}77p 3 I.0 E2 m "lj Ha! I.l [* EE l18_ l.25 1.4 i 1.6 L_ 4 150mm 4 6" dI % 4/ ih+,
~~f4*h I~~
48 L'^r ///f 7// sp 4 s o '" ' *"""E '8WHLM"' """ " 4 p* 7 mesud s!,ja*; us80 e i
4 lh l .1 3 3% ATTACHMENT C A m 4 Otc0 Etsvat 5YSTru 4h61'2'? SHET. 1 or,,, [ ~ g fri apr 12 14 MO:C2 1996 gg 3793 $18AhAP Verstw) 4.0 g pesert f iemient Mcdel format 51 AActet ter/te.ma I L emem tg% h[". + 1 - ( iltle : P90P 3 10*110* Output let 1 DEAD LOAD (DL) et4a ttImtaf (0AD5
~~d W~~
~~ulat sotaa tutAa TCRL om StuolmG stacing a v2 V3 mi m2 m3 k 1 SEAft h 105 JA 0.0 3.044360t 2 7.137547t t 2.0155221+1 3.930880t 15 3.209238E 15 0. etAmG JS 100.0 3.044360E 2~~
~~7. E3 75871 '~~
~~2.015522t*1 3.930880E 15 A.031043E 1 1.5675171 0 106 JA 0.0 3.MMot 2~~
~~5A3839t 3~~
~~3. 673 t T3r t 1.6 8800E 15 4.031043E*1 1.567517t +0 StAMG M+~~
Je 100.0 3.0 4%0t 2 7.8&3239t 3 3.6731734-1 1.668800t 15 4.107659t.1 1.5511371 0 107 JA 0.0 3.G+4360( 2 f.3019t't*0 -3.197319f*1 8.246880E 15 4.107659t*1 1.551137E 0 stAmG Je 100.0 3.M360E 2 1.3019114 0 3.197t.9t*1 3.246880E 15 2.893415t*0 2.3999071 1 108 JA 0.0 3.064360f-? 135232f 0. 5 31L33t
~~1 -3.625570( 14~~
~~2. 893415E *0~~
~~-2.3899071 1 stuG Ja 100.0 -3.k4360( 2 -1.325282i 0 = L110314 1~~
3. J5570t 14 6.524045t*1

2. 764339t *0 4
~~109 J4 0.0 3.%4360E-2 '. 32527M *C . 481769n t 3.52843C1-14 6.1240431 1 2.764339t*0 stuG k Je 100.0 3.044 Mot 2~~
~~1. 82529M~~
~~0 4.481769t*1 3.528430E 14 1.665805t.1 7.8571T71 1 h~~
~~119 JA 6.0 3.Wh0t 2 - t 40534 71 0 3.432063t*1 1.856850E 14 - 1. M5805E~~
~~1 -7.857177t 1 EEAMG 48 100.0~~
~~3. M 360E 2 1.4053471 0 1.4 3200t~~
~~1 1.b68501 14~~
~~2. 0476SM~~
~~1 7.%86721 1 111 JA 0.0 3 % 4 % 04 2 1.035459t-1~~
~~'. 780768f *0 2.00881M 15~~
~~2. 0476SM~~
~~1 7.%86T21 1 St uG y~~
~~015 39t ?SU6M*C 2.008810f 15 -2.477920t*1 - 9.850294t 1 Ja 100.0~~
~~3. N4360t -~~
~~S.3 M st 2.16 419t 1 5. 5 3 7240( - t 5 2.*?7920f*1 9.850294E 1 stAnc 112 JA 0.0~~
~~3. 0.h0E.~~
~~-8.336845E 1 1.16 6toget 5.537240(-15 2.756130f 1 1 030820(*0 JS 100.0 - 3.M%0E 2 O 113 JA 0.0 3.044 h0(-2 -f.728.'071 0~~
.390269t*' -1.5543106 14 - 2. 756130E

1 1.030820E*0 stAmG Je 100.0 3.0=4360f-?
~~t.778e07t.c . 390269t.1 1.554310E-14 1.65850t*1 5.987180E 1~~
},
~~114 Ja 0.0~~
3. 0-4 h0( 2 7.5"561M i

1. 43 M t*1 2.2339Act 14 -1.6555634 1 5 987180C 1 8(Anc 1 !,
~~JS 100.0~~
~~3. k4360f 2 7.5 7561M t~~
~~-1.M3 M t+1 2.2339sof-14 1.M T259t*1 4.686848t 1 7 11$ JA 0.0~~
~~3. MM01 - 2 1.5982tu t~~
~~. 69.334t *0 2.169100f 14 1.% 7250t*1 5.6868488 1 BEAMG JS 100.0 -1.044360( 2 1.59821M - 694 334 t~~
~~0 2.169100E 14~~
~~2. 09112 M~~
~~1 8.151300E 1 h~~
~~116 JA 0.0~~
3. M hof-2

9. 05 36M - 1 2 281023tet 2.706860f 54

2. 09112M
~~1 8.151300E 1 stAnc Je it* O 3 044360E 2 9.40536M t 2.231023E*1 2,70d860( 14 5 722991E 3 4.734224E 2 117 JA 1.521430t*1 - 3 0 435M '~~
~~2.543185E t~~
~~3. 073 h0( 2 1.541822f~~
~~3.646209t 2 stAMG .e h-Ja 100.0 -1.52'430(*1 3.0 43554 2 2.5 31851 1 3.073 %0E-2 1.236493tet 5.126371t 2 Y 118 JA 0.0 2.775920E-2 1.424964t*1 5.21519?f 1~~
~~3. 479660E - 15 1.191381t*1 3.309993t*0 SEAnc 4~~
JS 100.0 2.795020E 2 1.4249644 1 5.215t92t*t 3.479860E-15 5.765685f*1 1.569902t*1 119 JA 0.0 2.795920( 2 1,12 7136E.1 e.135 701t a t 2.003950t-14 5.765685f 1 1.5699021 1 SE4mc ~ JS 100.0 2.795920( 2 1.127136tet 2.1357014 1 2.003950f 1+ 1.9773831 1
~~5. 37445M~~
~~0 120 JA 0.0 2.795920t-2 8.9 b220(*C~~
~~3. 2 78 38f~~
~~1 5.82867t4 15~~
~~1. 97738.3 E.1 5. 374456E~~
~~0 stAnc Ja 100.0~~
~~'2.795920t 2 8.95 220(*0 3 270 38f*1 5.328670E 15 1 02566M a 2.80928)t*0 'd 121 JA 0.0 2.795920t 2 1.42987M *0 5,258 45E *0 0.~~
~~1. 02566M * '~~
~~2.809289t*0 EtAMG J8 100.0 -2.795920( 2 1.42957M~~
~~0 -5.258445t*0 0.~~
1.945894t*1 5.311571E*0 W 122 JA 0.0 2.7959201 2 3.03516*t*0 1.111939t*1 c. 1.945894t 1 -5.311571t*0 SEAnc g A IN.0 2.795920(-2 3.0P18.E 0 1.1119391+1 0. 7.10542?t 15 2.122434f - 15 =. O viite reon 3 10 iio-Output Set 1 DEAD LOAD (Ot) Set ID Value N M Set MAX / Nim Summary table N! ' Seesa End A AAlet forte minimm 1 118 0.027959 DU maa s sun t 11? 15.2143 Beems tral A Sheer 2 f orce minima 1 118 14.2496 [ me n isus 1 119 11.2714 g-W, Beems End A shear 3 f orce minisun 1 118 -52.1519 j-id, menisue 1 109 44.81 77 dMd Seen End A forwe minimm 1 108 3.625571-14 me a le. m 1 117 0.030734 ,O i 4 M.f minimm 1 109 65.2404 f hM., mea tma 1 107 41.0766 Mh; Seem (M A moment 2 j Mre*,, Seem tnd A Moment 3 minisam 1 122 5.31157 l max imm i 119 15.e99 QM p4yg c < BeJa End B Amtet force minisam 1 117 15.2143 me n iaue 1 118 0.027959 y Q[2; A ;, Sosu EM S Sheer 2 force miniaun 1 119 11.2714 '+ .l y maa ttem 1 118 14.2496 g & g' miniu m 1 109 -44.8177 5 -l l Seem fnd 8 Sheer) Force pr maaimm 1 118 M.1519 1j M Seen End 8 for we miniaun I 117 0.030734 maaimm 1 108 3.6255't-14 .5 g. Seen End 8 Moment 2 minimum 1 106 41.0766 t.N-@ T maa tam 1 108 65.2404 j i, w,g 2n$x ww.m mm k,h$h IN s mor . w lw g Lff ,? JW v ^
_.. _ -._simuur h I I ATTACHMENTN l %.u g ,,, us,,,,,,t,, ,3y y pp tri Ar 12 lu40:06 i m oc-syn stAnaAP ver.i.n 4.4i seport 1 tienent e ?.- pedet I [ fennet t 51 AA01st lar/tema ttemet s-g title a Per 3 10*t10* Outsmit let 1
~~DEAD LOAD (04) seem trui e nament3 minious 1~~
~~118~~
~~15.699 A~~
i manimum 1 121 5.31157 ); .11tle Pew 3 10*E10' ,Q[ Output let 2 = CSE 6tAe i4EuEu1 4040t {j ulA4 lutAA latAN TCstlica steluG stuoleG P v2 v3 ut m2 R3 105 JA 0.0 2.281530t*2 4.030591t*1 5.193237t+0 1.152003t 14 2.093015t 14 1.655167t 13 stAmG C M AA Jt 100.0 2.281530t+2 4.030591E
1 5.193237t+0 1.152000t 14 1.038647t+1 8.061183t*1 106 Ja 0.0 2.510000t*2 3,97 6 3tet 1.872070t+0 3.613319t 16 1.03364 71+ 1 8.061183t+1 EtAMG JS 100.0 2.510000t*2 3.97 & 3tet t. S T2070t + 0 3.6133201 14 1.24899SE*)
~~1.6327671+2 107 JA 0.0 2.88333M~~
2 3.907352t*1 7.893246t+0 6.400450E 14 1.248998t+1 1.632767t+2 BEAMG J3 100.0 2.f43330t

2 3.9073521 1 7.893246t+0 6.40045M 14 1.021205t+1 2.165091t+2 108 JA 0.0 3.037'50t*2 3.89773M

1 1.102912fet 1.297789t 13 1.021205t+1 2.16509tt+2 stAnc
~~(' JS 100.0~~
~~3. 03715M~~
2 3.897739t

1 1.102912tet 1.297790t 13 2.016248t + 1 2.695998t + 2 109 JA 0.0 3.93534M*2 2.27978et

2 1.556899t

1 1.8633cM*13 2.016248t+1 2.695996t+2 StAms
~~= Ja 100.0 3.935340t*2 2.2 79754t~~
2 t.556899t+1 1.863360E 13 4.16802M *0 3.455037t+1 110 JA 0.0 4.03637M+2 2.2TT211t *2 1.393929t+1 9.k2TT9f 14 4.16802M

0 3.455037t+1 stAMG J8 100.0 4.05637M

2 2.2T7211E*2 1.393929t*1 9.64278M 14
1. 27476M +1 2.269762t+2 111 Ja 0.0 4.4313&M *2

2. 261775t
~~7 t t t9139t + t 1.610a57t 14 1.274769t+1 2.269762t*2 stAMG J6 100.0~~
~~..+ 3138M~~
2
~~2..'6175 t * ?~~
~~t.tf9139t+t 1.610860E 14 3.919 789t~~
1
~~7. T2175 M~~
2 til JA 0.0 4.70101Ct 2 2.247503t*2 1.228142t+1 2.125687t 14 3.919759t

1 7.T21758t+2 BEAMG J5 100.0
~~4. 70101M~~
2 2.247503t

2 t.228142t+1 2.125690E 14 6.597604t+1 1.315305t+3 Q
~~113 JA 0.0 5.435300t*2 2,1835e9t*2 4.6286tt+1 1.8785511 13 6.597604 t +1 1.315305t+3 stAMG W 48 O J.0 5.435300t*2 2.18358vt*2 4.642561tet 1.878550C-13 5.454538t+1 1.273438t*3 114 Ja 0.0~~
~~5. 71418M~~
2 2.159171t

2 + 538887t*1 6.786921t 14 5.454538t+1 1.273438t+3 stAMG JS 100.0 5.714150t*2 2.15417tt 2 4.538837t+1 6.726920t 14 1.704756t 1 1.0433Nt + 3 115 JA 0.0
~~5. 885690t~~
~~2 2.112496t*?~~
~~4,50119TE+1 8.196640t 14 1.704756t*1 1.043399t+3 EFAMG -3 JS 100,0 5.885690t*2 2.11249M~~
~~2 4.501197t+1 8.196640f 14 8.529686t+1 8.839697t+2 3~~
~~116 JA 0.0 6.201050s 2 1.95615M~~
2 4.49014t*1 1.215221t 13 8.5 N68M

1 8.839692t*2 atAMG JS 100.0 6.201050t*2
~~1. 95615 SE~~
~~2 4.490104t+1 1.215220t 13 1.259558t*2 8.396118t+2~~
~~.117 Ja 0.0~~
~~1. 74 7770t~~
2
~~6. 27896M~~
~~2 8.863805E+1 5.576320t+2 1,891404t 11 6.402543E+2 staxG Je 100.0~~
~~1. 74 7770t~~
2 6.275969t*2 8.563803E+t 5.57632M

2 4.309570t+1 9.301316t+2 118 JA 0.0
~~1. 73081M~~
~~2 6.448189t*2~~
~~1. 343414t~~
~~2 1.81150M 12 2.82968vt + 2 1.04T800t+3 stAMG JS 100.0~~
~~1. 73961 M~~
2 6.44818 M

2 1.343414t + 2 1.8115004 12 1.091191t*2 3.212390t+2 119 JA 0.0 1.222220t*2 5.217201t+1 1.Sf3104tal 4.881519t 13 1.091191t+2 3.212390t*2 stAMG JS 100.0 1.2S822M*2 5.2172011 1 1.81310 stet 4.881520t 13 9.454545t+1 2.74039t+2 120 JA 0.0 1.224960t*2 5.*16-65E+1 1.371589t

1 1.84761M 13 9.454545t+1 2.764039t+2 stAmG JS 100.0 1.224940t 2 5.41663t 1 1.57tS89t+1 1.6476201 13 7.896502t*1 2.287262t+2 L
121 JA 0.0 1.02318M.2 6.340563t + 1 2.182795t+1 4.906365t 14 7.896502t+1 2.2872621+2 StAmG JB 100.0 1.023180t*2 6.3405&lt e t 2.182795t + 1 4.906360f.14 4.106642t+1 1.179174E+2 122 J4 0.0 9.045870(*1 6.738 t e tt e t 2.346653t+ 4.0647911 16 4.106642t+1 1.179174t+2 StAMG JS 100.0 9.045870t + 1 6.738141t*1 2.346653E+1 4.064790E 14 5.8116041 13 3.217644E 12 + fitte Petr 3 10-11C* W (6 . Neput set 2 - Ost ( Set 10 Vetue Set.. MAX /ulu Summary fede p' *g seem EM 4 Aalet f orce minisun 2 122 FO 4587 han isus 2 116 620.105 Seam End A Sheer 2 f orce minious 2 108 38.9774 {e masisue 2 118 644.819 L t wy; Some End A Sheer 3 Force NNaus 2 106 1.87207 maalsue 2 118 134.341 W -$Gf, Beam End 4 fortpe Minimes 2 105 1.1521 14 '7 D menisue 2 117 557.632 W f $+aan EM A moment 2 minisue 2 105 2.093021 14 ^ = maalaus 2 118 282.969
~~Kf Does EM A noment3 minisun 2~~
105 1.65117t.13 C maalaus 2 113 1315.31 i pf team EM 5 hiet force minious 2 122 90.4587 maalmJa 2 lie 620.105 M Seem (M 4 Sheer 2 f orce utnisun 2 108 38.9774 h y-7' ; manimum 2 tla 644.819 y Seems End B Sheer 3 f orce ninluur 2 106 1.87207 i M k N{ p maatsus 2 118 134.341 fhs W% yMW W +L "- A v :'"[s W gbn. ,q h* f 5 $W
-g:g& f " ATTACHMENiE y$n~ DICO ttavAt $ttttu 4316 1,2,3 $ OF T SHEET pel Apr 12 14:40:10 199o toport tienent QG]Q ~876amAP vercian 4.41 j" leadet ? Ft+eet $1Aa0fut ter/8ean Element h . Title : Peor 3 10*s10a , fp^ - thstput Set 2 + OSt minimm 2 105 1.152t.14 j, ~ 6 s ( team EM 5 Terem. nomiam 2 117 557.632 E-toen E M S enament2 minima 2 tN 5.811M.13 masimm 2 116 125.956 -Of seen (M e moment 3 minium 2 122 3.217kt 12 5l~ mes t am 2 112 1315.31 T I title t Peor 3 10* 10a h Cutput let 4 * $$t 8 TAN tLiaieI L0A05 aslAL Set Aa SMA8 10ellom stuolnG StuottG gr P v2-1/3
~~7 N2 143 74 105 JA 0.0 2.1980000 2 4.099140t+1 4.430953D0 1.498109t 14 2.721389E 14 1.804241t 13 8tAMG p~~
MAM b J8 100.0 2.1980000 2 4.0991400 1 4.43095300 1.4981900 14 8.86190M +0 8.1982800 1 7 106 JA 0.0 2.415M00 2 4.013853D 1 t. 81347M +0 3.68S437t 14 8.861907t+0 8.1982800 1 StanG . JS 100.0 2.41566CD 2 4.013853t+1
1. 81147M +0 3.68844M 14 1.108205D1 1.651527t+2 107 JA 0.0 2.771460 6 2

3. 953353D 1 6.43308D0 6.973581t*14 1,108205t*1 1.651127D 2 StAmG JE 100.0 2.T714606 2 3.953353D1 6.643308t+0 6.973580E 14 9.879538t +0 2.181795t*2 108 4A 0.0 2.9180900 2

3. 967103t
1 9.239869E*0 1.845373f 13 9.87?538D 0 2.181795t*2 SEAmG Je 100.0 2,918090t*2 3.967103D1 9.239869D O 1.84537M 13 1.792T72D 1 2.71313M* 2 109 JA 0.0 3.774530t+2 2.29658+D 2 1.406587t+1 1.9405891 13 1.792772t +1 2.71313M +2 alAMG JS 100.0 3.T745300 2 2,2965890 2 1.406587t+1 1.940590t*13
3. 74593M *0 4.570320t*1 110 JA 0.0 3.88W70D 2 2.N2517t *2 1.281861D 1 1.21694M 13

3. 74593M +0 4.570320 0 1 stAnc J8 100.0 3.8899700 2 2.292517t*2 1.281861D1 1.2169500 13 1.2114866 1 2.326387t*2 111 J4 0.0 4.2476406 2 2.2705T71+ 2 1.075913t*1 2.2312390 14 1.21148601 2.326387t*2 BEAMG Ja 100.0 4.2476400 2 2.2 7057?D 2 1.075983f+1 2.2312300 14 3.762248 1 7.78425 M
~~2 112 JA 0.0~~
~~6. W 800t+2 2.M14bt*2 1.15 3 702t~~
~~1 3.1980391 14~~
~~3. 762264D 1 7.78425M~~
~~2 St AM.~~
~~Ja 100.0~~
~~4. W 800t+2 2.2516M D 2 1.153702t + 1 3,19804DE 14 6.336983D 1 1.3220790 3 j~~
~~c 113 JA 0.0 5.205t50t+2 2.937925f+2 4.385423D1 2.4378090 13 6.336983t*1 1.322079D 3 stAMG }; I Je 100.0 5.2051500 2 2.93M25D2 4.38%23D1 2.43?B00E 13 5.26342M~~
~~1 1.268030E*3 114 JA 0.0 5.4711?M + 2 2.906557D 2 4.307533D1 7.7539118 14 5.26342601 1.2680300 3 stAMG y~~
~~Ja 100.0 5.47117M + 2 2.90655 7D2 4.30M33D 1 7.753910 0 14 1.74128 4 9.930184t+2 115 JA 0.0 5.6%M002~~
~~2. 8*539 7t + 2 4.276515 9 1 1.1347121 13 1.7412SM~~
1 9.930184t+2 StAmG Ja 100.0 5.6MM00 2 2.8453971 2 4.276515t+1 1.134710D 13 8.10182901 8.751695t+2 116 JA 0.0 5.9355406 2 2.43024D2 4.257928D 1 1.403442t 13 8 101829f*1 8.751695t*2 stAMG 3 1 JS 100.0 5.935540(*2 2.43024D2 4.257928t +1 1.4034900 13 1.195853t+2 9.010085t*2 112 JA 0.0 2.2651002 6.009562D 2 1.304075D2 5.780852t*2 1.864380D 11 7.013797D2 StAmG JB 100.0 2.2675100 2 6.009862 0 2 1,304075D2 5.7808500 2 6.340396t+1 9.6424730 2 118 JA 0.0 2.3612606 2 6.169588D 2 1.28299M*2 f.7299378 12 2.781M9t+2 1.0911440 3 StAMG Je 100.0 2.3612600 2 6.169888D 2
~~1. 28299M~~
~~2 1.729940 0 12 1.157358D2 4.6055500 2 119 JA 0.0 1,713880t+2 7.785009tel 1.877810t + 1 4.M3&ME 13 1.157358D2 4.6055500 2 stAMG O~~
JB 1C4.0 1.783880t+2 7.785009 0 1 1.877510D 1 4.753630t 13 9.9965800 1 3.912997t*2 e 120 JA 0.0 1.702690E+2 8.0125470 1 1.96247'D1 1.797178f 13 9.996560t*1 3.912997D 2 atAmc Ja 100.0 1.7026900 2 8.012587t+1 1.962473t+1 1.797170 0 13 8.309045t+1 3.1934900 2 %m E 121 JA 0.0 1.442950 0 2 8.92T264f + ' 2.301348t+1 5.10415M 14 8.309045t*1 3.19349002 stAMG JS 100.0 1.4429506 2 8.92T264t*1 2.301348t*1 5.1041600 14 4.303558t+1 1.63295402 a .. 122 J.4 0.0 1.2893500 2 9.331165t*1 2.45917M+1 3.996531t.14 4.30355801 1.632954D 2 StAMG u? Ja 100.0 1.2893500 2 9.331165t*1 2.4591764+1 3.996%0E 14 5.878191E 13 3.176413D 12 4 litle : P90P 3 10*110" ad R t d thatput set 6 55t set ID Value pgd let &luR/ Min Sammary Iobie MMimm 6 122 128.935 mo' hyg %. Seem EM A Aalet force Maalma 6 116 593.554 W m i ni== 6 107 39.5335 W team (M 6 Shear 2 force ,s. JW maa lam 6 118 616.969 rA 5ees EM A sheer) f orce ulnimm 6 106 1.81348 @6 M aa l== 6 117 130.408 , ^,' Seen EM A Tortpm minim m 6 105 1.498190 14
w
{W$ [s uasiam 6 117 578.085 ' team EM A moment 2 minium 6 105 2.721398 14 1> --N. g naulam 6 118 278.176 'J w, f "E [V Seem EM A moment) Minimm 6 105 1.80424t 13 y maala m 6 113 1322.08 J i .e.Y. t M. A.i..or.e 1nimm 6 IN ,28. m t, 3 masima 6 lie 193.554 %k
~~N ?a w yfe Y?~~
~~l w nn~~
~~ft $~~
W My M Ny. h-. .sv n A n I. O* ? p-
l ATTACHMENT c-s@rfe 4 4" i 3 My ' f fp s-Ws4 OtCO Cfevat 575114 4316 1,2,3 % fM) i' Fri Apr 12 14:40:14 1996 saport : Element $1 AAlthP Verelerg 4.41 k (! ,a mestet I $fAaDYut sar/seem timment %}
~~PecP 3 10=x10=~~
~~JM - [ a forent N-6f: ~fitte F -[ Owepwt let 6~~
~~sti minimm a~~
107 39.5335 4 1 Seem tid e Sheart force maatam 6 118 616.999 f i minim m 6 106 1.81348 f y i: (%., team Erd a sheer 3 force mas tam 6 117 130.408 i D~ minimus 6 105 1.49419t=14 2A Dean trd 8 forgue maalaus 6
~~17 578,085 t~~
minleue 6 122 5.l?l19t*13 h I~ team trd I feoment2 maalmun 6 114 119.585 6 122 3.17641t 12 e minimum i Seen Erd 8 masent3 Natam 6 til 1322.03 .^ 10 Walue ^ 'n fitle t PeQP 3 10"X10* let i firel win 6mm i 118 0.027959 NAX/plu Summary f ebte ${ ~- teen truf A Aalet f orse maaloue 2 116 620.105 i 118 14.2496
~~f a 6nimm 4~~~
team trd A theer2 force mant sm 2 118 6&4.819 minimm t 118 52.1519 S'_ Sean trd A Shear 3 f orce masisue 2 118 134.341 108 3.625571 14 1 k. minimm Seeuntid A forspe mestam 6 117 518.085 1 109 65.2404 eI", minim a 2 114 212.969 been Erd A moment 2 man t am alnlam i 122 5.31157 Q Seem trd A moment) mea tma 6 113 1322.08 g minisue i 117
~~15.2143 p '.~~
Seen Erd 8 Aslet force aaaisue 2 116 620.105 11.2714 1 119 minim m th Seem trd 8 theer2 force maalma 2 118 644.819 f 1 109 44.81TT minimm gu-tea sres C Sheer 3 force maatsus 2 118 134.341 ministan 1 117 0.030734 %. e Seen Erd 3 Tonym maatsue 6 117 578.085 i 106 41.0766 -!h seem truf 5 moment 2 mantman 2 116 125.956 4 minima minious 1 118
~~15.699~~
~~.s [d.Q V.~~
~~seem trd a moment 3 maatsam 6~~
~~112 1322.08 M', g . m ,,,+,% 5 kWiY uw -5sa:~~
~~5. jf n~~
~~ym-4 k: 1; q 37 ch c y 2+ e[ f[,- .j jl*i f. / ~, em~~
~~<3, %..~~
~~4. + Nj,< ey ., Wy n Jl map. o A ]' s % 3 s_,m, py4 w.s... a.= x l.Q*J. ;;;g R&W" s~~
%

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^
um
~~,q q m ]y k ,NK_ ,b L,, 4f3 .a W 4 g((M(3 Q; , l n 3p;2~~
~~n MN!~~
~~4-e q~~
~~r.~ ty 4, fi 4_hfy V p VT s mu V ' )Q*,s;,., 'J Mg jty 'Y_ "~~
~~4W;?u 4 Y-si~~
^ 9% Q[- ,f ' .Q. :!ye,.a - h. 5 hk o#;p%wls e M;e;+ ' i /Q.f A{d , e g-._, f g. , - g..Qi g. 4 jf f. *, ;.. ti
I h i eu ATTACHMENT d l IL ' #a g l ru- ~ C HK n Inf M mwer QEu [drIR$Y" N w -u awase m enu cAtcuuTO4 SET M k 14 g R?F' Enginecis & GENERAL. DC-5773 pf s g$4 pg 'o 3 Constructors - COMPUTATION _-PAEUM. FINAI. 00 A SHEET ,e p X - oATE FERMI 2 - CCHVAC SHEri OF DATE ~. s.h, PRCUECT_ LvALUATAvH vt_ %4 puvT TV sueutCT _. cys9tg_ssnyt; J o. 76230.502 p:t ;4.. ~;; - : I the b generated using t are he data contained in this attachmentSTARMAP is a companion program of g; b T lyses. STARMAP post processing f eature.STARDYNE which is used to perform the the tabulated data is to present the forces and L ductwork by each duct size for DL, OBE and SSE 7 9 of E The purpose Maximum and minimum values for each duct size are A moments in the conditions. 4 presented. P accesses the g '., Based on the commands issued by the preparer, STARM lysis runs and checked l in tabula.r form. prints the dataagainst the string analysis outputs by the checker. contained in the following Q ?!I The string analysis outputs are W calculations: R CCHVAC Concern Resolution TaskDuct String Analys y
~~7' s.DC-5763 2268 System Series gg.~~
y CCHVAC Concern Resolution TaskDuct String Analy bk. ' DC-5764 y? 2848 System Series A> CCHVAC Concern Resolution TaskDuct String Analys s yy DC-5" 65 e; and 412d System Series IM 2849 h' CCHVAC concern Resolution Tasknuct String Analysis e 4D DC-5766 k 2850 System Series 35E' 4y CCHVAC Concern Resolution TaskDuct String Analy N DC-5767 h ' gk ![,.' 4316 System Series
~~^ : ~..~~
~~.:na Ufh f-A m .m 'Y$I~~
~~h.-f{ TlN 5 %:~~
~~M@ Mi n 0s~~
~~ca.~~
~~m$N$ ~h,l [:i~~
~~O em y~~
-[ hk;;t -H e. [ L sc gg ,)fh-f dd ~
ATTACHMENT W M w& W g Q-OF W .4 0100 ttu/aC 1151tu 4316 6 & T N*M D i thw Apr 18 12:49:02 1996 N. 4 Stae w version 4.41 aeger : [tsesnt Model
~~S u~~
_ formet 1 Staa0fut Ber/Seem tie *wat -4 ~ y .;1;* title 1 Pt0P 3 16*t16* p Outsut let 1 DEAD LCAD (Mt ,, 4 ", ( 8iAm tLtatut L0A05 at a. [;- ARIAL SatAt $NE AR Tot $!CN $tlCl4G StuothG ' ' ~ M Mt P v2 V3 af m2 su 4 61 JA DJ 2.90799:( 4 '. 4 %0 A t. 2
~~1. 95118M~~
~~1 2.15764M *0 1.349383t*1 1.737938t 1 SEMG Je 100.0~~
~~-2.90798;t.2 .*360ht 2 1.98118M *1 2.157M0t*C 2.612947tel J.2251571 1 62 JA 0.0 6.45870ct.t 1.01984t.1 4.509343t*y 1.29894M~~
~~1 1.063407t*1 6.60C884 1 SEAMG JS 100.0 6.45870CE 1 5.019t%t 1 5.509163t*0 1.298940t*1 2.1465871-1 1.664068t*0 63 JA 0.0 7.43600ct 2~~
4. 90799?t 4 0,01824*t 1

2. 61299M
~~1 4.157639t *0 3.225157E 1 SEAMG JB 120.0 7.436 mci d ?.9ml?t 4 '9.018243t*1 2.61299Ct+1 1.420638t*1 3.0434081-1 M~~
~~JA 0.0~~
~~43609C( 4 L 90 587t 2~~
~~9. 98826;t~~
1 2,612MCE

1 1.420 384*1 3.0434081 1 st 4MG.
~~JS 100.0 7.4360 N 4 2.9079521 2 -9.988269t*1 4.61299Ct~~
1 1.1M331t*2 2.861659t 1 65 44 0.0 7.436@0E 2 2.617t321 1 1.059312t*2 2.612 N04+1 1.166331t*2 2.861659t*1 6tAMG 48 100.0 T.43609M 4 2.617&I2! 1 1.059312t*2 4.612990t*1 2.5395031 0 5.806720E 1 66 JA 0.0 7.43409Cid 2.4171L12t 1 - 8.84 7069t

1 2.612990t*1 2.539503t*0 5.806T20t*1 StAMG J8 100.0 7.4360901 2 4.6178321 1 8.547c691 1 2.612990t*1 1.C20690t*2 8.751781t 1 67 JA 0.0 1.7635t2t'?
~~1.8.0 % f 1 2.92967M*0 2.63 450t 1 S.907958t*1 2.53924M*0 8tAMG JS 100.0 l.7635 ?:(~~
3.54ht 1 4.92967M *0 4.0,44!LE *1 8.468507t*1 1.96111M*0 58 JA 0.0 5.763510( 1 3.840864t 1 2.621031t+1 2.634450t*1 8.468507E*1 1.96311M *0 stAMC J8 100.0 5.76351M 1 3.84G86*t 1 2.621031t=1 2.63445 M

1 4.53444 1 1.386957t*0 69 4A 3.0 5.7635tX ?
~~1.84 N t 1~~
~~4. 94 9095 t~~
~~1 2.6 W 50t*1 4.53696M*1 1.384987t*0 SEAmG A~~
~~JS 100.0 5.76351C1 1 5.bO86*t 1~~
~~,9+9095t*1 4.6 W 5M*1 2.L M f+1 8.108571t 1 70 JA 0.0 1,763110t 1 3.840%t 1 6.159552t*1 2.634450t*1~~
~~2. M t*1 8.108571t 1 &EAMG Je 100.0 5.76351C1 1 3.840864t 1 6.59552t*1 2.63445Ct+1 8,517389t +1 4.9091321 1 71 JA 0.0 2.431360t*2 4.454554t 1 4.617797t = 1 0.~~
D. 2.392184t*15 BEAMG Ja i00.0 2.431340E 4 4.45455 4 1 2.617797f 1 0, 1.3088991 1 2.2272T7E 1 72 44 0.0 t 90331M *2 . 414554r-1 4.6177971-1 1.78113M 15 1,308899t 1 2.2272TTE 1 EtAMG p Ja 100.0 1.90331C1 4 i 4541141 1 2.61T797t 1 1.781130t 15 9.3 m 671 1 1.596067t*0 t l4 73 JA 0.0 7.227890t*1 1.3 m 34t 1 6.50874M 1 1.15985Ct+0 1.14529Ct*1 1.942758t+1 SEAMG ,;t JS 100.0 7.227890t*1 1.3m34 1 6.50874M 1 1.159850t*0 1.259193t*1 1.966864tet 7 14 JA 0.0 1.T64230t*1 1.3 m 344 1 6.5C874M 1 1.15985W 0 1.2591934 1 1.966864t*1 stAMG s i JS 100.0 1.7M 23M
~~1 1.3 m 344 1 6.50874M 1 1.159850(*0 1.335151t*1 1.982940t*1~~
~~1. 3 m 341 1~~
. 6998511 1 1.9829 M *1 1.335151t*1 1.159853t+0 stAMG 6.50875ct-6.50875 C5. '1 75 JA 0.0 1.3 m 344 1 4.6998518 1 1.98294M*1 1.389998t 1 9.990953t*1 JB 100.0 1 - T6 Ja 0.0 6.50875M 1 1.3 m 34f 1 4.540627t*1 1.98294CE*1 1.389998t*1 9.990953t 1 SEAMG Je 100.0 6.508750t 1 1.3 m 34t 1 4.540627t+1 1.98294CE*1 3.660311t+1 9.302186t 1 D T7 JA 0.0 6.50875M.1 1.1308371 1 5.53033M
~~1 1.98294Ct 1 3.660311t 1 9.302186t 1 stAMG JS 100.0 6.508MCt 1 1.13:5871 1 5.53033M*1 t.982940t*1 4.793593t +1 7.9824411 1 S~~
TS Ja 0.0 6.50875CE 1 1.13*8871 1 3.331870t 1 1.98294ct.1 2.793593t*1 7.982441t 1 SEAMG 48 1Go.0 6.50875M 1 1.13G887t 1 3.33187CE*1 1.982940t*1 8.344489t+1 6.09838M 1 '9 JA 0.0 6.508750t 1 1.1308871 1 4.066599t*1 1,982940t*1 8.344449t+1 6.09838M 1 SEAMG J5 100.0 6.5C8 MCt 1 1.130887t 1 2.066599t 1 1.98294CE*1 5.9327684 1 4.T78638t 1 "1 f 80 JA 0.0 1.130890t 1 4.5C874M 1 3.877812t
~~1 5.932770f*1 1.982940t*1 -4.778638t*1 SLAMG B~~
JS 100.0 1.130490E 1 6.5C874M 1 3.8778328 1 5.932T70t+1 2.542490(+1 2.817069E 1 81 JA 0.0 1.130490t 1 6.5C874M 1 8.888291t*1 5.932770t+1 2.54249ct.) 2.817069t*1 SEAMG =0 Ja 100.0 1.130490E 1 6.50874M 1 8.888291E*1 5.932T70t*1 1.290424t*2 1.040627t*0 ^ 6'". 82 JA 0.0 6.82171CE-15 2.42141CE 1 1.269527t+2 5.932 TTCt +1 1.290624t+2 1.040627t+0 stAMG JB 100.0 6.82171CE 15 *2.12141M 1 1.269527t
~~2 5.932770t*1 2.851580t*) -8.329932t 1 83 Ja 0.0~~
-6.8217101-15 2.62161CE 1 8.7720511 1 5.932770t*1 2.85tS80t*1 8.3299521 1 ftAMG J8 100.0 6.82111Ct 15 4.62ta1M 1 9.772051t *1 5.932T70t.) 6.288896t*1 5.598235t 1 hl 84 JA 0.0 8.307860t 2 1.17535Ct 1 3.0779064 1 2.98804Ct+1 1.071179t+1 3.446331t 1 stAMG JS 100.0 8.302860t 2 1.1555Ct 1 3.077906t*1 2.988*40t*1 4.032144t+1 -1.494918t 1 14 _ 85 JA 0.0 8.3028601 2 1.17515CE 1 4.9142 Tit *0 2.98804M *1 4.032144t 1 1.4949184 1 stAMG. h'M ~ JS 100.0 8.302S604 4 1.15 55CE 1 -4.9142?1t*0 2.98804CE*1 4.854302t+1 4.71T7721 2 64 JA 0.0 6.3?25605 4 1.13C544 3 1.136343t *2 2.98804M
~~1 1.819441t*1 2.381550t*3 SLAMG~~
~~+ JS 100.0 8.302360t 2 1.33014 4 3 1.1363431 2 2.98804Ct+1 1.428254t +2 4.266931t 3 lt 87 JA 0.0 8.302860E 2 1.33C5444 3 1.382109t~~
~~2 2.988040t*1 1.428254t *2 4.266931t 3 stAMG 1p JO 100.0 8.30286CE 2 1.33054 4 3 1.382109t*2 4.98804CE*1 3.846945t* 2 6.5953844 3 88 JA 0.0 0.~~
~~5.03939M 2 2.2M666t*2 7.2338808 12 5.240121t+2 3.T79547t 2 BEAMG ON 48 100.0 0. 5.0.1939M 4 2.294666t*2 7.233880E 12 6.864745t+2 2.116546t-3 89 JA 0.0 5.55112M 15 1.039396t 2 2.672868t~~
~~2 3.538500t 12 6.864745E+2 2.116544t 3 BEAMG.'~~
t JS 100.0 5.551120E 15 5.039396t 2 2.6T2868t*2 3.538500t 12 6.977C05t+2 0. 5'- 90 JA 0.0 0. D. 1.468943t+2 5.934920E 14 -6.9TT005t*2 0. BEAMG1 ~$ Ja 100.0 C. D. 1.468943t*2 5.936920t 14 3.428038t+2 0. 91 JA 0.0 0. O. 1.090633t*2 6.294960t 14 3.4280384*2 0. SEAMG [ s m&, ..x y. - +n r e wm 7gy m.
-4 i d \\ ATTACHMENT D M hp SHEET % or,,,1 (, Otto 00mva0 $ttitu 4316 6 8 7 D (- 7'/"O - 3 TV, Thu Apr 18 12:49:06 1996 A' 4 81AhmAP vertf ort 4.41 Report t tLtaent [3 h *y M leadet t p Forset. t 51AA0tht ter/ teem tienent k.. N fitte t PROP 3 16N16" v;SU ~~ thstpaat let 5
~~OLAD LOAD (DL) 8 tam (Ltuttl LOADS~~
[b aulat satae latAA toasicM sinolmG SthotnG e vi v3 at m2 m3 6 JS 100.0 0. O. 1.09063312 6.294960t 14 7.461723t*1 0. [ StAm N' 92 JA 0.0 6. C. 4.56965M*1 *T.327470E 15 T.461723D1 0, et A#eG. e-l' JS 100.0 0. O. 4.56965M
~~1 T.327470E 15 2.279671t*0 0.~~
~~93 JA 0.0 0, 0. 4.206035t*0 8.570920t*14 2.279671t *0 0. StAAec JB 100.0 C. O.~~
~~206035t *0 8,570920t.14 1.64002tt 12 0.~~
94 JA 0.0 1.61016Ct t -.13431st 2 2.0 0862 D I 1.294690tel 3.117368D 1 2.151903t 1 etAnc Ja 100.0 -1,61016ct 1 6.3343131 2 2.040862DI F.294690t*1 T.210746D1 1.2&2565E 1 95 JA 0.0 1.6101608 1 4.134318t 2 3.572086t*1 7.294690t*1 F.210746t*1 1.252565t 1 stamG JS 100.0 1.610160t 1 4.334318t 2 -3.572086D 1 7.2946900 1 4.617819D 1 4.132267D2 96 JA 0.0 S.302 %0t+2 1.446060D 1 5.516570D 1 5.119060D1 5.197097t*1 4.1322671 2 stAseG J5 100.0 S.302S60t 2 1.4460605 1 5.$ toltet.1 5.119060D 1 2.438813t*l 3.095033D2 91 JA 0.0 8.302560t 2 6.90634?t 2 1.76T296D t 5.119060E*1 6.430296D 1 3.602644t 2 ELAmG Ja 100.0 8.302460D2 4.906342t 2 1.767296t
~~1 5.119060t*1 5.L417t3D1 1.236455t 2 98 JA 0.0 9.33777;t 2 2,411574t 2 4.7M64M 1 7.7510J0D1 5.029484t*0 5.236455t 2 stA#eG~~
( C JS 100.0 9.337770t 2 2.411574t 2 .75589pt 7.751030D1 a.988716D O 3.9668501 3 49 JA C.0 9.337770t 2 2,411574I 2 5.661363D I T.51030t*1 5.958716D O 3.956850D 3 stamG i JB 100.0 9.3377701 2 2.4115 7.D 2 5.e41363t*1 7.751030 D 1 1.19559M*2 4.4390860 2 h 100 JA 0.0 8.302540D 2 1.1555CD 1 l.06604 7t *1 2.988J40t*1 4.5%302D1 4.11TTT21 2 StAMG JS 100.0 8.302560D 2 1.1M550D 1 1.066047D 1 2.933040D 1 4.498242t*1 S.644109D 2 e 101 JA 0.0 8.302860D 2 1.15550D1 1.191366D 2 2.938040t*1 4.498.242t e t 8.M 4109D 2 atAmG (/ - 45 100.0 5.302860t 2 1.1 55500 1 1.191366 D 2 2.98sc4U+1 5 ?%37D0 1.255869D 1 s 71*0 1.255569D 1 atAMG 102 JA 0.0 S.30256M.T 1.155508 1 1.25240M
~~2 2.980040D 1 J6 100.0 8.30286ct 2 f.15550t t 1.222409t*2 2.968040D1 4.~~
53D 1 2.137532t 1 113 JA 0.0 0.30286ct 2 t *305440 3 6.48tMIDI 2.983040D 1 6.w sDI 1.313642O 3 8tAmG 48 100,0 8.302860t.2 1.330%403 6.44t?9tt*1 2.948040D 1 1.819441D1 2.381550D 3 4 114 JA 0.0 9.302S60t 2 1.446060t t 6.to2995D I 5.119060D 1 2.438813D 1 3.096033t 2 atAmG ~ Ja 100.0 8.302860t.2 1,446060t 1 - 6.162995D s 5.119060D 1 3.865351t*0 7.913413t 2 O 115 JA 0.0 8.302860D 2 1.44060t i 1.7080618 2 5.119060D 1 3.865351t*0 7.913413D 2 BussG Ja 100.0 8.302860D 2 1.4460600 1 1.703061D2 5.119060D1 5.318337tet 1.274325D 1 116 JA 0.0 8.302860t 2 e.446060D 1 1.792talt*2 5.119060D1 5.318387t*1 1.274325D 1 4tAseG '~ L 48 100.0 8.302860D 2 1.4460CD t 1.M21818 2 5.119060D 1 1.87595D2 2.35487DD I 4 12T JA 0.0 8.302860D 2 4.906342D 2 l.8a7723! 1 5.119060D1 1,078609D 2 7.711274t 4 etAmG J5 100.0 t.30286M 2 4.906342t 2 5.50T72501 5.119060 D 1 6.430298D1 3.602644t 2 12$ J4 0.0 5.132N001 -3,8909 GD I 4.382396D1 1.0514G0D1 S.449105D1 4.935000t.) stAMG JS 100.0 5.832090D 1 3,890949D1 4.392396DI l.05t490D 1 8.84T373t*0 3.330267t*1 h 129 JA 0.0 5.83209M 1 3.890949D1 1.405695D1 1.0514900 1 B.84T373D 0 3.33026TE 1 stAMG JS 100.0 5.&320900 1 3.890949D 1 !.405695t*1 +1.051490D1 *2.102364D 1 1.159853D 0 4 [W 4,7 18tle : Peop 3 16*n16* Q, ? ,0utput Set 1 OtAD LOAD 10L3 set la itenue F
~~h. -',~~
A*f L " Set MAX /mlu $6ssary table mintam 1 80 % 11309 !V Nt ^ leen EM A Aalst f orce mealam 1 71 243.136 ulniam 1 80 0.65087 M 8een truf A sheer 2 f acce men tam 1 71 0.44546 Minimm 1 89 267.281 ( m a teen EM A theer3 Force 7 u @?if mealam 1 116 179.218 V ninfase 1 75 19.8294 R, An. . Seem (M A fortpe maaina 1 98 TT.1103
~~ZJ minimm I~~
~~90 691.701 A 1-Y - M W' M $ F M' ? Seen EM A momemt mea f am 1 65 116.433 RW Minima 1 67 -2.53925 W~~
F
~~seem EM A moment 3 mes tam 1~~
74 '9.6686 N Minleum 1 71 243.136 g6 4 %9AM i teen EM S AAlet f orce maalam 1 60 0.11309 JM4 ulnimm 1 71 0.44546 W ' " " g-bJ: o. Some EM e thear2 f orce 5 ~" maalam 1 80 0.65087 g MIntius t 116 179.218 .J ! Sese trut 8 Sheer) Force maalam 1 89 267.28T fQ Nintam 1 98 TT.5 t03 4 . Seas truf a fortwo menima 1 N 19.8294 A W,sp minimm 1 116 18T.596 I[ [, *, E Seem trui 5 maamt2 7 % %. u t dv mhl hgh 3 sv J N}} + [ "[& 'jy m u? %_Q& a Q,Ly %_y ,,h0h ~lhk
ATTACHMENEi@ gP SHEET 4 OF N
~~tc0 00mvAc sv$1t= 4316 6 s 1 DC.6 D3 stA = e m on 4.&i~~
~~%, i4 12:49:30 i996 geport 3 ((ement model 1-Format $1Aactat ter/Sean Eleavet s 3 i< _i _ f fille s P90P 3 16 116* V' ~ htsut let 1~~
~~CLA0 LOAD (St1~~
~~$s, resisue 1 39 697.701 h* team ind 4 acaent3 m1M aus 1 74 19.8294 " ~ me n t eum 1 67 1.96312 o" title : Pe0P 3 16*t16+ b Dutsut let 2~~
~~048 etAu (Ltataf L0A0$~~
~~{p{- f AstAt intAt thtaa 104$10m etheleG StielmG~~
~~n HAM P~~
~~v2 v3 at m2 m3 61 JA 0.0 3.0304308 4 1.250959(4 6.60402M~~
~~0 5.085057t*0 1.34978M*0 6.027569t.1 stAmc Ja 100.0 3.030433*2 1.2509501 4 6.604920E.0 5.085040t+0 1.6713815 1 1.115318t+2 0~~
~~62 J4 0.0 4.7060 0t*2 4.6762tSt*1 2.452649t*0 6.g588M*0 1.19561&t 1 1.030564t 2 StAJeg Ja 100.0 4.T06*4M*2 4.676215t*1 2.452291 0 6.g5 EsM + 0 1.072389t*1 1.481048t+2 63 JA 3.0 1.60736M~~
2 3.201578td 2.21034M

1
~~1. 6713 7M~~
1 1.085061t*0 3.115338( 4 stAmG g4 Je 100,0 1.407360f 4 3.201575t

2 2.210366t*1 1.67135M +1 1.5022334 1 2.280372td g
~~JA 0.0 1.42818M*2 3.222969(4 2.438754t*1 1.67137M~~
~~1 1.502233t*1 2.280372t *2 ltAnc JS 100.0 1.&231$0t*2 3.222969t*2 2.438754t*1 1.67138M *1 2.97716M *1 2.968775t *2 65 JA 0.0~~
1. 7064 Mid 4,183360td 2.85532M*1 1.67137H +1 2.97716M+ 1 2.968775t*2 atAMG Ja 100.0 1.7064001 4 4.18336M 4 2.855320t+1

1. 67138M
~~1 4.532008t*0 3.10713M +2 So JA 3.0~~
~~1. 7565 0M~~
2 4.15 2111 t

2 2.486303t*1 1.671375t+1 4.53200SE*0 3.10111M 4 StAMG Ja 100.0 1.7565Mf +2 4.15211114 2.484303t*1 1.6713SM*1 3.102537t*1 7.330!67t 4 67 JA 0.2 2.2658Nt*2 9.3779e31 1 1.3392561+1 2.626131t+1 2.6549791 1 7.535945t+2 stAnc '
Ja 100.0 2.265890t*2 9.3779434 1 1.389256t+1 2.626130t+1 6.+1500tt+1 6.338523t*2 P 68 JA 0.0 2.33849Cl*2 9.4508331 1 1.509921t+1 2.626131t*1 4..A 001t*1 6.338523t+2 stAac IJ Ja 100.0 2.3354GCt*2 9.6508338 1 1.509921t*1 2.626130t*1 5.746889E*1 5.19265M*2 69 JA 0.0 2.41190M 4 9.4484448*1 1.307125t*1 2.626131t*1 5.7&&83M
~~1 5.19265M*2 stAmc f^~~
Ja 100.0 2.41190Cf 4 9.448444t*1 1.5071M t*1 2.626130t+1 7.70769M +1 4.142927t + 2 70 JA 0.0 2 A494201 2 9.405681t*1 2.120149t*1 2.626131t + 1 7.707695t+1 4.142927t+2 atAnc JS 100.0 2.46M23 4 9.401681t*1 2.120349t+1 2,26130t+1 9.044899t*1 3.618a5M 4 i 71 JA 4.0 1.2350708 4 2.850971t*2 5.64230M +1 5.1243084 13 5.6470ME 13 3.061645t*12 stAMG p. d JB 100.0 1.23507M 4
~~2. 850971 E~~
~~2 5.8423091 1 1.12431M.13 2.921155t*1 1.425485E 4~~
~~'4 72 JA 0.0 1.1801108 4 2.61910M +2 5.523230t 1 1.080232t*12 2.921155t+1 1.425485t4 stAmG 48 100.0 1.1803108 4 2.81910M 4 5.523230t*1 1.080230t~~
~~12 1.991884t+2 f.011677E*3~~
'3 JA 0.0 9.001790t+1 6.492465t+1 8.195870E+1 2.385819t*2 1.564333t+2 2.8814591 4 stAmG k' JS 100.0 9.001790t*1 6.492465t+1 a.195870t*1 2.355820td 1.962119t*1 1.82813M*2 ^ T& JA 0.0 8.840160t*) 3.4094T3t*1 9.030214t+1 2.335819t*2 7.982119t+1 1.8281164+2 SumG E Ja 100.0 8.849160t*1 S. 4094 T3 t e l 9.03021&t t 2.385820t 4 1.277 tom 4 9.503740t*1 75 JA 0.0 9.3 % CE*1 9.117254t+1 8.840100t*1 9.503741t+1 1.277166( 4 2.38561M
~~2 StAMG JB 100.0 9.3 % 0t+1 9.117254t*1 6.84010M +1 9.50374M +1 2.963536t +1 1.96179M4 M~~
~~76 JA 0.0 1.022980t*2 1.052T71t *2 8.919983t*1 9.503741t*1 2.96353M +1 1.961796E 4 stues M Ja 100.0 1.022980t 4 1.052T7184 8.919983t~~
~~1 9.503740t+1 2.992M5t+1 1.9031421 4 l~~~
17 JA 0.0 1.22243Ct d 9.066749t*1 1.836709t+1 9.503741t + l 2.9922558 1 1.903142t+2 MAms 7 Ja 100.0 1.222430t 4 9.066740t+1 1.836709t*1 9.5037&M +1 1.585913t+1 2.053438t*2 78 44 0.0 1.277400t+2 9.524842t*1 1.544490t+1 9.503741t+1 1.585913E+1 2.053438( 4 stAms ,7 ~ 48 100.0 1.277400t
~~2 9.5248421 1 1.544490(*)~~
~~9.503740t + 1 2.407081t+1 3.038&O9t + 2 @^ 79 JA 0.0 1.41485M*2~~
~~9. 99537M *1 1.31605M *)~~
~~9.503741t+1 2.407081t+1 3.038409t4 StAmt Ja 100.0 1.484850t*2 9.99537M*1 1.316058t+1 9.503740t + 1 2.97431M + 1 3.98376M~~
2 30 JA 0.0 9.998640t*1 1.661554t d 1.498362E+1 2.974317t + 1 9.503740t*1 3.95376M

2 SEAmG t
~~Ja 100.0 9.99864M + 1 1.4615 Sat~~
2 1.496542t+1 2.974324 1 8.25318tt*1 3.513827t *2 41 JA 0.0 1.000310( 4 1.532215t 4 2.4140921 1 2.974317t.1 8.255111t 1 3.513827t*2 SEAMG Ja 100.0 1.00031M

2 1.532215t*2 2.616092t*1 2.97432M*1 7.713160t+1 3.890 4 8t+2 t.
~~82 JA 0.0 5.319080(4 1.329731t *2 3.&O1641t+1 2.974317t*1 7.713160t+1 3.890648t+2 StAmc @p,~~
M Ja 100.0 5.31908M*2 1.329731t 2 3 &01641t*1 2.974320t

1 5.910100t+1 3.009894t*2 P
~~83 JA 0.0~~
~~5. 311590t~~
2 1.306864t*2 2.598567t*1 2.974317t

1 5.910100t 1 3.039994t+2 atAMG; JS 100.0 5.311590t*2 1.306864t+2 2.598567t+1 2.974320t*1 4.5491223+1 2.614038t+2 i
84 JA 0.0 3.191300t*2 4.342993t+1 1.180071t + 1 1.482878t+1 2.817654E 1 1.3091'4b 2 BEAmG JS 100.0 3.191300( 4 4.342993t*1 1.180071t*1 1.482f +M+ 1 1.6096530 1 6.047247t+1 ( '., 85 JA 0.0 3.173020E *2 4.444817t*1 9.3914048 0 1.48257tt +1 1.609653t 1 6.0&T247t + 1 StamG "A" Ja 100.0 3.173520b2 4.4448171 1 9.3914044 0 1.4825300 1 1.215294t*1 2.1M418t+1 86 JA 0.0 1.655750D 2 2.12371861 6.190431b 1 1.&82878bt - 4.368994t+0' 4.266301b 0 stAMG ,w G: Ja 100.0 1.655750t4 2.123718D1 6.190431t+1 1.4828800 1 8.60080161 3.102499t+1 ~ %A 87 JA 0.0 1,6159905 4 2.086502t+1 6.&23320t+1 1.682878 6 1' 8.600801t+t 3.102499D 1 atAnc. BN ' JS 100.0 1.615990D 2 2.086502E 1 6.423320D 1 1.482850b 1 1.979811D2 6.M8110t + 1
~~1..~~
~~88 J4 0.0 5.02092001 7.397476t *1 8.640717t+1 2.905591 6 12 2.752236t+2 1.267357t+2 timeGb 's ^ Je 100.0 5.020920tel 1.397476t*1 8.640717t+1 2.905590 0 12 3.352293b2 1.421062t+2 l; Ah:k, O p~~
~~sfh, 4e,.,a ~~~
+ l WOkh
ATTACHMENY Y, n. $h
~~SHEET T op 41 I~~
~~OECO CCnvAt 191114 4316*6 & 7 Oc.-57D thy Apr 18 12t&9114 1996 St&BRAP Vertien 4.41 Report : Element 6 y 4 M-Model 3 M ,formet STAA0fut ter/ team itement ~$' d G, 4$c/ N /O." .18tte~~
P90P 3 16*E16*
~~i MM L tutsut Set 2~~
~~Ost StAm 1tIat#I e0 ADS i~~
}h*. ', ; r * + AntAL Sut at thtAt foestou t%lhG Stu0 gag P v2 v3 mi m2 st3 h ^g G 7% 89 JA 0.0 4.3448%t*1 7.609602t*1 9.242253t+1 8.761757t*13 3.352293t+2 1.421M2t+2 BEAMG t&; - StAM JS 100.0 4.34480ct *1 7.609602t*1 9.242253t+1 8.76176M *13 3.389864t+2 1.434942t+2 90 JA 0.0 2.698000t+1 2,711921t*1 6.518958t+1 3.06590t*14 3.389884t+2 1.436942t*2 atAMC JS 100.0 2.698000E+1 2.71592tt*t 6.518958t +1 3.06M904 16 1.81930M
2 7.897279t +1 91 JA 0.0 2.010180t*1 2.'95099 1 1.576952t +1 4.05CSul 14 1.819306t+2 7.8972Mt +1 MAMG JS 100.0 2.010150tal 2.375094*1 5.576952t +1 4.0508?ct 14 4.429689t*1 2.026945t*1 92 JA 0.0 8.433610t

0 1.237415t*1 2.7&2912t+1 5.1684TTL 14 4.489689t+1 2.026945t*1 MAMG
~ JS 100.0 8.438610t*0 1.23?&15t+1 2.742982t *1 5,188480t 14 1.476195t*0 6.823556t 1 y 93 JA 0.0 7.747810t 1 1.258958t+0 2.T23607t+0 8.032943t*14 1.476195t+0 6.82355M 1 taAMG I JS 100.0 7,76787 ( 1 1.258958t+0 2.723607t*O 8,0329&M 14 1.837587?I2 1.2486064 12 i 94 JA 0.0 2.273960t
2 S.0147371+1 1.13 t elm + 1 2.277363t +1 3.027864t+1 1.74681M

2 StAMG h
Je 100.0 2.273960t*2 $.014T371* 1.13161M +1 2.2773608 1 2.168977t+1 5.359649t+1 95 JA 0.0 2.221520t*2 7.502123 fat t.349790D 1 2.277363t*1 2.1689TTt*1 5.359649t+1 SOMG =5 JS 100.0 2.22152;t*2 7.502123E.1 1.349790 0 1 2.277360t +1
~~1. 79600M~~
1 1.47557M*2 96 JA 0.0 2.01685Cl*2 1.1334&aD 2 f.69146M *1 2.6059448 1 1.2T3195D 1 1.45570D 2 5tAMG JS 100.0 2.016850D 2 '.13348-D 2 f.691460( *1 2.60595CD 1 9.689453t+0 9.M 9893D 1 Of JA 0.0 9.122&T0D1 6.2 T7952D 1 t.354512t+1 2.6059648 1 3.36668CD 1 4.201351D1 stAMG Je 100.0 9.122470t*1 6.277952D 1 1.354512t*1 2.605950D1 3.695907t+1 6.1934T3D1 98 JA 0.0 1.101 AICD 2 2.836919D 1 1.289677t + 1 4.449791t *1 8.062724t+0 6.193473D1 MAMG h
48 +00.0 1.10161Cl*2 2.136919D1 1.2896TT!*1 4.449790D 1 3.385105t*1 3.004393D1 99 JA 0.0 1.177550D 2 3.663949D 1 1.82339M+1 4.449791D1 3.385105t*1 3.004393t+1 MAMG JS 100.0 1.177150D2 1.64394Gt*1 1.823396D 1 4.449790 0 1 ' 489949D 1 7.651791D1 i 100 JA 0.0 3.159610D 2 .5056221 1 3.69299CD 0 l a328781*1 1.215294D 1 2.1M61SD 1 StANG JB 100.0 3.15961;D2 4.505622D 1 9.69299CD0 1.482S80D 1 1.249722D I 3.369874t+1 0-101 JA 0.0 3.054760D2 5.4C2987D I 3.02955M *1 1.482578D 1 1.249722t*1 3.369874t+1 stAMG , r Je 100.0 3.054760 0 2 5.402957D1 3.02955H+1 1.482&s0D1 9.430302t+0 4,693546D1 'l IC2 JA 0.0 3.04631CD2 5.491312D 1 3.221936D 1 1.432378D1 9.439302D0 4.69354M+1 SOMG 'j- JS 100.0 3.04431CD 2 5.498312D1 3.22193M + t t.482330D 1 2.734230t*1 8.419445 D 1 113 JA 0.0 1.729sacD 2 2.475047D I 5.828649D1 1.&S2878D 1 4.495102D 1 1.704767t+1 SOMG d-Jt 100.0 1.72964CD2 2.4750471*1 5.828649t+1 1.&82180D1 4.3M994t*0 4.266301t+0 116 JA 0.0 2.00240002 1.137397t
~~2 f.816841tet~~
~~2. 605964 +1 9.689453t*0 9.M9893t+1 SOMG j~~
~~JS 140.0 2.002400D 2 1.13739 7t~~
2 f.816841D1 2.605950D I 1.12591M

1 6.M 2515t + 1 7
115 JA 0.0 1.755650D2 1.21441tD 2 4,260479D1 2.605644t*1 1.125916D 1 6.752%15D1 SEAMG T Ja 100.0 1.755650t*2 1.214411 0 2 4.240479D 1 2.60595M *1 1.957237t+1 5.151390D1 116 JA 0.0 1.T3646002 1.220893D 2 4.434335U1 2.605944D1 1.957237t+1 5.151390D1 MAMG D JB 100.0 1.736460D 2 1.220893D2 4.434335D1 2.60595CD) 5.054826t+1 1.070790D 2 N? 127 JA 0.0 8.20347M+1 6.502392t*1 1.694093 D 1 2.605944t*1 3.291898t+1 1.919258D 1 SUMG g 48 100.0 8.20347CD 1 s.502892D 1 1.394093t+1 2.605950D1 3.366680D 1 4.20135 tD 1 S 128 JA- 0.0 2.M531CD2 9.339417t*1 1.950506D 2 8 &S8141D1 9.191974t+1 3.62&898D 2 SEANG y "J # J8 14J.0 2.8453tCD2 9.33941TD1 t.950506D 2 8,88814M *1 3.242550D 2 2.310967D2 b 129 JA 0.0 3.040780D 2 1.043614D2 1.929514(+2 8.888141D1 3.242550D 2 2.310967P 2 stAMG mX U JS 100.0 3.040780D2
~~1. 043614 t~~
2 1.929514*2 8.83814C01 7.342149D 2 2.38581M* 2 Title : Peor 3 16's16*
~~_O Output let 2 DM let 10 value~~
~~9 hh~~
. Set MAX / Min Summary table Ni. ' Seem tid A Aalet f orce minisus 2 93 0.77679 P maa tous 2 82 531.908 h? i O Y, Seem Erd A Sheer 2 Force Minious 2 93 1.25896 mea tsue 2 65 418.336 v. D ys Seem trd A theer) Force m woue 2 62 2.45269 4 maniaun 2 128 195.051 + sg C; minisue 2 90 3.06759t*1&; mesisue 2 73 ? 238.582 b
~~4 ;;~~
"I' team trd A fortpe Seem trd A sument2 minisue 2 T1 5.64707t 13 . j meslaus 2 90 338.988 .I p','* minteus 2 71 3.06165D12 M .~ Ny - seem E s1 A moment 3 menisus 2 67 753.595 4 J f F -- ninlaus 2 93 0.77679 l' . k%i < team (M S Arlen Force 0"N paaleum 2 62 531.908 7 ulnimm 2 93 1.25496 mealsus 2 65 418.336 jQ Sean Erd a sheer 2 Force - [p g 4 %*6x 9 1 %k 74 Q$9,Jf ynsv _ I
ggp N ATTACHMENT V " r 9ms SH W 0 -OF N ~ ttC0 C: vat 5151tn 4316 6 61 DC.-3 M thw Apr 18 12:49:18 1994 h $1ARAM Vet alon 4.41 aecort a fleasnt a-( Model t f ormat t $fM0 tut $sr/ teem Element g_ v_ _, [* Iltle P90P 3 16 116" tuttnat Set 2
~~088 minious 2~~
62 2.45269 -O tems tras S Shear 3 f orce e mesisue 2 128 195.051 C minisus 2 90 3.06T59t*14 Y ~ . Seen Ersi e fortpe maa taue 2 73 238.582 Q'q. . team End 8 Momenti minisue 2 93 1.83759 0 12 W 'V nos tous 2 129 T34.215
~~i minteue 2~~
~~93 1.24461D 12 .g.Q WM 4 Seen ind 8 mmment3 c maa true T2 1011.68 title : PacP 3 16*116 {p_ Outpat let &~~
~~551 8taa t41 min 1 L0a0$~~
A lA4 sutAt IntAA 10A 510ei stM0thG StuoluG P V2 V3 M7 M2 M3 kI FI' 61 JA 0.0 4.784180D 2 1.92tt9sD2 0.595883t + 0 8.15196800 1.117401t+1 9.534323t *1 htAMG fb atAM Je 100.0 4.7&4183 2 1.921896D2 8.595883D 0 0.151970D 0 2.5971MD1 4.69241M
~~2 62 JA- 0.0 7.12 7D M *2~~
~~?.7N8101 3.560317D0 1.011323t*1 1.946162D 1 1.656822t+2 StAMG at 100.0 7.12 TMCD 2 7.79ta tt*1 3.560317t+0 1.011320D 1 1.836786t~~
1 2.55026tt+2 63 JA 0.0 2.133570D2 5.063$ 1D I 2.03t52$t+1 2.597159D 1 8.151974t+0 4.69241M*2 ttAMG Nf" JS 100.0 2.13357M

2 5.06354802 2.031525 D 1 2.597160D 1 1.659916D I 3.49080M.2 J3 64 JA 0.0 2.168760t*2 5.09560?p 2 2.222553t+1 2.597159t*1 1.65991M

1 3.490806D2 atAMG d-Je 100.0 2.168760D2 5.0WO ?t

2 2.222553 9 1 2.591160D 1 2.944760D 1 4.760603D 2 65 JA 0.0 2.640060t*2 6.387T44D 2 3.056911tel 2.597159t+1 2.944760D 1 4.760603t+2 StheG JS 100.0 2.640060D 2 6.38T7+4D 2 3.056911Dt 2.591160D1 7.270539t*0 4.644605D 2 66 JA 0.0 2.724780D 2 6.33456302 2.7935032+t 2.591159D1 7.270539t+0 4.644605t+2 stAMG r
~~Ja 100.0 2.7247801 2 6.334543D2~~
~~2. M3503 D t 2.597160D1 3.745391t+1 1.109039D 3 W-67 JA A.0 3.5C97002 1.49+ 7s5D 2 2.221&37t+1 4.290548 1 3.177159D 1 1.1315371 3 stAMG rife -~~
Je 100.0 3.567770D 2 1.494765D2 2.221837t+1 4.290760t+1 6.062682D 1 9.505003t+2 68 JA 0.0 3.69049002 -1.491495t+2-2.264259t+1 - 4.290754t+1 6.0626821*l 9.505003t*2 atAMC O-J8 100.0 3.69049CD2 1.491495D 2 2.264259t+1 '4.290760t+1 9.10T238t+1 7.832209D 2 - t" ?WJ 7 T' 69 JA 0.0 3.61419CO2 1.468273D2 2.413789DI 4.290754t*1 9.107238D 1 7.832209t*2 SEAJeG ' Je 100.0 3.61414Ct*2 1.44927tD 2 2.413789 D 1 4.290760D 1 1.232226D 2 6.3M52902 70 JA 0.0 3.910960D 2 1.443334t* 2 2.604935 t + 1 4.290754D1 1.232226D 2 6.3795290 2 StAMG V Ja 100.0 3.9109600 2 1.441334D 2 1.604935t*1 4.290760DI 1.423407D2 5.692247t+2 71 JA 0.0 1.13998;D 2 4.576129D 2 1,018979D 2 8.2749071 13 9.416251t*13 4.8008190 12 SEAMG JS 100.0 1.819980E
2 4.576121D2 1.011979D 2 8.274910D 13 5.059897t+1 2.288064b 2 72 JA 0.0 1.81201CD 2 4.5110MD2 9.52895M

1 1.624978D12 5.059897t+1 2.288064E+2 StAMG JB 100.0 1.81201CD2 4.52300*D 2 9.5239166 1 1.624980D 12 3.43903tD2 1.623248D3 i
~~T3 JA 0.0 1.403750D2 1.059473D2 't.302581D2 3.84332 M~~
2 2.657849D 2 4.680513t+2 SEAMG Je 100.0 1.403750 0 2 1.C89* T3D 2 1.30258tD 2 3.843330D 2 1.355844t+2 2.944992t+2 74 JA 0.0 1.39698CD2 1.391475D2 1.487306D2 3.843326t+2 1.355844 D 2 2.944992E+2 SEAMG Jt 100.0 1.196950t*2 1.391475 t + 2 1.48730M + 2 3.84333cD2 2.012528D 2 1.537418D 2 N[ '

N:
75 JA 0.0 1.5554500 2 1.503058t + 2 1.39666M+2 1.5374189 2 2.012528D 2 3.843321t+2 st#e4 Ja 100.0 1.555450D 2 1.50305402 1.396666D 2 1.537410D2 4.8235i9t+1 3.10752M*2 76 JA 0.0 1.740850t*2 t.724476D2 1.402118t*2 1.537418D 2 4.823529t+1 - 3.10752M*2 StAMG n' ,d/ JS 100.0 1.740850t*2 1.T24476D2 1.402118t+2 1.537410D 2 4.905502D 1 2.992850D2 X 77 J4 0.0 2.143730D 2 1,483142t*2 2.473209D1 1.537418D 2 4.905502t*1 - 2.992850D 2 St#eG ' JS 100.0 2.143730D 2 1.488142O 2 2.473209D 1 1.531410D 2 2.502026D 1 3.241143t*2 l' 78 JA 0.0 2.2522901 2 1.560734D2 2.260606D I 1.537418D 2 2.502026D1 3.241143D 2 LtAMG 4 Je 100.0 2.25229CD 2 1.5607321 2 2.260606D I 1.537410D2 2.51?O7M+1 4.881094D 2 0, JE 79 JA 0.0 2.52059X*2 1.631445C+2 2.010574D1 1.537418D 2 2.517076D1 4.881094D 2 St#eG D J8 100.0 2.520590D 2 1.637445t*2 2.010574 D 1 1.537410D 2 4.086TT8t*1 6.438180t*2 So JA a.0 1.638010D 2 2.610915D 2 2.049790t+1 4.086782t+1 1.537418t+2 6.438180D 2 SE#eG y J8 100.0 1.638010D2 2.610951D2 2.049790t+1 4.086 Mot +1 1.329435t 2 5.685760t+2 <= 31 JA 0.0 1.638760t*2 2,745495D2 2.591860D1 4.086782D1 1.329415t 2 5.685760D2 SEAMG Je 100.0 1.638760D 2 2.743495t+2 2.591840t*1 4.036790D 1 1.164721D2 6.582749t+2 w 82 JA 0.0 1.009770t*3 2.381678t*2 3.59t T43t+ 1 4.0867821 1 1.164721t+2 6.582749E*2 BEAaeG JS 100.0 1.009770 0 3 2.341478D 2,3.591743D 1 4.08679Ct+1 9.444381D1 5.091635D2 83 JA 0.0 1.008350D 3 2.342956D2 3.046613D 1 4.086782D i 9.444381t+1 5.091635t+2 stAMG Y ' ' ~ Ja 100.0 1.008350D 3 2.342956D2 3.046613t*t 4.08679CD 1 7.029585t+1 4.58141M+2 84 JA 0.0 6.047230t+2 7.291355D1 1.53 t952D1 1.652638D1 4.170111t+1 2.210T33t+2 SEAMG 2 JS 100.0 6.0472301 2 7.298355U1 1.531952t*1 1.652640t+1 2.049954t+1 1.023966t+2 <(% 85 JA 0.0 6.013980D2 7.486027t*1 1.410941 D 1 1.6526386 5 2.049954t+1 1.02596M
~~2 BiAMG~~
,s J8 100.0 6.013 %0D 2 7.486027t*1 ta1094tt t 1.652640D 1 1,160619t*1 3.697700 0 1 C' 86 JA 0.0 -1.124360D2 3.331965t.1-6.811655t+1 1.652638D 1 3.824478D 0 7.285942D0 StAMG. . 4 . QMb AVQ 8 % +' Q> n 3, %Lr + w an 9 Q+,Qg. gam
___----_, 8 L,.,8 g g. I O V 4,4 8 ~ OI SHEET 7 or' (er 7.g,Q E. l f ye M.- T '7'O f Th, d Ofc0 c: m e sistta 4316 6 & 7 6 thu Apr 14 12:49:22 1996 $16mmAP version 4.41 aeport tienent mestel - t N,~ t $1AA01st ter/$eem Itecent .{ 4 ++ 99 - 'ferset 3f7 Paar 3 ' 16*E1P - filtte i9, i;0Jtput tot 4 * $$t StAm (LtutuI LO60$ ~y_- h totAa satAa toast,;u - Soclus Espotec Mem m3 m2 mi y Axla4 V3 g3 SEAM 3.12436M *2 3.331965t*1 6.811655t+1 1.65240t*1 9.539 s t*1 4.90212M+1 v2 W* h% $7,, 44 0.0 3.04854M + 2 3.27151?t+1 6.949899t+1 1.65208t+1 9.539684t+1 4.90212M*1 ' stams P b '. m 3.048540t*2 3.2715118 1 6,949899t +1 1.652640t*1 2.166909t+2 1.k444M + 2 JS 100.0 3.0182164*2-2.00mW2 stAmG 88 Ja 0.0 9.534340f*1 1.320084t+2 9.036019t*1 3.068556t*f2. Je 100.0 9.534340t*1 1.320084t*2 9.036019t *1 3.064550t*12 3.64852M*2 '
~~2.220249t+2 ' atAMG~~
~~%~%, ' JS 100.0- ? ' 87 JA 0.0 8.2504401 1 1.3322Nt+2 9.478935t+1 1.459507t.12 3.k8520t*2 2.220249t*2 J8 100.0 8.25%4M~~
~~1 f. 3522221 2 9.47893M +1 1.4595005 12 3.68731M+2 2.24442M*2 90 J4 0.0 5.12334M+1~~
4. 250244t + 1 7.0102Mt+1 4.11069M.14

3. 6873tM *2 2.24482M*2 SEAmG I
~~J8 100.0 1.123340t+1 4.250244t+1 7.010264t*1 4.11069Ct.14 1.997093t*2 1.23337?f~~
~~2 41 JA 3.0 3.81722M *1 3.740560t*1 6.099764t+1 5.23050M.14 1.99709M+2 1.233379t+2 StAmG 48 100.0 3.81T223 1 3.740560t+1 6,0997Mt*1 5.280810t.14 4.97945M +1 ' 3.1AA W (+{~~
~~-g, 52 JA 0.0 1.60245M*1 f.93448M *1 3,04164M 1 6.48162M 14 4.97945M*1 3.168864t+1 atAmG J8 100.0 1.60245 M~~
1 1.9 M48M *1 3.041686t+1 6.481630(*14 1.645198t+0 1.067850t*0 93 JA 0.0 1.450 7M

0 1.970202t*0 3.035420t*0 1.232874t.13 1.645198t+0 1.067850t+0 stAmG JS 100.0 1,4750701 0 t. 970202t

0 3.035420t*0 1.232870t *13 2.231934t 12 1.611519t.12 9+
~~J4 0.0~~
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~~Js 100.0 4.29605Ct+2 f.511513(+2 1.48327M el 2.268460t*1 2.585169t+1 9.130815t+1 s 95 JA 0.0 4.1973/0t+2 1.412454t+2 1.F m 8*1 2.268461t*1 2.585169t+1 9.130815t+1 EEAmG N J8 100.0 4.1971?M~~
~~2 1.412458t*2 1 u'80M +1 2.268460t+1 2.074624t+1 2.800347t*2 96 - JA 0.0 3.8250$ct + 2~~
~~2. t t 0T2M +2 1.877750t*1 2.855 Mot *1 1.137607t+1 2.800347t+2 StAmG T~~
~~J8 100.0 3.825080t*2 2.11072M.2 1.877M0t+1 2.855840t+1 1.14 552t+1 1.8258171 2 97 J4 0.0 1.70236ct+ 2 1.14009M*2 1.52395M *1 2.85584M + 1 3.692619t+1 T.83855M+1 stAmc 4 at 100.0 1.70236M~~
2 1.16000M+2 1.523958t*1 2.s*i5840t +1 4.114078t+1 1.157248t*2 98 JA 0.0 2.055MM*2 5.13462M *1 1.48176M + 1 4.921935t+1 9.252667t*0 1.157248t+2 StAfeG Ja 100.0 2,055684*2 5.134629t +1 1.48176M+1 4.921930t+1 3.wm9t *1 4.85492H+1 99 JA 0.0
~~2. 20056M~~
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2 T.59C569tel 1.429837t+1 1.652640t +1 1.3770684+1 5.6a642M+1 it 101 JA 0.0 5.78755M

2 9.06527Mel 2.898947t+1 1.6526381+1 f.377D68F+1 5.68442M*1 SEAmG JS 100.0 5.78M5Ct+2 0.06527M+1 2.898947t+1 1.652 Mot *1 f.475580t +1 7.874M5t*1 102 Ja 0.0 5.T7147x

2 4.220195t*1 3.054093t+1 1.6520Me t 1.475580E + 1 7.874795t + 1 stAmG 48 100 0 5.T7t'. M *2 4.220195t+1 3.05409 M + 1 1.652640t+1 3.182864t+1 1.41068M

2 113 Ja 0,0 3.26562M

2 3.92809cf*1 6.59084M

1 1.65 263M

t 5.021079t +1 2.6M219t+1 stAMG st 100.0 3.26562M *2 3.92809C(+1 6.590846t+1 1.65240t+1 3,8246TM*0 7.285942t+0 114 J4 0.0 3.M760C(+2 2.1180$M*2 1.96689H +1 2.855 kM

1 1.164552t+ 1 1.825417t*2 stAm7+
~~J-JS 100.0 3.797600t*2 2.118055t + 2 1.96689M~~
1 2.85584M+1 1.539347t*1 1.2493T4t+2 115 JA 0.0 3.327950t

2 2.2529858 2 3.89683M+1 2.85584M + 1 1.539347t+1 1.249374D 2 MAses J8 100.0 3.327950E+2 2.252985D 2 3.896832t+1 2.855840t+1 2.329994E+1 8.785005t+1 1
~~lie JA 0.0 3.291410D2 2.20737t+2 4.060855t+1 2.855840t+1 2.329994t+1 8.788005t+1 SEAmG V"' J8 100.0 3.291410t*2 2.20737t+2 4.060855t+1 2.855840t+1 5.067647t+1 1.87563M+2 I - 127 JA 0,0 f.52551M~~
~~2 1.19775M *2 1.912912t+1 2.8558400 1 3.25M88D1 3.055049t+1 etAMG v ~~~
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~~7. 08558D 1 128 JA 0.0 4.542470t*2 1.4152680 2 3.126312D 2 1.4T7100D 2 1.447852D 2~~
~~'J.701071t+2 stAmG - Ja 100.0 4.542470D 2 1.415264D 2 3.126382D 2 1.4771100 2 1.204270D2 3.T835T102 129 J4 0.0 4.8489900 2 1.63587M~~
2 3.094343D 2 1.477100D 2 5.2042700 7p Ja 100.0 4.868990D2 1.635879t

2 3.09434M *2 1.477110t+2 1.17793M+3 3.84332tD2 -
~~' ~ c .y y,. rette i re 3 is vi6- -I s value p Output Set 6~~
~~SM set to -~~
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- 4 l a p =4 ~ R ,t g. ATTACHMENT C ~ ,y yu" SHEETdOF_ h MCO Cf;w%4C $Y11tm 4314 6 & F thw Apr 18 12169:26 1996 DC,e$ 7D L ' $1AmmAP versten 4.41 R epor t n (lement i h' , j,- 5 stedet. ' 4p.; y ' f orest ' t STA40 fat ter/ teen Element ' I $N / Title PecP 3 16*s16* mesisue 6 6T tt31.54 + [ 4 - tutput let & * $$( s't minisue 6 93 1.47501 Sean End 8 Aalet ferte 4.. mealoue 6 52 1009.T1 I minteus 6 93 1.9702 J tone (rd a neer2 f orce mes t eue 6 65 638.774 minleue 6 93 3.03542 4 -- teen Erd a Sheer) Force g wea tsue 6 125 312.634 A minina 6 90 4,11069t*14 men taut 6 73 384.333 Seen trd a f ormae minf eue 6 93 2.231931 12 team trd 8 pasenti maa lam 6 129 11T7.93 4 +;y minisue 6 93 f.61132t 12 Seen Erd a sc==nt3 maa lam 6 72 1623.25 fille Pe0P 3 16*116" set ID veLue 5 d; finet MAX /mlu $mry f ebte mintam 1 60 0.11309 p seen (nd A Aalst force f1 maa tan 6 82 1009.77 mininn 1 80 0.610&? tesen tre A pear 2 Force men t osa 6 65 638.T74 2 5 Ii fr minina 1 89
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~~3. s 706 f 714 1.48613M *2~~
.t.298940tel a.791524t*1 3.3100&t 1 SEA >G JS 100.0 6.4587001 1 3.6704 T714 t.486138t d 1.298940E*1 6.799641t+1 3.M59241 1 15 Ja 0.0 6.4587006 1 3.6704771 2 7.328703t*1 1.298940t.1 6.79W1D1 3.645924D1 atAMG l J8 100.0 6.45870CD 1 3.6704T7t d ' 328703tel 1.298940t*1 4.s0114M*0 3.952409D 1 56 44 0.0 6.458T00f 1 1.89M23t 4 1.690020t*1 1.298 h M *1 6.801744D 0 3.952409D 1 alAMG as 100.0 $,4567001 1 1.5942814 <1.69C020D 1 1.295040t*1 2.158942D 1 4.11E34M 1 17 44 0.0 6.458700D t t.8962M 4 1.000558t*0 1.298940DI 2.158942D 1 4,11634M 1 stAmc ^ JS 100.0 6.458700D 1 1.896428D 2 1.0005584 0 1.298940E
1 2.0713931 1 4.2842641 1 58 JA 0.0 6.458700t.1 4,130723t4 7.13025SD) 1.298940D1 2.071193D1 4.284284D 1 StAmG Ja 100.0 6.458T0001 4.4307231 2 T.&30253D1 1.29394CD 1 8.922869D 1 3.861595t 1 59 JA 0.0 6.458700t 1 4.830723( 4 -1.4319531 4 1.298940E*1 3.922869t*1 3.861595E 1 SEAMG Ja 100.0 6.458100t 1
. 5307234 2 1.435953D2 1..9894001 3.64197tt*1 3.433907t 1 i 60 Ja 0.0 6.458700E 1 +1.01999H 1 2.361193t*1 1.298940D1 3.641978D 1 3.4389071 1 SEAMG JS 100.0 6.458700D 1 1.0198964 1 4.361193D1 1.298940D1 +1.08040Tt*1 -6.600656D 1 103 J4 0.0 8.302860D2 1.15550t 1 1.357612t*2 2.9830a.M *1 9.110383D 1 2.1375321 1 SEAMG 1 D JS 100.0 8.302360E 4 1.175550D 1 1.357612r 2.98304M*1 1.25044tt*2 2.431419D1 104 J4 0.0 8.302360t 2 1.11808 t 1 1.4 2 M 6' J 2.953040t*1 1.250441D 2 2.4314191 1 atAMG j 48 100.0 8.302 McD 2 1.516084t 1 1.42254 2 2.9850400 1 5.391587D1 1.6T23771 1 l 105
~~4 0.0 4.30286C(4 1.5180848 1 1.371562D2 2.9580400 1 5.391587D 1 * ).672377t-1 5tAAG l~~
h JS 100.0 8.302360t+2 1.518084t 1 1.371562t*2 2.988040D 1 1.962683t*1 1.292856D 1 .e 106 J4 0.0 8.302860t 4 1.5180848 1 2.15244?D2 2.9&SO4M*1 1.962683D1 +1.292856D 1 SENeG : s J8 100.0 S.302860D 2 1.118084D1 2.152442D2 2.958040D1 7.343787D 1 9.13335M.2 107 Ja 0.0 8.302860t+2 3.057310D2 41.029071t*2 _ 2.968040t*1 T.343787t*1 9.133356D 2 stAMG JS 100.0 8.3023600 2 3.05 n100 2 +1.029071t*2 2.958040t*1 2.946927t*1 6.07604M 4 108 J4 0.0 8.3025401 4 3,05731M 4 S.930628t*1 2.98304001 2.946927t*1 6.076046t 2 SEAMG I J8 100.0 S.302860t 2 3.05n10D2 S.93062M
~~1 2.988040D 1~~
-1.18 T755D 2 3.018736D 2 109 J4 0.0 8.30286CD 2 +3.057310E 4 7.910563D1 2.958040D1 1.18T755(4 3.018736D 2 stAmG JR 100.0 8.302860t.2 3.05T3104 4 7.910563t*1 2.953040t*1 +1.5&3284t*2 1.4900315 2 i 110 Ja 0.0 8,302560t 2 3.0$T310D 2 7.400530D1 2.983040D1 1.553264td 1.490081(4 stAmG p JE 100.0 8.302860D 2 3.05T310E 2 7.400530t*1 2.984040t*1 1.768297t*2 T.257540D3 til Ja 0.0 8.302860t 2 3,0573101 2 2.TS3951t*2 2,968040t+1 1.768297D2.T.257540D3 8tAMG 112 JA 0.0 .s.302 N D 2 1.330544t 3 5.387743D1 2.988040D 1 1.072309D2 3.8573400 4 stAng JS 100.0 8.30286CD 2 3.057310D 2 2.7139518 4 2.983040t*1 1.072309D 2 3.857340D4 s y l ff ; Je 100.0 8.30256CD 2 1.130544 D 3 5.389743D1 2.988040t*1 6.680784t*1 1.383642D 3 C 117 JA 0.0 8.302860D 2 1.444060D 1 1.867384D2 5.119060D 1 1.85975t*2 2.358870t 1 stAmG JS 100.0 8.302860t 2 1.446060s.1 1.867384td 5.11906M*1 4.342821D2 2.7203&5t 1 118 _ Ja 0.0 8.302860t 2 1.705123D 1 2,151119t*2 5.119040t*1 2.342821t*2 2.720 %5D 1 stAMG - 4 p JB 100.0 8.302860D 2 1.705123D1 2.151119t*2 5.119060D1 1.267261D 2 1.867824t 1 l 4 ,t 119 JA 0.0 8.30286ct 2 1.705123E 1 4.100116D2 5.119060D 1 1.267261t*2 1.867824D 1 8tAMG b( JS 100.0 .$.302860D 2 -1.705123! 1 2.100116D2 5.119060t*1 T.422319D1 1.4415431 1 s g-120 JA 0.0 8.302560E 2 1.705123t i 1.423837D2 5.119060t*1 7.422319t+1 1.441543D1 stAmG y JS 100.0 8.302360E 2 -1.7051231 1 -1,423887t*2 5.119060t*1 1.098204D 2 +1 015263D 1 L 121 .1A 0.0 8.302860t.2 2.131919D2 2.608791t *1 5.119040t*1 1.098204D 2 1.0152631 1 stANC : y-a k> mm w+
l 1 i-ja MT f ATTACHMENff: w l putw h. oy 9 t Otto CCuva: Sflita 4316 6 6 7 t>c.- s75 IN A P IO lIIbb5$ b P ) $1At=AP Verliert 4.41 Report n (tement g ; s foraat i 11Akotat lor / Stem fleawat 7' litle : Pt0P 2 17.5" OlAmtitt (ktsut $et 1
~~DEAD LOAD (CL) giae iLtn(4i L0A0$~~
E-t (; anlat Sat aa tutAt 1045104 5tu0 lug 8tuolhG SEAM P V2 v3 mi m2 K3 Ja 100.0 8.3025604 2 2.13191 4 2 2.60879tf*1 1.119060(*1 S.373246t*1 -8.0207082 2 U 122 JA 0.0 8.302860E'2 2.13191 4 2 1.248705t*1 5.119060t*1 S.3732461 1 8.020708t 2 atAsoc I J8 100.0 S.302860t 2 2.1319191 2 1.24870$t*1 1.119060t*1 7.12454't*1 5.88878/4 2 123 2A 0.0 S. 3:2M01 2 2.'3191H 2
~~2. 25640M~~
~~0 5.119 N t.1 7.124541t*1 5.8887E51 2 atAMC Ja 100.0 8.3023601 2 2.13151PI-2~~
~~2. 25640M *0 5.119 E t*1 7.0102214 1 -4.822829t 2 y~~
124.i A 0.0 S.302S%'t 2 2.t319 ut 2 2.513925t*0 1.119 N t*1 7.010221E*1 4.822829t 2 BEAmd i at 100.0 8.302560E 2 2.13191;t 2 2.813925t*0 5.119060t 1 -7.080569t*1 4.289649t 2 125 'A 0.0 8.302360t 2 2.13191M 2 1.552143t*2 5.11906M *1 7.08056M *1 4.28964M 2 st w Ja 100.0 8.302 Social 2.1319ut 2 -3.552143t*2 5.119 N tat -1.5960931 2 3.7568691 2 4 126 JA 0.0 8.302560E 2 *. M65*2t 2 0.899777t
1 5.119060t*1 1.596c93t

2 3.7568691 2
~~'at AMC JB 100.0 9.302560t 2~~
~~.906342t 2 L S997T71 1 5.11M60t*1 1.078609t*2 7.711274E 4 f..~~
~~s title Pt0P 2 17.5* DI Antite Y cutsut let 1~~
~~Ot AD LCAD (Ctl 2~~
let mat /mit 5 rnary foote $tt 10 d*Lwe Seem trw$ A Asist f orce m i a t n es 1 103 0.053:29 W =a s ina 1 53 0.e 587 0 h Been trul A %Acer2 f orce m iriina 1 60 0.50199 a; maninus 1 50 0.71964 I I' lean Erd A Sheer) f orce minina 1 til 278.395 me n ina 1 125 355.214 I E Is team Erd t 'ornse m inium 1 53 -12.9894 I me nina 1 117 $1.1906 S_ Y,5 M Seen Erts A Namnt2 . Minium 1 104
~~125.044 Y~~
A meninn 1 '118'" " 234.252 d 1~{. Beam trd a navnc3 minina 1 58 0.42M3 i-manian 1 48 0.37655 Sean E rd 8 A s t e t f or c e minina 1 53 0.64587 'I men ina 1 103 0.083029 min an 1 50 0.21964 i 8eam fed t thear2 force t masina 1 60 0.50199 teen Erd a sheer) f orce minina 1 125 355.214 i m sina 1 111 278.345 h a A Seam Erd B f or@e mintam 1 117 51.104 9, man ina 1 53 12.9894 1-
~~N 8een tre a manent2 minina 1~~
117 234.282 g ma n ina 1 103 125.0 4 y seem Erd 8 m e ts min nm 1 60 0.66009 1 gs m an ina 1 57 0.42S43 7_ q_ fitte : PeoP 2 17.5" OI Amitta 1 (. A%5** QJtput48et.1ACSt%%,,,,_., 8 TAN,ti,t',Mt4i t0A0$ 4*. 3 g [ antat satAa sataa Ica$1cm stuotu; stuoluc y( SEAM P W2 V3 Mt m2 K3 I Q-45 JA 0.0 1.714950t*2 1.8758062 2 2.221213t*1 1.085057t = 0 3.679138t*0 2.041113t*2 SEAJeG 7;n Je 100.0 1.714950t*2 1.875806t*2 2.2212t3t*1 5.085060(*0 1.0444721*1 2.T79907t*2 f 46 JA 0.0 1.742080t*2 2.325022 1 1.521701t*1 5.085C57t*0 1.044472t*1 2.779907t*2 stAMC = JS 100.0
~~1. 742080t~~
2
~~2. 32502M~~
~~1 3.521701t *1 5.085060t*0 2.254518t*1 2.917240t*2 e(~~
~~47 JA 0.0 1.994610t*2~~
~~5. 662674t~~
1 1.125535t*1 5.0850571 0 2.254518t*l 2.91720X

2 stAMG 6
J8 100.0 1.99461CE*2 5.662674t*1 1.325535t*1 5.085060t*0 8.722641t+0 3.196320t*2 i - 48 JA 0.0 L 112740i'2 2.781925t*1 4.792656t*0 5.0850571*O 8.T22641t*0 3.196320t*2 5(AMG .;B 100.0 2.112740t*2 2.7319251 1 4.7926564*0 5.08506M*0 1.2464T7t*1 3.001225t*2 f w 49 JA 0.0 2.144850t*2 2.1549 75 t
~~1 7.1111051 1 5.085057t*0 1.246477t+1 3.001225t*2 stAMG L(~~
~~,1 JS 100.0 2.144850t*2 2.1549 75 t~~
~~1 7.711105t 1 5.085060t*0 1.296489t*1 2.822380t+2 s~~
~~50 JA 0.0 2.279580t*2 6.6063251 1 1.955040t*1 5.085057t*0 1.294489t*1 2.822380t*2 stAMG .1 J8 100.0 2.279330t~~
~~2 6.606325t*1 1.955040t*1 5.085040E 0 2.898503t*1 2.400221E+2~~
~~~ 8 ,( 51 JA 0.0 2.767270t *2 5.9355231 1~~
~~1. 375495t~~
~~1 5.0850571*0 2.898503t*1 2.400221t+2 Staic~~
~~' \\. JS 100.0 2.167270t~~
2 5.935513t 1 3.375495t 1 5.085060t*0 4.303418t*O 1.994175t

2 52 JA 0.0 2.959740t*2 1.25947%.2 5.153V021 0 5.0850571 0 4.303418t+0 1.994575 t

2 stAMG JS 100.0 2.959740t*2 1.2594791 2 5.153902t*0 5.085060t*0 7.349780t*0 6.027549t+1 53 JA Q.0 3.590470t

2 4.655760t*1 1.7730381 1 6.645830t*0 1.135128t*1 2.650189t*2 stAMG -
~~4 42 [ h_h i- -[ k.\\' [~~
~~mum m~~
umi %A m[4 ATTACHMENT D 3 3.y. W* ctc0 ccavat testra 4316 6 & 7 SHEET U OF h D c.-5773 - thu AF 18 12347159 M 6 ~$1AanAP Version 4.41 aeport a t iesent modeL forset t St Aaptnt ser/seem ttenent W Y fitte : Pep 2 17.5= DIAMitte C Cutput let 2 Det 5 TAN ILtMIuI L0A0$ ] - 9 ~ ulat tutAt tutAt 104510N SIM0luo StW0 lug i StAm P V2 V3 MI M2 "3 C J8 100.0 3.590470t
~~2 4.655760t*l 1.TT30381+1 6.6458 W +0 1.760265t 1 2.81138M+2~~
~~$6 JA 0.0 3.663250t*2 2.447496t*1 3.57300&t 1 6.M5880E*0 1.760265t+1 2.81138M~~
~~2 SEAMG J~~
~~JS 100.0 3.663250s 2 2.a&T&86t*1 3.573004t*1 6.M5880t +0~~
~~f. 757675t e l 2.920139t*2 15 sa 0.0 3.9 tit &M*2 a.094056t+1 1.7760951 1 6.645880t+0 1.75765t+1 2.920139t+2 BEAMG i~~
~~48 100.0 3.911160t*2 6.09&O%E 1~~
~~1. 776099t + 1 6.M5880t~~
0 6.879418t

0 3.172690t+2 56 JA 0.0 4.0073 Mt *2 3.15729M

1 6.784382t*0 6.9 5880t*0 6.8794 tat *0 3.172690t 2 SEANG 43 100.0 6.C07390t*2 3.157290t *1
&,7843821*0 6.64558M +0 9.71668M +0 2.921534E+2 57 JA O.0 4.0J2850t+2 3.2022341 1 2.559678t*0 6.645880t+0 9.716686t*0 2.921534t*2 stAMG -- -Jg 100.0 -- 4.032850t*2 3.202234t+ L,2.559678t*0. 6.6&S850t*0 1.116391t+1 2.684345t+2 58 JA 0.0 4.137MM
~~2 9.45%29te t 1.89462M+1 ' ' 6.645880t*0 1.11639tt+1 - 2.684345E+2 ?tCAMG v-W-.~~
~~Ja 100.0 4.13 766M~~
2 9.45%29t*1 1.894626t+1 6.645880t+0 7 4537tM+1 1.964339t*2 59 JA 0.0 4.505750t

2 8.5577:41 1 3.455530tet 6.645880t+0 2.451710t*1 1.964339t+2 stAMC 4
~~J8 100.0 4.505 750t~~
2
~~8. 55 770&t~~
1 1.455530t*1 6,M588ct

0 1.6493501 1 1.231912t+2 60 4A 0.0 4.652220t*2

.508787tel 6.047841t*0
~~6. M5880t~~
0 t.M9350E

1 1.2319121 2 6tAMG Ja 100.0 4.652220E*2

.50875'l*1 6.047841E*0 6.4588CE*0 1.19561&E 1 1.03056&t 2 103
~~'A 0.0 3.03MSM *2~~
~~5. 579829t~~
~~1 3.30&814t*1 1.4828781+1 2.734230t*1 8.419445E+1 BLAMG Ja 100.0 3.037980t +2 1.5 M829t + 1 3.394814t*l 1 &82880t.1 3.540505t 1 0.757753t+1 h'~~
~~104 JA 3.0~~
~~2. 941720f *2 6.633847t*1 3.63196M +1 1.4828788 1 3.540505t*1 9.757753t*1 atAMG Je 100.0 2.941720E*2 6.633847t*1 3.631968tel 1.482880t+1 1.809355t+1 6.527219t + 1 105 JA 0.0 2.93572M~~
~~2 6.585679t 1 3.517155t+1 1.&82578t + 1 1.807355t*1 6.527219t+1 StAMG L~~
E Ja 100.0 2.9357'0!*2 6.58H79tel 3.517155t+1 1.482880E+1 1.069717t+1 4.958602t*1 D M M W -'- 1064 JA, 0.0 -2.513390(+2 6.771515t+1 5.312523t+1 1.482878t*1 1.069717t+ 1 4.9586 N *1 SEAMG i - / Ja 100.0 2.513390t*2 6.7715151 1: 5.312523f+1 i'1.482880t+1 " 1.882413t*1 ' 0 3.8%205:+1,. ~ : ;gg ~(- 107 JA 0.0 2.406070t
2 1, T78914 1 3.714211t+1 1.482878t+1 1.882413t+1 3.434205t+1 atAMG Je 100.0 2.4069 70t

2 1.T78916t*1 3.714211t+1 1.482880t+1 3.012899t+1 2.654057t+1 108 JA 0.0 2.389&30t*2 1.678068t )
~~1.5042604 1 1.487878t+1 3.012899t+1 2.654057t+1 stAMG - ( c JS 100.0 2.38943M~~
~~2 1.678058t*1 3.504260tet 1.482880t+1 6.341527E*1 2.423538t+1 109 JA 0.0 2.375510t *2 1.62 % 991 1 3.3587625 1 1.482878t+1 6.341527t+1 2.423538t+t stAMG I~~
~~Je 100.0 2.375510t*2 1.6256995 1 3.3587625*1 1.482880(*1 8.0022871 1 2.719024t+1 x 110 JA 0.0 2.3M3 70t~~
2 '. 60 7721t

1 3.290649t*1 1 &S2878tet 8.0022871 1 2.719026t*1 ntANG J8 100.0 2.3M370t *2
~~1. a077218~~
1 3.290645t*1 1.482880t*1 8.820416t*1 2.936506t*1 ill JA 0.0 1.So94.M

2 3.?08-25t+1
~~7. 22&4 TM *1 1.6828738 1 8.820416t+1 2.936506t+1 EIAMG JB 100.0 1.8694&Ct*2 6.708425t*1 7.224478tel 1.482880t+1 8.80162M *1 3.612529t+1 O~~
~~112 JA 0.0~~
~~1. 745810t~~
~~2 2.592235t*1 5.770275tet 1.482878t+1 8.80162M +1 3.612529t+1 SEAMG E~~
st 100.0 1.745810t*2 2.592235t*1 5.770275tel 1.&82880t+1 6.495102t 1 1.704767t +1 p 117 J4 0.0 1.718860t*2 1.2248 8t*2 4.611601t*1 2.6059&&t*1 5.054826t*1 1.070790t+2 SEAMG g J5 100.0 1.718860t*2 1.2246 8t*2 4.611601tel 2.605050tel 6.182025t*1 1.292645t+2 4 118 JA 0.0 1.519050t 2 8.486238t*1 5.410813t+1 2.60594&t+1 6.182025t+1 1.292645t+2 stAMG-k Je 100.0 1.519050t*2 8.6862381 1 5.410813t+1 2.60595M*1 3.513T39t+1 8.768885t+1 M 119 JA 0.0 1.506980t*2 8.4491231 1 5.294115t+1 2.605944t+1 3.513739t+1 8.768485t+1 B4AMG Jo 100.0 1.106080t*2 8.449125t*1 5.294155t*1 2.605950t*1 2.237926t*1 6.730190t 1 6. 120 JA 0.0 6.895100t*1 8.621267t*1 3.78264M
~~1 2.60594&t+1 2.23792M+1 6.730190t+1 stAMG i,~~
J8 100.0 6.895100t*1 8.6212671+1 3.782&4M +1 2.605950t+1 2.801&55t +1 5.014649t+1 121 JA 0.0 5.052470t') 3.034%2t+1 6.601162E+0 2.60594&t+1 2.801455t+1 5.014669t+1 REAMG h JB 100.0 1.052470t 1 3.034%2t + 1 6.601162t*0 2.605950t +1 2.2232664 1 3.533514t+1 tr 122 JA 0.0 4,785470tal 2.983023t*1 3.65169+t+0 2.60594&t+1 2.22326M a l
~~533514t+1 stAMG~~
~~,~ Ja 100.0 4.781470t*1 2.983025t*1 3.65 %94 t +0 2.605950t 1 1.979411t+1 a e45571t+1 123 JA 0.0 6.58968M +1 2.957729t~~
~~1 2.15947t*0 2.605944t+1 1.9794titel 3.645571E+1 SEAMG '~~
~~J4 100.0 4.589660t~~
1 2.95T729tet 2.1596671*0 2.605950t*1 1.97543 t t *1 4.654506t+1 eS, 124 JA 0.0 4.493560(*1 2.949911E*1 2.194869t*0 2.60594&t+1 1.9754311 1 4.654506t+1-stAMG J8 100.0 4.493560(+1 2.949911tel 2.196869t*0 2.605950t 1 2.001554t+1 5.245206t 1 f
125 JA 0.0 6.021590(*1 7.210919t** 8.5276634 1 2.60594&t.t 2.001554t*1 5.2452064+1 stAMG Q-JS 100.0 6.021590t*1 ?.210919t*1 8.521663t*1 2.605950t+1 3.980227t+1 6.164411t+1 126 JA 0.0 7.95481f1 1 6.564910t+1 2.0944344 1-2.605944t+1 3.980227t+1 6.164611t+1 stAMG JS 100.0 7.9548101 1 6.564910t*1 2.094434t+1 2.605950t*1 3.291898t+1 1.919258t +1 ?t' c. title P40P 2 17.5" Oluatite 94 Out:4; Set 2 - Cet
~~D M.~~
-Set MAX / MIN Swsnery table let 80 Value ',# N-5een EM A Aalen Force minisue 2 124 44.9356 masisue 2 60 4 5.222 Reen Erd A Shear 2 Force Minisue 2 110 16.0TT2 't* '?% ~ G h Q &- waa&r m ~
_mm_-.-.- ~ h Q[MGV4 mm he ATTACHMENT D ttco c:evat $ttite 4316>6 & 7 SHEET I 0F b + N N-bc.-STO 1 % e i8 12:'8:03 1** 2' .1-ve,eien 4.a t eser t t Eleaent i g, permet $1907:t ser/seen Ete ent d ) 1' I j, \\ . Title 1 Peop 2 17.5* 01Amt1Et ' Nt;ut let 2
~~Ott maaina 2~~
45 187.581 seem and A sheer) f orce minium 2 49 0.nm m.una 2 125 85.2766 2 ' tems EM A f orcpe min 6 mm 2 &S 5.08506 l menina 2 117 26.0594 3*'. *042 teen tems & amenti " t ain8 2 'I i &S 2 j : menina 2 111 g ggaun,nt) m inina 2 109 24.2354 i .. i ma 2 +6 310.632 lean ind 4 Aust f orce " $ n i an 2 12& &4.9356 l t mas tam 2 60 465.222 8ese End a sheer 2 f orge minina 2 110 16.0772 l 2 i h, mee tna 2 45 187.581 leen End b thear3 f orce a 6 nima 2 49 0.7711' 9 maa t .e 2 125 85.2?&6 y lema End 8 forgue " 6 nina 2 45 548506 mani on 2 117 26.0595 NJ sema tro 8 mwent2 minma 2 51 4.30342 .a. 6 am 2 110 88.2042 l 319'0'II II leem ( M 6 mw ent3 "inina l 'Il .632 h naa 6nm 2 47 Iltte : PacP 2 17.5+ c l Ams t t a 2 k Output 5et 6 * $12 t Pr 8 Am tLtatut 1, 0 A D S 1, Es u t AL sktA4 IntA4 108110m H M0l#G SIMDIWG l h4 St#64 w-4,. 4 ~ JS 100.0 2.687890t 2 2.84311SD 2 2.2&&502t*1 8.151970E+0 1.008031D 1 4.185314D 2 66 Ja 0.0
~~2. 718240E~~
2
~~3. 740304 t~~
1 3#3736D1 8.151966t*0 1.008031t 1 4.185314t+2 SFAmG as 100.0 2.71824N +2 3.740304D 1 3.083736t

l 3.151970D0 2.03507&D 1 4.3953*2t + 2
&7 'A 0.0 3.105780D 2 8.905734D1 1.647156D 1 8.15196M + 0 2.03307& D 1 4.395392D2 SEAMG l 3 J8 100.0 3.105780D2 P.905734D 1 1.47156t+1 8.151970D 0 1.0331DD1 4.782388D 2 f il La J4 0.0 3.294060D 2 4.42991291 4.25925600 8.1519680 0 1.033173D 1 4.782388D2 ntAMG JS 100.0 3.294060D 2 4.4299121 1 4.2592560 0 8.151970t+0 1.311258D 1 4.483481t+2 )- 49 JA 0.0 3.345510D 2 4.570815D1 1.112925t*0 8.151968D 0 1.311258D1 4.483481E+2 eDMG 4 l as 100.0 3.345510D2 e.5 7081tD 1 1,11292500 8.151970D0 1.373457t+1 4.210492t*2 50 JA 0.0 3.56192002 1.02462&D2 1.719482t+1 3.151968D O 1,373457D1 4.210492t+2 stAMG Je 100.0 3.561920D 2 1 u24624t.2 1.719482D 1 8.151970t+0 2.614420D1 3.594272D2 51 JA 0.0 4.3556000 2 9.420531D 1 2.954109t+1 8.151968D O 2.6144200 1 3.594272O 2 BEAMG ~ s l ' J4 100.0 4.355600D 2 9.420531t+1 2.954109 D 1 8.151970D 0 6.948345DO 2.98778SD 2 i : C-52 JA 0.0 4.668880t+2 1.845567t+2 7.575459 0 0 8.151968D 0 6.948345D 0 2.987788t*2 stamG d Je 100.0 4.448880D 2 1.885567t+2 7.85459t +0 8.151970D 0 1.117401t+1 9.534323t+1 U~ 53 JA 0.0 5.&00290D 2 7.403140t+1 1.636592D1 1.011323t+1 1.518827t+1 4.011855D 2 atAnc ; N JB 100.0 5.4002900 2 7.401160t+1 1.636592t+1 1.0113200 1 1.822017t+1 4.235978D 2 54 Ja 0.0 5.504160D 2 e 016213t*1 3.140161t*1 1.011323D1 1.822017t.1 4.255978D 2 stAsos JS 100.0 5.504160D 2
~~.0162131 1 3.1401611 1 1.011120E 1 1.80&3900 1 4.412756D2~~
~~$5 JA 0.0 5.876410D 2~~
~~9. 71&T39D 1 1.593488t+1 1.011323D 1 1.80439001 & 412756D2 SEAMG 1~~
JS 100.0 5.876410D 2 9.71&T39t+1 1.593488t+1 1.011320D 1 1.112714t+1 4.750413t+' t l 4 56 JA 0.0 6.025060D 2 4.915697D 1 5.440827t+0 1.011323E+1 1.112714t+1 4.750413D 2 BEAMG M JB 100.0 6.025060D 2 4.915697D 1 5.440827D 0 1.011320t+1 1.41451st+1 4.3679710 2 57 JA 0.0 6.064560t+2 5.045079t
~~1 4.149610D 0 1.011323E+1 1.414518D 1 4.367971t+2 stAMC-JS 100.0 6.064530t+2 5.045079D1 4.144610D 0 1.011320D 1 1.676014t+1 4.007011t*2~~
~~( 58 JA Q.0 6.223020D 2 1.429751t~~
2 1.690209t+1 1.011323t+1 1.676014D 1 4.007011t+2 etAMG J8 100.0 6.223020t*2 1.429751t

2 1.690209D 1 1.011320D 1 2.696644D 1 2.952591t+2
~~+M-59 JA 0.0 6.80897Ct*2~~
~~1. 298870t + 2 3.043195 D1 1.011323D 1 2.696446t+1 2.952591t+2 BEAMG~~
+ J8 100.0 6.808970D 2 1.2988?ct 2 3.043195 D 1 1.011320t+1 2.387717t*1 1.845978t+2 l Q7 60 JA 0.0 7.042020t+2 7.508723D 1 6.034504t*0 1.011323D1 2.387717D1 1.845978t+2 etAMG- ~ Ja 100.0-7.042020t+2 7.508728t+1 6.036504 0 0 1.011320D1 1.946162D 1 1.656822t+2 +03 JA 0.0 5.755630D2 9.351465D 1 3.194333t*1
~~1. 52638D 1 3.182864D1 1.410686D 2 8tAMG' g(..~~
JB 100.0 5.755630D2 9.351465t+1 3.194333D1 1.632640t+1 3.914044D1 1.635368t+2 y., 104 JA 0.0 5.572570t *2 1.108148D 2 3.523607t+1 1.652638D 1 3.914044t+1 1.635368t+2 SEAmG l Y Ja 100.0 5.572370t +2 1.108148D 2 3.523607t +1 1.652640D 1 2.275159 9 1 1.095265t+2 l l 105 JA -1.0 5.561140D 2 1.1003&SD 2 3.433285t+1 1.65263SD 1 2.2751599 1 1.095265t+2 BEAMG i Ja 100.0 5.541140t*2 1.100388D 2 3.433285t+1 1.6526400 1 1.566511D1 8.327159D 1 vt ,;g b v(p. m . qs y z b f h idhh. b g g' n
g.'&j k: f.,,4 $psh i ATTACHMENT D ~ 0t(0 t(av&C tilltu 4316 6 6 ? - SHEEL O._or N thu.pr 18 12:48:07 IM6 - N* N 51AAmA# Version 6.41 Report n (tcaent hodet t s +++ Nw*wp.~ v Ap4g:,, ly 'N y; Forset a 51Aa01ht ser/ team tienent ' kf-title : Paw 2 17,5' 01 Antila icf' a; output let 6
~~t$t~~
~~' A3-s 8LAu ILIatut-LCADS~~
~~O asiat DrAs Dtas lealton atm0iva Heing i~~
~~' MAm p v2 v3 m1 m2 m3 ~ 1. 106' JA 0.0~~
~~4. 75 T710D2 1.130515t*2~~
~~.891621t*1 1.652638D1 1.566511t*1 8.327159D 1 StamG j~~
J8 100.0 . 75T710D 2 1.130515D2 4.891621D 1 1.652400 1 1.847585t *1 6.416573t*1 107 JA 0.0 4.55520CD2 2.901440D 1 3.85 746CD 1 1.65263M *1 1.867585f*1 6.414573t*1 HAMG JB 10C.0 e.555200t*2 2.901&&0t.1 3.857460D 1
~~1. 452MCl* 1 3.450958D1 4.399734D 1 108 JA C,0~~
~~521810D2 2.TM171t*1~~
~~3. 70329 )t~~
1 1.b52638D1 3.&50958D1 4.199I)4D 1 StAMC 481M 0

. 52 t s t 0D 2 2 '35171D1
3. 703293D 1

1. 65 %3t
~~1 6.96&347t+1 3.859009D1 109 JA C.0~~
~~..*S5320t *2~~
~~2. 6.8.*81t~~
~~1 1.5 9 7502D 1~~
~~1. 65263tD1 6.968347t*1 3.859009t*1 MAMG J8 100.0 e.49532Ct*2 2.M87811 1 3.597902D1 1.652McD 1 $.742353D 1 4.269775t*1 110 JA 0.0 4.68173M~~
2
~~2. 519121t~~
1 3.1491&5 t

1 i.65263M*1 8.T&2353D1 4.269775t

1 StAmG J8 100.0 4.481730D 2 2.61912tt*1 3.549165D 1 1.6526400 1 9.622307t*1 4.195M8D1 111 Ja. 0.0 3.531712D2 t.100397D2 6 4 8214t*1 1.65263St*1 9.622307t.1 4.195M891 atAnc g
J8 100.0 3.5317t;t*2 ' 100J9?!*2 o M8214t*1 1.652 MOD I 9.921908D 1 5.709969D 1 til 24 0.0 3.N60 Ttt *
.126325Di s.154339t*1 1.652635D 1 9.921908 u t 5.709969t*1 stAmG Ja 100.0 3.2964T;D2

.126121D1 6.554336D1 1.652M cD 1 1,021079D1 2.679219f 1 it? Ja 0.0 3.25710Ct 2 2.! sit 65t.2 4.207776D 1 2.815SeCD1 5.0674 7t*1 1.37563M.2 StAp4 J8 100.*
~~3.25700CD2 2,*64761t*2 . 20TT7 A~~
~~1 2.855340D1 6.0779948 1 2.28C8T2D 2 h~~
~~118 44 0.0~~
2. t T71 T*.D 2 1.456T33t*2 5.0443e591

2. 855 5.C01 6.0TT994D 1 2.2808T2t*2 stAmG 1
~~P 48 100.0 2.3 T7170t *2 t aS6733D 2 5.k4349t ) 2.85584091 3.614882t*1 1.551485D 2 L 119 JA 0.0 2.854172D 2~~
1. &8104 TD 2 e.068642t*1 2.85554CD1 3.614882D 1 1.551485D2 StAmc JS 100.0 2.854170D2

1. 48104 TD 2 4.448682t*1 2.85584cD 1 2.446178D1 1.193130D 2 R
120 JA C.0 1.236480D2 1.508343t*2 3.7&O141D1 2.S$1840t*1 2.446178t*1 1.193130D 2 etAmG Ja 100.0 1.286480D 2 t.504343D 2 3.760141D 1 2.8516ACD 1 2.659055t*1 8.8375094 1 121. JA 0.0 9.25199001 5.5823T21 1 6.2671321 0 2.855&e00 1 2.659c51D 1 8.837509t*1 HAmG 2.145TT7t*1 6.019889t+1 %~2.85564091 h% e 'Jo 100.0 9.251990t *1 s - 5.582372D1 6.267132t*0 2.855840D1" ' 2'1457TTD1* E019889t*14 MAm8 hMir$ r 122 JA 0.0 8.720280DI S.506998D 1 4.01T325t*0 J8 100.0 8.720280D 1 5.5069918 1 4.017325 D 0 2.8516409 1 1.922356D 1 6.227289D 1 123 JA 0.0 S.328320t*1 S A69577D1 3.0807510 0 2.855840t*1 1.92235M
~~1 6.22T2899 1 84AmG A~~
~~44 1CC.0 S. 32!U 2001 5.4MSTTiet~~
~~3. 080751D0 2.853S4Ct )~~
~~1.91452t1 1 8.21092M~~
~~1 124 44 0.0 8.13514CD 1~~
5. 45 T9404 1 3.0998105 0 2.855540t*1 1.914527D 1 8.21092M *1 SEAMG 44 100.0 S.13514*D1

5. 45794CD1 1.099810D 0 2.85554001 1.935724t*1 9.34922TD1 t25 Ja
0
~~' 10270 t.2 ' E 931!!.2 5 465681t*1 2.85554001 1.935Ti&E*1 9.349227t~~
~~1 5tAMG J8 1G0.0 1.1CJ T0;D 2 ' fS931SD 2 f.*65681t*1 2.85154 01 3.550034t 1 t.098349D 2 126 JA 3.0 1.4TT57CD2 1.20T504t 2 2.066616D1 2.35534CD1 3.550084D1 1.098349t*2 SEAMG S~~
~~L J8 100.0 1.4TT570D2 1.20T50*r*2 2.066616D 1 2.85584ct+1 3.2566&SDI 3.055049D 1 ,t'y 1 litle : Peer 2 17.5 a OIAmitte k. cwipui Set 6~~
~~sst~~
~~~ h' @\\v $et MAX /mlu $mery table $tt IV Velue (gf Seem tid A &alet f orce minimm 6 124 81.3514 s maalam 6 60 704.202 I'. Sees Erd A Deer) f orce minim m 6 110 26.1912 4'~~
~~x maa t an 6~~
45 284.312 ? , Some trul A Deer) Force minim m 6 49 1.11293 g 7 masimm 6 125 74.6568 F minim m 6 45 0.15197 Seen Erd A f oro.e maalan 6 11T 28.5554 4 team Erd A moment 2 minisue 6 45 6.22303 h i' 'Y + maa tam 6 112 99.2191 9); p~j ' Sean Erd A moment 3 m 6nieue 6 109 38.5901 + no m nimm 6 48 478.239 t o i' T* team ind e Atlet force minima 6 124 81.3514 a> maaimm 6 60 704.202 i y Se m Erd 8 Shear 2 forte minteam 6 110 26.1912 D'?' maaimm 6 45 284.312 h Seen trd 8 shear) force minimm 6 49 1.11293 ,h
~~d menteue 6~~
~~125 74.6568 ~" ap,! J~~
~~f..,~~
~~Seen trd a tercpe miniaun 6 45-8.15197 3 .X =( maatsue 6 117 28.5584 2 seem tre 8 moment 2 minimm 6 51 6.94435~~
~~N e,~~
E Seem trd a masent3. men t am - 6 til 99.2191 h 4 A minlaue 6 112 26.7922 s W meaimm 6 47 478.239 3 V 4; og ;3 y"* Y Dg4 . p gg IQ t, y @* NQm@ O.b bl
'^'""-**""'peai-=..(, m,g n,_ 5 '. hb f 2xq :v v ATTACHMENT D ~s' 1 %{, y w c .s Mhie SHEET h Of h etco c:=nc sesta= 4316 6 4 r u OC.- 9 73 .u. el ime,,., 2 ir.5 omita set to vetve rinet w / mis s m e, tebie h se erd a anset force u tnina 1 tos o.ca3c29-7 m.n ian 6 60 704.202 - minina i 60 0.5019' A sem and a sheer 2 sorce maniam. 6 45 264.312 /a l' h/ Seem (nd A Shear) force miairus 1 111
~~278.375 masinum i~~
125 355.214 minian 1 53 12.9994 ka seem End a forcpe 1 11T 51.1906 meninn - Seem (rd a moment 2 minina 1 104 125.044 useinn 1 118 !}4.282 team tre a met 3 min 6an 1 58 0.42843 mon ian 6 48 478.239 6 53 0.64581 m inina f Seem (rd 8 Anlat force monisue 6 60 704.202 ) 2"y. Beam trd 8 Sheer! Force a 6aina 1 50 0.21964 16 ass ina 6 45 284.312 team (rd 8 theor3 Force minian 1 123 35),214 (. masine 1 111 273.3M d sia m e 117 51,1906 Seem tre e f ores e 4, man ina 6 Ill 28.5) $. [. team Erd a moment 2 minian 1 117 234,282 y mas tne 1 10] 12!,eh4 Vf. '~ jj h} Beam trd 8 Marent3 m ininD 1 60 +0.660C9 g ustlap 47 475.237 r i; - y' - i; 279 c.' R?e? ; 4.*-. 8 e m an,,W4 5EwCy Q gh - _ g:
~~y$ NN y-+ s: n w : m_ q.n g g~~
~~m, -y ~ 6*Wl Q f m g.~~
~~1. N &~~
~~. m 3, t e w.yh j q b 3.< aik 3 s t:I I. r ~ yq.~ k i, - $^ s~~
~~s Kw..n 9'N, 4Q ' s '~~
~~3 y .U : o Dn ^i, r g [l _' #rQ w.~ %;9~~
~~s.. >~~
~~I-y i, ~ j e - 3 w :1~~
~~p I~~
~~n'"'f f,h - n ..M g,l. ct ep i. C.,. ~~n s p c + p,;.. '. z a~~
~~45 J fb' x;&;~~
~~-s Y.- L gLg 3p.:mw: 'b. W' W'W t %[ ce- .r w o- ',, & 4,.g - ? ji. W.?. p. g;, L & r y. t..,. p y y.e~~
~~yp.~~
~~.;~;y. .n '*i 8 . w *ds e e + u 3,Q pg W,%.y, ^~~
2
~~.m +, ,r eqc(x,3-e -{ c,. 7 / o =4 s; E#$.]O[N ,m w-< 4~ l' [ ^ s. 'lf;~~
~~f h~~
~~L.,: +, ? i g,- ffy { 5.".,[,%9 'j ' q_? nW.wl.- .,tp. -~~
~~1'%'~~
~~,a (t - 7"' p t , h L,, ? 'E? yQ. ny. ", w. 'v w4 (' ? ?u s %;.ymp y, Q* s ,yW** 3Q h;194 e , ?p,QM I 7,., W%W n~~
~~g v,r.,c ya <~~
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"4Wuuu===umuss.mgrim mais em
~~1 ATTACHMENT E s~~
Q 1L ~ i W. weri l Kswr ts= va S HEV 3 CAN I f E*' 3syynseems Engineers & GENERAL j ~ ~ Constructors COMPUTATION FINAL Voto O E E PREUM. qg g SHEET { ll ~ *
~~I FERMI 2 - CCINAC X~~
~ W WE DATE NECT _ AUUATIOt7 Ur.WTG. uuu t. SUnJECT - SVGTEM-GERIEC l J1 76230.502 j p p t n I 1 The data contained in thic attachment are generated using the i STARMAP post proccasing f eature. STARMAP is a companion program of STARDYNE which is used to perform the system string analyses. f The purpose of the tabulated data is to present the forces and [ moments in the ductwork by eacn duct size for DL, OBE and SSE conditions. Maximum and minimum values for each duct size are also 1 presented. ?: i i . Based on the commands issued by the prqparer, STARMAP accesses the t Working iiles saved by STARDYt:E during the string analysis runs and prints the data in tabular form. The data are then spot checked r against the string analysis outputs by the checker. The string analysis outputs are contained in the following b calculations: y f MN 'DC-5763' ^^ =- - CCiWAC-Concern-Resolution,TasL b (.. Duct String Analysis and Support u.aluation of t 2268 System Series e i DC-5764 CClWAC Concern Resolution Task i Duct String Analysis and Support Evaluation of j 2848 System Series M DC-5765 CCINAC Concern Resolution Task h [ Duct String Analysis and Support Evaluation of '[ 2849 and 4126 System Series E B c DC-5766 CCIWAC Concern Resolution Task R Duct String Analysis and Support Evaluation of j 2850 Systen Series w j._ DC-5767 CCitVAC Concern Resolution Task i Duct String Analysis and Support Evaluation of 6 4316 System Series s; f-6 ~ /,Qi 'I ,j, if. s l,- '. ' 4., ( i (*;'; j M e ,y1 Q,;y E /j-1 l 6.,' 4Qr& p .l t vf(N;., ji;% ( 40, ks hc h Ma;7 s
4

~~a y. m 7 hf ~~~
~~i' m (,~~
y. 4 / -t + j $p7j
ATTACHM,ENT4M@" . !o wa, s
~~tCO CCwvat lf 5 flu 4116 6 4 7 7 tL * #4'lI~~
[' tN Apr 1812:49:02 1994 $1M2*.** Vertlert 4.41 Report t ttement ) 860 del formet i 11 Amwn,! *-*/ am t t,,,ng ( p 'M till6 1 P90P 3 16*I168 Output let 1 9t AD LOAD (04) ttAa ttimieI L0A05 ? '3 t h AIIAL SutAt lat At 104110e StuDitG Stuotte P v2 v3 mi m2 m3 61 44 0.0 2.N7584 2 7.*36094t 2 1.98t185tet 2.157640t*0 1.3493&3t*1 1.7379381 1 atAaeo C DEAm Jt 100.0 2.F 79act 2 -7.43609 t-2 1.98tt85tet 2,157640t*0 2.412987t = 1 3.2251576 1 62 JA 0.0 6.458700( 1 4.01989e4 1 1.509363t*0
1.29894M

1 1.0M407t*1 6.6008864 1 MAMG JS 100.0 6.458700t 1 5.0198964 1 1.509363t*0 1.293940t*1 2.146587t 1 -1.664068t*0 O Ja 0.0 1.4 %790t*2 2.9079821 2 9.018243t*1 2.612990t*1 2.157639t*0 3.2251571 1 atA>G JS 100.0
+7.43609M 2 2,907982t 2 3.018243tet -2.6129901 1 5.4206381 1 3.043408( 1 s t, 64 Ja 0.3 ?.4 3Wct 2 2,9079s?f 2 9.9&a249tet 2.612990f*1 1.4206344 1 -3.0434081 1 stAMG JS 100.0 1.436090t 2 2.907961t 2 0.0&M69t*1 2.612990t*1 1.166331t*2 2.861659f 1 65 JA 0.0 7.4%090t 2 2.617852t t 1.0593121 2 2.612990t+1 1.166331t*2 2.861659t 1 atAmG 1 JS 100.0 1.4 % 0901 2 2.6171325 1 1.059312t*2 *2.H2990t*1 2.539503t*0 1.806T20t=1 i 66 JA 0.0 7.436090t 2 2.617K321 1 - 8. 84 7069f
I 2.6129908+1 2.539503t

0 5.80672CE 1 StAmG 1_@
~~Ja 100.0 4 7.4%09Ct 2 2.61783?t t 8.S47069t*1 2.612990tet 1.020690t*2~~
~~8. 5 17818 1 P~~
67 JA 0.0 %.70510t 1 3.84086*( t 2.929676t *0 2.6344501 1 8.907958t*1 2.13924M*0 StanG JS 100.0 4,7051M 1 3.540A6.t t 2.929676t *0 2.634450t*1 8.468507t *1 1.96311M *0 4 f4 4A Q.0 5.7631104 1 3,54C8ME t 2.62103tt*1 2.634450t*1 8.4685071 1
~~1. 94311M *C StAmG Je 100.0 4.ft351M 1 3.8408c t 1 2.62103ttet 2.63445M~~
1 4,536960t*1 1.386987t*0 69 JA 0.3 5, *6t 41 1 1 %086 t 1

.940095tet 2.6b5M*1 4.5 3696C(

1 1.386987t*0 6(AMG x
~~JS 100.0 i.7M510t 1 3,kC86*[ 1~~
~~.4 9045tet 2.6b501 1~~
~~2. 5866Mt~~
~~1 S.1085711 1 70 JA 0.0 5.705tM 1 3.8408648 t~~
~~6. 759552t~~
~~1 2.634450t*1 2.886682t*1 4.1081714 1 StAmG Je 100.0 4.76351M 1 3.840864t 1 6.759512t*1 2.634450tel 8.517349t*1 4.909132t 1~~
~~'T 11 JA 0,0 2.4313M~~
~~2 4.4545541 1 2.61TN71 1 0.~~
~~O. 2.392184t 15 StAmG JS 100.0 2,43 t hM 4 4.4545544 1 2.6tT797t 1 0. 1.308899t 1 2.227277t 1 72 aA 0.0~~
~~1. 4C3310f * ?~~
4N

2 4 t ??37t 1 1.781130s 15 -1,308899t ? - 2.2272T71 1 StamG st 100.0
~~-1,9033106 2~~
.*5 15,6 1 2.st T?97t 1 1.78113.1 15 4.377%'t.i 1.5 96067t

0 T3 Ja 0.0 1.227644 1 1.37534t 1 6.504746t 1 1.159850t*0 1.14529M*1 1.942 58t*1 DEAmG M,
Ja 100.0 7.2278408 1 1.3T75341 t 4.5087465 1 1.159850t*0 1.259193t*1 1.9668645 1 74 JA 0.0 1.76423 4 *1 1.377534t t 6.504746t 1 1.15tJ50t*0 1.259193t<1 1.966844t*, 4E7mG F Ja 100.0 -1.764230fet 1.3T534t.1 6.50874M t 1.159850t*0 1.335151t*1 1.98294W D 75 JA 0.0 t.5085Ct 1 1.3T55 4 1 4.69995tt t t.982940t+1 1.31515tt+1 1.1598531 4 W mG JS 100.0 0.5045Ct 1 1.375341 1 4.699511t 1 t.98294M +1 1.389998t*1 9.N 09531 1 76 JA 0.0 6.5085 0t
~~t 1,375345 t 4.5406??t*1 1.982940f*1 1.389998t*1 9.990953t 1 ttAmc JS 100.0 6.504 5CE ?~~
~~?.37534t.t 4.540627t*1 1.982940t*1 3.660311t*1 9.302184 1 / TT JA 0.0 6.504504 1 .130887t 1 5.530334t*1 1.9329 0t*1 3.660311t f 9.30218M~~
stA40 Ja 100.0 6.50*501 1 1.130887t f 1.530338t e t 1.9829ectet 2.793593t*1 7.982441t 1 TS JA 0.0 6.50a5*t 1 1,1305871 1 3.331870t e t 1.9829 0t*1 2.793593t*1 7.9824418 1 StAMG Ja 100.0 6.50650t.1 1.1308371 1 3.331870t e t 1.982940t*1 0.344489t*1 6.0983E3t 1 D
~~is 79 44 0.0~~
~~508750t 1 1.1308871 1 2.066599tel 1.982940t*1 8.344489t*1 6.0983831 1 StAMG Je 100.0 6.50850t 1 1.130887t 1 2.066599t+1 1.982940t*1 5.932768t*1 6.7756381 1 1~~
~~80 JA 0.0 1.1304?Ct 1 6.5087465 1 3.877&32!*1 5.932770t*1 1.982940t*1 4.T786384 1 stamG Ja 100.0 1.130890t 1 6.56874Al t 3.8778322*t -5.932 77Cl~~
1 2.542490f 1 2.617069t 1 31 JA O.0 1.130890t 1 6.50874M 1 8.88829ttel 5.922770f*1 2.54249M

1 2.817069t 1 st AmG -
Ja 100.0 1.13C890t 1 6.5087461 1 8.888291t*1 5.932770t*1 1.290624t*2 1.040627t*0 82 JA 0.0 6.821710E 15 2.621610t 1 1.269527t*2 5.922770t*1 1.290624t*2 1.040627t*0 alAMG Ja 100.0 6.821710(-15 2.621410t 1 1.2(9527t*2 5.93277M *1 2.851580t*1 8.329952t 1 83 JA 0.0 6.82171M 15 2.621610t 1 S.772051tet 5.932770t*1 2.85155M*1 8.3299125 1 StAMG Ja 100.0 6.8217108 15 2,621610t 1 8.TRc5 tt e t 4.932770t*1 6.283596t *1 5.598235t 1 84 JA 0.0 8.302860t 2 1.15550f t 3.077906t al 2.984040t*1 1.077179t+ 1 3.4463315 1 SEAmG Ja 1FJ.0 - 8.302860E 2 1,155501 1 3.077906t
1 2.983040t*1 4.032144t*1 1.4949182 1 85 JA 0.0 8.30286M 2 1.15550t f 4.91427tt*0 2.988040t*1 4.012144t*1 1.4949181 1 stAMG J8 100.0 8.302860t 2 1.17555W 1 4.914271t*0 2.983040tel -4.654302t*1 4.TITTT2C 2 n
~~JA - 0.0 - 3.30256M 2 - 1.330544t~~
~~3 1,1363431*2 2.988040t*1 1.8194411 1 2.181550C 3 stAmG~~
+ JS 100.0 6.302860t 2 1.330544t 3 1.136343t d 2.983040t*1 1.428254t*2 4.266931t 3 6/ JA 0.0 8.302860t 2 1.330544t 3 1.382109E*2 2.985040t*1 1.428254t*2 4.266931t 3-8(AMG -r Ja 100.0 8.302t40t 2 1.330544t 3 1.382109t*2 4.988040t*1 3.8469454 4 6.595384t 3 4 88 JA O.0 0, 4.039396t 2 2,29466M4 7.233850t 12 5.24012*1+2 3.T795471 2 atAmG Ja 100.0 0, 5.0193961 4 2.29466M*2 7.233880t 12 6.86474M
~~2 2.t1654M 3 39 JA 0.0~~
~~-5.5511201 15 4.039396t 2 - 2.672868t~~
2 3.53850ct 12 6.864745t

2 2.11654M 3 stAMG Ja 100.0 - 5 *511204 15 5.03939M 4 2.672864t*2 3.5385001 12 6.97700$t

2 0.
90 JA 0.0 0. 0. 1.468943t*2 5.9 %9201 14 6.977005t*2 0. SEAmG ../ JS 100.0 0. O. -1.4689431 2 4.936920E 14 3.428038t*2 0. b(" ^ 91 JA 0.0 0, 0, 1.0906331 2 6.294960t-14 3.428038t*2 0. 8(AMG - r.L . e,r
~~i. 79' 5J Y~~
g3 ~- mf sy w~ m&& M m, Q_
_h ...e AlTA,CHMENTP* t %o. 0(C0 : wv&C STittu 4316 6 4 7 SM[{ y '2.4 J' ) b S W. thw att 18 12:491M 1996 [ 51AanAP version 4.41 Report a (Leme t n g, Formet $1 Anovut ter/ seas tienent a .3 ( N' litle t P40P 3 16*s16' ~ Output let 1 Ot AD LOAD (CLt g(An tttatui t0A0$ ( f ( w ( [ astA4 SMEAR SutA4 1CallCet StkO1NG S!W0 lug 4 p v2 v3
f

2 "I
~~Jo 100,0 c. O. -1.090633D 2 6.2949601 14 7.461723b t 0. y gg An I 92 JA 0.0 c. 3. 4.56945CE~~
1

7.32747CE

15 7.461723D1 0.
~~SEAMG D Je 100.0 c. O. 4.569650D1 7.327470t~~
~~15 2.279671DO 0.~~
r 93 JA 0.0 3. O. 4.206035t*0 8.570920E 14 2.279671D 0 0. Stan0 F Jg 100.0 L 0-4,206035Do.s.57c920t 14 1.640021t a 12 0. 94 JA 0.0 1.alG igt - t .,33+315t 2 2.040862D 1 7.294690t.1 3.117368t.1 2.151903D 1 StAMG E JS 100.0 1.6101gt.1 . 3343tH 2 2,0 0862D 1 1.2946900 1 7.210746t+1 1.282565t-1 95 JA 0.0 1.6101MD 1
4. 334318t.2 3.372086D 1 7.294690D1 +7.210746D 1 1.282565D 1 SEAMG 4-0 J8 100.0 al.6101606 1 4.3343181 2 3.5720868 1 7.29469CD1 4.617819D 1 4.1322671 2 8.3025604 2 - 1.44606cD 1 5.51657cD1 5.119060D 1 5.197097D 1 *4.132267t*2 etAMG I
M % *w % -~96-4A.0.0. 8.302860D 2 1.446o60f 1 " *5.516570D 1 # 5.119060D1 ~ 2.438813 Dis 3.0980331 2 +9 i Ja 100.0 k 97 JA 0.0 6.302soct-2 4.906340t 2 1.767296D 1 5.119060D 1 6.430298t*1 +3.602M48 2 stAMG Js 100.0 6.3028606 2 4.906342f 2 1.767296t*1 5.119060E*1 5.841783t+1 5.236455t 2 h 98 JA 0.0 9.3377701 2 2.411574t 2 4.756649t 1 7.75103CD 1 5.028484D0 5.236455D 2 BEAMG Ja 100.0 9.33T770E 2 2.411574t 2 4.786649D 1 7.51030D 1
~~5. 98871M *0 3M86850D 3~~
{ 99 JA 0.0 9.337770t 2 2.411574t 2 5.661363D1 7.751010D1 5.988716t*0 3.95685CD 3 stAMG r (' Ja 100.0 4.337770D 2 2.4115748 2 5.661363D 1 7.51030D 1 1.195592D2 4.439086D 2 t-100 JA 0.0 8.30286M 2 1.17555CD 1 1.0660 7D1 2.98804CD1 4.854302t+1 4.717772t 2 stArc t Je 100,0 B.302860D 2 1.17555CD 1 1.066047D 1 2.98804001 4.498242t+1 8.M4109D 2 / 101 JA 0.0 8.302560D 2 1.15550s 1 1.1983661 2 2,95304Ct 1 4.498242t+1 8.644109D 2 SE A)*G f st 100.0 8.302360D 2 1.175550D 1 1.196366D2 2.988040D1 5.076437E*0 1.255869D 1 1 102 JA 0.0 8.302 M 0t 2 1.15MCE 1 -1.282409D 2 2,988040D1 5.0768371 0 1.255869D 1 8tAMG ~ Je 100.0 S.30286M 2 1.175550t 1 1.282409f*2 2.988040t+1 9.110353D 1 2.137532D 1 113 JA 0.0 -8.302860f 2 *1.330544E 3 6.481791D 1 2.96304CD1 6.680784t+1 1.383642D 3 StAMG b Je 100.0 8.302S60D2 1.330544D 3 6.481791D 1 +2.98804CD1 1.819441D1 2.381150D 3 e_ 1 114 JA 0.0 8.302360t 2 1.44606CE 1 6.162995D 1 1.119060D1 2.438813D1 3.098033D2 StAMG ( Ja 100.0 8.302560t 2 1,4460608 1 6.162995t*1 5.119060D1 3.865351E*0 7.913413t 2 115 JA 0.0
8. 302560D 2 1.446060t 1 1.708061D 2 5.119060D1 3.845311D 0 7.913413t 2 alAMG 48 100.0 S.3023600 2 1,44606tD 1

1. 708061t + 2 5.119060D 1 5.318387D 1 1.274325D 1 116 A
3.0 3.302$6M 2 t.4460601 1 1.7921811 2 1.119060D1 5.318387t*1 1.274325D 1 8tAMG J8 100.0 S.3028601 2 1.4-6060t>1 1.7921811 2 5.119060D1 1.8 5975 t. 2 2.35&870E 1 V 127 JA 0.0 S.30286M 2. 906342t 2 - 5.80772*D 1 5.1190+0D 1 1.078409D 2 7.T11274t 4 8tAMG JS 100.0 8.302360E 2. 9063421 2 5.507725D 1 -5.119060D1 6.430298D 1 3.6c?644E 2 128 JA 0.0 5.83209ct 1 3.890949D 1 4.392396D 1 1.05149CD 1 8.449105D t 4.9380000 1 StAMG i 1 Ja 100.0 1.13209CE 1 3.890949D 1 4.392316D1 1.051490D 1 8.847373D 0 3.330267D 1 t* 129 JA 0.0 5,832NCE 1 3.830949t 1 1.405695D 1 1.05149CD 1 8.847373D O 3.330267D 1 stAMG JS 100.0 5.132090t t 3.890949t 1 1.405495 D 1 1.051490t.1 2,102364 D 1 1.159653D O i .-8' 11tle : PtCP 3 16*a16" i DJtput let 1
~~Ot A3 LOAD (04 )~~
Set NAIMt1N SJanary I.ble Set 10 V419e l [J Seam (M A Aalet force Minina 1 80 0.11309 masina 1 71 243.136 i Beam ind A Shear 2 force Minmm 1 BJ 0.65087 f maa tam 1 11 0.445&6 Q. ;. .)_ [ Beam End A Sheer) force Minium 1 89 267.287 maaina 1 116 179.218 9 p@ Seen End A Tor @ e minim a 1 75 19.8294 maalam 1 98 77.5101 J' _ Z Some End A Momenti Minimm 1 90 697.701 '.(, maniam 1 65 116.633 Beam trus A Mosent3 m inina 1 67 2.53925 ? y ? k-Maalam 1 74 19.6686 }. Sete EM S Aalet f orce Minisue 1 71 243.134 'T f [7-maaina 1 80 0.11309 r / Bene ind S Shear 2 Force nintam 1 71 0.44544 Manimm 1 80 0.65087 4 i ; pp team End 8 Sheer) force m5iam 1 116
~~179.218 I~~
~~maaina 1 89 267.237 "f (M,b t Dean EM S fortpe ulniam 1 93 77.5103 A-maalam 1 75 19,8294 {f" r i team ( M S Moswnt2 Minim m 1 116~~
~~187.598 y~~
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~~Sese ind a masent3 ( f ma: Inn 1 67 1.96312 j 'i title : P97 3 16*I16* i tutsut let 2~~
~~CM 8t48 iLtnia1 10405 A41At 5=t At lutAa 10R$10N MuoluG tinMNG 1~~
~~p y; v3 mt M2 M3 I 61 JA C.0 3.0L3 t *2 1.280959D 2 6.604920t*0 1.085057t~~
~~0 7.349780t*0 6.027569D1 StAMG~~
~~? ?.~~
~~ggg, W~~
~~JS 100.0 3.%3 f 2 t. 25WD Z~~
~~6. pWOD 0 5.035060f*0 1.6N81D1 3.115338t* 2 I~~
62 JA 0.0 4.706 x D 2 476215 D I 2 452689t*0 6.M5850D 0 1.195614D 1 1.0305M D 2 stAMG f J3 100.0 4.7060.cD2 4.676215E 1 2 452t&D0 6.M5E3000 1.072389D 1 1.481048t*2 [ 63 JA 0.0 1.407360 0 2 3.201578D2 2.210364D1 1.671378t*1 5.085061t*0 3.115338t*2 atAMC JB 100.0 1.40736CD 2 3.201575D2 2.210%6D 1 1.671380t*1 L5022 m +1 2 2803 m *2 M JA 0.0 1.42818;D 2 1.222%9f *2 2.435754D 1 1.67137St*1 1.502233t*1 2.2ac37 D 2 atAMG h U J3 100.0 1.4291CI 2 3.222 % 71 2 2.4 33 754t
1 1.67135cD 1 2.977166D 1 2.968775 t

2 65 JA 0.0
~~1. 706 90t 2. 183160 D 2 2.855320D 1 1.671378tal 2.977166t*1 2.9687BD2 atAMG as 100.0 1.7064EO 2.18336cD 2 2.555320D 1 1.67133 D 1 4.532008D 0 3.107136D2 p/~~
~~66 JA 0.0~~
~~1. 7%5KD 2. 15 211~~
D 2 2.456303D1 1.671378t*1 4.532008D0 3.10713M

2 stAMG b
~~Je 100,0 n ?56500E *2 . 1521111 2 2.*8630H+1 1.67135st.1 3.102537D 1 7.330367t *2 67 JA 0.0~~
~~2. 26549Cl~~
~~2 9.377965p t~~
~~1. 38925M~~
~~1 2.626131t*1 2.654979D 1 7.535945t*2 atAMG 7~~
JS 100.3 2.265890E*2 9. 3 ? ? 91 3D1 1.3892%D 1 2.626130D 1 4.135001D 1 6.3385 m *2 + k-63 JA 0.0 2.33849002 9.450&!!D1 1.509921D1 2.6261311 1 4.135001D 1 6.338523D2 SDMG h Jr 100.0 2.33549CD 2 9.450433D1 1.509921E*1 2.62630D1 5.746539D 1 5.192656D 2 d." 69 JA 0.0 2.4119 W 2
~~3. 484eet*1 1.307125t*1 2.626131t*1 5.746839D1 5.19265M* 2 stAMG~~
[- JS 100.0 2.41190CD 2 3.448 4*D1 1.507125D I 2.626130D1 7.707698D 1 4.142927t*2 70 JA 0.0 2.469620D 2 L 40%81D'. 2.120349D 1 2.626131E*1 7.707698t*1 4.142927t*2 8tAMG h JB 100.0 2.469420D2 9.4056s it
~~1 2.120349 9 1 2.626130D 1 9.044899D 1 3.618354D2 i~~
~~.?' 71 JA 0.0~~
~~1. 235070D 2 2.850971t*2 5.842309D 1 5,124308D 13 5.M7068D 13 3.061645D12 stAMG~~
^- l-JS '00.0 1.235070D 2 2.350971D 2 5.842309D 1 5.124310E 13 2.921155D 1 1.425485D 2 i T2 JA 0,0 1.180310D 2 2.8191060 2 5.523230D1 1.080232t 12 2.921155t*1 1.425485t*2 stAMG Ja 100.0 1.180310D 2 2.31910N 2 5.523230D 1 1.080230E 12 1.991&S4D2 1.011677t*3 Y 73 JA 0.J 9.00179CD 1
~~6. 92465D1 S.195870D1 2.135819D2 1.584333D 2 2.881&59D 2 StAMG f.-~~
I J8 100.0 9.0017900 1 6.492465t*1 3.195870f*1 2.185820D 2 7.982119D 1 1.82813M* 2 76 JA 0.0 8.849160t*1 8.4094731 1 9.030214t*1 2.385319D 2 7.982119t*1 1.828136D2 BEAMG { Ja 100.0 S. 84916CD1 5.404473t*1 9.03021&t 1 2.385820D2 1.2U164D2 9.503740D1 r
~~1 JA 0.0 9.346640f 1 9.1172548 1 S.34010C D 1 9.503741t*1 1.2T7166D i 2.185816t*2 StAMG JS 100.0 9.346640t*1 011725eD1 S.84010CD 1 9.5037400 1 2.963536D 1 1 % 1796D 2 e~~
~~76 r 0.0 1.022980f *2 1.052771t~~
2 8.919983D 1 9.503741t

1 2.963536D1 1.961796D2 stAMG i-b b.
Jo 100.0 1.022980 D 2 t,052771D 2 8.919983D 1 9.503740 0 1 2.992255t*1 1.903142D 2 77 JA 0.0 1.22243CD2 9.044749t*1 ).836709D1 9.503741E*1 2.992255t*1 1.903142E*2 stAMG i 44 100.0 1.222430D 2 9.066749D1 1.536707t*1 9.503740t*1 1.585913t*1 2.051438D2 E 4 78 JA 0.0 1.2 77.0CD 2 9.5245 21 1 1.544490t*1 9.503741t*1 1.585913t*1 2.053435E+2 stAMG Ja 100.0 1.2 77400(*2 9.524342t*1 1.544490t*1 9.50374C D 1
~~2. ' 07081D 1 3.0384090 2 79 JA 0.0 1.414850D 2 9.99537601 1.316058D 1 9.503741t*1 2.407081t~~
~~1 3.035409t*2 SLAMG q:~~
~~s g-JS 100.0 1.41485CD 2 9,995376t*1 1.316058t*1 9.503740t*1 2.974116D 1 3.9&376M*2 $0 JA 0.0 9.f %640E*1 1.4615841 2 1.498M21~~
~~1 2.974317D 1 9.5037400 1 3.9&3764D 2 stAMG m~~
i-7 JB 100.0 9.996640D 1 1.461584t*2 1.&98362t*1 2.974320D1 8.255111D1 3.513827D 2 / 31 JA 0.0 1.000310D 2 1.532215t*2 2.4140921*1 2.974317t *1 8.255111t*1 3.513327t*2 stAMG JB 100.0 1.000310t 2 1.532215D2 2.414092t*1 2.974320 0 1 7.713160D 1 3.89048D 2 y t 4 82 JA 0.0 5.31908M
~~2 1.329731D2 3.401641D 1 2.974317E*1 7.713160E*1 3.890648t*2 stAMG t~~
~~Je 100.0 5.319080t*2 1.329731t~~
~~2 3.401M1DI 2.974320D1 5.910100(*1 3.039894t*2~~
(; 83 JA 0.0 5.31159CD 2 1.306864D2 2.598567t*1 2.974317t*1 5.9101000 ) 3.039894D2 stAMG 4 L J8 100.0 5.31159CD2 1.306So4D 2 2.598567t*1 2.97&l20D1 4.549322t*1 2.61403SE*2 C-- 84 JA 0.0 3.19130002 4.342995D 1 1.180071E*1 1.482378D 1 2.817654t*1 1.309144t*2 atAMG (- y JS 100.0 3.1913000 2 4.342993D 1 1,180071D1 1.482880E*1 L 609453t*1 6.047247D1 (- 85 JA 0.0 3,173820t
~~2 4.444817t*1 9.391404D0 1.482878t*1 L609653t*1 6.047247E*1 'stuG P_~~
JS 100.0 3.1738200 2 4.444817t+1 9.391404t*0 1.482830t+1 1.215294t*1 2.1g618t*1 i g 86 JA 0.0 1.e5575CD2 2.123718t+1 6.190431D 1 1.482878t*1 4.368994t*0 4.266301t*0 stAMG Ja 100.0 1.655NCO 2 2.123718t') 6.190411D 1 1.482830 D 1 S.600801t+1 3.102499t*1 { 87 JA 0.0 1.61599CD 2 2.086502D1 6.4233200 1 1.082878D 1 8.600801D1 3.102499t*1 atAMG Je 100.0 1.615990t*2 2.086502t*1 6.423320D 1 1.482550E*1 1.979871t*2 6 M8110D? t 88 JA 0.0 5.020920D1 7.397476t*1 8.640717t*1 2.905591t 12 2.75223M *2 1.24735 7Es timG JS 100.0 5.02092CD 1 7.397476t*1 8.640717t+1 2.905590r -12 3.352293D 2 1.421062t*2 i p %- i ,. b 'dw?)] f a
~~, i, j ' ;~~
~~..%. j + p;. g p a~~
~~w..L w, m 3, W.~~
ATTACHMENT e W Ot00 c:mv40 sisttu 4316 6 4 r SHEET L OF_ N, thw Apr 18 12:49:14 1996 't;,C.. [*] 7 g 11AamAP verti m 4.4' 8eport (lement 4 modet 8 . Forset t Stand 1ht Ser/ team Elenerit .g i e.E fitte t P90P 3 16*u16* s v -f - Output let 2
~~Cat J~~
atAa ILtniut t040$ 1 AllAL $Lii8 $ NEAT 104810W B(disG stu0lWG f'~ M AM P v2 V3 at m2 m3 89 JA 0.0 4.344&Oct*1 f.6v4021 1 9.242253D I 8.76t757t 13 3.352293D2 1.621M2t*2 - M AmG + y JB 100.0 4.3448J001 f.6096 cit *1 9.24N53D1 8.761760E 13 3.389884t*2 1.4 M942D 2 90 JA 0.0 2.698000D1 2.115921tei 6.518958t*1 3.06759CE.14 3.38986&t*2 1.4M942D2 ttAsoc J8 100.0 J.6980CCD1 2.7159?it*t 6.518958t*1 3.0675904 14 1.819304 2 7.897279D 1 91 Ja 0.0 2.010tacD1 2.395y w t 5.576952t*1 6.0508684 14 1.819306Di F.897279D 1 StamG J8 100.0 2.010180D1
2. 395099t *1 5.57695M*1 4.050870D 14 4.&a%89D1 2.026945D1 92 J4 0.0 8.4 3MtM *0 1.2374tStet 2.?42982t*1 5.18A T7t 14 4.48%8991 2.026945D I stAmG Ja 100.0 8.4356 Kt*0

1. 237415 t
~~1 2.742982t*t 5.158480t.16 1.476195t*0 6.823556t 1 93 Ja 0.0~~
~~?.7678701 1 1.258958D0~~
~~2. 72M07D0 8.032943D 14 1.476195D0 6.823556D 1 StAPG l~~
JS 100.0 1.76787tt-1 1.258958D0 2.T23607t *0 8.032940D 14 1.837587D 12 f.248606D 12 94 JA 0.0 2.2T3960D 2 S.014737t e t 1.131410t*1 2.2TT363t*1 3.027664D1 1.74681M +2 stApoG JS 100.0 2.273%Ct 2 S.016T37tet 1.13telotet 2.2TThotet 2.168977t *1
5. 3596&9t *1 95 JA-0.0 2.Nt52CO2 7.502t23D t 1.349790t*l 2.2 TTM3D1 2,1689T71 1 5.359649t*1 StAmG et 100.0 2.221520t*2 1,502123D 1 1.3497900 1 2.2TT360t *1 1.796006D1 1.475570D 2 96 JA 0.0 2.016MCD 2 1.1334Et.2 f.691460DI 2.40$f 44f d 1.2T3198D1 1.4755 ?CD 2 BtA#eG JS 100.0 2.01M50D2 1.1314E D 2 f. 691460D I 2.605950f *1 9.689453D0

9. 649393t
~~1 91 Ja 0.0 9.1N670D 1 6.277752t*1 1 354512t*1 2.605mt 1 3.366680D1 4.201351tal StAnc JB 100.0~~
~~9. I224 TOD 1 f..?T79521+1 1.35&S121*1 2.605950D 1 3.695907D1 6.1934T3D 1 98 JA 0.0 1.101610t*2 2.S36915t*1 1.284 771+1 4.i49791t*1 S.062T24D 0 6.1934T3t~~
~~1 SIMeG J8 100.0 1.101610D2 2.8M9196 1 1.289677D1 4.449790t+1 3.385105t*t 3.004393D 1 3~~
~~99 JA 0.0~~
~~1. t T7550D 2 3.663949D1 1.8233M D t 4.449791t )~~
3.385105t*1 3.004393D 1 stMiG Jo 100.0 1.1TM506 2 3.663949Df 1.82339M 1 4.449790D1 6.489949t*t 1.651791D 1 100 JA 0.0 3.15410D 2 4.5056Nt*1 9.692990D 0 1.482875t *1 1.21529't*1 2.16&618D 1 atAfeG ,s. 48 100.0 3.15 410D 2. 505622t*t 9.692950D0 1.482S$00 1 1.249722tel 3.36987&D1 101 JA 0.0 3.05676CD 2 5.4029671 1 3.029556D t 1.482818D t 1.249722D1 3.369874tet SEMeG =f' JS 100.0 3.05476cD2 5.402987tet 3.029556D 1 f.&S2580t*1 9.4393021 0 4.693546D1 102 JA 0.0 3.0463100 2 5.498J121 1 3.22193M
~~1 1.&s237so t 9.459302t*0 4.6935&4D1 atAseG d~~
~~J8 100.0 3.0463106 2 5,4983t ne t 3.221936D 1 1,682550D1~~
~~2. T34230t~~
~~1 8.419445D1 til JA 0.0~~
1. 729ECI +2

2. 6 7504 7t.1 5.828640D 1 1.tS2878p t 4.495102D1 1.704767t*1 alAseG Ja 100.0

1. T29840D 2 2.4 M M 7 tat 5.825649D 1 1.48258cD 1 4.368994D0 4.266301D0 114 JA 3.0 2.00240CE*2 1.137397D2 1.816&&1t*1 2.605 m D 1 9.689453DO 9.649893t*1 SEAMG JS 100.0 2.00260CD2
~~.. t 3 73975 2 1.81684ttet 2.605950D1 1.125916D1~~
6. F525 t3D1 115 Ja 0.0

1. 755650D 2
~~?.2 t&411D2 4.245479t*1 2.6059 4DI 1.125916D) 6.752515t*1 SEA #ec 48 100.0~~
~~1. 75565 CE~~
~~2 1.216411t*2 6.2404791 1 2.605050D 1 1.957237t*1 5.15t390t*1 116 Ja 0.0~~
~~1. 73646M~~
2 1.220893D2 4.436335D 1 2.605944t

t 1.957237D1 5.151390D1 atA#eG JS 100.0
~~1. 736 60D 2 t.220893D2 4.436335t e t 2.60595X*1 5.05&S26D 1 1.070790t*2 V,~~
12T JA 0.0 8.201470t*1 6.502892D1 1.394093D1 2.605 m tet 3.291896t*1 1.119258D 1 StAseG h:. JS 100.0 8.201470D1 6.502392fet 1.t94093D I 2.605950D1 3.m% t 6.201351 tat 123 JA 0.0 2.545310D 2 9.3394171 1 1.95050M
~~2 8.88314tD 1 9.19197&D1 3.624898D2 atAMG I~~
JS 100.0 2.845310D 2 9.333417tet 1.950506D 2 8.83314f s1 3.24255062 2.380%7D2 129 Ja 0.0 3.060780D 2 1.043614t*2 1.9295t&D 2 8.888'.tDI 3.242550D2 2.310967t+2 StAseG JS 100.0 3.040780t*2 1.04M1&D2 1.929514t*2 8.8N140D1 7.342149t*2 2.385416D 2 W fille a PROP 3 16*E16* 3 f Outgaat let 2 =- 058 - ~ 10 Value Set. max /intu Swenary table let tese EM A A444L f orce m in man 2 93 0.77679 s maa(aus 2 82 531.908 minteun 2 93 1.25896 ' b] yl:, , tese EM A Sheer 2 f orce ^* maatsun 2 65 418.3 % ,M E Sees Ital A sheer) Force utnisue 2 62 2.45269 mailsum 2 128 195.05i .Y P Some trd A f orme minisun 2 90 3.06759t = 14 m6sisue 2 73 '38.582 tema tres A moment 2 minivue 2 ?! 5.647071 13 ~q' C T me nisun 2 90 U8.958 n team Erd A secswnt3 winisun 2 ?! 3.061655 12 'T p maa tsun 2 67 753.595 p 4'~ W M* d/ team Erd 8 Aslal f orce min (sue 2 93 0.77679 menisue 2 82 531.908 [ dL I" seem ind 8 Shear 2 force minisue 2 93 1.25896 T 4'r maalsum 2 65 418.3 M - h'.W*; 1 -A, }{f h** n t;_ %p de s. %g; ,y A,u .n ~h
l !fe dh*MN 1 www Mme a ATTXCHMENT e t - ?W - Otto C;nvAc stsitu 431A.e 4 7 G OF g g SHEET thw Apr 1$ 12149818 1996 g (. sp]] }. 11AanAr version 4.4g 8'90ft i II'"""8 Mee t f orma t 51AADYtt Ser/ team tie =ent fitte 1 Pe0P 3 16*t16" - Chstsnet Set 2
~~Cet i~~
Seen Erd g nese) f orce a t Mous 2 62 2.452M maa tsun 2 128 195.051 Dene Erd a torpe minisun 2 90 3.0675 9t*14 masisus 2 73 238.582 seam Erd s mamat2 miMaun 2 93 1.UMM 12 i men taun 2 129 734.215 Seem trW 8 m m at3 mintsus 2 93 1.24861t 12 nas tsun 2 T2 1011.64 1 title 1 PtCP 3 16"t16" 'i thstput set 6
~~lit st4u ILEatu!~~
~~L0A05 An at tutAs ShtAR IC*$lom SIMoluG StuothG d p agan a v2 v3 af "i "3 d et 'JA 0.' 0~~
~~4. 784180t~~
2
~~1. 92139M~~
2 8.595883t *0 8.1510680 0 1.117401t

1 9.534323t+1 stAMG Ja 100.0 4.78418;t 2 1.92189d*2 8.595883t*0 8.151970t+0 2.5H164D1 4.69241M+2 62 4 0.0
?.127790t*2 '. 796681D 1 3.5603171 0 1.011323t+1 1.946162D1 1.6568221 2 atAMG Ja 100.0 7.12779;p2 7.7966811 1 3.560317D 0 1.0113200 1 1.83678M + 1 2.550261t+2 63 JA 0.J 2.13357;D2 5.063548D2 2331525D1 2.197150D1 S.151974Do 4.69241M*2 MAMG Je 100.0 2 13357CE *2 5.063548D2 2.0315258 1 2.5971 M D 1 1.65991M
~~1 3.49080M + 2 64 JA 0.0 2.168760D2 5.09840?D2 2.222553D1~~
~~2. 597150t *1 1.65991M~~
~~1 3.49080M+2 BEAMG Je 100.0 2.168760D2 5.098607t*2 2.222553D1 2.Se7160t+1 2.944760 D 1~~
4. 760603D 2 65 JA 0.0 2.640060D2

6. 38774*D 2 3.056911D 1 2.597159t+1 2.944760t+1 4.760603D2 SEAMG Je 100.0 2.640060D2 6.387744 t
~~2 3.056911t +1 2.591160D 1 7.27053M +0 4.644605D2 64 JA 0.0 2.724780D 2 6.334563t*2 2.N3503t*1 2.597159t*1 7.27053M *0 4.M460$D2 8tAmG Je 100.0~~
~~2. T24 730t *?~~
a.336563D 2 2.793503tel 2.5971MD1 3.745391D 1 1.109039t*3 67 JA 0.0 3.56797ct.2 5. 494 765 D 2 2.221837t+1 4.290754t*1 3.177159D 1 1.131537t +3 atAmc i: as 100.0 3.54797; D2 1.494765D 2 2.221837D 1 4.290760t+1 6.062682t+1 9.505003t+2 6.8 JA 0.0 3.69049CD2 1.491495D2 2.2M25M
1 4.290754D 1 6.062682t+1 9.505003D2 BEAMG as 100.0 3.690490D2 1.491495D2 2.264259D1 4.2907Mt *1 9.107238D 1 7.8322090 2 69 JA 0.0 3.8141900 2 1.469275D 2 2.+13789D 1 4.290754t+1 9.107238D 1 7.832209D 2 StAMC Je 100.0 3.814190t*2 1.469275t*2 2.413739 D 1 4.290760D 1 1.232H M +2 6.379529t+2 70 JA 0.0 3.910960D 2 1.443334D 2 2.604935D1 4.290754D 1 1.23222M +2 6.379529D 2 stAMG
~~i as 100.0 3.910960D2 9 443334t *2 2.604935t*1 4.2907M D 1 1.423407t*2 5.692247t*2 71 JA to 1.839980D 2 4.57M 29D2 1.0119ND2 8.274907t~~
~~13 9.416251013 4.8008196 12 BEAMG z~~
~~40 160.0 1.839980D 2 4.5 76129t~~
~~2 1.0119 Nt*2 8.274910D 13 5.059897D 1 2.288064D2 r~~
72 JA 0.0 1.812010D 2 4.523009t 2 9.52395M + 1 1.6249781 12 5.059897t*1 ' 2.288064t*2 BLAMG Ja 100.0 1.812010D 2 4.5230N O 2 9.525956D 1 1.6249504 12 3.439031D 2 1.623248D 3 x T3 JA 0.0 1.40350t 2 1.089473D 2 1.3025311 2 3.84332M + 2 2.657849t+2 4.680513t+2 stAMG JS 100.0 1.40350t 2 1.089473D2 1.302581D 2 3.843330D 2 1.355844D 2 2.944992D 2 i j, 74 JA 0.0 1.396980D 2 1.39145 D 2 1.487306D 2 3.843326D 2 1.355844t+2 2.944992D 2 stAMG O Ja 100.0 1.396980D 2
~~1. 391475 t~~
2 1.48T30M.2 3.843330D 2 2.012528D 2 1.537418t+2 75 JA 0.0 1.555450D2 1.5f 3058D 2 1.396666D 2 1.53741M

2 2.012528D 2 3.M3321t*2 BEAMG Je 100.0 1.555450t*2 1.50305S4 2 1.396666D 2 1.537410D 2 4.823529t+1 3.10752M+ 2 76 JA 0.0 1.740850t*2 1.7244764*2 1.*02118D 2 1.137418D2 4.823529D 1 3.10526D 2 SEAMG 5
4 Je 100.0 1.740850t*2 1.724476D2 1.402118D2 1.337410t*2 4.905502t+1 2.992850D2 TT JA 0.0 2.143730t*2 1.488142D 2 2.473209D 1 1.537418D 2 4.905502D 1 2.992850t+2 stAMG- + - Ja 100.0 2.143730D 2 1.4tS142D2 2.473209t*1 1.537410D 2 2.502026D 1 3.241143D2 78 JA 0.0 2.252290D2 1.560732D2 2.26060M *1 1.537418D 2 2.502026t+1 3.241143D 2 atAMG Ja 100.0 2.252290D2 1.560732D2 2.260606D 1 1.537410D 2 2.517076D 1 4.881004 t + 2 + 79 JA 0.0 2.520590D2 1.631465 D2 2.010574t*1 1.537418t+2 2.517076t+1 4.881094t+2 BEAMC 1h-Ja 100.0 2.520590D2 1.637465 t
2 2,010574D1 1.537410t+2 4.046T78D1 6.4381806 2 80 JA 0.0 1.638010D 2 2.610955D2 2.049790D 1 4.086782t+1 1.537418D 2 6.438180D 2' StAMG Ja 100.0 1.638010 D 2 2.610955D 2 2.049790t + 1 4.084790t+1 1.329435t+2 5.685760t+2 at JA 0.0 1.638760D 2
~~2. 743495t~~
2 2.591860t

1 4.084782D 1 1.129415t+2 5.685760t*2 BEANG
-JS 100.0 1.638760D 2 2.743495D2 2.591860D 1 4.086790D 1 1.164721t+2 6.582749t*2 82 .JA 0.0 1.009770D3 2.381678D 2 3.591743D 1 4.0867821 1 1.164T21t +2 6.582749 0 2 stAMG W: JS 100.0 1.009770D 3 2.381678D2 3.591743D 1 4.086790t+1 9.444381t+1 5.091635D 2 i4 83 JA 0.0 1.008350t*3 2.342956D 2 3.046613D 1 4,086782t+1 9.444381t + 1 5.091635D 2 StAMG Je 100.0 1.00a350t*3 2.34295M
~~2 3.046613D 1 4.086790t+1 7.029585t+1 4.58141M*2 Q.~~
84 JA 0.0 6.047230D2 7.298355D1 1.5319521*1 1.652638D 1 4.170111t+? 2.210733t*2 SEAMG , f.. JS 100.0 6.047230 0 2 7.298355Da 1.531952D 1 1.652 Mot + 1 2.049954E+1 1.025966t+2 L\\ 85 JA 0.0 6.013980D 2 7.486027t+1 1.410941t*1 1.652638t+1 2.049954t+1 1.025966t+2 stAMG Je 100.0 6.013980D 2 7.486027t*1 1.410941t*1 1.652640t+1 1.1606190 1 3.69T100t+1 86 JA 0.0 3.124360D2 3.331965D1 6.811455t*1 1.652633D 1 3.824678D 4 7.285942D 0 StAMG. A (,M. I xy& MP x%x c uA2
.m, .......i w& ATTACHMENY U ?y ~ Otto Ctuv10 D$tta 4314 6 4 7 SHEET 7 0F M Thu Apr il 12 49:22 1996 D C 5~]*Q $1A8%AP version 4.41 seport t tienent M pedel au f formet 5tAactht tar /seem tienent . Y O' 7.: wu7 Title s PROP 3 16*n16' g. N Output let 8 * $$2 etAm ttIutar tCAO$ ~ d#' AI1AL Sut&R $NtAt 10R$104 SEND!a4 MuoluG V2 V3 mi m2 84 3 Ja 100.0 3.124360D 2 3.331965D1 6.8116558 1 1.6524 0t*1 9.Sh6kt*1 4.902126D 1
~~h. ",~~
SLAM 87 JA 0.0 3.048540D 2 1.271511tet 6.94989W et 1.652638D 1 9.5396&4DI 4.90212M *1 st AmG - JS 100.0 3.0 85 0t*2 3.271519t*1 6.9*96WD t t.652640t*1 2.14909D2 1.0444466 2 AS JA 0,0 9.534340D 1 1.32008.t*2 9.0160194 1 3.06855M 12 3.018216D 2 2.008663D 2 4tAmG JS 100.0 9.534%;D1 1.320064D2 9.0360t9tet 3.064550t*12 3.648520D2 2.220249D2 39 - *A 0.0 8.2504400 1 1.352222t*2 8.478933D1 1.459507t 12 3.M8520D2 2.7202499 2 StAmG
l 100.0 S.250 4CD1 1.352222t*2 9.4 78933D 1 1.4595001 12

3. 68731M
2 2.244826D 2 90 JA 0.0 5.123340D1

.250244D t

41026. D 1 4.11069M 14 3.68731M

2 2.244626D 2 8tAmG Jo 100.0 5.123340t

1 4.250244D1 7,010264 D I 4.1106900 14 1.99709H + 2 1.233379t*2 91 JA 0.0 3.817220D1 3.740560f*1 6.0997M D 1 5.2808060 14 1.997093D2 1.233379D 2 BLAmG JB 100.0 3.81722001 3.740560D1 6.099764t*1 1.28081CD 14 4.97945M*1 3.168864D1 92 JA 0,0 1.602450D 1 1.934480D1 3.04168M*1 6.48162M.14
~~4. 9 7945M~~
~~1 3.168864 tat stAmG JB 100.0 1.602450(*i~~
~~1. 93448M *1 3.0416aM~~
~~1 4.481630D14 1.M5198D0 1.06785M *0 g~~
~~93 JA 0.0~~
1. 4 750 70t = 0 1.47020 1*3 3.03542000 1.2323740 13 1.M51Pho 1.067850D 0 stAMG JB 100.0 1.475070D 0 1.970202t*0 3.035420D0 1.2324704 13 2.2319341 12 1.611519D12 94 JA 0.0 e.296050D2 1.511513t*2 t 41327;t*1 2.2684611 1 4.604463D 1 3.225342t*2 atAMG J8 100.0 4.296050t*2 1.511513D2 1.4132 7tD 1 2.268460D 1 2.585169t*1 9.130815t*1 95 JA 0.0 4.197370D 2 ' 4t245tD 2 '. k480M
1 2.268461D I 2.585169t*1 9.130815t*1 stAM J4 100.0 4.197370t

2
~~1. 1245M~~
~~2 1.M480M *1 2.268.t4t*1 2.074H4Dt 2.800347t*2 9$~~
~~Ja. 0.0 3.8.5080D 2 2.110724 2 1.877750D1 2.n* 5840D I 1.137607t*1 2.800347t+2 SEAMG A 100.0 3.825080D 2 2.110T2M~~
2 1.877750t*1 2.5h840D1 1.1M552t *1 1.825817D 2 97 JA 0.0 1.7023600 2 1.160096D2 f.523958D 1 2.855840 0 1 3.692619D1 7.8385588*1 SEAMG Jt 100.0 1 ?C2360D 2 1.16009eD2 t.123948Dt 2.3558.M

t 4.114073D1 1.157248D 2 98 JA 0.0 2.055630t*2
~~5. ? 34&lSD1 1.481769D 1 4.921935t*1 9.252667t*0 1.157248D 2 Stama JB 100.0 2.0556804 2 5.13462M~~
1 f.4 SIT 69t*t 4.921930D I 3.u m 0D1 4.8549221 1 99 JA 0.0 2.200560t*2 6.75065SD I t.834495D 1 4.?219351 1 3.RAMA9t

1 4.854922D1 SEAMG
/s 100.0 2.200560D 2 6.75065M *1 1,834498D I 4.921930D 1 7.144685t*1 1.337639t*2 100 JA 0.0 5.a86950f*2 7.590569D 1 1.429837D 1 1.65263M *1 1,160619t*1 3.697700D 1 stAmG 48 100.0 1.986950D 2 7.590569t*1 1.4N837D 1 1.652M0D1 1.377068D1 5.686426D 1 101 JA 0.0 5.787550D2
~~9. coS 27M~~
1 2.89894 7t

t 1.652638D 1 1.377068O1 5.686426D 1 SEAmG 5
,5 100.0 5.757550D 2 9.065276D t 2.898947t*t 1.6526400 1 1.475580D1 7.874795t*1 i 102 JA 0.0 5.771470D 2 9.220195t 1 3.054093D 1 1.652638D 1 1.471580D 1 7.874795t*1 SEAMG Je 100.0 5.T71470D 2 9.220195D1 3.054093D1 1.65240D 1 3.182864D1 1.410686D2 113 JA C.0 3.2656200 2 3.G 2SNCD1 6.5908.M
t t.65263M *1 5.0210T9D) 2.679219D 1 SEAmG

s 100.0 3.2656204 2
~~3. 92SNCE~~
1 6.59CoaM e t 1.652M ot 1 3.524678D0 7.285942t*0 114 JA 0.0 3.79760CE

2 2.114051D2 1.966892D I 2.855840D 1 1.1645521 1 1.825817t*2 stAMG Ja 100.0 3.7976000 2 2.118055D 2 1.966892t+1 2.855840D1 1.539347D1 1.249374t*2 115 JA 0.0 3.327950D2 2.252985D2 3.896&32D1 2.855840D1 1.539347D1 1.249374D 2 StamG JS 100.0 3.327950D 2 2.252985D2 3.896&32D 1 2.855840D 1 2.329994DI S.78800$D 1 7
116 JA 0.0 3.291410E*2 2.263737t*2 4.060855D1 2.855840D 1 2.329994D1 8.788005 D 1 StAmG JS 100.0 3.291410D 2 2.263737D 2 4.06c85 '*1 2.8558400 1 5.067647D 1 1.875636D 2 .,;W 127 JA 0.0 1.525510D 2 1.197753D2 1.912912tet 2.85584CD 1 3.254688D1 3.055049D1 J Ja 100.0 1.525510D2 1.197753D 2 1.912912D 1 2.855840t*1 3.692619D1 7.&38558D 1 ?28 JA 0.0 4.142470D 2 1.415268D 2 3.126382D 2 1,477100D 2 1.4478521 2 5.701071D 2 stAmG r Ja 100.0 4.542470D 2 1.415268D J L 126332D 2 1.477t t 0D2 5.204270D 2 3.783571t*2 129 JA 0.0 4.8659904 2 t.635679D 2 3.094343D 2 1.4 77100t
2 5.204270D 2 3.783571D 2 stAMG J8 100.0 4.868990D2 1.635879t

2 3.N4343Di 1.477110D2 1,177933D 3 3.843321t*2 (g.
title : PROP i 16*t16" 2 thstput let 6 1st Set ID Vetue g NAX/Mlm Sumnery table minisun 6 93 1.47507 g $ct i Seen EM 4 Anist f orce maaieus 6 82 1009.77 2 S, ninteue 6 93 1.9702 {, team (M A Sheer 2 f orce mas inue 6 65 638.774 minisue 6 93 3.03542 g , Been EM A she6r3 f orce masisun 6 128 312.638 ulnisue 6 90 4.110/0 14 @1, team ( M A for m e ,,,,,, a masisue 6 73 384.333 ' ' "W 3 {6 -- Seen tnd A moment 2 L minisue 6 71 9.41625E 13 C i maalsue 6 129 520.427 Q minisue 6 71 4.800828 12 M ,5
~~Seen tM A moment 3~~
~~- QQ~~
~~.A 3d- ~ M_ h fkk I M iM y m mm * # Mygvjh.~~
~~m. p, m~~
Q&& $_. , {&w e -) %? w. 3-0100 COMv&C l'17tW 4314*6 4 ? % vim. Thu ape it th 69:26 1996 D C T 'M ' STAAmAP version 4.61 neport i ste nt model - t forest ST A40 tut tarttene tienent n fitte PROP 3 16*t16" A.p' Ostimat Set & * $$t m. maalauu 6 67 1131.54 '~* ulnieue 4 93 f.4750F 7 Bean trui 8 Aalet f orce maaina 6 82 1009.TF .J ulnina 6 93 1.9702 i-Seem trut t Sheer! force [... maaina 6 el 634.774 minf ase 6 93 3.03$42 3 . team Erd 8 Eheor3 f orce 1 mea lam 6 128 312.638 ( minina 6 90 4.11069t 14 l; tens tnd 8 forcpe maala n 6 T3 184.333 minina 6 93 2.23t834 12 !X tems trd 8 acewat2 mas toun 6 129 11TT.93 minimm 6 93 1.611521.t2 [,- to w End I mesent) un s teus 6 72 1623.2$ Title PROP 3 16"X16" let 10 Value finst R41/m!4 lugnary table minina 1 80 0.11309 team trut 6 Aalet f orce masieue 6 82 1009.77 minina 1 80 0.6508F (" Denn Erst 6 shear 2 force maa lam 6 61 638.776 minteus 1 89 +267.25f (i teme Erd A thear) force men ina 6 128 312.618 RJ minieue 1 7%
~~19.8294 maala n 6~~
~~T3 384.333 team test & tortpe 66 minleus 1 90 697.701 '44 team tre a moment 2 masina 6 129 520.42T minina 1 67 2.53925 7;g ' team Erd A masent3~~
~~1. +~~
~~ma n teus 6 61 1131.54 minina 1 T1 243.136 ? -6 team trd 8 Aalet f orce maalesa 6 82 1009.T7 N min (an 1 FI 0.44146 &{; Y' tea trd a sheer 2 f orce maala n 6 65 638.T74 m e nt%m 1 116~~
1?9.218

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~~team trd a $neer) f orce p 1. maaleu 6 128 312.634 minina 1 96 +77.3103 h;, _ - team End t forcy.m manteun 6 73 384.333 minieue 1 116 187.398 team trd 5 moment 2 maa tam 6 129 11T7.93~~
~~J ty minisus 1~~
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~~$1 Atma~~
~~Versiers 4.48 t wort 1 Element modeL~~
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y,i AxlAL SNEAR SutAt 1048104 StuothG . HuoluG vi v3 af m2 m3 + 45 Ja 0.0 2.90MtX 2 3.606261t 2 8.694793t + 1 2.157640t+0 1.104174t*0 2.754138t 1 stamG . N AM Ja 100.0 2.90798M 2 3.8062611 2 8.694793t*1
~~2.15 7MM *0~~
~~+ 4.15349M + 1 2.9311306 1 46 Ja 0.0 2.90798M + 2~~
.767652t 2 1.46693M*2 2.157640t+0 4 tlM9M+1 2.9311306 1 8tAnc Je 100.0 2.907980E 2 4.767652t 2 1.46693M + 2 +2.157640t+0 9.268959t +1 3.367370E 1 47 JA 0.0 2.907980t 2 4.7676521 2 7.320735t +1 2.157M0f*0 9,268V59t+1 3.36737M 1 stAmG 48 1D0.2 2.90MS01 2

.7676521 2 - 7.520T35(+ t 2.1574 0t+0 2.969145t*1 3.765469t 1 8 JA 0.0 2.9079801-2 4.85504M 3 1.985413t+1 2.157kot+0 2.989145t+1 3.765469t 1 stAmG JS 100.0 2.9CMBat 2 4.855MM 5 1.98543M+1 2.157kM

0 4.726399t +1 3.6792371 1 49 JA 0.0 2.90M!CE 2 9.85509M 3 1.95356tbo 2.157kM

0 4.726399t+1 3.6M237t 1 stAAG JS 100.0 2.907980E 2 0.855MM 3 f. 95356M +0

2.15 764M

0 4.89733M + 1 3.593005t 1 SJ., A 0.0 2.907GB06 2 L 19ti.1*t 1
~~i. t10505t *l 2.157 kot+0 4.897316t+1 3.5930051 1 StAmG h~~
Ja 100.0 2,90798M 2 2.19M 148 1 8.130505t+1 2.157kM +0 1.193022t+2 1.6931071 1 51 JA 0.0 2.90798M 2 2,19M 16t 1 1.405958t + 2 2.157640t+0 1.193022t+2 1.6931071 1 stAmG JB 100.0 2.90MSM 2 2.19M 148 1 1.405955t +2 2.15764M*0 5.125055t+0 2.5071935 2 52 JA 0.0 2.90 M80t 2 7.43604t 2 0.30442t+0 2.157 Mot +0 5.125055t+0 2.50719M 2 stAmG J4 100.0 2.90758M 2 ?.436cht 2 9.309442t 0 2.15780(+0 1.349183t+1 1.73M38t 1 53 JA 0.0 6.458700E i 1.451239t 2 1.22680M+t l.29BMot+1 3.438058t+1 3.3T5584 1 5tAMG JB 100.0 6.458 N 04 1 t,*51*34t 2 7.22680M*1 1.29894M +1 6.798524t*1 3.31005t*1 54 JA 0.0 6.458700E 1 3.6704 T71 2 t.48611M*2 1 298940E*1 6.798524t+1 3.310075t 1 SEAMG Ja 100.0 6.458700t 1 3.6704T71 2
1. 486 t 38t + 2 1.298hM *1 6.'99641t+1 3.645924t 1 55 JA 0.0 6.4587001 1 3.6704 T71 2 7.32870M*1

1. 29894M *1 6.799641t+1 3.M5924t 1 stamG JS 100.0 6.458700E 1 3.6'04 7't 2 7.328703t e l 1.298% M +1 6.801744t*0 3.952409t+1 1
4 56 JA 0.0 6.4587004 1 1.8 4 284 2 1.690020t*1 1.298%ot*1 6.801744t*0 3.952409( 1 StAmG I Je 100.0 6.458700t 1 1.89M 284 2 l.690020t+1 1.298MoE+1 2.158942t+1 4.1183444 1 W 57 J4 0.0 6.4587005 1 1.896428E 2 1.000558t+0 1.298%0E + 1 2.158M2t +1 4.118346E 1 stAmG 4 JB 100.0 6.45870M 1 1.89M28t 2 1.000558t*0 1.293960(*1 2.071393t+1 4.284284t 1 58 JA 0.0 6.4557004 1
.8307238 2 7.83P58t+1 1.498%Ct

1 2.071393t+1 4.2842844 1 atAac
=3-J8 100.0 6.458700t 1 4.t30725t 2 7.83025M+1 1.298%M + l -4.922869t*l 3.8615951 1 59 J4 0.0 6.458700t 1 4.83?72M 2 l.43598M*2 -1.298940f*1 8.922869t+1 3.8615954 1 StAmG s'7 JD 100.0 6.4587001 1 6.8307238 2 1.4359&M
2 1.298M ot*1 3.641978t+1 3.4389071 1 60 JA 0.0 6.458700t 1 5.01989M 1 2.34119M*1 1.29894 X + 1 1.641978t*1 *3.438907t 1 stAMG Ja 100.0 6.458700t 1 5.01989M 1 2.361193t*1 1.29894M*l 1.0804071+1 6.6008864 1 103 JA 0.0 8.302S60t 2 1.1 555Ct 1 1.3576f2t*2
~~2. 98804M~~
~~1 9.110383t*1 2.135328 1 H AMG i~~
~~JB 100.0 3.3028Wi 2 1.1755504 1 1.357612t*2 2.9880*0E+1 1.250441E*2 2.431419t 1 + 104 Ja 0.0 0.30286M 2 1.51808et 1 t.422565t~~
2 2.953040t

1 1.250441t + 2 2.4514195 1 BEAmG
~~~ Ja 100.0 6.30286M 2 1.518084t 1 1.422565t+2~~
2. 98804M + 1 5.391587t*1 1.6723771 1 105 JA 0.0 8.302860E 2 1.5180848 1

1. 371562t +2 2.984040t+1 5.391587t+1 1.6T23T71 1 6tAmG JR 100.0 8.3025606 2 1.5*S0848 1 t. 371562 t + 2 2.98804M
~~1 1.962683t+1 1.29285M 1 i~~
~~tre JA 0.0 8.3028601 2 +1.516084t 1 2.t52442t*2 2.98304M~~
~~1 1.962683t+1 1,292856E 1 "AMG O}~~
JB 100.0 8.302860t 2 1.5180&t 1 2.152442t + 2 +2.988040t*1 7.343787t+1 9.13335M 2 e 101 44 0.0 8.302860t 2 3.057310E 2 1.029071t +2 2.988040t+1 7.343787t+1 -9.1333Mt 2 SEAMG J5 100.4 8.302860t 2 3.0573101 2 - 1.029071t + 2 2.988040E+1 2.9469275 1 6.076044E 2 108 JA 0.0 8.302860t 2
~~3. CST 310t 2 8.930628t*1 2.988040t +1 2.946927E*1 6.076046( 2 stAmG g~~
~~JS 100.0 8.302860E 2 3.05T310t 2 - 8.930628t~~
l 2.98804M *1 1.18775*.t

2 3.018736t 2 109 JA 0.0 8.302860E 2 3.057310t 2 7.91056M+1 2.98804M +1 1.18755t + 2 3,018736t 2 StAMG JS 100.0 8.302860E 2 3.05T31M 2 7.910563(+1 2.988040t+1 1.583284t+2 1.490081t 2 110 JA 0.0 0.302860E 2 3.05731M 2 7.400530t+1 2.988040t+1 1.583284t*2 1.490081t 2 stAMG y
Ja 100.0 8.302860t 2 3.0573101 2 7.400530E+1 2.988040E+1 1.768297D. 7.25754M 3 111 JA 0.0 8.302860E 2 3,037310t 2 2.783951t+2 2.988040t+1 1.768297t+2 ?J37540t=3 stAmc p 9 Ja 100.0 8.30286M 2 3.0573 tot 2
~~2. 783951t *2 2.988040t +1 1.072309D 2 A.837340t 4 F~~
112 JA 0.0 48.302860s 2 1,330544t 3 5.389743tel 2.988040t*1 1.072309t +2 2.857340t 4 stAmG Je 100.0 8.3028604 2 1.330544t 3 5.38974M*1 2.988040E+1 6.680784t+1 1.3&l*421 3 117 JA 0.0 8.302060t 2 +1.446060t 1 1.867384t*2 5.119060t+1 1.875975t *2 2.358870t 1 StAMG JS 100.0 8.302860t 2 1.446060t 1 1.867384t+2 5.119060!+1 -2,342821t+2 2.720385t 1 M t . 118 JA 0.0 8.302860t 2 1.70512M 1 2.151119t+2 5.119060t*1 2.342821t+2 2.720385t 1 stANG Ja 100.0 8.302860t 2 1.7051234 1 2.151119t+2 5.119060t+1 1.267261t +2 1.867824t 1 119 JA 0.0 8.302860E 2 1.705123t 1 2.100116t+2 5.119060t*1 1.26726)(+2 1.8678241 1 stAMG 44 100,0 8.302860E 2 1.705123t 1 2.10011M +2 1.119060E*1 7.4223195 1 1.441543t.1 120 JA 0.0 8.3028604 2 1.705123t-1 1.423887t+2 5.119060t*1 7.422319D 1 1.441543t 1 atAMG'
~~.;b R~~
~~Je 100.0~~
~~8.302860t 2 1.TM123t-1 1.423887t+2 5.11906M *1 1.098204t*2 1.015263t 1 121 JA 0.0 8.302860t*2 2.1319191 2 2.608791E*1 5.119060t*1 1.098204t+2 1.015263E-1 stAMG~~
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' ATTACHMENT MW
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248705D 1 5.119060tel 1.124541DI 5.688788E 2 123 JA 0.0 S.10286 4 2 2.13191002 2.286400D0 5.119060D1 7.124541t*1 i 488788D 2 atAmG 48 100.0 8.302840 0 2 2.t319196 2 2.286400D 0 5.119C60D1 7.010221D1 4.32282tt 2 124 JA 0.0 9.30286002 2.1319t&t 2 2.81);25t*3 5.119060D1 1.010221D1 4.822829D 2 BE An'*
J8 100.0 8.302860t 2 2.13 trt902 +2.813925t*0 5.119060D 1 1.080569tel 4.289849D 2 125 JA 0.0 8.302560t 2 2.131914t 2 3.552145D2 5.119060D t 7.080569D1 4.289649t 2 atAMG Je 100.0 8.302860t 2 +2.13191902 3.5 tit 43D2 5.189060t*1 1.596093t*2 3./56869D 2 126 JA 0.0 8.30286 4 2 4.906342t 2 6.879777D1 5.119060D 1 1.596093t*2 3.756869D 2 atAMG JS 100.0 8.302560D 2 4,906342O 2 6.999777t*1 5.11906M
1 1.078609t*2 1.711274t 4 title

Pa0P 2 17.5* OIAmitta T
OJtgut let 1 DE AD LOAD (04) let 10 Value ,L Set MAX /uts $wsmery f ebte Seem End A Aslet f orce mnimm 1 103 0.083029 maalan 1 53 0.64587 Q Some End A Sheer 2 Force =Mine 1 60 0.50199 maa tam 1 50 0.21964 s+y Seen trd a Saeer3 f orce mint am 1 111 278.395 man ian i 125 355.214 [$ a f naim t $1 12.9894' team trd A forcpe maalan 1 117 51,1906 f 5' team Erd A Mumient2 minism 1 104 125.044 maa f am i 118 234.282 Y N' leam trd A moment) minimm 1 58 0.42343 'eas t ase 1 &8 0.37655 J 3 Bema trd 8 Aalet Forte mininst t 53 0.64557 y maa 6nsa 1 105 0.083029 1 team trus 8 theori f orce mininse 1 50 0.219M maume f 60 0.50599 seem trus t Shear 3 Force nintam i 125 355.214 maalma i ill 278.395 e+
~~f '~~
Seem truf 5 tercpe minim a 1 117 51.1906 manina f 53 12.9894 4 Seem tid e acaent2 minim m 1 117 234.232 6: '7 maaima 1 103 125.044 1 Seem Erd a nament3 mintam 1 60 0.66009 6 maninn 1 57 0.42543 ) -d* Title PROP r 1T.5= plantite yJ INtput let 2
~~Osi 654m tttuiu1 (OA0$~~
~~l-y A4 M b ' AxlAL SutAt SNEAR toastou sim0 lng S(N0lue n P V2 V3 NV m2 M3 1 45 JA 0.0 1.714950D 2 1.575806D 2 2.221283t*1 5.085057t*0 3.679138D O 2.06til3t*2 speeG 9tAft Je 100.0 1.114950D 2~~
~~1. 57580et~~
2
~~?.221283t*1 1.085060f*0 1.0444T2t*1 2.779907t*2 46 JA 0.0~~
~~1. 742080D 2 2.32502CD 1 3.5217015 1 5.0850571*0 1.044472D1 2.77V907t*2 BCAMG Ja 100.0 1.742050E*2 2.325020D1 3.521701D1 5.08506M*0 2.254518D1 2.917240D 2~~
~~+1 = 47 JA 0.0 1.994610t*2 5.662674D1 1.825535D t 5.08505?D0 2.254518D1 2.917240D 2 SEAnc Je 100.0 1.994610D 2 5 662614t 1 1.825535D1 5.085060D0~~
~~8. 722641t *0 3.196320E*2 Sh~~
~~.l ; 48 JA 0.0 2.112740D 2 2.781975D1 4.792656D O 5.0850571 0 8.7226410 0 3.196320D 2 SumG N. Ja 100.0 2.112740D 2~~
2. T51425t *
4.792656D 0 5.085060D 0 1.246477D1 3.00122SE*2 49 JA 0.0 2.144850D 2 2.134v75 t

1 7.711105t=1 5.0850571*0 1.2464TTD1 3.00)225t+2 StAMG JS 100.0 2.144850D2 2.8349 75t

1 7.711105 D 1 5.085060D0 1.296489t*t 2.822380ta2 Q
50 JA 0.0 2.279380D2 6.606325D 1 1.955040 D 1 5.082057t*0 1.29M89f*1 2.8223800 2 stAMG f Ja 100.0 2.279380D2 6.606325D 1 1,955040D I S.085060D 0 2.898503D I 2.400221t*2-51 JA 0.0 2.767270D 2 5.935523D1 3.375495tet 5.0850571 0 2.898503D1 2.400221t+2 stAMG 4:
f
. Je 100.0 2.767270D 2 5.935523D1 3.375495Eal 5.045060D0 6.303418D0 1.994575D 2 \\' 52 JA - 0.0 2.959740D2 1.259479D2 5.153902t*0 5.085057t*0 4.3.33418D0 - 1.994575t*2 St.AMG e = Je 100.0-2.959740D 2 1.259479D2 5.153902D 0 5.085060E*0 7.349780t*0 6.027569t*1 53 JA 0.0 3.590470D2 4.65576cD1 1.773038D 1 6.645530D 0 1.13512sD t 2.650189D2 stwG Q
~~j hN.~~
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~~tot 4(Aa tt(ateI t0605 a~~
~~h 7 Antal thtH tut At 1cas10e Nie ttG MuottG e il v3 at m2 m3 J8 100.0 3.5906 ?M~~
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t 6.k%85M

0 1.160265DI 2.8 t t 38M

2 L'
~~H AM $6 Ja 0.0 3.M3250t*2 2.66 F69M O 3.5 T300&D 1 6.M58.50t*0 1.7602Ht+1 2.81138M *2 8 TANG ,f, 48 100.0 3.2125M~~
~~2 2.66749M*1 3.5T3004t*1 6.645880D0 1.5765t *1 2.920139D2~~
~~$$ la 00 3.911140f*2 6.C9405M e l I.776099D 1 6.kS t.8M *0 1.757675t *l 2.920139D2 SIAmG 48 100.1 3,911160t*2 6.094056t*1 1.T76099f*1~~
~~6. 64588M~~
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0 4.M5880t*0 6.87941M

0 3.1T260t*2 SEAMG 3
~~s8 100.0 . 00T3 Mt*2 3.11F29CD 1~~
. T54382t

0 6.645880D0 9.Tt668M *0 2.9215%t*2 i
~~ST 44 0.0 e. 032850D 2 3.202234tet 2.5196T8DO 6 H5880t*0 9.T1M86D0 2.9 J4 100.0 6.0328%D2 3.Nf 2MD t 2.S$96TH+0 6.64588M~~
0 1.1163 tit *1 2.684345t*2 58 Ja 0.0 4.137t&t

2 9.45 H9t*1 1.894626D I 6 M1880t*0 1.1163 tit *1 2.684345t*2 StamG se 100.0
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6. 4588M *0 2.45371Drot 1.964339t*2 19 Ja 0.0 C50575002 8.H. 0 O t 1.4 HUM e t 6,k5850D 0

2. 4HFl0t *1 1.964339t*2 etano J8 100.0 6.5057501 2 8.H TT06t e t 3.45553M e t 6.Hl880t*0 1.kt350t*t 1.231912t*2 60 44 0.0 4.45H2:D2 4 $08787Di 6.H T841D0 6 H1840D0 1,H9350F *1 1.231912t*2 HAuG 48 100.0 4.652H0f*2 4.108787t*1 6.047841t*0 6.645 t.80t *0 1.19561&l*1 1.0305Mt*2 106 44 0.0 3.03fv8ct*2 LS Fi929t a t 1.194814 0 1 1.482878tet 2.n4230tel 8.6196458 0 $tAmG I
~~+ 48 100.0 3.03480D2 6.579829fet 3.384816t*1 1.6t2880D 1 1.5405058 0 9.M T53t~~
1 104 sa 0.0 2.941720s*2 6.63384Tret 3.63ttset.1 1,68 378D1 3.54050 Met 9.T57MM e l StamG 48 100.0 2,961TED 2 6 613847t*1 3.6319t.M

1 1.682880tet 1.809355t d 6.12T219tet 3
~~105 JA 0.0 2.935TMt*2 oS856Mid 3.512155Dt t.482878D1 1.809355t*1 6.527219Dt M AMG J8 100.0 2.93572M42 6.5856Mt e t 3.51Fl55t d 1.482880D t 1.069787t d 4.954602t*1~~
~~f6 J4 0.0 2.113!?Of *2 6.T?iS11t*1 5.112523Dt 1.48187H +1 1.0H117t e l 4.958602t*1 H AMG J4 100.0 2.5133*cD2~~
6. Tf t515t d Lil2 2!t d 1.48tft80D t 1.842&I3D 1 3.8M205t*1 107 Ja 0.0 2,406910t*2

1. T7891M
~~1 3.Ttuttt*1 1.682878D 1 1.8824t3D1 3.834205t*1 Stamo 9~~
~~J4 100.0 2.&O6910t*2 1.T7891M 4 3.7142titel 1.482880tel 3.012899t*1 2.654057t*1 108 Ja 0.0 2.329430t*2 1.67808M~~
1 3.$04260tet 1.48287M d 3.01899t*1 2.654057tel StAMG J8 100.0 2.3894 W 2 1.678088t d 340460t*t 1.482880tet 6.341527t e t 2.423538D 1

E i
~~109 JA 0.0 2.37H t0D 2 1.62569vD 1 1.356T62tet 1.48287M el 6.341527t+1 2.4353M *1 H ANG J8 100.0~~
2. t T55 t-D 2

1. 625699t
~~t 3.358?Mt*1 1.482880D 1 8.00H87td 2.71902&D1 110 JA 0.0 2~~
Stet 2 1.60TTitt*1 3.29049tet 1.482878t*1 8.00 n 87tet 2.719024t*1 HAmG ..h J8 100.0 iFDD2 1.6JTT21t*1 3.290649t *1 1.482880tel 8.820616t d 2.93650M*1 . 111 JA 0.0 440D 2 6 1084$D) 1.2244T8t*t 1.4828784 4 8,820416t*1 ' 2.936506t*1 StAMG J8 100.0 s440D2 6.70845t e t 7 2244T8Dt 1.&82880f*1 8,80162 Met 3.612529t*1
=
~~112 J4 0.0 i.T&5810t*2 2.$ 94435D1 1 TT02TH 1~~
~~1. 6828TM~~
1 8.801MM

1 3.612529t*1 StANG t>
~~J4 100.0~~
1. F&$810D 2 2.192235t*t

1. TT02 T5t
1 1.4828800 1 6.495102DI 1.70676TD1 lif Ja 0.0 1.71&S608 2 1.22&h8t*2 4.611601D1 2.60594&8 4 S.0548?M*1 1.0 TOT 90t*2 6fAMG J8 100,0 1.11886M*2 1.H&848t*2 6.6116M D 1 2.605950D1 6.182025td 1.292MSD2 6@, -
V 118 Ja 0.P t.519050D2 0.68623 tdt 5.4108tM*1 2.605944tet 6.1820251 4 1.292645t*2 StAMG J4 100.0 1.lt9050t*2 8.68438D 1 5.&t0813t*1 2.W910D I 3.513739D1 8.766885tet 119 JA 0.0 1.5M980D2 8.4491230t 5.294tl5t*1 2.6v5944t e l 3.$13T39D1 8.F64885t d SEAMG J8 800.0 1.506980D2 8.4491231*1 1.D41554*) 2.605950D1 2.23792M *1 6.T30190t*1 p 120 JA 0.0 6.8951000 1 8.t.2 tutt e 3.T8264M 4 2.60$M4D t 2.23792M 4 6.T30t90D 1 S J8 100.0 6,895100 0 1 8.62126 Trol 3.782&&6D1 2.605950D1 2.801455D1 5.014469D) 121 JA 0.0 5.052470D 1 3.0M56201 6.6011M D 0 2.60594&D1 2.801455DI J8 100.0 5.05247M O 3.034562t d 6.601162D 0 2.605950D 0 2.2232MDI 3.53351st*1 tu JA 0.0 4.T854T001 2.983023D1 3.653694t*0 2.605944tet 2.223266( 4 3.533514t4 SEAMG s8 100.0 4.7854Mtd 2.983013D1 3.65M94t*0 2.605950D1 1.9T9411D 1 3.6455T1D1 fu JA 0.0 4.58968M e t 2.957729t*1 2.159u.TD 0 2.6059641 4 1.979411t*1 3.6455T1D1 8tAMG }/- c6 J8 100.0 4.589650td 2.95TT29D 1 2.tl966Tt*0 2.605950D1 1.97543tf*1 4.654506D 1 124 JA 0.0 4.4.*3%CD 1 2.949911t
~~1 2.19486900 2.60594&D ) 1.975431D1 6.654506D1 StAMG~~
), A J8 100.0 4.493560t d 2.94991184 2.194869D0 2.605950D1 2.001154D1 5.24520M*1 1*' 125 JA 0.0 6.021$9M O F,210919t*1 8.52TM314 2.605944t*1 2.0015545 4 5.245206td H AMG - y ~ J4 100.0 6.0215900 1 T,210919t*1 8.5H663D1 2.605950D t 3.980U7t d 4.1M 6 t it *1 126 JA 0,0 7.95&J1M H 6.564910D 1 2.0944MD 1 2.6059+4D I 3.980227D1 6.146118 4 H AMG JS 100.0 T.956810D 1 6.$6491001 2.094434tet 2.605950D 1 3.291898t*1 1.919258D 1 title Pe0P 2 1T.58 Otamitte
~~p h~~
~~Output let 2~~
~~CSE let 10 Vetue~~
~~. h~ %{(,(),, + 2; Set MM/u(8 sonnery table ulnieus 2 124 44.9356 e ~ maaleue 2 60 465.222 Sees truj & &alet f orce j mieu. 2 110 16.Orn W Q,2 t< 8. tr.: 6 v.r2 t m e g M[f'g u 2^~~
Q
\\ en 1
, p m==-- 8-- ATTACHMENWN i L _ g' M s.$. ' w ttt0 Etwvat l? tite 4316 4 6 7 gy jj the Apr 18 128'8 03 19 % D Ca ' Ml3 g,g y, n,,g,n 4,4g tesort I lieneet N tornet i 11201mf Ser/tene (teinent ef i, y s c title Pew 2 17.5" BIAmitte O meatma 2 &l 18I.III 6een Brud A thear3 80,c, minian 2 49 0.Ulti me inn 2 in 8s.2766 a 6ninn 2 41 I.08 W ~ been truf A tercue men ian 2 117 N.0594 team truf A Ameat2
t al"*
I 'I 3'0III' i,' maa tan 2 ill 88.2MI j go trug i siament3 s t atan 2 109 24.2354 i ,s m *s tna 2 48 319.632 seem teus 8 Aalet f orse nietan 2 124 44 M356 masina 2 60 465.N2 leen trui 8 Shearl f orte 8 t nian 2 00 16.0U2 mestan 2 41 187.581 team traf I theer) fo'te
~~laima 2~~
0 0.UlH i M. mas tne 2 ili 85.2766 ntan 2 45 $.085% o lean trwl 6 fortue me.6nn 2 11T 26.0595 team tro 8 manent! s tat *in i 11 4.303'2 a s s ina 2 110 88.2M2 team truf a manents mininn 2 112 I T.04 U y .. in n 2 4T 319.632 r 9~ title a te0P 2 17.l* OlAuffit etAm ttIatui LOAD $ + g4 h -- tutsut let 6 a lit Antat Int aa satas toal10m simotes titolhG
I y*
~~gga P v2 V3 at m2 8L3 el JA 0,0 2.8379Et 2 2.S.3118t*2 2.244502t e l 4.15196M *0 6.22303M*0 3.1729MW2 StAssG 4 JS 100.* 2.687890t~~
2
~~2. 843116t~~
~~2 2.244502t*1 8.11197M*0 1.0080311 1 4.1853Mt*2 4~~
~~e 46 JA 0.0 2.71824M*2 3.740304tal 3.083 T3M~~
1 8.11196M

0 1.006031t*1 4.185314t*2 etAseG J8 100.0 2.71824M*2 3.T40304t*1 3.083T3M *1 8.151970t*0 2.035074t*1 4.395392t*2 47 sa 0.0 3.105 78M

2 8.905 m tal
~~1. M T1$M~~
t 8.15 t hM

0 2.035014t*1 4.395392t*2 6tAsee Ja 100.0 3.1057S0t*2 4.905734tet

MT1SM*1 8.151HM

0 1.033173t*1 4.T8238M*2 48 JA 0.0 3,294ket 2 4.42991M*1 4.25925 M

0 8.151968t*0 1.033173tel 4.T8236At*2 6tAseG JB 100.0 3.294MCtel 4.42991M*1 4.2$925M*0 8.111970E*0 1.31125M*1 4.483481t*2 O
~~49 JA 0.0 3.34511M~~
~~2 4.570416t*1 1.112925t*0 9.111968t*0 1.3112584*1 4.483481t*2 StAmo Ja 100.0 3.34111CE*2~~
~~4. 57081M~~
~~t 1.112925t*0 8.15197x*0 1,373457t*1 4.2104921*2 10 JA 0.0 3.56192M.2 1.02662.I 2~~
~~1. 71948M~~
1 8.tli9t4t*0 1.3T3417t*1 4.21049M

2 atAsoc JB 100.0 3.161920t*2 1.0244248 2
~~1. T1968M~~
1 8.1$197M

0 2.61442M*l 3.$%272t*2 11 JA 0.0 6.355600t*2 9.420S31t*1 2.956109f *1 8.15196M*0 2.6M420t'l 3.5MIT2t*2 StA#eG l
~~JS 100.0 4.*15600t*2 9.420131t*1 2.956109E*1 8.1119fM~~
0 6.948145t*0 2.98TT88t* 2 52 JA 0.0 4.M8A50t

2 1.835567t+2 T.875459t

0 0.11196M

0 6.948345t*0 2.98TT8M*! stA#ec 4
~~t -h JS 100.0 4.Ma&S0tel 1.8855671 2 7.875459t*0~~
~~8. tS 197M *0 1.117401t*1 9.134323tet~~
~~[' 53 JA 0,0 5.400290t*2 T.40316M~~
~~1 1.6Ml92tal 1.011323t*1 1.11882Tt*1 4.011855t*2 MApeG JS 100.0 5.400290te!~~
~~7.403160t*t 1.636592t*1 1.011320t*1 1.822017t*1 4.2559TM*2 u $4 JA 0.0 1.5041604*2 4.016213t*1 3.H0161t*1 1.011323t*1 1.88017t*1 4.255978t*2 etases~~
/
~~i 4 Ja 100.0 s.10416N I 4.016213t*1 3.140161t*1 1.011320t*1 1.604390t*1 4.412T564*2 6 il JA 0.0 1.87M lM~~
2
~~9. 714 T39t~~
~~1 1.5934&8tet 1.0113231 1~~
~~1. 8M 390t~~
1 4.41275M

2 Stase0 JS 100,0
$ 87M10t*2 9.T14T39tet 1.19M88tel 1.01132M et 1.112Tittel 4.750413t*2 ? 56 JA 0.0 6.025 40t*2 4.915697t*t $.44082T1 0 1.011323t*1 1.112714t*1 4.T50413t*2 etano Je 100.0 6.025060t*2 4.91569ff*1 1.*40827t*0 1.011320t*1 1.4M51M*1 4.36T971t*2 V(', .57 JA 0.0 6.064580E*2 1.0450T9t *1 4.H961M *0 1.011323t*1 1.414118t*1 4.3679T1t*2 SEAsso . A-JB 100.0 6.064580t*2 5.M5079t e t 4.14961M *0 1.011320t*1 1.676014t*1 4.007011t*2 18 JA 0.0 6.N8020t*2 1.429751t*2 1.690209t*1 1.011323t*1 1.6760Htet 4.007011t*2 etAsos JS 100.0 6.2280204*2 1.42975tt*2 1.690209t+1 1.011320t*1 2.69664M
1 2.952591t*2 59 JA 0.0 6.8089 fot

2 1.2988T0f*2 3.H3195t*1 1.011323t*t 2.69664Hel 2.952591t*2 StAreG JB 100.0 6.8089704*2 1.298870t*2 3.M3195t*1 1.011320t*1 2.38UlTt*1 1.84S97M*!
60 JA 0.0 T.042020t*2 T.508728tet 6.036SMt*0 1.011323t*1 2.38Uttt 1 1.845978t*2 st Apoc " JB 100.0 T 0420201 2 T.508T2St*1 6.014504t*0 1.011320t*1 1 k6 h2E*1 1.656a22t*2 103 JA 0.0 5.T5%&30t*2 9.311465t*1 3.19433M*1 1.65263N *1 3.1&2864t*1 1.410686t*2 stAsec JB 100.0 S. 75563M
2 9.351461t*1 3,194333t*1 1.612640t e t 1stuo44t*1 1.635368t*2 1M JA 0.0 5.54570t*2 1.10848t*2 3.523607t*1 1.65263M

1 3.9% % 4 *1 1.635368t*2 ofAmo
~ ..(. JS 100.0 $ 54570t *2 1.108u8t*2 3.523607t*1 1.65240t *1 2.271159t*1 1.095265t*2 l Q' 10$ JA 0.0 5.561 H M *2 1.1003&St*2 3.433285t*1 1.65263M *1 2.275159t*1 1.095265t*2 Stapes Q J6 100.0 5.561140t*2 1.10038st*2 3.433285t*l 1.652640t*1 1.566511t*1 8.3tT159t*1 hL3 > a a 44 1 a, N Qp' . j M@[M gw i% ~ Qd W l yh2 %
D
~~ATTACHMENT DI t~~
~~tit *J Clavag tigita 4316 6 6 f SHCCI 1 % y [ %~~
~~d Yo 1N Apr 1612i+8:071996 StatmAP vereien 4.41 8 5.>r t tie nt j~~
~~essent i ,e.,-L F: format I $1&h0 tut Ber/6 tee element 'J)*Q title t Peup 2 1F,1* OI Amttl8 T Output let 6~~
~~S14 Stas itIate LOAD 1 re i N~~
~~Atlat tetAS $ntAs icallts Stuotto Nuolac P v2 tr3 et m2 m3 106 JA 0.0~~
4. T17710t *2 1.130$15t*2 4.891621t*1 1.H2 Hat *1 1.566111t*1 8.321119t*l HAmG MAM JB 100.0

4. 75 Tf1 M
~~2 1.13011%t*2 6.ff t&2tt e t 1.H2MCl*1 1.66T18)(s t 6.4141738*1 t0F Ja 0.0 4.lll20M *2~~
2. 90144M *1

3. sit 46 Met 1.65263M *1 1.Bo?585t+1 6.4145T3t*1 StANG Ja 100.0 4 $$$200t*2 2.60144M
1 3.81146M e t 1.6526+No1 3.4%095M*1 4.399T14t*1 108 Ja 0.0 4.l2181M

2 2.T35111t*1 3.703293 tat 1.612H8t el 3.45095M * )
~~4.399T34bi ttAmo + Js 100.n 6.521810t*2 2.73%111t*1 3.703293t*1 1.61284M*1 6.96H4Pt*t 3.859009t*1 109 Ja 0.0 4.691320182 2.ka?81tet 3.$97902tet t. Ht63H e t~~
6. 96814?t e l 3.859009D 1 H %mG J8 100.0 e.49%520t*2 2.kar$1t*1 1.197902D t

1. H 28M
~~1 8.742313t*1 4.26frT5tet 110 JA 0.0~~
~~6. 461 TIM~~
2 2.619121t*1 3 $69165tet f.H H35t*1 8.F42313t*1 4.269TT5t*1 Stamc JS 100.0 4.481 T30D 2 2.619121181 1.$40141D 1 f.65264M

l 9.6223071*1 4.195938D1 til JA 0.0 3.131FICD2 1.1003fft*2 6.M8214Dt 1.H263Bl*1 9,622107t*1 4.59193M* 1 HAmG J8 100.0 3.131710D 2 1.10c3tTt*2 6.48214t v t.61264M e l 9.921906t*1 5.709969t*1 til Ja 0.0 1,2960ft't *2 6.1263 M t

1 6.S $43 39t

t 1.652HN o1 9.9219084*1 1.709969t*1 StamG J4 100.0
~~3. 29e.c f ct~~
~~2 4.t263MDt 6.554339t*1 f.612640t e t 5.021079t*1 2.679219t*1 t~~
~~117 JA 0,0 3.21790002 2 269161t*2 6.20TTf6tet ' 2.911840t~~
1 1,0HMfD1 1.87563M

2 8tAmc J8 100.0 3.217 m 4*2 2.269145t*2 6.20 T716D i 2.41184M

1 6.077994t*1 2.2808T2t

2 Ill JA 0.0 2.lTF170t*2 1.484T13t*2 1.04434ttel 2.451840t*1 6.077994t*l 2.2806T2O 2 atAmG J8 100.0 2.6T717M

2 1 *t4T33t*2 5.W348D t 2.HS840t*l 3.6147.828*1 1.ll1485t*2 119 JA 0.0 2.854110D 2 1 J81067t *2 4.9686&2tel
2. Hl640t e l 3.614&a28*1 1.151485t*2 StAMG J4 100.0 2.454170 0 2 1.48104 TI* 2 6.9484.828 1 2.815640t e t 2.4461Tf.D1 1.193130D 2 120 JA 0.J

1. 2 &o48M
~~2 1.10&l43t*2 3.?4034ttel 2.811840D1 2.4461?M*1 1.193130D 2 HAmo J8 100.0 1,2866604 2 1.90041t*2 1.1603 1 tat 2.811640D 1 2.6190$$le) 8.137509t *1 12t JA 0.0 9.2S it*C4 + 1~~
~~%.1823T2t*1 6.267132D0 2.8%$40D1 2.6190t$t*1 3,83T509t*1 6tAMG Jo 100.0 9.25199M~~
~~1 1.582172t*1 02&F13200 2.811840tel 2.1457171 1 6.01$h89t*1 122 JA 0.0 8.T20280D I l.10699tD 1~~
~~6. 0 t T325 t~~
~~0 2 8H86M *1 2.141TTT!* l 6.019689t*1 StAMG JS 100.0~~
~~8. T2028M e l 1.10699tD1 4.01 T3Mt~~
0 2.85$ 4001 1.9223$6D1 6.227289D1 123 JA 0.0 B.12832M *1 1.* H$ TTt

1 3.080711t+0 2.85584 M

1 1.922356tel 6.227289tel SIAmo J8 100,0 8.328320D1 1.44H771 1 1.060711t*0 2.811640D1 1.914$27t*1 8.21092M e t t(4 JA 0.0 B.131140D 1 1.45194N o 1 3.0W8 t M

0 2.85th M *1 1.914$27t*)
~~6.210926t*1 SEAmG J8 400.0 8.1311400 1~~
~~1. 6 % f 94 M~~
1 3.099810D0 2.851640t*t 1.935724t*1 9.349227t*1 til JA 0.0 1.102700t*2 1.20931N*2 f.4H 681tet 2.815640t*1 1.9357248 1 9.34922Tt*1 StAma J8 100.0 1.102Toct*2 t.< 093141 2 f.465681D t 2.811840D1 3.$80064t

1 1.09049D2 126 JA 0.0 1.4TT570t=2
~~1. 201504t~~
2 ll6MIM e t 2.81584M

1 3.580084t *1 1.095349D 2 6tamG J8 100.0 1.4TT5 7M

2 1.2050.t*2 2.h661Mel 2.8% B6M

1 3.25668tD 1 3.0$1049t e t title : Per 2 tf.)" clAmstte c
thsttwt let 6 * $18 sei in veive j mma S-r9 teue minissa 6 1M 81.3114 set t*/ Seen Irvi 6 Aalet f orce mes6mm 6 60 704.202 i mintass 6 110 26.1912 e k Bene tres & Sheer 2 f orce g mes issa 6 45 264.112 e . 1 n,e minimm 6 49 1.18293 - O Mi - M team traf 6 sheer) force monimm 6 12$ 74.6568 minium 6 41 8.15197 teen EM 6 terem mes6mn 6 117 2 8.1% 64 G min 6 sue 6 el 6.22303 6een Erd A skenentl ,t-mea 6 sus 6 112 99.2191 ,i annleun 6 109 38.5901 4 S ,$een traf A esament3 maalam 6 48 4T8.239 ( VL mieleue 6 124 S t.3114 '? D Some frui t Aalet f orte mentam 6 60 704.202 minimm 6 110 24.1982 E Dean trst 8 Deer! Force g mes tam 6 45 284.312 tt minimm 6 49 1.11293 Dean tr<l B Deer 3 Iorce 4 = G '. maa ina 6 125 74.6368 m i n 4== 6 45 8.11197 4 F 6een trad 8 for s e mea 6mm 6 11F 28.%S84 5y a %b* minim m 6 51 6.94831
~~u***<-~~
~~yi'a Deem tres 8 masent2 V ' metlam 6 til 99.2191 M m(atam 112 26.7922 p met teue 6 47 478.239 U~~
~~Dean tres e nament3~~
~~+3 y ;. _b '- _jh k$ +~~
~~Ma 4~~
Qyd i
L s,
i~
~~. v l ( J' + m o u.,u i,,,te o,..., l-\\TTACHMEn. f.-,". Ib M 7 V L fitte i tow 2 17.5 pit atta SHEET 'D C~~
~~. 1 %~~
j c first mu/ute 56,sery f ate set to vetue i seen ard 4 Asset perse m i n t a, i io) .o.0a3029 maa t an 6 60 704.202 less inst & l',eerl f orce nint aus 1 60 0.50149 ass tam 6 45 264.312 team f ra A Sheor) f orce minim a t tti 27s.395 ?' esa lam 1 12$ 3%$.214 ,/ Seere trd A terred a6ntan 1 13 +12.9894 mei tnse 1 tlF 11.1906 ii tone tid 4 nomenti minimm 1 104 + 12$. k4 maalaus 1 118 234.282 ( Seem trd 4 Ansat1 alnimen i $8 0.4 643 esa sun s 48 478.239 5 s i Seem trd 6 Asist forte ein6mn 1 11 0.64587 + me s ima 6 60 104.202 l Bene trd I thear2 f orce min 6mn 1 $0 0.219M se s t asi 6 0 264.312 ? Deme trW 9 theer) forte m ininue 1 125 315.214 t ma s teum 1 til 278.391 ? lese Erd g f orge minima t it? 11.1906 t ma s t an 6 11F 28.1584 team trd I met 2 a 6 nin si 1 117 234.242
~~a s t an 1~~
~~103 125.044 l Dean led 8 met 3 m in 6 mm 1 60 0.66009 p, ea s t usa 6 67 478.23 P y r-i 7. \\ 't.. ) wX. a I y E -d, a., t: r.t ~k p, 9 k G p, .o e 1 j.-~~
~~. /^~~
g cd.i.. r w 44 Y s . 5 e 1 - hl 1 '\\x,I. ? A f_f1 . s ) ( [ A,j-l- .; 3 v-4q.. O i,: .4 y I %-h?, s,[ ' _.y d 7' p 4_ A.- 3 )# F %a ..,Ne a 4 j [ ,a-- t L cw! A; Clh:(. ~ '/, i , i h.f. e g. $.d. ~ N',.e ?~ ! k. w 6 I W $'h' ?T ' <x4',' '.t. +( y ;., A6 + ' : ;ji .s ge .s
~~' t, w.~~
f6 4 W,
0 ATTACHMENTm M. m Y M* CICO (Nat $15f ta 4316 4 & T F44E6 T I S..__ QF M 9 C. ".1 '1 *" stAnaA9 vereina 4.41 I N Apr 18 th 45:31 N eesert e itement noel j ] - forest stAmotel sortseem ficaeat s t 5 fitte : Pty i 14" OlAmitti t t 4' Output let 1
~~MAD LOAD (04) d etam Ettatef LOADS AstAL~~
~~$ntAt Salas 10slita 6im0 tug Mt h JG i 8 4 MAm 9 v2 v3 at k2 8L3 i 1 JA 0.0 1.M71C0t*2 6.6160071 2 *6.970309t*1 2.994210t *1 2.06251M~~
2 1.T20562t*1 MAMG li 40 100.0 1.MF100t 2 6.61600TI 2 6.9703098 1 a 2. 9942 t M

f

3.199407t e l 4.045608 1 l
~~2 sA 0.0 1.MF t 001 2 6.41600ftal 3.58f60*tet 2.9962tM*t 3.19940ft e t +4.066560t*1 H amG 1 4 st 100.0~~
~~1. p F1004 2 6.61600?t 2 1.5S?604tet~~
2. 99421M

l 5.T69603tet 2.4825$8t l lt 3 sa 0.0 1.p 11 M 2 -0.6160C?t 2 3.325 94t

1 2.996210E*t l.F6%C3tet 2.41255M*1 stAmo Jo 100.0 1.M f100t 2 6.61600TI 2 3.025968t*1 2.994210tet *1.038825t*1 f.239567t*2 l
~~4 JA 0.0 1.66F10M 2 6.61600ft 2 6.0T0401t*1 2.99421M *1 1.02625t*1 4 2395671 2 st6mG JB 100.0 -1.66110M 2 6.616007t'2 6.0f0405t *1~~
2. 9941M e t 1.469r23t*2 5.646449f.2 5 JA 0,0 1.66F1Mi 2 *F.20Tta?t*1 6.02906Ft*1 2.994 21M e t 1.4697238*2 5.MM4 M

2 StAmo JS 100.0 1.u710C1 2 2.20tc8?t 1 4.02906?t*t 2.996210t*1 6.910944t*1 *4.474843(et I
~~6 JA 0.0~~
~~1. W 1004 2 2.20704?t 1 1.019704t*1 2.9941Ct a t 6.910M4t~~
~~1 8.474843t*1 StAMG JB 100.0 1.MT10Ct 2 2.2070871 1 1.019704t*1 *2.994210C+1 3.25T343t*1 1.638243t*0 T JA 0.0~~
~~+2.20 TOME 1 t.66 tos M~~
2 4.5 73575t

1 3.25 '340t

1 *2.994210t*1 1.638283D0 stAmG t
j Je t00.0 2.207Nf ' t.uf088A 2 4.5 T35 75 t e l 3.2573*M*1 4.643M0t e t 1.666124t*0 $ sa 0.0 2.2010Ki 1 .f470f f t 2 f.5 79941t *
~~3.25T140tet 4.M3460tet~~
~~1. 64124t~~
~~0 StAm0 J8 100.0 2.20109c8 1~~
~~1. 2 709!i 2 a,379941t*t 3.2513eM e t 1.322360t*2 1,682195t*0 9~~
A 0.0 2.22TCKt '

667M 81 2 1.0079 fat *2 + 3. 25 04 M

1 1.32220D2 1.682T95t*0 6tAmG t
~~Ja 100.0 2.207090t 1 1.M10$$f 2 1.0019748*2 3.25 T14M *1 1.654997t*2 1.68829M~~
~~0 10 JA 0.0 2.207090t t 5.950ctit 1 +4.853706t*1 + 3.25 04M *1 1.654992t*2 1.688796t*0 6tAMG J8 100.0 2.2070904 1 5.950c818 3~~
~~4. 85370M~~
~~1 1.25 T34M e t 3.590521 ten 1.7041&3t*0 l~~
~~11 JA 0,0 2.20tP9N 1 5.9500811 3~~
~~1. 6945 9t.1 3.25 mot e t 3.590521tel 1.T04183t+0 HAmG 1~~
JS 100.0 2.20109C4 1 5.9500818 3 1.494259D t 3.25 T14M *1 +2.02003TD 0 *t.T1608H+0 4 i 12 J4 0.0 2.20709Cf.1 l,750081t*3 3.lt190tD1 3.25 T34M *1 2.020037t*0 1.T16083t*0 stAmG JB 100.0 2.2070908 1 5.950c81t 3 1.61190TI*1 3.25 n4M *1
~~T.8258t?D 1 1.727983t*0 r~~
~~13 JA 0.0 2.207090t 1 3.950catt 3 6.06418 4 1 3.25 734M *1 T.3258 t ?t *1 1.72F983t*0 stamG st 100.0 2.20/0908 1 5.950081t 1 6.064139t~~
1 1.25G*0tet 1.189199( 4 a l.T35897t

0 t
~~J. f4 JA 0.0~~
2.2070%I 1 4.572321 1 5.693f13t*1 3.25734M *1 1.569199t*2 1.T35897t*0 stAMG Je 100.0 2.207050t.1 4.5?d32t*1 1.493713tet 3.25n40D1 4.lt995D1 9.5102 fM

2 g, '
~~il JA 3.0 2,20FD9CE 1 4.lT6&32t 1 9.038052t+0 +3.2504 Met~~
4.51995 t

1 9.51027M 2 BEAMG Je 100.0 2.20T09CE 1 4.1768521 1 0.038052t*0 3.25T14M *1 1.685383D 1 1.239044t*0 16 44 0.0 4,5fM30t + 1 2.2070871 1 3.890734t*1 1.885 80tet 3.25n43D1 1.239044t*0 stAmo Je 100.0 4.57683Cf t 2.20708?t 1 3.890734 D t 1.685180(* t 2.57875M*1 0.07980TD I 17 Ja 0.0 4.57683't 1 2.2010811 1 1.032016 0 2 1.88538M +1 2.5 7875 M

1 9.07980 Tral stAMG JB 100.0

.l?68324 1 2.20704?t 1 1:32036t*2 1,68538M e t 1.805930t*2 1.7691T82 1 18 JA 0.0 4.5FM 30t 1 1.M4015D 1 1.095357tet 1.885380tet 1.80193 M 4 1.16917M 1 stanc -
~~J8 100.0 4.57683C1 t a.6240158 1 f.095352t*1~~
I. 685 38M

1
~~4. 55512D1 2.T24149D 1 19 JA 0.0 4.5768300 1 1.624015t 1 2.858322D1 1.685380t*1 4.55512t*1 2.T24149D t stAmG 48 100.0 4,5768301 1 1.6260158 t 2.858322tet + 1. 885 3SM~~
~~1 6.0M 42t*0 3.K S?95t 2 20 JA 0.0 4.t ra3M. t 1.6240158 1 3.212930t *0 1.885380D1 6.03842?D 0 ').20879)t 2 stAmG J8 100.0 4.176&3001 l.624015t 1 +3.2129300 0 + 1.885380D 1 +1.206267t*1 3.34590M*1~~
~~{. 21 JA 0.0 4.5764300 1 1.624015t 1 3.91S T37t *1 1.885380D 1 1.20M67t*t 3.365908t*1 4 tam 0 i J8 100.0 4.5 7683M.1~~
~~1. 94015D 1 3.915T37p 1. l.84138M el 6.13514M~~
l 6.4109378 1 22 JA 0.0 4.576a30t.t 7.0990tu.3 3,900t g D 1 t,385380D 6.13574M*1 6.410937t+1 stAnc J6 100.0 6.5?M30t 1 7.09907M 3 3.900142tet 1.845310t*1 2.4552690 0 6.517423D 1 23 JA 0.0 4.5768308 1 1.C99016( 3 1.8t0519tet 1.ts5 3&M

1

2.855269t *0 6.5174 31 1 stAmG JB 100.0 4.Sf6830t 1 7.0990TSt 3 *t.870519t+1 al.685380t*1 *2.520252t*t 6.623909D 1
' 24 JA 0.0 +4.576a300 1 f.099073D 3 2.95910M e t 1.685380t*1 2.1202521*1 6.623909t 1 SEAmG 4 JS 100.0 4.576830t 1 7,0990738 3 2.959106tet 1.685180tet 1.91840T!*1 6.D0395D 1 25 JA 0.0 4.576a30D 1 7.0990tet 3 4.988T29t*1 1.885380tet al.918407t*1 6.T30395D 1 stAnc 48 100.0 4.572301 1 F.099078D 3 4,988729tet 1.885380t*1 9.401501D1 6.836881t 1 26 JA, 0.0 +4.576a30t.t 2.19568D1 5.M3320t*1
~~1. 885380t~~
~~1 +9.401501t*1 *6.8M88tt 1 atAmo JB 100.0 4.576830( 1 2.59756M 1 1.6233201 1 1.BM ucD1 1,8411388*t 1.M1744t.1 y~~
~~j 27 JA 0.0 3.9486r0D 0 2.5915684 1 4.140711t*0 1 k ' " St e t 1.645138tet.t.0824971 1 atAnc y Je 100.0 3.9486?0D0 2.5956M 1 4.740711t*0~~
~~1. L~~
~~.tet 2.864MTt*1 1.13&%0t*1 28 JA 0.0 1.296490t*1 2.5975688 1 1.893823D 1 1.% 3 hotet 2.8M667tel 1.1383 A *1 stAmG Je 100.0 1.296490t~~
~~1 2.59T568t t '1.893823t*1 1.5437400 1 *1.208tS3t*1 1.194223t*1 29 44 0.0 4.1768300 1 2.59 568t 1 s.240944tet 1.9503:0D 1 1.20stS3tet.r.449745t*1 stAMG 4~~
~~JB 100.0 4.57683001 2.59 568D t.s.24c944t*1 +1.95032ctet~~
~~2. t t1051D 2 1.394 h 7t+0~~
~~(- 30 JA 0.0 4.l?6830D1 5.8V11691 3.T.93247D 1 1.M03:04 1 2,13to$1g g. t.394MTD0 EL Amo. Je 100.0 4.5768301 1 5.895769t 3 F.932367t*1 1.950320t*1~~
~~6. 707568D0 1.410079t*0 31 JA 0.0~~
~~+4.576&3001 5.895769D3 2.1264021*1 1.950320(*1 6.707%8t+0 *1.410019D0 6tAMG~~
w
~~.YY &r~~
~~f M~~
~~%y m)p% w.,~ %)~~
k+
V % w.i y4 We.aw ,c ,u. ' ~
m i w%"i; gw ATTACHMENTC . Fw tit 0 (tavet Svltim 4314 6 & F SHECT W or b t he Apr 18 12:45 31 1996 9 q, gq ,j y
~~W eten 4.61 toport Etement h~~
~~J - t$tmAt 1A40 Tot lar/ team ilesent .n., q ry, 4 W.. M- '? 's '?E* a J C - H2 hr 1-~~
~~1 18* OIAmttle~~
$I4m iLtuiei t040$ g 3, tyfl (h 'We ft Ao (c.Aa (ell p /*
~~g. y~~
~~&XtAL tu( At lutat 10al10u MueltG Stacite P v2 v3 af m2 m3 e% JB 100.0 6.lT6510t 1 1.89%?60t~~
~~1 2.126402tet al.95032H+1 4.996106t*1 1.42179tt*0 tt Am N'~~
~~32 da 0.0 % sPSTTM 1 4.51232t 1 1.19875 Met 4.996100 fat *t.950122t*1 *t.621791t*0 lEAmG o de 100.0 l.895T704 3~~
~~.17M32t t 1.19679M*l 4.996100t*1.T.469732t*0 2.41537M*0 r~~
~~33 J4 0.0 1.895T70t 3 4.1TM32t 1 6.443234tel 6.996100t*1 T.669732t*0 2.41$$ TM *0 stAaC JB 100.0 l.8vlTT0t 3 6.1168321 1 -6.463234t*t 4.996100!*1 *1.52&&2$t*2 3.681365t*0 34 JA 0.0~~
~~1. 89% Tf 06 3 6.7484944 1 -1,316T29f*1 4.996100tet t.12&&2$t*2 +3.681365t*0 6tAmG st 100.0 1.89)T7tt 3 6.7606941 1 1.316T2H*t 4.PPo t0M~~
~~1 7.112535t*0 1.419Mit *0 15 Ja 0.0 S.895T70t 3~~
6. f e 9i.96t + 1 9.43194t*0 >&.996100fel T.11253M *0 1.459Mit *0 stamG JS 100.0 S.f95T70t*3 6.f496968 1

9. 63 t 9$ M
0 4.996100t*1 2.11133M

1 al.6500$91 1 36 Ja 0.0 6.76949M 1 1,69%f6H 3 +3.98763ttet..t.1183 30t

1 4.9961Mtet al.610059t 1 stAMG JS 100.0 6.7496Mt 1
~~%.89176H'3 3.981611t*l 2.118330t*l 9.813423t*0 1.56423(a t 37 Ja 0.0 6.7664ect t.%.895T698al 8.21T2 Sit *1 +2.118330E*1 + 9.81342 M~~
0 1.16162M*1 etAMG 48 100.0 6.7496*M 1 1.875764 43 8.2172$1t

l 2.11833Nel 1.131122t*2 1.4 T316M

1 38 Ja 0.0 6.T69690t 1 2.35$02tt 2 0.19106Tiel 2.118330t*1 1.331172t*2 1.47316M*1 StAMG Ja 100.0 6.74949Ct 1 2.3350211 2 8.59106?t*t 2.11833Ct*1 1.0375T7t*1
$.9213471 1 39 JA 0.0 6.T49690t 1 2.311021t 2 6.01818ttet 2.118330 fat 3.03 T1TTle t $.v21347t*1 StAMG JS 100.0 6.169600E 1 2.3)lC21t42 6.018t#2tet 2.lta33 Clot 1,66T2128 2 6.361601tal 60 sa 0.0 .. f8 ?6e0( + 2 1.68 19ft>3 t.23105Tt*1 1.3FIF70s*1 2.1T34918*I 2.11015Tt 1 StAmG JS 100.0 %.7876901 2 f.684t97t*3 1.2310S?t*1
~~1. 3~~
t TTot

1 4.911935tal 2.1436528 1
~~&l Ja 0.0 6.T876%t 2 1.6841971 3 f.822$T3t*1 1.311T7M e t 4.911931t*1 2.$436$1t*1 8tAMG Ja '00.0 4.T&7690t 2 1.4841971 3 + t.8225 73t~~
1 1,3FITTot*l 8.387613t*0 2.5TT1&Trat 42 JA 0.0 2.907950t 2 3.8062611 2 3.M197M

1 2.111M0t*0 1.193333t*1 2.1TF147t*1 stAmG JD 100.0 2.90T9808+2 3.806241t 2 3.66397 Wet *2.151640t*0 1.1041T&t*0 2.T541388 1 63 JA 0.0 6.45670Ct 1 1.4112191 2 3.7782038*1

1.288940t

1 1.201588t*2 3.8S M'4t 1 SLAMG e
Je 100.0 +6.4581005 1 1,61123H.2 3.778203t*1 1.29894 M + l +6.4T94T3tet 3.52396t *1 64 JA 0.0 6.458T00t*1 1.61123M 2 6.02093Tiel af.292940t*1 4.479473t*1 3.1 23968 1 StAmG 48 100.0 +6.458100( 1 1.65t239t 2 6.02093Tt*1 1.298940t*1 3.6380584+1 3.3TT1564 1 h, fille : PeoP 1 it* Otamtfie Cutput let 1
~~OtAD LOAD 40t) set 10 value A{'~~
~~let mas /mte Smary tot >te minina 1 2T +3.94847 Dens Erd A Antal force man inse 1 28 12.9649 h minina 1 36 0.6T691 !c Seem tre A theerl f orce meninse i 16 0.41768 l-m 4 Nam i IT~~
~~103.204 4~~
~~team trd A theer3 f orce masina 1 9 100.T97 minin a 1 32 +49.961~~
'~
~~29* ,6een trd A f ortue menina 1 1 29.9421 b min 6nse 1 18~~
~~180.593~~
~~~, a Q Dean Ltd A nammt2 3 masina 1 30 218.101 h J. minina 1 28 11.3836 14 Seem trd A moment 3 manieue 1 16 1.7359 D. '.N 9 minina 1 28~~
~~12.9649~~
~~$'T D ' ~ Deem tid 8 Aalet f orte ma n teue 1 27 3.9486F minieun 1 16 0.45T68 lese Erd 8 theer2 f orce masina 1 36 0.6?&91 mininen 1 9~~
~~t00.79T j~~
~~I* Deem trd 8 thear) f orce , = (/ Masina 1 17 103.204 nint eum 1 1 29.9421 ^ f '. (T', Beem trd 8 forme o j men f oun 1 32 49.961 minleum 1 29~~
~~218.101 M~~
~~lean Erd t enament2 mes teue i 11 180.%93 R M , '. j [ minin n 1 13 1.T319 '} ge~~
~~- ^'~~
~~Seen trd a nament3 menina i 28 11.9622 j[ N NIN m,A kn, am g; wu iy)P Y q g3 N( Y a~~
~~+%.p* JL '(*$~~
.M 4 tr jp w - ; ey; M IW
ATTACHMENT + t' 4 p. m; mT + N 2 hbb1 otto ttwat listtu 4316 6 i T D C 411 f 3, t. tici. 1 me 1 is+ ot Aatne l .). atAu itluteI LOA 0s I ^ k-Agggt $ptA8 $r!At 108SitA M k0lbG M@G i a-a v2 v3 at m2 M ., g-, ,j (f was ?w ' ' ' ' + 1 JA 0.0 1.311500D2 2.35514M
~~I 1.672901t*1 F.18944M*0 4.950203D1 6.196L56t*2 MAm8 I~~
~~I Je 100.0 1.311500D2 2.35514001 1.67290tt*1 1.189450t *0 T.6811&2t*0 6.914411'D 2 2 JA 0.0~~
~~1. 274 %M~~
~~2 2.291301D1 8.e t 000t *0 TJ8948t*0 T.C&M*0 6MW2 HW_~~
~~J3 100.0~~
~~1. 2 T416M~~
~~2 2.291331t*1~~
~~8. 610 T3M~~
0 T.18h m *0 1.3&&8W'1 T.093045t*2 3 JA 0.0 1.20540D2 2.046133 tat T.2626MD0 T. 8894&N

0 1.38481M*1 T.093085D 2 H AMC J6 100.0 1.20M60D 2 2.04135t a l T.262675D0 T.18h5M + 0 2.510205t*0 1.3404MD2
~~'I 4 JA 0.0 1.lT9980D2 2.021 m D t 1.456909D 1 T.189'6M~~
~~0 2.510205t*0 T.M04MD2 MAmG~~
= J3 100.0 1.1T9930D2 2.021366tet 1.65H09D1 T.18H5M *0 3.525UD1 F.628 m *2 5 JA 0.0 1.105480t*2 2.5 320'9D 2 1.u895tt e t T.t89448t*0 3.5275TT!*1 T 6608700 2 MAmo Jo 100.0 1.1054M D 2 2.532WD2 f M 8'51tal I 189'50t*0
~~1. M3321t*1 2.1T& TT9t~~
~~2 6 44 0.0 1.02650t*2 2.331 T+602 2.5M62tt*0 T.18h&M + 0 1.23321t *1 2.116TT9t*2 StAMG t~~
~~as 100.0 1.068650D 2 2.13 t T&4D 2 2.56062 tt *0 T.189450t*0 9.597383D0 1.002841D 3 N T JA 0.0 2.1M240t~~
~~2 1.0553s8D2 t.100668D 1 9.59738M *0 T.189453D0 1.002841t*3 StAmG Y~~
~~Je 100.0 2.1M260D 2 1.055368D2 1.10046M~~
~~1 L HP38M *0 I J2546H* t 8.5 m *2 5 Ja 0.0 2.02W D2~~
~~1. 04276M~~
2 2.06flSM *1 9.H T380D0 1.12546M*1 8.519699t*2 HAmG JS 100.0 2.028440D2 1.4276CD 2 2.061156t*l 9.59D8Pf *0 3.183204t

1 T.652634t*2 9 JA 0,0 1,969280t *2
~~1. *379'At~~
2
~~2. 420960t~~
~~1 9.HT380D0 3.183204t +1 T.652634D 2 SJAMG Ja 100.0 1.96N80D2 1.03795 CD 2 2.6220D 1 LSU380t*0 33842M*1 T.376MM*2 5~~
~~10 JA 0.0 1.594620t*2 9.TC2001D1 1.1 TT31M~~
~~1 L S U18M +0 3J842M*1 T.3T6 MODI stAmG i-J8 100.0 1.594620D2~~
9. 702001D 1

1. lTT118t e l 9.59T380t*0 8.60437FE+0 5.339994t*2 4
~~11 JA 0.0 1.480550D2 9 62672TI'l . W 187t*0 9.597380t*0~~
8. 8043T21 0 5.339994t*2 8t AJeG J8 100.0

1. 66055 M
~~2 J.62672*t*t~~
~~., W 387t *0 9.59738cD0 4.982 th t~~
0 4.1184 TM

2 l.
~~12 JA 0.0 1.293000t*2 9.626049tal 9.24WTD0 9.59738M +0 4.982T94D0 4 d WTot *2 HAMG ~ W Je 100.0 1.29300002 9.62604901 L249M2D0 9.HTJ8M *0 2.02U65D1 3.2W56Tt~~
~~2 i~~
~~F 13 JA 0.0 1.221630D2 9.707826t +1 1.&61263t*1 9.59 380D 0 2.02 TT6H +1 3.2W%Tt~~
~~2 H amG 2~~
~~Je 100.0 f.2*1630t*2 9.707826tet 1.661243tal 9.59 T380D 0 3.92u35DI 3.265225t*2 16 44 0.0 9.01260001 5.122991D 1~~
~~1. 7104 T9D )~~
9.597380t*0 3.924 35D 1 3.245225D2 StAMG JS 100.0 9.012McD 1 5.12299tt el 1.110419tel 9.597380D 0 4.T36225D 1 4.06M61t*2 1-15 JA 0.0 8.762380D 1 5.0M5Fotel 1.0 T0948D 1 9.59 T38M+0 4.736225t*1 4.063661t*2 etAnc 1*. at 100.0 8.TL2380t+1 5.064570D1 1.070968D1 9.597360D0 T.680345D1 4.81T475t*2 16 JA 0.0 5.381120t*1 8.9163498 1 1.454116D1 T.680mD1
~~9. HUB 3D0 4.81T&5D2 HANG j ;;~~
~~J4 100.0 5.38112CD 1 8.916349D I 1.&S4516D 1 T.68034M~~
1 1.2TT294t

1 3.6954 TTD 2 17 JA 0.0 6.696G M al 9.'1048.'t a i 2.55549D1 T.680 M L*)
~~1.2 TT294D1 3.6954TTt*2 HAmG J8 100.0 6.498440D 1 9.210982tel~~
~~2. 55549D t 1.6803400 1 5.229958t*1 3.06T308D2 18 JA. 0.0 9.185580D 1 1.092997t*2 1,774091D1 T.680 m t*1 5.229958D1 3.067308D2 stAmG l~~
~~J8 100.0 9.185580D1 1.09299 TD 2~~
~~1. TT40914 + 1 T.680340D 1 2.459T&Mel 1.T96629D2 b ;-~~
~~19 J4 0.0 1.063540D2 9.267910D1 5.474397D9 T.680 m t+1 2.459746D 1 1.198629t+2 8tAmG k~ 48 100.0 1.043540D2 9.267810tel 8.6 T& 39 PE~~
~~0 T,68034CD 1 1.652131t e t 2.249331D 2 9-20 JA 0.0 1.120440D2 6.013893tel 5.0840800 T.680 m t+1 1.65213 tD1 2.249331D2 StamG JS 100.0~~
~~1. ' 20440t~~
~~2 8.013893D 1 5.081608D 0 T 6803400 1 1.6142&M*1 3.43&399D 2 21 JA 0.0 1.251260t*2 5.624TTit=1 1.071018tet T.680mD1 1.61424M*1 3.438399t*2 atAmG W~~
~~J8 100.0 1.251260D2 5.676 TTit *1 1.071018D 1 T.6o0140D1 2.45941M~~
~~1 4.412655D 2 22 JA 0.0 1.535700D 2~~
~~6. 89%55 t~~
~~1 1.584119t e l T.680 W tet 2.4594tM*1 4.412455D 2 StheG i i J8 100.0 1.535700D2~~
~~6. 89%55t~~
1 1.586119t*1 T.68034 ^t

1
~~3. l45427D0 4.964942D 2 23 JA 0.0 1.600820t+2 5.Tunit*1 1.3 W 57t*1 T.680ND1 3.%542TD0 4.964942t*2 ttAMG JB 100.0 1.60G820D2 5.766 51t*1 1.3W52t~~
~~1 T 680340 D 1 1.98680M*1 5.6411TTD 2 24 JA 0.0 1.M63TOD 2 3.932&S3tel 1.384WD 1 T.680mD )~~
1.986803t*1 5.4411Mt+2 stAmo JB 100.0 1.T56370D2 3.932633D1 1.384 W t*t T.680340D1 3.694687t*1 5.504967t*2 25 JA 0.0 9.8215900 2 3,865737t*1 1.664723(*1 T.680MD1 3.69468Tt*1 5.50496TD2 MAMG JS 100.0 1.821890D 2 3.865737t+1 1.66&T23D 1 T.680340t+1 5.848175t*1 5.41715tt*2 q 26 JA 0.0 2.115790D2 T.928131E+1 6.370932t*1 T.680 (*1 5.84815 D 1 5.41T151t*2 HNcG c J8 100.0 2.11ST90D2 1.928531t+1 6.370932D1 T.680 Mot *1 1.TT9850D2 5.615085D2 ,y u-27 JA 0.0 2.2VJ240D2 T.7121&SDt 8.456811t+1 3.07965TT*2 1.n9850**2 4.n5174t*2 steG L JS 100.0 2.2002.0D 2 1.112188D1 8.456811t*1 3.079650D 2 5.8985ktet 4.596&O6t*2 28 JA 0.0 2.274500D2 T 94378tt*1 8.995266D 1 3.07965Tt+2 L 898%4t
1 4.59840M

2 Stanc
~~,g JB 100.0 2.276500D2 T.943731te t 8.995266D 1 3.079450D 2 2.13266102 4.628029D 2 29 JA 0.0 2.549610D 2 9.11 t T16t *1 6.517905t*1 1.201979t*2 2.132H1DE 5.436069D2 htheG y Ja 100.0 2.5496TM~~
~~2 9.1117164*1 64517905D1 1.201980t*2 1.MT574t*2 5.000213D 2 i~~
30 JA 0.0 J.928210D2 9,83805M *1 4.020690D 1 1.201979t*2 1.347574D2 5.080213D2 SEAMG 48 100.0 2.928210D2 9,8880558 1 4.020690D 1 1.201980D 2 3.41TMit*1 6.4H 38D 2 31 JA 0.0 3.10M30D2 9.&O95)TD I 2.094665t*1 1.201979D2 3.41TM1D1 6.MM38D2 til.MG - , q (. Ja 100.0 3.10h30D2 9.409)37t +1 2.09486H+1 1.201980D2 2.46M63t*1 T.6590/ TD 2 32 JA 0.0 9.1M070t*1 3.2033i58 2 1.%29 5t+1 2.668659t*1 1.20197M
~~2 T.85904TD2 DEAMG J8 100.0 9.164070D 1 3.203315t*2 1.562975t*1 2.468660D 1 8.939611D1 3.685030D 2~~
,,{ W' k M(.#[ gg69 'M M g?
ATTACHMENTM..e w m og u - N; %g m o 9 & * $ 1-} } g ~ t ST AAsp verslen 4.41 the Apr 18 12:45:43 19M { k' Report i E lement model t I-forset t staa0 tut sar/sene itement i l j l 's 'J title Pt0P 1 18' OlAmitta Cutgaat Set 2
~~06t l~~
~~6fAa tLtu(91 L040S 2 i anlAt $ntat $nt At 10ftlou Mu0lmG MuDlb4 I stAm P v2 v3 mi m2 m3 33 JA 0.0 9.552680tet 3.3062twel 3.032335t*1 2.uS65 M *1 8.9396 tit *1 3.685030t*2 HAmo Je 100.0 9.552480t*1~~
~~3. 3062 TM *2 3.032335tet 2.468M0t*1 9.509771tet 9.24404tt*2 34 JA 0.0 1.09368',t~~
2 2.230440t*2 1.59587M

t 2.468659t*1 9.509771tet 9.246041t*2 HamG j;'
~~Ja 100.0 1.093580t*2 2.23044M~~
~~2 1.1958? Met 2.4M M0t*1 6.124098t*1 5.481414t*2 35 JA 0.0 1.321964*2 2.1 2652t*2~~
~~1. 26914 0t + 1 2.4 2659tal 6.12409M *1 5.441414t*2 8tAmG i~~
~~l JS 100.0 1.3219604 2 2.196452 t~~
2 1.269140f*1 2.4M66Ct

1 2.T252Ntet 8.04T08N*2 le JA 0.0 2.1853708 2 1.65189&t*2 1.fBC21&tet 2.72529M*1 2.468M3t*1 8.047082t*2 SLAmo Je 100.0 2.18537tt*2 1.65 t 99M

2
1. 980274 + 1 2.T25300tet 4.T34317t*1 6.121260t*2 37 JA 0.0 2.172350t*2 t.626857t*2 2.W32M e t

2. 72529M
t 4.73431Tt*1 6.121260(*2 HAMC JS 100.0 2.17235M

2 1.626457t*2 2.M4322t*1 2.725300tet 8.k242M*1 4.065490t*2 38 JA 0.0 2.1M06M*2 1.k1141t*2 2.3126958*1
~~2. T2529M e t 8.M242M~~
~~t 4.06549nt*2 MAMG Je 100.0 2.14506ct*2 1.6 1161t*2 2.312695tal 2.72530C4*1 6.08183ed e t 2.35T150t*2 l~~
~~39 JA 0,0 2.16T5301 2~~
~~1. T2307M~~
2
~~1. 74 91&M~~
1
~~2. T2129M e t 6.08183M e t 2.351150t*2 stAmt~~
~~+81E0 2.1675308 2~~
~~1. T2307M~~
~~2 1.1691&M e t 2.7253 M et 5.422583tet 3.19079M*2 l~~
~~60 JA 0.0 2.385290E*2 3.98114Het 1.048737t*0~~
~~5. Tro r6M *0 3.344029tet 1.95813M~~
2 8tAmo Je ICO.0 2.3852901 2 3.18116 4 *1 T.068T37t*0 5.770760t*0 2.24054M e t 1.459962t*2 41 JA 0.0 2.42676M

2 3.T20&O&t*t f.9k840t+0
~~5. TT076M~~
0 2.2605484*1 1.45996M

2 6tAmo J8 100.0 2.6267801 2 3.T2060&tal 7.464860t*0 5.T70160t*0 6.760754t*0 1.51192M*2 i
~~5 42 JA 0,0 1.118200t*2 1.785f82t*2 1.119592t~~
~~t 5.0450571*0 T.294053t*0 1.11192M* 2 DEAmo 1~~
~~J8 100.0 1.118Z00t*2 1.785f82t*2 1.11959 Met 5.0tS06M~~
~~O 3.6T9136t*0 2.0611138 2 43 JA 0.0 3.565370t*2 6.037567tet~~
~~9. TT916M~~
~~0 6.64556M*0~~
~~3. 44256M~~
~~t 1.900715t*2 etAmG l~~
~~JS 100.0 3.565370t*2 4.03756Tiet~~
~~9. 779 t &8t~~
0 6.4 568x+0 1.599u rtal 2.259608t*2 44 JA 0.0 3.18151tt*2 4.67001Sf*1 1.690719t+1 6.6*5130t*0 1.599MT!*t 2.25960M*2 4tAmG Je 100.0 3.58151Cte2 a.67001 Blat 1.690719tal 6.645&Sct

0 1.135128tet 2.650189t*2 j
~~fille FROP 1 18' DIAmttta g Cutput let 2~~
~~04 f~~
Set EAX/nts 5tsamery table let 10 vetue Seem trd A Asist f orce minina 2 16 53.8112 masina 2 44 358.151 i 1 y Seam trd A theer2 forte a 6 n tam 2 4 20.2137 mestam 2 33 330,628 g< l. H sean trd A theor3 rw ee minina 2 6 2.56062 menina 2 28 89.9521
~~h. i.~~
~~l Seen trd A for@e ulninn 2 42 5.08506 a ) ?- ma.taus 2 27 307.9M~~
~~1.,~~
[ 4 Bees 4rd A manent2 minina 2 4 2.51021 .A-me Inn 2 2J 213.266 l. O{g.,t Dean trd A Nament) mint ase 2 41 145.996 i 1 masina 2 1 1002.64 %t Seam Erd 8 Asial Force ulnina 2 13 53.8112 i me: Inn 2 44 358.151 ,g a Beam Erd B Shear 2 Force u t niaan 2 4 20.2137 s mosiam 2 33 330.628 t (N Seam trd 8 theor3 force ulaina 2 6 2.56062 mast am 2 23 39.952T ,j O , Beam ind s f orme a 6nina 2 42 5.08506 4-maaina 2 27 307.965 > + ' ' ' S. W ' Sean Erd 8 momenti minina 2 3 2.51021 i @,'l Maalass 2 28 213.264 Seen Erd 3 saanent) minina 2 40 145.996 ,I g, Jt ma a l**m 2 6 1002.64 3* Iltte : en 18' pl Ams tte m . ~ytsei.or1 y W e 98Am ILtutof LOADS c*g gen. 3, d;*y ~ s. t AtlAL sutA4 ShtAt 10R$!04 Mh0lkC Stu0 lug -N MAM P v2 43 mi m2 m3 s l _4 [ 1 1 JA 0.0 2.06584M
~~2 3.94 W ot*1 1.463859t*1 6.29TT29t*0 4.331815t*1 1.02049t*3 HAMG l~~
gW 48 100.0 2.06584M*2 3.94 W Met 1.463859t*t 6.297T30t*0 6.726506t*0 1.035290t*3 2 JA 0.0 2.001930(*2 3.82265M*1 F.535638t*0 4,297T29t*0 6.726506t*0 1,035290t*3 stApac 1 l JS 100.0 2.00193M* 2 3.a22658tet 1.135638t*0 6.29773ct*0 1.218975t*t 1.059764t*3 l' &l$2 l m.. w:GWR jt I' & y;. o ym,. i - -r - i 33 q%e .e
ATTACHMENT *N f 9
~~I w"'.. s tic 0 CUv&C lolfte 4316*6 & T gg %y~~
~~'Id wwe+ 4' 1Na Apr 18 12:45:67 1996 Q C. * $119, 31Atmap veetien 4.61 lepott t ttenent g' stedel t s terest StA40tht teF/ tete Element J3. title Pe0P 1 te* 9t Amitte thaput let 6~~
~~558 y~~
~~Stan ItIat41 40A38 /, ul At tatat Sm4 A8 toallom stuotoG M uotb4 P til v3 at m2 a0 N 3 JA 0.0 1.84745Ct~~
~~2 3.3136T3D t 6.355743t*0 6.297729D0 1.211975t*1 1.059764te! St Apet O,~~
~~stAsl Je 100.0 1.88745cD 2 3.313673t*1 . 355T&3t*0 6.29773M*0 2.23964Tt*0 1.09652M~~
3 4 JA 0.0 1.83909002 3.18704 1 1 1.2 T4 H TD1 6.297T29t*d 2.23964Tt*U l.096526D 3 DDMG JB iM.0 1.839090D2 1.18 T044D t 1.274827tet 6.29773M*0

08T259tet 1.1644&M

3 5
~~JA 0.0~~
~~1. fl073M~~
2 3.79025M*2 f.2TitMD1 6 a97729t*0 3.08T254

1 1.164&tD) 6tAmG JS 100.0 1.T10T30D 2 3,T9025N*2 f. 2119Mie t 4.29 FT3M *0 1.525297D 1 3.44 T257D 2 6 JA 0.0 1.M M 80t*2 3.48904 tP2
~~2. 44504M *0 6.297729D 0 1.525297D1 3.44T257D2 6t A C JB it0.0 1.kM80t~~
~~2 3.&t904tt*2~~
~~2. 4650&M~~
0 6.29TT30D 0 1.1351T001 1.309397D3 7 JA 0.0 3.2 T411M

2 1.62323T1 2 9.66M4800 1.135tTM*1 6.297130f*0 1.509397D 3 tramG JB 100.0 3.274110D2 1.62323TD2 9.696448t*0 1.135tTM *1 1.00H6T!*1 1.2828T003 8
~~JA 0.0 3.03542M~~
2 1.59709 tP 2 1.80TPSTiel 1.1351 Tot **
~~1,00826TD1 1.282870t*3 6tAMG st 100.0 3.035420D2 1.59 T09 t t~~
~~2 f.80T957tet 1.135110 0 1 2.606223t*n 1.15404M*3 9~~
~~JA 0.0 2.947260D 2 1.566442D2 2.tN500D1 9.135170t*1 2.806223t*1 1.1540&M*3 stAMG Je 100.0 2.64T260t*2 1.586442t*2 2.1N50001 1.1351T0D1 3.50518M *1 1.1132TM*3 10 JA 0.0 2.3H82M~~
~~2 L4 TOT 24t*2 L C3 rT04D t 1.135 t TM *1 3.505th0t*1 1.1132TN*3 st Asoc JB 100.0 2.392820t*2~~
~~1. 6 TC T2.D 2 t. 05 TT04 t~~
1 1.1351TM*1 8.12 &540D 0 0.1H T06t*2 11 Ja 0.0 2.225950t

2 1 *S1169D 2

.4099760 0 1.1351TM*1 8.12454M *0 0.1H TOM

2 StAMG JS 100.0 2.H5950D 2 1.*51165D2

.* 099 76D 0 1.135 t TM *1 8.21k92t*0 6.441815t*2 1
12 JA 0.0 1.95&l30D 2 1.63t T&4t < 8.303016D0 1.135810D1 8.2164Ht*0 6.441815t*2 atAmG J6 100.0 1.t54930t*2 1.439744D 2 8.303016t*0 1.1351T00 1 2.048T1t*1 5.324Tl?t*2 t-43 JA 0.0 1.8533rct*2 1.4495 t TD 2 1.290338D1 1.1351T001 2.066a11D 1 5.324T57t*2 6tAmG Je 100.0 1.8533 T00 2 1.4495tT!*2 t.290338tet 1.135170D 1 3.283T5t
1 5.2895TM

2 14 JA 0.0 1.426820D2 8.241073D t 2.05012601 1.135tTM*1 3.k&375t *1 5.2095TM

2 BEAMG JC 100.0 1.426820D2 8.241873t*t 2.0501264*)
~~1.135170t*1 T.5%451D1 6.4&O6TTD 2 m 13 JA O.0 1.418270D 2 8.02444te t 1.712276tel 9.135 t TM~~
~~1 T.53445TD1 6.4406TTI 2 6tAssG Je 100.0 1.418270D 2 8.0264*.8D1~~
~~1. T1H TM~~
1 1.135tTOD1 1.264053D2 T.5?M3M

2 s
16 Ja 0.0 0.45500D1 1.451983t*2 1.995299D t 1.244053t*2 1.135170t*1 T.51M18D2 ttAmG J8 100.9 8.45590E*1 1.45 t 98M *2 f.995299tel 1.2&&c50f*2 1.905305t*1 5.T28983DI if JA 0.0 1.018J30C+2 1.502540D2 2.939372D1 1.264053t*2 1.90530$D1 5.T2890D2 stAMG Ja 100.0 1.018330D2 1.502540D2 2.939372D1 1.24405M *2 6.119109t*1 4.6%404t*2 it JA 0.0 1.4503200 2 1.719378t*2 1.687048D 1 1.244053D2 6.1191090 1 4.04404t
~~2 stAmo Je 100.0 1.450320t*2 1.T19378D 2 1.6670&8D i 1.244050D 2 ! TT301Ttal 2.T91750D2 19 JA 0.0 1.653090D 2~~
~~1. 46 T26M~~
~~2 9.929839t*0 1.244053D 2~~
3. /T30 t TD1 2.791750 0 2 StAac Je 100.0 1.653090D 2 1.4T26362 9.929839D 0 t.24405002 2.818U6D1 3.695T0M*2 20 JA 0.0 1 T77990D 2 1.212129t*2 S.0160%f*0 1.2&&C53D2 2.818826D1 3.695706D2 SEAM 4 JS 100.0 1.TTT990t*2 1.272T29D2 8.016094D0 1.24405M*2 2.712055D1 5.01491t*2 j
~~21 JA 0.0 1.WO630D 2 0.994943D 1 f.tl9038tet 1.2&40538 4 2.712055D1 5.631491D2 DEAm4 ti Je 100.0 1.990630t 2 8.994941D I 1.159C 3M~~
~~1 1.2440*0D 2 3.690549D1 T.188TT5t*2~~
[ H JA 0.0 2.453410D2 1.05813M*2 2.24785 tD I 1.244053t*2 3.499569f*1 T.168775t*2 stAmc JS 100.0 2.45a410D2 1.050136D2 2.241851DI 1.2M050t*2 5.13766800 8.020392O 2 h,. 23 J4 0.0 2.559400D2 8 9623280 1 2.090134D1 1.244053D 2 5.131668t*0 8.020392t*7 stAmG 's Ja 100.0 2.559400D2 8.9H328Dt 2.090134D 1 1.2&&050D 2 3.099855D 1 8.7254T9D 2 24 JA 0.0 2.812560D 2 6.581301D t 2.021854tal 1.264053t*2 3.099855tel 8.T25479D 2 SEApeG Je 100.0 2.812560D 2 6.581301t*1 2.021854t*1 1.244050D 2 5.938809D 1 8.7981T4t*2 25 JA 0.0 2.919210D2 6.610306t*1 2.139M?D t 1.244053D2 5.936809f*1 8.79tt T&t* 2 SDJe4 Je 100.0 2.91H10t*2 6.61030AD 1 2.139643D 1 1.244050t*2 8.935021t*1 8.6544M
~~2 26 JA 0.C 3.3975T0D2 1.24265 D2 1.02456TD2 1.244053D2 8.93502tt*1 8.65& MOD 2 etAm4~~
~~%s JD 100.0 3.1975TOD2 1.24 654D i 1.0**45671 4 1.24405DE*2 2.897660D 2 8.864043t*2 21 JA 0.0 3.543170D 2 f.23300 0 2 1.35188 tD2 4.85M86D 2 2.89T660D2 T.51T392t*2 et weG = JB 100.0 3.54317002~~
~~1. 23300M~~
2 1.351881D 2 4.85N4D2 1.00M19t

2 7.203543t*2 28 JA 0.0 3.M3090(4 1.2704 t tD2 1.438632D2 4.852286D2 1.006419D2 7.203543D 2 DEApeG Je 100.0 1,663090D2 1.270411D2 t.43863M

2 4.852290D2 3.4049Ut*2 7.24939M4 29 JA 0.0 6.101690t*1 1,449143(4 1.021991D 2 1.90M60D 2 3.&049278 4 8.512034t*2 ttAMG Je 100.0 4.101690t*!
1.449143t*2 1.02799 tt 4 1.908860D2 2.140604( 4 T.18 '250D 2 30 JA 0.0 4.1152900 2 l.672tND2 6.248572t i 1.90M60D 2 2.140604t4 T.98N1002 8(AMG JS 100.0 4.115290D 2 1 H2122t*2 6.248572D 1 1.908860D2 5.551803D1 1.00435M*3 , ' 11 JA 0.0 5.00004M*2 . 562497t*2 3.379018D1 1.908860D 2 5.551803D1 1.00435M* 3 StamG = <( JS 100.0 5.000040t*2 1.562497t*2 3.379078Dt 1.908860D 2 ' 3.TT8000D 1 1.2425T9D 3 + .( 32 JA 0.0 1.508MnD 2 5.i6195tt*2 2.454 Trote t 3.TTT997t e l 1.90&s58D 2 1.2425790 3 stAmc J8 100.0 1.508640t*2 5.161951( 4 2.454 TTODI 3.775000D 1 1.433444D 2 6.11T362t*2 33 Ja 0.0 1.532950D2 5.32922184
~~4. 548891t *1 3.TTT997t*1 1.433444D2 6.11736214 StAMG 3-@w&.Tw Ok pg gn~~
&,&,f W D W rf 'w e W;d % dM gw t. h. i W?.%- %g, ~ _ -, _ _ _ _
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~~s inse 6~~
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ML20210E320

Text

0. 5 X RJfo i X 11

=

0.256 + 0.328X(W/T)X(Fy/E)**0.5

0.256 + 0.328X(W/T)X(Fy/E)**0.5

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