ML20210E320
| ML20210E320 | |
| Person / Time | |
|---|---|
| Site: | Fermi  |
| Issue date: | 06/11/1996 |
| From: | Chiou C, Yu H WISCONSIN PUBLIC SERVICE CORP. |
| To: | |
| Shared Package | |
| ML20134M106 | List: |
| References | |
| DC-5773, DC-5773-R, DC-5773-R00, NUDOCS 9611250099 | |
| Download: ML20210E320 (125) | |
Text
{{#Wiki_filter:_ _ _ _ _ . _ - - _ _ _ _ _ _ _ _ . _ _ _ _ _ _ _ _ - _ _ . Enclosure 4 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)
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4 DBim CALCt'LAllON COVER SilEET et.os 60 ofary PageI me%.wg 3 -w+A ~ 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
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[ Hochanical/ Civil lI) 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
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40% M w.G - '*4~ , j ;-f ~ M) Restsion Summary m. x . Original inuuc. Effective section property calculations and evaluation of 20$'LJ..' 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. i{ h This calculation in part of the basis for EDP-28147. j hd PART.': PREPARA T10N. ret 1EH*. AND APPROl'AL I Prepared us C H uA/C+- YI CHION A) SiFn [1l 6 4' N - I' #16', Date ib YM Date i,WJ Vrso6 Cbeeked IIy e .. Q B) Sign ll0)l-dudyLW $A p 7
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Table of Contents
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- Purpose e ' '*
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' Methcdology c II t
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$b, '} Refenners .
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![:,N; ;. (A) Effecttive Section Properties for Rectangular Ducts Overall Duct Stress Evaluations for Hectangular Docts 13 38 yd (ii)
Evaluation of ACME leek 1.ongitudinal Seams for Round Ducts 71t 4 (C) en.. ft ~ kg Atuchments u o@ M '
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M s { fg' . Attachment A: Summary of incam Element leads for System 43141 9 1. 12c W Summary of Ikam Element leads for System 43162 8 j e Attachment 11: 1 Summary of iteam Element Loads for System 43163 5 ' _,2 E [' Attachment C: n' ; s?w
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Attachment D: Summary of Ikam Element lads for System 43166 l 4j y
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Attachment E Summary Of 11eam Element Loads for System 43167 21 ) m T I h[ , Attachment F: Duct Database 3 9 3 N(hk, g ,m .
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[ 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.
l The overall revalidation program, referred to as the *CCllVAC Concem Resolution Task" is an 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. 4 Pressure calculations are contained in calculations DC 5714 and DC 5758, (Ref. 3 & 4). De results o 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 on the drawing series where they appear, to facilitate correlation. a
- NON RlGID DUCT AND DUCI' SUPPORT _SYSTDIS;
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> ,w. 7 STRING ANALYSES, SUPPORT AND ANCli.QRAGE EVALUATIONS
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DC 5762 DC 5763 Generic Evaluations 2268 System Series '2, x 2848 System Series 02 DC 5764 2S49 and 4126 System Series a b DC 5765 > 4 y fb 56 ; DC 2766 DC-S767 2850 System Series 4316 System Series i C 'c Mk M ' Q < EFFECTIVE SECTION CALCULATIONS AND DUCT EVALUATIONS 4 My o A h: Doct Skin Stress Evaluations Under internal Pressure t , _ Q1 DC 5768 W :' i J.W DC 5770 2268 and 2848 System Series a Q p, Q& t ..
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DC 5772 2850 System Series ll 4316 System Series l' i DC 5773 1 1 s
) ElGID DUCT AND DfE_ SUPPORT SXSTEM EVALUATIONS ;
s j h' ' DC 5774 Rigid Doct and Duct Supporu l i .; ; ) i' IDGT.NI.DE_CONDlIlONLYALVATIONSDEfillELLSAEEIY_F ELATED _D_UCT AND D 1 SUPPORT SYSTEMS l :
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'nds calculation contains the pr<xess, methodology and results of rectangular duct 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 r- 43163,43166, and 43147. String analysis systems referred to above correspond ) t
" 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 b Duct string system 43166 has one (1) round duct site of 17.50' diameters as we f rectangular duct sire 16*x16*. Round duct wenion propedies are included in C l
(Ref. 6), and the structural adequacy of round duct has be
, (Ref. 5).
evaluations of rectangular duct (including the calculations of effectu e sect;on pro in this calculation bawd on the string analysis results contained in Attachment D o t ) There are two (2) wyc sections (Q-344 and Q-348) in string analysis system 431 configuration of wyc section Q344 was utilized in duct panel stress evaluation 4 internal pressure of 14' v.ater gage. The efore, the acceptability nf wyc " m section the as built configuration.
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Duct string system 43147 has Iwo ( ) round duct sites (17.50* and 18.00* diameters (1) rectangular duct site 16*x16*. Round duct section properties are included 5767 (Ref. 6). The structural adequacy of round duct has (Ref. 5). evaluations of rectangular duct (including the calculations of effective section prop in this calculation based on the string analysis results contained in Attachment .n E of
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Duct string systems 4316-1,4316 2 and 43143 i have re of effective section properties and overall stress evaluations for rectangular duct based j analysis results contained in Attachments A through C of this calculation. There sections (Q318 and Q 309) in string analysis system 43161. Evaluation results of
' 318 st.bject to a maximum intemal pressure ili off 14' water gage tion Q318 have concluded th is based ,
_( adding stiffener)is required (Ref,5). Therefore, the acceptab ty o wye sec . nM
. on the modified configuration.
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?' 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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P MrruoDolitGy , - n Duet strings of 4316 system series include five (5 design criteria (Ref.1) and documented in this calculation: - 1. Feview duct attributes such as duct size and duct configuration. Update duct database for string analysis system to include duct s 2. duct configurations. Duct database is included in Attachment F of this c 3. Calculate effective !.ection properties for each rectangular duct sire utiliain FORTRAN program ' DUCT 24'. The output of DUCT 24 program is inte formatted as regular hand calculation sheets for checking purpose. i , Effective section properties for OBE and SSE caws are calculated per The duct orientation is shown in Fig, 3.4 3 and Fig. 3.4-4. g_ ) , For each duct size, the following inputs are required for DUCT 24 to comp D.7 effective section properties: '
- Width of duct (W) y
- lleight of duct (11) e p
Gy
- Duct sheet bare metal thickness (t) ,; )
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- Effective length factors (Ky and Kr)
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of string analysis model. directions and for duct elbows or duct segme
. unection, Maximum Ly and Lz lengths are determined for each duct sire, ..
; ,I c Calculate duct longitudinal stresses due to: x )
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W he masimum (accid:nt) pressure considered for duct in -string analysis 6 systems of 43161,43166,4316 7 and a small straight =e g portion.of
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g g k 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.
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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
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Dead load and global seismic load obtained from string analysis. M w - 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. ( l b- -) .," M a V , - wi : 4
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$""' 9 " 77 so 76?30.507 o.n o.n i exc, systern series e a The following forces are used in stress calculations and are dettnnined by l
enveloping the maximum and minimum forces at Beam Ends A and D: i Axial Force (Fx)
- Shear 2 Force (Fy) y .l
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; j l y' in the enveloping process for dead load, absolute values are used.
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- 5. Calculate duct suess allowables per Section 3.5.4. i
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'[' 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 Calculate total duct longitudinal stresses per load combinations. ;
% 6.
- 7. Evaluate duct structural adequacy based on total duct longitudinal stresses.
i, Duct is considered to behase as a beam globally. j .~ l :- Calculate in plane shear stress due to dead load + global seismic load.
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- 9. Evaluate duct in-plane shear stress vs shear stress allowables for longitudinal seams and identify cases, if any, wherethat the calculated shear stress is greater than 1.0 s , ksi.
[ l 10. Update duct database to include duct internal pressure, longtudinal stresses and she stresses for cach duct sire. 4 i- 11. Verify that total duct longitudinal stresses are less than the longitudinal stress margins 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 compression and calculated longitudinal stress per EQ. (3.6.12). The total duct y 7 1
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longitudinal stress in tension is compared to the sum of longitudinal s , 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 l
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f hJ 12. Document results. h# l 'l ', l A LOTUS 123 program *DUCSTitS* is developed and used to accomp!!sh the wor !
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ltem Nos. 4 through 9 and 11. The output of DUCSTitS h intentionally formatted as regu l calculation sheets for checking purpse. l :. v. ( . I p +'. , l ,- l i p. i il t {b i.. , i _ y L ,,) . V. . ' N L ,. . y .
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) 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-L $768. : A
~~
Calculation (C) contains the structural adequacy evaluation of the ACME Icek longitudinal seams for
-) round duct. De calculated OBE shear stress is 403.9 psi which is less than the ODE shear stress allowable of 5775.9 psi. .
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]} [ RffERLNCES , 1 .
- 1. CCl!VAC Duct and Duct Support Qualification, Fermi Design Criteria No FERMI DC-762301, Revision 0, Dated 3/15/96.
L
- 2. NRC letter dated Decemtier 7,1995, ' Fermi 2 Control Center ifcating, Ventilation and Air Conditioning (CCllVAC) System, including Safety Evaluation on the Same Subject *,
6 3. DECO Calculation DC 5744. Revision 0. i
, n 4 DECO Calculation DC 5758, Revision 0. .
l' I' 5. DECO Calculation DC 5768. Revision 0. , ! u. (f 6. DECO Calculation DC 5767, Revision 0. I 3, 7. DECO Specification 3071 32,
- Insulation of Piping and Mechanical Equipment', Revision li, j 1 Dated 12/13/95. .
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- 8. AISC Manual of Stect Construction 7th edition and 8th Edition.
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1 - DUCT NODE NODE LENGTH Ky KZ
; SIZE I J Ly LZ 14X14 300 285 3'-11' 3'-11' 2.0 2.0 l i' p' 285 280 28-2" 28-2" 2.0 2.0 1
! 7 200 260 8'-0" 8'-0" 2.0 2.0 l
. 260 250 6'-6" 6'-6" 1.0 1.0 l I 250 240 8'-6" 88-6" 1.0 1.0
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)'; 240 230 o'-6" 6'-6" 1.0 1.0 B' 230 220 5'-5" 5'-5" 1.0 . 2.0 .
}lS .r -
220 210 3'-7" '3'-7" ~ 1. 0 * * ' 2 . 0 ~ >$ -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 a 170 150 8'-0" a'-0" 1.0 1.0 '
! 63 150 140 7'-0" 7'-0" 1.0 1.0 I j. to 140 13b 135 120 l'-5" 5'-7" l'-5" 5'-7" 1.0 1.0 2.0 2.0 l i
- . 9 120 100 9'-2" 9'-2" 1.0 1.0 i 4
f 200 335 6'-5" 4'-6" 1.0 2.0 i j J [ 335 320 320 310 6'-5" 7'-0" 3'-3" J'-10" 1.0 1.0 2.0 2.0
)
g l- P 310 175 7'-0" 4'-6" 1.0 2.0 l 1 i hu
- Uso Ly =
LZ = 96" 96" Ky = 2.0 KZ = 2.0
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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 87.4421 Z -IN**4 AXIS: Izz = TXW**3/6 + TXilXW**2/2 = FULL SECTION RADIUS OF GYRATION ABOUT Y - AXIS (Iyy/Ag)**0.5 = 5.7155 IN Ryy FULL=SECTION RADIUS OF GYRATION ABOUT Z - AXIS 1 Rzz = (Izz/Ag)**0.5 = S.7155 IN YIELDING STRESS = .3300E+02 KSI 1 MODULUS OF E!ASTICITY = .2900E405 KSI ALPHAc PER EQ. (3.4.1-2c) FOR llEIGitT(!!) OF DUCT:3.4966 ALPHAc = 0. 2's6 + 0.328X(ll/T)X(Fy/E)**0.5 = DETAc PER EQ. (3.4.1-2c) FOR WIDTil(W) OF DUCT 3.4966 DETAc = 0.256 + 0.328X(W/T)X(Fy/E)**0.5 = 6 CALCULATE Ag FOR AXIAL TENSION ODE & SSE y (A) 3-FULL SECTION AREA, Ag=2X(W+11)XT= 2.6768 IN**2 e 4- (B) CALCUIATE Acx FOR AXI AL COMPRESSION EFFECTIVE LENGT!! FACTOR (Y) = 2.0000 3-UNDRACED LENGTH DETWEEN SUPTS (Y)
= 96.0000 IN KL/Ry = 33.5930 pJ. 2.0000 m EFFECTIVE LENGTil FACTOR (Z) = = 96.0000 IN
.K UNBRACED LENGTil BETkEEN SUPTS (Z)
KL/Rz = 33.5930 Q k,f KL/Rmax = MAX (KL/Ry,KL/Rz) = 33.5930 Fe = TT**2XE/(KL/Rmax)**2 = 253.6293 KSI
;s.
Fe.GT.Fy/2, Fn=FyX(1.0-Fy/(4.XFe))= 31.9266 KSI i
- 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 ,
v = .3203 4.4839 IN o He = RJioiXH = M B ETA i .CT. B ETAc .
- RHoi=(0.41+0.59X(Ty/Fa)**0.5-0.22/DETAi)/BETAi
-t" = .3203 ,
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- We a RilOiXW = 4.4839 IN
[. , .8573 IN642
- y. EFFECTIVE AREA, Acx_OBE = f
~ SSE CASE
[ 24.9426 Fa = 1.5X(ra/1.92) = 4.5181 P 4.5181 ALPHAl=1. ALPilA1.GT. ALPHAc, 05 2 /SQRT 4. 0) X (H/T)X (Ta / E )
'.. RilOi= ( 0. 414 0. 59X ( Ty/ Ta) *
- 0. 5-0. 2 2 / ALPilAi) / ALPIIAi
- K = .2302 lio = RitolXil = 3.2224 IN '
BETAi.GT.BETAc, Ril0i= (0. 41 + 0. 59X ( Ty/ Ta) *
- 0. 5-0. 2 2 / DETAi) / BETAi
= .2302 We = PJIOiXW = 3.2224 IN e
p EFFECTIVE AREA, Aox_SSE =
.6161 IN**2 M. EFTECTIVE Ac AXIAL AREA= FOR ANALYSIS:1.6465 IN**2 ANALYSIS M.
~ = .114 3 E-01 Pr*
- 2 g,( CALCULATE Iey, FOR BENDIND MOMENT Hy
-* (C)
'x; ~ OBE CASE m Pa = 0.6*Fy = 19.8000 1.6434 b 4.0255 ALPilAi=1.
BETAi =1.052/SQRT( 052 / SQRT ( 2 4. 0) X (ll/T) X ( ra / E) *
- 0 P
- 0. 67=3.GT. ALPilA1. LE. ALPilAc ,(1.358 - 0.461/ALPilAi)/ALPHAl Ril0i O = .6556 4.5895 IN W 0.511oy = 0.5 X Ritoi X 11 =
k Y> DETA1.GT.BETAc, R110i= ( 0. 41+ 0. 59X ( Ty/ Pa) *
- 0. 5-0. 2 2 / DETA1) / DETA1
= .2775 1.9424 IN 0.5Wey = 0.5 X Ril01 X W =
?
R FOR Hy, Iey'OBE = 39.1661 IN**4 x, Sey ODE = 5.5952 IN**3
-iJ c4 ;6
%a. ' - SSE CASE '
T O-Q*' 29.7000 2.0127 . Fa = 0.9XTy = QRT(24.0)X(ll/T)X Fa/E)**0.5= 4.9302 ~! O ALPilAi=1.052/S .' if BETAi =1.052/SQRT( 4. 0) X (W/T) X Fa / E) *
- 0. 5=
~
p 0.673.GT. ALPilA1.LE. ALPilAc, + R- 1U101 = (1..5609 358 - 0.461/ ALPilA1) / ALPHAi O O ' '
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=T. DETAc , TA1) /BETAi l' BETA 1.G Ritol=(0.41+0.59X(Ty/Fa)**0.5-0.22/BE
= .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 K (D) CALCUI. ATE 102 W
r - OBE CASE 4.0255 19.80004.0)X(ll/T)X(Fa/E)**0,5= 1.6434 Fa = 0. 6
- Fy =/ SQRT ( /E)**0.5=
i ALPilAl=1.052BETAi =1. 052 /NAi)/ALPNAi SQRT( 24. 0) X (W /T) X (F
- ALPilAi .GT. ALPNAc,Rlloi=(0.41+0 59X(Fy/Fa)**0.5-0.22/ ALP
= .2775 1.9424 IN 0 . 5110 2
= 0. 5 X RJfo i X 11 = ,
' l 0. 67 3 07 BFTAi .LE.DETAc,Ritol = (1.358 - 0.461/DETA1)/B (i r = 65$6 4.5895 IN
- if
- 0. 5Wo z = 0. 5 X Ritoi 39.1 XW = 661 IN *
- 4 TOR Mz, 10 2'OBE = 5.5952 IN**3 Soz OBE = .
- SSE CASE '
4 29.7000 4.9302 i Fa = 0.9XFy =/ SQRT( 4.0) X(ll/T) X(Fa/E) *
- 0.2.0127 5=)**0.5= ;
?:
4 ALPilAi=1.052BRTAi =1 052/SQRT(24.0)X(W ALPilAi .GT. ALPilAc,Ritoi=(0.4140.59X(Fy/Fa)**0.5-0.22 A
= .2003 1 4018 IN ' h O . 5110 z = 0. 5 X Rlloi XAi)11 0.673.GT.BINA1.LE.DETAc, =
/BETAi ,:
Ritoi == (1.358 - 0.461/DET 3.9263 IN
.5609 0.5Woz = 0.5 X Ritoi X = W = 33.1428 IN**4 4.7347 INa*3
,s , ,
fj ' a FOR Hz, Ioz SSE = Soz'SSE 28 1714 IN**4 102 ***4ALYSIS == m <4
' .1359E-02 FT**4 ,
*1 u DE & SSE '
'N ' CALCULATE Ay FOR Y-DIRECTION SilEAR O y, (E) 1.3384 IN**2
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r SilEAR AREA, Ay = 2XWXT == .9294E-02 FT**2 - ..
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(F) CALCULATE At FOR Z-DIRECTION SHEAR OBE & SSL SHEAR AREA, Az = 2XHXT = 1,,3384 IN**2 n = .9294E-02 FT**2 x
- s. . '
(G) CALCULATE Ixx FOR TORSIONAL M0HENT Mx OBE & SSE FOR Mx, Ixx ANALYSIS = 131.1632 IN**4
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,f A.02 String Analysis No. 4316 - 2 NODE LENGTH Ky KZ DUCT NODE g $ SIZE J Ly L2 . %'s ............................_____.-----....--...--......---
200 I 220 9'-2" 9'-2" 1.0 10 t 19X19 7'-9" 7'-9" 1.0 2.0 220 235 k' 235 250 3'-4" 7'-0" 38-4"
*/'-0" 1.0 1.0 2.0 1.0 250 260 1.0 1.0 270 8'-0" 8'-0" 260 88-4"
.0 1. 0 270 280 8'-4" 7'-5" 7'-5" 1.0 1.0 280 295 1.0 2.0 I4 300 l'-1" l'-1"
~
295 3'-4" 1.0 2.0 300 310 3'-4" N. 310 330 6'-6" 6'-6" 1.0 1.0
$< 6'-8" 6'-8" 2.0 3.0 330 340 2.0 1.0 F 340 350 6'-10" 2'-4" 1.0 360 6'-10" 4'-6" 2.0 350 1.3 D 360 370 6'-10" 4'-6" 2.0 2.0 1.0 6'-10" 4'-6" h-_
W> 350 385 400 6'-10" 4'-G" 2.0 1.0 ~ 185
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' EFFECT. PROPERTIES FOR DUCT SIZE W(IN)XH(IN) .0478 IN
' DUCT SHEET BARE METAL THICKNESS =
FULL SECTION AREA, Ag = 2*(W+H)*T = 3.6320 IN**2 FULL SECTION MOMENT OF =INERTIA ABOUT 218.5735 Y - AXIS: IN**4 Iyy TXH**3/6 + TXWXH**2/2
=SECTION MOMENT OF INERTI A ABOUT Z - AXIS:
i , FULL 218.5735 IN**4 l Izz = TXW**3/6 + TXHXW**2/2 = i1 FULL SECTION KADIUS OF1.7S67 GYRATION IN ADOUT Y - AXIS: s Ryy = (Iyy/Ag)**0.5 = FULL SECTION RADIUS OF GYRATION ABOUT Z - AXIS:
, Rzz = (Iz z / Aq) * *0. 5 = 7.7567 IN
- YIELDING STRESS = .3300E+02 KSI i
y
- x .2900E+05 XSI MODULUS OF ELASTICITY =
e i o,- [ ALPHAc PER EQ. (3.4.1-2c) FOR HEIGHT (H) OF DUCT: 4.6540 ALPHAc = 0.256 + 0.328X(H/T) X(Fy/E) * *0. 5 =
; % N BETAc PER EQ. (3.4.1-2c) FOR WIDTH (W)=OF DUCT:
0.328X(W/T)X(Fy/E)**0.5 4.6540 .x L BETAc = 0.256 4 < . l[ l
~
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OBE & SSE Y l CALCULATE Ag FOR AXI AL TENSION
; pp (A) .
' C.
FULL SECTION AREA, Aga2X(W+H)XT= 3.632B IN**2 ...., j f-
. lR d
p' 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 2.0000
$ ;_ 91 KL/Ry EFFECTI =VE LENGTH FACTOR (Z) = 93.0000 IN
= <,
UNBRACED LENGTH BETWEEN SUPTS (Z)
' .a r, ,
? KL/Rz = 23.9792 7 i i f[$je 7; "
KL/Rmax = MAX (KL/Ry,KL/R2) Fe = TT**2XE/(KL/Rmax)**2 =
= 23.9792 497.7681 FCI 32.4531 KSI
, j;h !
W Q: l h Fe.GT.Fy/2, Fn= FyX ( 1. 0-Fy/ (4. XFe) ) = r . i hJ -1: Ef@i 3
- OBE CASE fY
! S 6 g% Fa = Fn/1.92 = 16.9026 5.0477 5 i_ 0@h M'th v ALPHAi=1.052/SQRT(4.0)X(H/T)X(Fa/E)**0,5= S.0477 i
- BETAi =1.052/SQRT(4.0)X(W/T)X(Fa/E)**0.5= m Y ALPHAi.GT ALPHAc, @*
RHOi= ( 0. 41+ 0. 59X ( Fy / Fa) *
- 0. 5-0. 22 / ALPilAi) / ALP 11A1 ,7' 6
hw
= ,2359 4.4823 IN
.M '
He = RHOiXH = t ; a4 r_ g BETAi.GT.BETAc,
'RH0i=(0.41+0.59X(Fy/Fa)**0.5-0.22/ BETA 1)/BETAi Qg dr. Q y
f My
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J - P We = RlloiXW = 4.4823 IN 1 E , EFFECTIVE AREA, Aex_OBE = .8570 IN**2 g (,
- SSE CASE r
Fa = 1.5X(Fn/1.92) = 25.3540 6.1821 4 ALPHAi=1. 052 / SQRT ( 4. 0) X (H /T) X( Fa / E) *
- 0. 5= 6.1821 BETAi =1. 052 / SQRT(4. 0) X (W/T) X ( Fa/ E) *
- 0. 5=
ALPHA 1.GT.ALPHAc, RilOi= (0. 41+ 0. 59X ( Fy/ Fa) <
- 0. 5-0. 2 2 / ALPHAi) / ALPilAi
= .1644 lie = RilOiXII = 3.2195 IN K BETAl.GT.BETAc, Ritoi = ( 0. 41+ 0. 59X ( Ty/ Fa) *
- 0,5-0. 2 2 / BETA l ) / BETAi
= .1694 We = P.110iXW = 3.2195 IN
? ._ EFFECTIVE AREA, Aex_SSE = .6156 IN**2 g
6 D ^ EFFECTIVE AXI AL AREA FOR AN* LYSIS: 2.1242 IN**2 Ao ANALYSIS = 7 '"
= .1475E-01 FT**2
;%y-( .,
(C) CALCULATE Iey FOR BENDIND MOMENT My f[ - OBE CASE ) 1 19.8000
' W Fa = 0.6*Fy =
ALPilAi=1. 052 / SQRT(24. 0) X (H/T) X ( Fa / E) *
- 0,5= 2.2303 5.4632 BETAi =1.052/SQRT( 4.0)X(W/T)X(Fa/E)**0.5u -
0 673.GT.ALPilAi.LE.ALPl!Ac, a, L.? RIIO L = ( 1. 3 58 - 0. 4 61/ ALPHAi) / ALPHAi , W; u .5162 Q
- 0. 511ey = 0. 5 X Ritoi X 11 = 4.9039 IN i 97, BETAi.GT.BETAc, y, 1 SF- Bitola ( 0. 41+ 0. 59X ( Fy/ Fa) *
- 0. 5-0. 22 /BETAi) /BETAi it ?S
.2071 Cl-y?
i ,,
' ' ' =
1.9674 IN l.f. , M 0.5Wey = 0.5 X RI:01 X W = ~
~
m FOR My, Iey~ ODE = 82.4054 IN**4 1 Sey OBE = 8.6743 IN**3
@2 .
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=
c 6.6910
- BETAl'=1.052/SQRT( 4.0)X(W/T)X(Fa/E)**0.5= -
0.673.GT.ALPRA1.LE.ALPRAC, RHOi- = (1. 358 - 0,461/ ALPHAi) /ALPHAi 10 A A M '%0
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!, k" 0.5 Hey a 0.5 X RHOi X H = 4.1360 IN' , .- I BETAi.GT.BETAc, Ritoi= ( 0. 41+0. 59X ( Py/ Fa) *
- 0. 5-0. 22 / BETAi ) / BETAi i
E e = .1493 j It 0.5Wey = 0.5 X RHOi X W = 1.4184 IN ; i l FOR My, Icy SSE = 69.2832 IN**4
~ SSE = 7.2930 IN**3 l
. f ', ' Sey Iey-ANALYSId = 58.8908 IN**4 g
= .2840E-02 FT**4
% CALCULATE Iez FOR DENDIND NOMENT Mz 4 (D)
- 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 2.2303
- . h BETAi =1. 052 /SQRT( 2 4. 0) X (W/T) X ( Fa / E) *
- 0. 5=
ALPHA 1.GT.ALPHAc, 4.. 9,A RHOi=(0.41+0.59X(Fy/Fa)**0.5-0.22/ ALPHA 1)/ALPHAi ' , : s' = .2071
- 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 1- D 5162 4, i N$ " 0.5Wez = 0.5 X Rlloi X W = FOR Mz, Iez OBE = 82.4054 IN**4 4.9039 IN 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(jg , BETAi =1.052/SQRT(24.0)X(W/T)X(Fa/E)**0.5= ALPHAi.GT.ALPHAc, 2.7316 4 l l
~+L RHOi=(0.41+0.59X(Fy/Fa)**0.5-0.22/ALPHAi)/ALPHAi 9
= .1493 i O. Silez = 0. 5 X RIIOi X H = I u 1.4184 IN -
- 0.673.GT.BETAi.LE.BETAc, Rl!Oi == (1.358 - 0.461/BETAi)/BETAi $
4 Jg n v. .4354 s c
] '- D,7 0.5Wez = 0.5 X RHOi X W = 4.1360 IN f- I i
h FOR Mz, Iez SSE = 69.2832 IN**4 , EU '
;: p;T Soz~SSE = 7.2930 IN**3 -
I2 ' 4 pg Iez ANALYSIS = 58.G908-IN**4
^W
' J.t l
l j.y 2 = .284(E-02 FT**4 , l
, ;.5 :,. %q[ '
, - Sf3db , .(E) CALCULATE Ay FOR Y-DIRECTION SHEAR OBE & SSE : ?j , my, . x,:; ;
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- jp. SHEAR AREA, Ay = 2XWXT = 1.0164 IN**2
; fa
= .1261E-01 FT**2 ;y
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w 1.8164 IN**2
+ SHEAR AREA, Az = 2XHXT = !
% = .1261E-01 Pr**2 !
i
~i (G) CALCULATE Ixx TOR TORSIONAL MOMENT Mx ODE & SSE e
FOR Mx, Ixx ANALYSIS == 327.8602 IH**4 !
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" 320 300 6'-10" 6'-10" 1.0 1.0 M' use Ly = 84.0" Ky = 1.0 Lz = 51.0" Kz = 2.0
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W. EFFECT. PROPERTIES FOR DUCT SIZE W(IN)XH(IN) 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 - IN**4 31.8667 AXIS:
Iyy = TXHa*3/6 + TXWXH**2/2 = *
-FULL SECTION MOMENT OF INERTIA ABOUT Z - IN**4 31.8667 AXIS:
Izz = TXW**3/6 + TXHXW**2/2 = i FULL SECTION RADIUS OF GYRATION ABOUT Y - AXIS: L Ryy = (Iyy/Ag)**0.5 = 4.0825 IN .-
- o FULL SECTION RADIUS OF GYRATION ABOUT Z - AXIS:
$ 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:2.5707 N ALPHAc = 0.256 + 0. 323X (H/T) X (Fy/ E) *
- 0. 5 =
i BETAc PER EQ. (3.4.1-2c) FOR WIDTH (W) OF DUCT: 2.5707
= 0.256 + 0.328X(W/T)X(Fy/E)**0.5 =
o: BETAc l: iO CALCULATE Ag FOR AXIAL TENSION OBE & SSE i T (A) i' d' . FULL SECTION AREA, Aga2X(W+H)XT= 1.9120 IN**2 ,'- "b (B) CALCULATE Acx FOR AXIAL COMPRESSION
,r
# EFFECTIVE LENGTH FACTOR (Y) = 1.0000 UNBRACED LENGTH BETWEEN SUPTS (Y) = 84.0000 IN
($T ~ KL/Ry = 20.5757 EFFECTIVE LENGTH FACTOR (Z) = 2.0000
, ya UNBRACED LENGTH BETWEEN SUPTS (2) = 51.0000 IN W : 4 KL/RZ = 24.9848 P* KL/Rmax = MAX (KL/Ry,KL/Rz) = 24.'9848 1 Fe = TT *
- 2 XE/ (KL/ Rmax) *
- 2 = - 458.5064 KSI ?
;: Fe.GT.Fy/2, Fn=FyX(1.0-Fy/(4.XFe))= 32.4062 KSI 'i .
w
,j M - CBE CASE #
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$g~' Fa = Fn/1.92 = 16.8782 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-rw RHOi=(0.41+0.59X(Py/Fa)**0.5-0.22/ ALPHA 1)/ALPHAi He = RHOiXH 4.3398 IN , b,l4
[d 0 . 1 BETA 1. GT. B ETAc, ( RHOi=(0.41+0.59X(Fy/Fa)**0.5-0.22/BETAl)/BETAi i 9.D {d g OM)
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We = RHOiXW = 4.3398 IN EFFECTIVE AREA, Aex_OBE = .8298 IHa*2 e js ' s .m
- SSE CASE g.
Fa = 1.5X(Fn/1.92) = 25.3174 E ALPHAi=1. 052 / SQRT ( 4. 0) X (ll/T) X ( Fa / E) *
- 0,5= 3.2514
[ 3.2514
- BETAi =1.05?/SQRT(4.0)X(W/T)X(Fa/E.)**0.5=
- ALPHAi.GT.ALPHAc, y Rlloi=(0.41+0.59X(Fy/Fa)**0.5-0.22/ ALPHA 1)/ALPHAi i
= .3125 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
L EFFECTIVE AXIAL AREA FOR ANALYSIS: 1.2547 IN**2 z
*- Ae ANALYSIS =
~
= .8713E-02 FT**2
((^~ A .; CALCULATE Iey,FOR BENDIND MOMENT My R. (C) o W - OBE CASE i 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
[ 2.8754 pc BETAi =1.052/SQRT( 4.0)X(W/T)X(Fa/E)**0.5= 6 0.673.GT.ALPHAi.LE.ALPHAc, f'th Ritoi == (1.358 - 0.461/ALPHAi)/ALPHAi
.8223 4.1116 IN 0.5 Hey = 0.5 X RilOi X ll =
h3 F BETA 1.GT.BETAc, RIIOi= ( 0. 41+ 0. 59X ( Fy/ Fa ) *
- 0. 5-0. 2 2 / BETAi) / BETAi d = .3809
'gh'g O.5Wey = 0.5 X RHOi X W = 1.9044 IN ,
{' 17.0251 IH**4 FOR My, Iey 0 ' = J Sey O /. = 3.4050 IN**3 o< Epf N@f , , 1
- W- ~ '
hE-kE ' - SSE CASE & " Q~ Wn Fa = 0.9XFy = 29.7000
; @ .' 1.4377 >-
7' ALPHAi=1.052/SQRT(24.0)X(H/T)X(Fa/E)**0.5= 3.5216 BETAi =1.052/SQRT( 4.0)X(W/T)X(Fa/E)**0.5= li 0.673.GT. ALPHA 1.LE.ALPHAc, t Rlloi == (1.358 - 0.461/ALPHAi)/ALPHAi n. Q h([/,. .7215 9,' .ah - f h\; QQ h2 ${O%U-dy hkb j de ?g f fp M* gJ '-
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5""' N " ll oati~ onw 7 ao 76230.502 I sutuccf System Series ku V' ra , i 4 . ,ic 0.5 Hey = 0.5 X R}{0i X H = 3.6077 IN D ++- BETA 1.GT.BETAc , s,.
- i, ;
Ritoi=(0.41+0.59X(Fy/Fa)**0.5-0.22/ BETA 1)/BETAi ($f"$ = .2753 i 0.5Wey = 0.5 X RilOi X W = 1.3764 IN
\ u FOR My, Iey SSE = 14.3740 IN**4 o
Sey SSE = 2.8748 IN**3
; 3 Iey~ ANALYSIS = 12.2179 IN**4
= .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 2.8754 ALPHAi=1.052/SQRT( 4. 0) X (il/T) X ( Fa / E) *
- 0. 5= 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
IA = .3809 0.5Het = 0.5 X RHOi X H = 1.9044 IN il O.673.GT. BETA 1.LE.BETAc,
&( . Ritoi = (1. 358 - 0. 4 61/ BETA 1) /BETAi p = 8223
;.7 4.1116 IN
% 0.5Wez = 0.5 X RHOi X W =
FOR Hz, Iez OBE = 17.0251 IN**4 v - Sez OBE = 3.4050 INa*3 . h *e
;1
- SSE CASE Fa = 0.9XFy = 29.7000 pr;. 3.5216 K ALPilAi=1.052/SQRT( 4.0)X(H/T)X(Fa/E)**0.5= 1.4377
& BETAi =1.052/SQRT(24.0)X(W/T)X(Fa/E)**0.5=
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- e
-O.673.GT. BETA 1.LE.BETAc, m q n
77 0-- Riioi == (1.358 - 0.461/DETAI)/BETAL a.. :
.7215
- 3.6077 IN
[
@M, 0.5Wez = 0.5 X RH0i X =W =
SSE 14.3740 IN**4 r FOR Ma, Iez_SSE = 2.8748 IN**3 kg Sea- 12.2179 IN**4 W Iez ANALYSIS =
~
= .5892E-03 FT**4 ,
;Og w.
'M h CALCULATE Ay FOR Y-DIRECTION SHEAR OBE & SSE N:i (E) c:r W .9560 IN**2 T1 SiiEAR - AREA, Ay = 2XWXT =
n/ = .6639E-02 FT**2 . l w e - c y ai
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F j i's g p P ' ( '* J CALCULATE Az FOR Z-DIRECTION SHF.AR OBE & SSE
)! SHEAR AREA, A2 a 2XHXT = .9560 IN**2
$ [ = . 66 3 9 E-0 2 FT**2 (G) CALCULATE Ixx FOR TORSIONAL HOMENT Mx OBE & SSE 1 ,f l' FOR Mx, Ixx ANALYSIS = 47.8000 IN**4
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/} A.04 String Analysis No. 4316 - 6 DUCT NODE NODE LENGTil Ky KZ SIZE I J Ly L2 6 --_................................_ ...___..........--___.
775 4'-9" 4'-3" 2.0 1.0 ( 16X16 7~20 2.0 1.0
- 100 775 6'-5" 38-7" 775 120 6'-5" 2'-11" 2.0 1.0 J 2.0 1.0 120 1014 l'-8" l'-8"
'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 1.0 205 220 4'-8" 5'-0" 1.0 1.0
't 1.0 1.0 220 1011 0'-4" 5'-0" J 245 7'-0" 7'-0" 2.0 2.0 A 2011 150 355 5'-0" 5'-0" 1.0 2.0 8 2'-2" 1.0 2.0
' ~
Il 355 375 2'-2" 6405 415 18-7" l'-7" 1.0 2.0 FEp 5'-0" 1.0 2.0
- 415 220 5'-0" ..
H , m g3 Use Ly = 84.0" Ky = 2.0 , p M:: 35' i bz = 84.0" Kz w 2.0 , s .m.. , g, e t ,
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2 - r EFFECT. PROPERTIES FOR DUCT SI7E W(IN)XH(IN) : 16.0X16.0 I
. DUCT SilEET DARE METAL THICKNESS. = .0478 IN . .
P* - FULL SECTION AREA, Ag~= 2*(W+H)*T = 3~0592 IN**2
* / yt; FULL SECTION MOMENT OF INERTIA ABOUT Y - AXIS 1, Iyy a TXH**3/6 + TXWX11**2/2 = 130.5259 IN**4 l 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 g A7 PHAC PER EQ. (3.4.1-2c) FOR HEIGl!T(ll) OF DUCT: 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 FULL SECTION 'AkEA, Ag=2X(W+H)XT= 3.0592 IN**2 if e<
~
(B) CALCUIATE Aex FOR AXIAL COMPRESSION EFFECTIVE LENGTH FACTOR (Y) = 2.0000 < !' %, UNBRACED LENGTH BETWEEN SUPTS (Y) = 84.0000 IN I
$' KL/Ry = 25.7196 n- EFFECTIVE LENGTH FACTOR (Z) = 2.0000 t p UNDRACED LENGTH BETdEEN SUPTS (Z) = 84.0000 IN d.- KL/Rz = 25.7196 "
KL/Rmax = HAX (KL/Ry,KL/Rz) = 25.7196 Fe = TT**2XE/(KL/Rmax)**2 = 432.6004 KSI
$ Fe.GT.Fy/2, Fn=FyX (1. 0-Fy/ ( 4. XFe) ) = 32.3708 KSI t l
C 4 - OBE CASE My ?: 9 h, , Fa = Fn/1.92 = 16.8598 :$ 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
,1 ALPHA 1.GT.ALPHAc, ,
, /L 76 R110i= ( 0. 41+ 0. 59 X (Fy/ Fa) *
- 0. 5-0. 2 2 / ALPHAi) / ALPHAi !
4 fM
= .2788 n, ,@;
He = RHO 1XH = 4.4609 IN i' 41 4;Wx. ' BETA 1.GT.BETAc, - 7 {y'i, . RHOi=(0.41+0.59X(Fy/Fa)**0.5-0.22/BETAi)/BETAi sa .2788
. Mn-fa .
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f Duct Evaluation of 4316 sua;tcf Systein Series Jo 76230.502
) , _
u. t Y y l We = RHOiXW = 4.4609 IN j , s. EFFECTIVE AREA, Acx_ ODE = .8529 I N '.
- 2
[ f.. , l L I; [ - SSE CASE I ; Fa = 1.5X'Fn/1.92) = 25.2897 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 i
ALPIIA1.GT. ALPHAc, j RII0i= ( 0. 41 + 0. 59 X ( Fy/ Fa) *
- 0. 5-0. 2 2 / AI.PHAi) / ALPilAi f
= .2003 1 He = RilOiXII = 3.2055 IN g
BETAl.GT.BETAc, Rifoi= ( 0. 41+ 0. 59X ( Fy/ Fa) *
- 0. 5-0. 2 2 / DETAi) / BETAi
(
?
= .2003
/ s We = RHOiXW = 3.2055 IN
( s ,( O - EFFECTIVE AREA, Anx SSE = -
.6129 IN**2 +
j EFFECTIVE AXIAL ARPA FOR ANALYSIS:
; Ae ANALYSIS =
1.8360 IN**2
= .1275E-01 FT**2 .
.3 t y (C) CALCULATE Iey, FOR BENDIND MOMENT My i ' ;.
- OBE CASE N
.'; Fa = 0.6*Fy =
., 'T 19.8000 1.8782
- ALPl!A i= 1. 052 / SQRT ( 24 . 0 ) X (ll/ T) X ( Fa / E) *
- 0, 5 =
( f BETAi =1.052/SQRT( 4. 0) X(W/T) X( Fa/ E) * *0. 5= 4.6006 i t O. 673.GT. ALPilA1. LE. ALPHAc, i RilOi = (1.358 - 0.461/ALPilAi)/ALPHAi iL t;
= .5924 "
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 i
= .2443
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; i h19* - SSE CASE WJO
& - v ;v;
- Fa = 0.3XFy =- 29.7000 D i[ f ALPilA i=1. 052 / SQRT ( 2 4. 0) X (H/T) X (Fa / E) *
- 0. 5= 2.3003 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 j y Rlloi == (1.358 - 0.461/ ALPHA 1)/ALPHAi *J'n ,
r r- .5032 %s 3, (n 1. Q N $U W"
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',- Duct Evaluation of 4316 so 76230.502 J SuaXCT System Series 3 1 f
0.511ey = 0.5 X RitOi X li = 4.0259 IN 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 Iey SSE = 45.8814 IN**4 SSE = 5.7352 IH**3 FOR Hy,Iey~ Sey ANALYSIS 38.9992 = IN**4
= ,1881E-02 FT**4 ' +- $. CALCULATE Ioz FOR DENDIND MOMENT Mz (D)
Q b - OBE CASE Fa = 0.6*Fy = 9.8000 4.6006 i ALPitA i= 1. 052 / SQRY ' , 4.0)X(H/T)X(Fa/E)**0.5= 1.8782 DETAi = 1. 052 / SQRT(2 4. 0) X (h/T) X ( Fa / E) *
- 0. 5=
2 ALPHAi.GT.ALPHAc, RilOl = ( 0. 41 t 0. 59X ( Fy/ Fa) *
- 0. 5-0. 2 2 / ALPilAi) / ALPilAi 4
= .2443 L
- 0. 51iez = 0. 5 X R}{Oi X H =
1.9543 IN 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 54.3355 W= 4.7389 IN
% FOR Hz, Icz OBE = IN**4
$9 Sez[OBE = 6.7919 IN**3 IA . .
bi - SSE CASE R Fa = 0.9XFy = 29.7000 5.6345
$h '
ALPHAl=1. 052 /SQRT( 4. 0) X (ll/T) X ( Fa/ E) *
- 0. 5= 2.3003 fi- BETAi =1.052/SQRT(24.0)X(W/T)X(Fa/E)**0.5=
ALPilA1.GT.ALPHAc, m b Ritoi= ( 0. 41+0. 59X (Fy/ Fa) *
- 0. 5-0. 2 2 / ALPilA1) / ALPHAi 7;
= .1762 ~
1.4097 IN
',Q 0.5Hez = 0.5 X RitOi XH=
0.673.GT.BETAi.LE.DETAc, W RIIOi == (1.358 - 0.461/BETAi)/DETAi c
.5032 4.0259 IN f[
0.5Woz = 0.5 X Rlloi X =W = 45.8814 INa*4 ' t FOR Mz, Iez SSE = 5.7352 IH**3 Sez[SSE 38.9992 IN**4 b"
- Ie ANALYSIS == .1881E-02
~~
FT**4
+
(( CALCULATE Ay FOR Y-DIRECTION SHEAR OBE & SSE - l k (E) SilEAR AREA, Ay = 2XWXT == 1.5296 IN**2
.1062E-01 FT**2 4 ' "l VO 4 k .
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$UBKCT System Series so 76230.502 l"
a. l , E
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(' (F) CALCULATE Az FOR Z-DIRECTION S!! EAR OBE & SSE SHEAR AREA, Az - 2XHXT = 1.5296 IN**2
; '3 -
= .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
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- y. suaxcr System Series -3\;
,. p. . , f, " . , e g ; io A. Effective Section Properties Calculations for ,. Rectangular. Ducts (Con't)
. s:
r~ 3 A.05 String Analysis No. 4316 - 7 , , <
- LENGTH Ky Xz W M DUCT NODE NODE J Ly LZ m.$
SIZE I .. .. v- .. . ..... . . ............ .................. .... 1.0 720 715 6.00' 7.58' 1.0 " J, 16X16 1.0 1 715 710 1.58' 7.58' 1.0 W(. 705 1.42' 1.42' 1.0 2.0 g@** , 710 2.0 c
- 705 701 4.0' 4.08 1.0 d 715 725 4.0' 4.0' 1.0 2.0
- Ky = 1.0 Use Ly = 72"
- tev,, e LZ = 48" Kz = 2.0 4.:
- b. .. _ +
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- % DUCIN.010 r *- INPUT FILE = ;
OUTPUT FILE = DUCOUT.010 ,
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PnOJECT DECO FEPMI 2 - CCHVAC # " Dart o*rt . Duct Evaluation of 4316 Jo 76230.502 ., SuostCT Systen Series- n
*
- N
~$ yl <
kI p h EFFECT. PROPERTIES FOR DUCT SIZE W(IN)XH(IH) .0478 IN: 16.0X16.0 DUCT SilEET BARE METAL THICKNESS = 3.0592 IN**2
-FULL SECTION AREA, Aq = 2*(W+11)*T =
FULL SECTION MOMENT OF INERTIA ABOUT Y - IN**4 130.5259 AXIS: Iyy = TX11**3/', + TXWXHa*2/2 = J FULL SECTION r.OMENT OF INERTIA ABOUT Z - AXIS: Izz = TXW**3/6 + TX11XW**2/2 = 130.5259 IN**4 FULL SECTION RADIUS OF GYRATION ABOUT Y - AXIS: Ryy = (Iyy/Ag)**0,5 = 6.5320 IN 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:3.9596 ALPliAc = 0.256 + 0.328X(H/T)X(Fy/E)**0.5 =
BETAc PER EO. (3.4.1-2c) FOR WIDTH (W) OF LUCT: 3.9596 BETAc = 0.256 + 0.328X(W/T)X(Py/E)**0.5 = E. w (A) CALCULATE Ag FOR AXIAL TENSION OBE 6 SSE J' 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)
KL/Ry = 11.0227 i EFFECTIVE LENGTil FACTOR (Z)
= 2.0000 a n = 48.0000 IN 7' UNBRACID LENGTil BETWEEN SUPTS (Z)
KL/Rz = 14.6969 p KL/Rmax = MAX (KL/Ry,KL/Rz) = 14.6969 - g Fe = TF*
- 2XE/ (KL/Rmax) * *2 = 1325.083032.7945 KSI
!y? Fe.GT.Fy/2, Fn=FyX ( 1. 0-Fy/ ( 4. XFe ) ) = KSI ,[
- OBE CASE [
Fa = Fn/1.92 = 17.0805 i ALPilAi= 1. 052 / SQRT ( 4. 0) X (ll/T) X ( Fa / E) *
- 0. 5=
4.2730 4.2730 % BETAl = 1. 052 / SQRT ( 4. 0) X (W/T) X ( Fa / E) *
- 0. 5= ;
4;t ALPilA1.GT. ALPilAc, *
' Rlb)i= ( 0. 41+ 0. 59X ( Fy/ Fa) *
- 0. 5-0. 2 2 / ALPliAi) / ALPIIAi ,
g = .2758 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 ax: L4. '
= . 2 5 .iS r
'di B.
?
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% y h" . - i x g.
- y.
- m lL Mi[ Mi
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X - y PAQJECT __ Deco FERMJ ? - CIH'/AC Duct Evaluation of 4316
"" Sb cart oart
;o 76230.502 suostct System Serien
;f y We = RiiOiXW = 4.4132 IN .
),;
y EFFECTIVE AREA, Aex_OBE = .8438 IH**2 n JJ n .- N
- SSE CASE 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, i RitOi= ( 0. 414 0. 59X ( Fy/ Fa) *
- 0. 5-0. 2 2 / ALPilAi) / ALPilAi
[f #
= .1983 He = ElloiXil = 3.1722 IN J 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 a
= .1273E-01 FT**2 l (C) CALCULATE Icy FOR BENDIND MOMENT My
- OBE CASE
{ Fa = 0.G*Fy = 19.8000 ALPilAi= 1. 052 / SQRT ( 2 4. 0) X (ll/T) X ( Pa / E) *
- 0. 5= 1.8782 Ji 4.6006 BETAi =1.052/SQRT( 4.0)X(W/T)X(Fa/E)**0.5=
- 0. 67 3.CT. ALPilAi . LE. ALPi!Ac, I- ,
Ritoi == (1.358 - O.461/ALPl!Ai)/ALPHAi : 3
.5924
$ O.51{ey = 0.5 X RilOi X H = 4.7389 IN BETAi.GT.BETAc, t
Ritol=(0.41+0.59X(Fy/Fa)**0.5-0.22/DETAi)/ BETA 1 '
.2443 .s?'
N = 0.5Wey = 0.5 X RH01 X W = 1.9543 IN
/e- .
} 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 f ( .5032 , ,. ,
^ "_ 3 y n L% %= ;} , a _
h E f
'9' , $ ;g \ Es . ;?g '
fi \ < 9.3 1_ y, +. , 6
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- 92 " oart 04r1 Duct Evaluation of 4316 Jo 76230.502 SufutCT System Series 0.5 Hey = 0.5 X Ritoi X H = 4.0259 IN BETA 1.GT.BETAc,
' R110i= (0. 41+ 0. 59X ( Fy/ Fa) *
- 0. 5-0. 2 2 /BETAi) / DETAi
= .1762 r 0.5Wey = 0.5 X RHOi X W = 1.4097 IN ?
FOR My, Iey~SSE = 45.8814 IH**4 SSE = 5.7352 IN**3 Sey~ Iey- ANALYSIS = 38.9992 IN**4 c--
= .1881E-02 FT**4 j
s. (D) CALCULATE Icz FOR BENDIND MOMENT Mz k '
- CBE CACE hl: R m '
Fa = 0.6*Fy u 19.8000 4.6006 g 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=
E ALPHA 1.GT.ALPHAc, RilOi= ( 0. 41 + 0. 59 X ( Fy/ Fa) *
- 0. 5-0. 2 2 / ALPHA 1) / ALPilAi I = .2443 L
- 0. 511ez = 0. 5 X RH0i X 11 = 1.9543 IN C
0.673.GT. BETA 1.LE BETAc, i( Ritoi = (1.358 - 0.461/ BETA 1) / BETA 1 M' = .,5924 s. 0.5Woz = 0.5 X Ritoi X 54.3355 W= 4.7389 IN T FOR Mz, Iez OBE = IN**4 k* - Soz_OBE = 6.7919 IN**3 i
- s. ,
- SSE CASE if t Fa = 0.9XFy = 29.7000 5.6345
$* ( g ALPHAi=1.052/SQRT( 4. 0) X (il/T) X ( Fa / E) *
- 0. 5= 2.3003 BETAi =1.052 / SQRT(24. 0) X (W/T) X ( Fa/ E) *
- 0. 5=
ALPHAi.GT.ALPHAc, J' RllOi= ( 0. 41 + 0. 59X ( Fy / Fa ) *
- 0. 5-0. 2 2 / ALPHA L ) / ALPilA i II"
= .1762 ?
h 0.5Hez = 0.5 X RHoi X H = 1.4097 IN A (f 0.673.GT. BETA 1.LE.BETAc,
,.6 Rlloi = (1. 3 58 - 0. 4 61/ BETAi) / BETAi r' .5032 '
F 4.0259 IN g%~ 0.5Wez = 0.5 X Ritoi X W = = 45.8814 IN**4 % Uf FOR Mz, Iez SSE -
= 5.7352 IN**3 W
Sez SSE ! 8f~ Icz ANALYSIS == 38.9992 IN**4 ' Y
?* ~
.1881E-02 FT**4 KL ' CALCULATE Ay FOR Y-DIRECTION SHEAR OBE & SSE f (E)
- t v SHEAR AREA, Ay = 2XWXT = 1.5296 IN**2 _ [
y = .1062E-01 FT**2 7
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' Ect Eva lu.s t i o4316 n'r!" Ac ;ao 76230.502 &
'. v S utLKCT System Series
!V 1 'j sk
- y. .
i CALCULATE Az FOR Z-DIRECTION SHEAR OBE & SSE k 9i. (F) S!! EAR AREA, Az = 2XHXT == 1.5296 IN**2
- 26 .1062E-01 FT**2 .
+
~ " "
',- (G) CALCULATE Ixx FOR TORSIONAL MOMENT Mx OBE & SSE FOR Mx, Ixx ANALYSIS == 195.7888 INa*4
.9442E-02 FT**4
,4 Ay/A j q .-
INPUT TO IxxSTRING ANALYSIS (STARDYNE Izz Az/A FORMAT): { A Iyy 1881E-02 .8345E+00 .8345E+00
.9442E-02 .1881E-02 t # .1273E-01 c ~
l$? ' ' k
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' rz. .-
g.i q B. Overall Stress Evaluations for Rectangular Ducts .p :[ ff s B.01 Duct String Analysis No. 4316 - 1 . .. . c (( x W (in) == 14
. u Duct Size: H (in) = 14 L t (in) 0.0478 {
Bare Metal Thickness: = 0.0516 <=== Enter Value Daro Metal + Coating: Q Section Properties (based on bare metal thickness): ~.-. } 7 Arg (in'2) = 1.6768 ; F Gross areat Axco (in*2) = 0.857324
~
' Effect. area (OBE): Axes (in*2) = 0.616123 Effect. area (SSE):
s Effect, moment Iyyo (in*4) ==39.16619 39.16619 S of inertia (ODE): Izzo (in'4) = 33.14285 e fr Effect, moment Iyys (in'4) Izza (in'4) = =33.14285
@ of inertia (SSE): Any (in*2) 1.3384 Effect, shear area:
Anz (in*2) = 1.3384 b-H Torsional moment Ixx (in*4) = 131.1632 ft(?' of inertia:
/ Torsional section* Sxx (in*3) == 18.7376 modulus: 30 4 Stiffener or C.A. spacing:1 KLy (in) =
(in) = 192 Effect. length: 192
$ KLz (in)
R Radius of gyration: ry (in) = 5.715476 rz (in) ==5.71547 33.59300 6 7 Maximum of KL/r: (KL/r) max
.g; _
o s, Material Properties (une coated metal thickness for weight): h, y ' E (ksi) (ksi) == 29000 J- -Modulus of Yield strength: elasticity:Py 33 (ASTM A526/A527) U^ Fu (ksi) = 45 (ASTM A526/A527) Ultimate strength:
- r Unit weight: w (lb/ft*2) = 2.909274 ns I.oad Data:
h , Inter, prost.ure : Po(in of v.g.) = 8 <=== Enter Value
<=== Enter value h'p Inter pressure: Ps(in of w.g.)
Correlation factors: C1 C2
=
=
=
14 0.84 <=== Enter Value 1.27 <=== Enter Value i
^
s-; 677', 659' & 643'):- C.v . Panel vibration input (enveloped El.
- p. v. - ,
OBE (4% damping) using maximum of 3 directions
. $. g:
l . A
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- 1 oaTE DaTE Duct Evaluation c1 4316 SUtutCT System Series Jo 76230.502
+
ACCons (in g's) = 1.9
+
ACCoev (in g's) = 1.86 rm! ~ ACCovt (in g's) = 2.1 y, ACComax (in g's) = 2.1 gg SSE (7% damping) using maximum of 3 directions: ACCsns (in g's) = 1.52 ACCsev (in q's) = 1.52 ACCsvt (in g's) = 1.27 ACComax (in g's) = 1.52 . Element Forces from String Analysis No. 4316 - 1
", (enveloped & in element coordinates)
. Dead load: 192 <=== Enter Value 0 Fxd (1bs) =
32 <=== Enter Value Fyd (1bs) = Fzd (lbs) = 164.3 <=== Enter Value E(' Mxd (1b-ft) = 122.9 <=== Enter Value Hyd (1b-ft) = 306.8 <=== Enter value Mzd (1b-ft) = 130.6 <=== Enter Value b; Global seismic loads: OBE: Fxo (lbs) = 586 <=== Enter Value h" Fyo (1bs) = 574.9 <=== Enter Value
#y '
Fzo (1bs) = 155.4 <=== Enter value Mxo (Ib-ft) = 594 <=== Enter Value_-
& Myo (1b-ft) = 594 <=== Enter Value- *1^ Mzo (lb-ft) = 1617.6 <=== Enter Value E 731.8 <=== Enter Value M SSE: Fxs (lbs) =
711.3 <=== Enter value-Fys (1bs) = 7' Pzs (lbs) = 225.9 <=== Enter Value " pt Mxs (lb-ft) = 861.9 <=== Enter Value 4 ( j,L, Mys (lb-ft) = 861.9 <=== Enter Value ' Mzs (lb-ft) = 2000.9 <=== Enter Value
,t.
a
' o
-; A) Internal pressute stress:
1 Q Longitudinal tensile stress in duct= plate 4.162136 per EQ. (3.6.1-1): fxpts (kni) e fxpto (ksi) = 2.866097
@(d- Longitudinal compressive stress at= duct corner 6.292754 per EQ. (3.6.1-2): fxpcs (ksi) g' - fxpco (ksi) = 4.33326G ,
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+
e Ek q_ . 3' QM x k w;h - ,
- a. <
..=w .. . 4 m YY I " '
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- 4 SusJECT
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[L OBE CASE: Longitudinal tensile stress in duct plate fxsto (ksi) =1.045423 f- per EQ. (3.6.1-3): Longitudinal compressive fxsco stress (ksi)at=1.580580 duct corner per EQ. (3.6.1-4): h SSE CASE: Longitudinal tensile stress fxsts in duct plate
- i L
- per EQ. (3.6.1-3): (ksi) =0.842768 f
Longitudinal compressive stress at duct corner fxscs (ksi) =1.274186
' per EQ. (3.6.1-4):
shall be combined Note: The stresses calculated under B)ia v SRSS . with those calculated under D) ' i H
, C) Dlate stresses due to dead load when combined w th #
OBE Axial tons, stress: fxdto (ksi) = 0.071<27 (' Axial comp. stress: fxdco (ksi) = 0.223952 Dending stress: f bzdo ( ksi) = 0.280098 fbydo(ksi)= 0.657996 1 Shearing stresses:
'O' Y-dir. ftydo+fvydo (ksi) = 0.102617 i
Z-dir. ftzdo+fvzdo (ksi) = 0.201466 El SSE: Axial tons. stress; fxdts (ksi) = 0.071727 Axial comp stress: fxdes (ksi) = 0.311625 S ' -- Bending stress: fbzds(ksi)= 0.331003 fbyds(ksi)= 0.777579 ,_ Shearing stresses: : A ' Y-dir. ftyds+fvyds (ksi) = 0.102617 y(y 1 Z-dir. ftzds+fvzds (ksi) = 0.201466 t D) Plate stresses due to global seismic loads - ((,h' OBE:AxialAxial comp. stress: fxgto tens. stress: (ksi) =0.218918 fxqco (ksi) =0.683522
~
^-
Dending stress: fbzgo(ksi)= 3.469277 w f bygo (ksi) = 1.273955 - ,e D' 't Shearing stresses:
?'b Y-dir. f tygo+fvygo (ksi) =0.809954 '
f Z-dir. ftzgo+fvzgo (ksi) =0.496520
% fxgts (ksi) =0.273386 J[
k SSE: Axial tens. stress: fxges (ksi) =1.187748 ^
.[
~V Axial comp. stress:
IE Bending stress: f bzgs (ksi) = 5.071246
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.i. f bygs (ksi) = 2.184470 if Shearing stresses:
s Y-dir, ftygs+fvygs (ksi) =1.083436 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 I o: OBE: fto=fxpto+(fxdto+fbydo+fbzdo)+((fxgto+fbygo+ ksi f bzgo) "2 +f xsto"2)
- 0.5= 8.947000 -
Fto (Allowable) = 0.6*Fy = Fto >= 19.8 ksi l' - fto, OK <=== SSE: fts-fxpts+(fxdts+fbyds+fbzds)+((fxgts+fbygs+ ' fbzgs)'2+fxsts"2)'O.5= 12.91857 ksi ksi Fts (Allowable) = 0.9*Fy = Ftn >= 29.7 fts, OK <===
- $3 , 3 1
- .3%
E.2) Combined axial compression & bending stresses l4 > CBE: fxco(per EQ. (3.4.1-3)) == fxdco&fxgco ksi 0.907474 ' Fao (Allowable) = Fac = 16.62842 ksi s, Fno (0.6*Fy) = 19.8 ksi - 4
? For fxco/Fao <= 0.15: 19.8 ksi (
U Fbyo = Fbzo = A For fxco/Fao > 0.15: 132.3285 kai i e Feyo =
- l: Fezo = 132.3285 ksi U- fxgo(using full area)= ( Axco/ Axq)
- f xco
= 0.290645 ksi Fbyo = 19.75651 ksi 4, i 9.
i % Fbzo = 19.75651 kai
?
-;j#p.
For this case, fxco/Fao = 0.054573 <= 0.15 . USE Fbyo = 19.8 ksi 'b P Fbzo = 19.8 kai dE
+. .
g x , m Overall interaction coefficient (IC): Vf{ u
> p. IC=(fxdco/Fao+fbydo/Fbyo+fbzdo/Fbzo)+(fxpco/Tmo)+ f ,.
4 M ((fxgco/Fao+fbygo/Fbyo+fbzgo/Fbzo)~2+ y (fxsco/Fmo)'2) 0.5 = 0.571492 <= 1.0 OK <=== . [; " ~ fco-fxpco+(fxdco+fbydo+fbzdo)+((fxgco+fbygo+
$r M. f bzgo)
- 2 +f xsco'2)
- 0. 5= 11.14756 ksi n y,4 i p[*.*
SSE: fxes(per EQ. (3.4.1-3)) = fxdcs+fxges
= 1.499374 kai , :p
-Fas(Allowable)= 1.5*Fao = 24.94264 ksi
=
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Duct Evaluatton of 43 6
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Fms (0.9*Fy) = 29.7 kai i= 7 For fxco/ Fan <= 0.15: 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-- ((fxges/ Fan +fb ( f xacn/ Fmo)
- 2 )0.5 ygs/ Fbys
= + f bzgn/ Fbzo) 0.556752 <= 1.0*2+
OK <=== f csa f xpcs+ ( f xdes+ f bydn + f bzds) + ( ( f xqco + f bygs+ y( f fbzgn)'2+fxscs'2)*0.5= 16.25203 kai av - . ff F. 3 ) Combined in-plano chear stress 4 J+ g 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) u 2.704437 > F: Maximum chcar allowable (0.4*Fy): ,* 4 Fvmo (kni) = 13.2 ..; 3 7 Use shoar allowable: M F Fvyo (ksi) = 2.704437 M &Q;y Fvzo (kai) = 2.704437 _?y y' ' 41 - Combined chcar utrossen in Y-direction: F fyyo (kai) =(fyydo+ftydo)+(fvygo+ftygo)
* = 0.912571 . ,p fvyo <= Fvyo,ox <===
hR. k Combined shear strenson in Z-direction: fvzo (kni) =(fvzdo+ftzdo)+(fvzgo+ftzgo) WE h. '??? T~
= 0.697986 ww 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 L nQ u_ .h a _
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longitudinal seams (per EQ.3.5-3): A Fvys (ksi) = 3.940012 Fvzs (ksi) = 3.940012 4 Maximum shear allowable (0.52*Fy): U Fvas (ksi) = 17.16 Use shear allowable: Fvys (ksi) = 3.940012 Fvzs (ksi) = 3.940012 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
<===
Maximum in-plane shear stress = fvzs <= Fvzs[OK ks
~
? 1.186053 -.
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moJECT _ Deco FERML2 - CCH'/2C Duct Ev tuation of 4316
"" #' ,' #. 0^ t3 0^'E *)
ao 76230.502 1 ! sueJECT System Series ,1 m, l
+ +
, +=
2 q_ p:> \ . n: Qg
.B. Overall Stress Evaluations for Rectangular Ducts (Con't) {!
hh d = , c W. 4316 - 2 ; B.02 Duct String Analysis No. . ~ ! W (in) = 19
- x, Duct Size: 19 i H (in) =
= 0.0470
~
Bare Metal Thickness: t (in)
= 0.0516 <=== Enter Value ,
Bare Metal + Coating: ,
~ , ~
<. v a y-
;i Section Properties (based on bare metal thickness):
p Gross area: Axg (in*2) = 3.6328
- . 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 Effect. shear area: Asy (in~2) 1.8164 7" Asz (in*2) = 1.8164 j
I f!j Tor:lional moment Q .. of inertia: Ixx (in*4) = 327.8602
;N ri-
- Torsional section dM modulus:
Sxx (in'3) == 34.5116 { Stiffener or C.A. spacing:1 (in) = 30 ,
- h* Effect. length: KLy (in) = 164
'E.
3u KLz (in) 186 t gg, Ra'dius of gyration: ry (in) = 7.756717 T@ rz (in) = 7.756717 o/ Maximum of KL/r: (KL/r) max = 23.97921 gp . ~ - 6,
% Material Properties (use coated metal thickness for weight): ,
h w p .
'I Modulus of elasticity: E (ksi) = 29000 PR
- Yield strength: Fy (ksi) = 33 (ASTM A526/A527) 7u (ksi) = 45 (ASTM A526/A527)
, N Ultimate strength: 0
.g g Unit weight: w (lb/ft*2) = 2.909274
$[ '
Load Data: q,k. pw j i MP ' Inter. pressure: Po(in of w.g.) = 6.5 <=== Enter Value' "I Q Inter.. pressure: Ps(in of v.g.) = 6.5 <=== Enter Value e p; 47 Correlation factors: C1 = 0.34 <=== Enter Value -W M C2 = .1.27 <=== Enter Value (1 af w ~k 1 Panel vibration input (enveloped El. 677', 659' & 643'): ' SM :q py,; II . OBE (41 damping) using maximum of 3 directions: M1
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en0xet DFCo FFRf:1Ll - C C fi"M. .- __,_.- i@~ ~ s auct Evaluatten et 43it tif_ 76210.502 d cuoxcf System Serien __ l V ACCons (in g's) = 1.9 I ' ACCoev in g's) = 1.86
= 2.1 ACCovt in gs)
V = 2.1
#~ ACComax in g s)
( ssE (7% damping) using maximum of 3 directions: i,j e ACCons (in g's) == 1.52 J I
ACCnev (in g's) = 1.52 ACCovt (in g's) 1.27 ACCucax (in g's) = 1.52 f [: 4316 - 2
~
k Element Forces from String Analysis No.
' de ,' (enveloped & in element coordinates) s 9; ,
t Dead loads 309.3 <=== Enter Value Fxd (1bs) = 80.3 <=== Enter Value a f D.) c Pyd (1bs) = Fzd (lbs) = 159.3 <=== Enter Value i ... Mxd (Ib-ft) = 102 <=== Enttr Value
,f.
Hyd (lb-ft) = 343.9 <=== Enter Value Mzd (lb-(t) = 122.9 <=== Enter Value
~
v, y T' Global seismic loads: r t
' ODE:' Fxo (lbs) = 715.7 <=== Enter Valuo Fyo (lbs) = 443.3 <=== Enter Value
'/ e Fzo (Ibs) = 145.3 <=== Enter Valus
'1' Mxo (1b-ft) = 449.7 <=== Enter Valuo
' Myo (lb-ft) = 556.6 <=== Enter Value Mzo (lb-ft) = 873 <=== Enter Valuo g
- SSE: Fxs (lbs) = 1005.9 <=== Enter Value .
l Fyn (lbs) = 621.3 <=== Enter Valuo L. Fzs (lbs) = 207.7 <=== Enter Value y Mxs (1b-ft) = 610.4 <=== Enter Value 6 Mys (lb-ft) = 782.2 <=== Enter Value' d Mzs (1b-ft) = 1207.3 <=== Enter Valuo , 4, V s. g: < - e; A Internal pressure stress:
' 'd r h)umrMkmew[EdIEa~19ensilofutresseingduqt Long m
a plate m _ . 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 r ( fxpco (ksi) = 3.773094
.g. '
D) Panel vibration stress: n (.
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N"o OBE CASE: 7
' Longitudinal tensito stress in duct plate per EQ. (3.6.1-3): fxato (ksi) =1.045423 i Longitudinal compressive stress at duct corner por EQ. (3.6.1-4): fxsco (kni) ='.580580 SSE CASE: '
, s
,. .e,.
' T Longitudinal tensile stress in duct plate per EQ. (3.6.1-3): f xsts (kni) =0.842768 i
Longitudinal compressive stress at duct corner
'.~ per EQ. (3.6.1-4): fxsca (ksi) =1.274186
>> shall be combined lhte The stresses calculated with thoso calculated under D) under B)iav SRSS .
g
-{ C) Plate stresses due to dead load when combined with l
t: OBE Axial tenu, stress fxdto (ksi) = 0.015140 W( Axial comp. stress fxdco (ksi) = 0.360900 y1 Honding stress: tbrdo(ksi)= 0.170020 3S (bydo(kai)= 0.475751 h Shearing stresses K Y-dir. ttvdo+fyydo (ksi) = 0.079674 7, g .- Z-dir, ftzdo+fvzdo (ksi) = 0.123167-w fxdts (ksi) = 0.08$140
.'4 SSE:Axial Axialcomp.
tens. stress stress: fxdcs (kai) = 0.502469 ( Dending stress: tbzds(ksi)= 0.202221
, tbyds(ksi)= 0.565850
? Shearing stresses:
'N
?. Y-dir, ftyda+fvyds (ksi) = 0.079674 Z-dir. Itr.ds+fvzda.(ksi) = 0.123167 *
, }g
$ D)
Plate stresses due to global seismic loads a f-yo ODE:'6xial Axial tens. stress: f xgto (ksi) =0.197010 fxgco (ksi) =0.835101 , comp. stress l hi Dending stress: tbzgo(kai)= 1.207709 s
% fbygo(ksi)= 0.770001 4+,
E"'
- Shearing stresses Y-dir. ftygo+fvygo (kni) =0.400418
'., if
[y. .. Z-dir. L'tzgo+fvzgc (ksi) =0.236358 . 4 y% a* SSE:Axial Axial comp, strosci fxqts tens. streus (ksi). =0.276893 fxges (ksi) =1.634123 3
- t. fbzgs(kni)= 1.986511 i Bending stress - a Qt i ;
Q;] .- :d) V yA b ). h, k *" hg % i: A,y y/ [A n
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/ 1 . pl d . , 1 ~ . fbygs(ksi)= 1.287044 Y Shearing stresses
?(3 Y-dir. f tygs+ f vygs (ksi) =0.554291 ! r Z-dir. f tzgs+fvzgs (ksi) =0.326588
[ [ , E) Overall strous evaluation: I E.1) Combined axial tension & bending strouses J I) ' O OBE: fto=fxpto+jfxdto+fbydo+fbzdo)+((fxgto+fbygo+ k s ., j
" tbzgo) 2+fxnto*2)*0.5= 5.639451 ksi 19.8 i ' in Fto (Allowable) = 0.6*Fy = Pto >= fto, OK <===
f. !' i SSE: fts=fxpts+{fxdts+fbyds+fbzds)+((fxgts+fbygs+ ksl tbzgs) 2 + f xsts
- 2)
- 0. 5= 6. 997 914 l 29.7 ksi l Fts (Allowable) = 0.9ery = Pts >= fts, OK <=== '
l A < (. i E E.2) Combined axial compression & bending stresses 1xco(per EQ. (3.4.1-3)) == fxdco+fxgco ksi i
$ OBE:
lL . 1.196001 4- Fac = 16.90263 kai
- $I Foo (Allowable)Fmo (0.6*Fy) =
=
19.8 kai i ? li L For fxco/Fao <= 0.15: kai Tbyo a Tbzo = 19.8 l 0 For fxco/Fao > 0.15: 334.0561 kai Feyo = Fezo = 259.7055 ksi l ; f dj fxgo(using full area)== (Axeu/Axg)*fxco i 0.282151 ksi c.
" e 1
- _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 i 6;- g Pbzo = 19.8 kai -
+ overall interaction coefficient (IC):
h s IC=(fxdco/Fao+fbydo/Fbyo+fbado/Fbzo)+(fxpco/rmo)+ l {! ((fxgco/Fao+fbygo/Fbyo+fbzgo/Fbzo)*2+ 4 ( f xsco/ Fmo) ' *t ) 0.5 = 0.413820 <= 1.0 + %- OK <=== , }7[ fco=fxpco+jfxdco+fbydo+fbzdo)+((fxgco+fbygo+- 7 fbzgo) 2&fxsco*2)*0.5= 8.006242 ksi
> - y{a ~
j n SSE: fxes(por EQ. (3.4.1-3)) = fxdes+fxges 1 ; Q J
= 2.136593 kai ..
",J W ksi m f j; Fas ( Ali.owable) = 1. 5
- Fao = 25.35395 .
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^ Duct Evaluation of 4316 ;o 76230.502 SunJtct Systen Series 1 0
U{ Fms (0.9*Fy) = 29.7 kai For fxes/ FanTbys <= 0.15:
= Fbzs = 29.7 ksi 1
f' For fxes/ Fan > 0.15: 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 '
For this case, fxes/Fas = 0.084270 <= 0.15 kL USE Thys = Fbzs = 29.7 29.7 kai ksi 6 overall interaction coefficient (IC): n;p u newm % m% .,. ._.
~ 1C= ( f xden/ Fas+ f byds / Fbys+f b2ds / Fbas) + ( f xpcs/ Fan)'?~*"", '"
((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+
, tbzgs)*2+fxscs*2)'O.5= 10.11403 kai
,(
@ E.3) Combined in-plane shear stress OBE:
Allowabic chear stress for ducts with Pittsburgh lock I longitudinal seams (per EO.3.5-1): t Fvyo (ksi) = 2.316954
?L Fvzo (ksi) = 2,316954
'g,*qi - Hax4. mum shear allowable (0.4*Fy); 13.2 3 0 Fvmo (ksi) =
9 Use shear allowableFvyo (ksi) = 2.316954 L k ' Tvro (ksi) = 2.316954
/ _, .
h' Combinedfvyo (ksi) shear=(fvydo+ftydo)+(fvygo+ftygo) stresses in Y-directions 0.480093
;( =
fyyo <a Fvyo,0K <=== 't-
$3 Co7bined shear=(fvzdo+ftzdo)+(fvzgo+ftzgo) stresses in Z-direction:
rh ' fvzo (kni) 0.359525 .. 9; p ', _ i r .-
, =
fvzo <= Fvzo OK <=e= + .' t-kuk t hq Haximum in-plane shear stress = 0.480093 1 q f.4w ,
$$ F. 3 .,
tj t 7 Allowable shear stress for ducts with Pittsburgh lock E s:@o: . N
</M & Tj:
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#1 9 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 rvzs (ksi) = 3.475431 s Haximum shear allowable (0.52*ry) = 17.16 0' ryms (ksi)
/. '
000 shear allowablet Tvys (ksi 3.475431 ) - Tvzs (ksi)) == 3.475431 ' e Combined shear stresses in Y-direction =(fvyda+ftyda)+(fvygs+ftygo) f vya (ksi) ,. i = 0.633966 <=== b e fyys <= Fvyn,0K ( > Combined chear stresses in Z-directions fvts (ksi) 0,449756
=(fv2dn+ftzdo)+(fvzgs+ft29s)
L ,
=
OX <=== , g_ fvts <= TVZo1kn Maximum in-plane shear strero = 0.633966
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, l 1 .
D. Overall Streun D.aluations for Hectangular Ducts (Con't) D.02 Duct String Analysis No. 4316 - 2 (Con't) [ 19 Duct Size: W (in) = 19 k H (in) = 6 = 0.0478 3 Daro Hotal Thickness: t (in)
= 0.0516 <=== Enter Value d Dare Metal + Coating:
Section Proportien (based on bare inctal thick ess):
> Axg (in~2) = 3.6328 Group area:
E Effoct. area (OBE): Axco (in*2) = 0.857022 r' Effect. area (SSE); Axes (in"2) = 0.615559 l Effect. moment lyyo in*4) = 82.40558 N}}. of inertia (ODE) : Izzo (in*4) = 82.40558 Effect. moment Iyys ((in*4) = 69.28337 f y' of inertia (SSE): Izzn (in*4) == 69.28337 Any (in*2) 1.8164 Effect. shoal area: 1.8164 l7 i Asz (in~2) = Torsional moment 327.8602 of inertia: Ixx (in*4) = lL'i- g Torsional nection , 34.5116 K! modulus: Sxx (in*3) =
= 30
% Stiffener or C.A. spacing:1 (in) 4 Effect. length: KLy (in) = 164 186 KLz (in) r 7.756717 Radius of gyration: ry (in) a M '.' [ n rz (in) =
=
7.756717 23.97921 l${ Haximum of KL/r (KL/r) max M Haterial Propertien (use coated metal thicknens for weight): ? Modulun of clasticity: E (ksi) = 29000 Yield strength: Fy (ksi) = 33 (ASTM A526/A527) Ultimate strength: Tu (kni) = 45 (ASTH A526/A527) Unit weight: w (Ib/ft 2) = 2.909274 Load Data: . e.- Inter, prensure: Po(in of v.g.) = 8 <=== Enter Value gi 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 ue Panel vibration input (enveloped El. 677', 659' & 643');
.[
m;i - ODE (4% damping) using maximum of 3 directions: ,
, ,'1,
, %, ll-x ;
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, Duct Evaluation of 4316 Jo 76230.502 .,,
7 susJCCT - System Series . 141,
+ '
,3 ACCons (in g's) = 1.9 '
ACCoeV in q'sh = 1.86 ACCovt in gsD = 2.1 in g sj = 2.1 M ACComax SSE (7% damping) using maximum of 3 directions: Q-- u { ACCans (in g's) == 1.52 ACCsev (in g's) = 1.52 1.27 1
*- ACCsvt (in g's) b' ACCamax (in g's) = 1.52
- g; x,; from String Analysis No. 4336 - 2 4
- Element Forces (enveloped & in element coordinates) 6-Dead load: 309.'s <=== Enter Value 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: K> Fxo (1bs) == 715.7 <=== Enter Value OBE:* Fyo (1bs) = 443.3 <e== Enter Value 145.3 ;=== Enter Value-Y- Fzo (lbs) = 449.7 <=== Enter Value
$; Mxo (lb-ft) 556.6 a== Enter value 1,
Hyo (Ib-ft) == 873 *.'=== Enter Value 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) 610.4 <=== Enter Value
- v. Mxs (Ib-ft) == 782.2 <=== Enter Value,
>: Mys (1b-ft) 1207.3 <=== Enter Value_. y e Mza (Ib-ft) =
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) '
g fxpto (ksi) = 2.866097 L 1.ongitudinal compressive stress T por EQ. (3.6.1-2): fxpcs (ksi) at duct corner
= 2.328814 s
- ?w _
fxpco (ksi) = 1.603649 ~ -a y 3 3,g
.y B) Panel vibratjon stress:
- g. E"g
- g. .-g a . ,{k
.hg e -[; \ps I .l%
j
.:. w I .
x_-
c
* =< w s. . . ,. o __ .
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"" O " ~ 0*ft 0411 Duct Evaluation of 4316 so 7G230.502 i l ta;eatet Systen Series _
m
; 4 c y.
! f, q
'l OBE CASE:
- Longitudinal tensile stress in duct platef xsto (ksi) =1.045423 3
l ,' per EQ. (3.6.1-3): Longitudinal compressive stress at duct corner fxsco (ksi) =0.584939 ( per EQ. (3.6.1-4):
" SSE CAS,':
y Longitudinal tensile stress fxstsin duct plate C per EQ. (3.6.1-3): (ksi) =0.842768 7 Longitudinal compressive stress at duct corner per EQ. (3.6.1-4): fxsca (ksi) =0.471549 l_ shall be combined
'
- Note: The stresses calculated under B)ia v SRSS .
with those calculated under D)
, t C) plate stresses due to dead load when combined with
,i OBE:Axial Axial comp, tons. stress stress: fxdto fxdco(ksi) (ksi)== 0.085140 0.360900 l w' Dending stress:
- tbzdo(ksi)= 0.170020 tbydo(ksi)= 0.475751 ",
Shearing stresses: Y-dir, f tydo+f vydo (ksi) = 0.079674 [j i Z-dir. ftzdo+fvzdo (ksi) = 0.123167 i SSE:Axial Axialcomp. tons. stress: stress: fxdco fxdts (ksi) (ksi) == 0.085140 0.502469 I{ Bending stress: fbzds(kai)= 0.202221 A fbyds(ksi)= 0.565858 i ff Shearing stresses: I r p. Y-dir. f tyds+fvyds (ksi) = 0.079674 % p, 2-dir. f tzds+f vzds (ksi) = 0.123167 % d sz s D) plate stresses due to global seismic loads M f
. e OBE:AxialAxial comp. tons. s.ieers: fxgta (ksi) =0.197010 stress: fxgco (ksi) =0.835101 E.
y E Bending stress: fbzgo(ksi)= 1.207709 . 4 tbygo(ksi)= 0.770001 m ., q M $. Shearing stresses - V 1H Y-dir. f tygo+fvygo (ksi) =0.400418 ,j T Z-dir. f tzgo+fvzgo (ksi) =0.236358 b fxgts (ksi) =0.276893 , 7 SSE: Axial tons, stress N Axial comp stress: fxges (ksi) =1.63412'l s fbzgs(ksi)= 1.986511
,. . M
{E. g, :; Bending stress - g ee f
& y@J l ;M
- n i h, ,
u: . l-c. q~f: 4
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- tbygs (ksi) = 1.287044
[L Shearing stresses: J-Y-dir. ftygs+fvygs (ksi) =0.554291 Z-dir. ftzgs+fvzgs (ksi) =0.326588 E) Overall stress evaluation: E.1) Combined axial tension & bonding stresses OBE: fto=fxpto+(fxdto+fbydo+fbzdo)+((fxgto&fbygo+ ksi fbzgo)*2+fxsto*E)*0.5= 6.009959 19.8 kai y: p Fto (Allowable) = 0.6*Fy = Fto >= fto, OK <=== f xdts+ f byds+ f bzds) + ( ( f xgts+f bygs+ F3E: fts=fxpts+l2+fxnts*2)*0,5= 8.664460 ksl (bzgs) 29.7 kai Fts (Allowable) = 0.9*Fy = Fts >=-fts, OK <=== f' E.2) Coobined axial compression & bending stressos ' OBE: fxco(per EQ. (3.4.1-3)) == fxdco+fxgco 1.196001 ksi f,
"; = Fac = 16.90263 k91
;.H '
Fao (Allowable) Fmo (0.6*Fy) = 19.8 kai p for fxco/fao <= 0.15: kai Pbyo = Fbzo = 19.8 , th For fxco/Fao > 0.15: kai
?; Feyo = 334.0561
! Fezo = 259.7055 kai
; fxgo(using full area)== (Axeo/Arg)*fxco kai s 0.282151 19.78317 kni Fbyo =
'r 19.77840 kai
[k [ Fbzo =
\
s For this case, fxco/Fao = 0.070758 19.8
<=kai0.15 fiw USE Fbyo = .'
$ Fbzo = 19.8 kai ,,
9 m t overall interaction coefficient (IC): 1 . N . IC=(fxdco/Fao+fbydo/Fbyo+fbzdo/Fbro)+(fxpco/Pmo)+
- ((fxgco/Fao+fbygo/Fbyotfbzgo/Fbzo)*2+ 0.287144 <= 1.0 p,c (fxsco/Fmo)*2) 0.5
=
1 '.
. OK <=== 's IR v
u fco-fxpco+(fxdco+fbydo+fbzdo)+((fx co+fbygo+ " kai fbzgo)~2+fxsco*2)*0.5= 5.48331 ,, , f$. y :)c 1 Ds SSE: fxes(per EQ. (3.4.1-3)) == fxdcs+fxgcs 2.136593 kai ' 1" 25.35395 kai Fas(Allowable)= 1.5*Fao =
-;Q a w$
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"" b#1 " ~I 1 ~ pit Duct Evaluation of 4316 so 76230.502 SUGXC f System Series
- tk Y<
h Fan (0.9*Fy) = 29.7 kai ' n
'P For fxcs/FasTbys <= 0.15:
= Fbzs = 29.7 kai
% A For fxcs/Fas > 0.15: 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 29.7 <=kai 0.15
>"> USE Fbys =
kai j Fbzs = 29.7 i i overall interaction coefficient (IC): - e IC= ( f xdes / Fas+ f byds/ Fbys+ f br ds / Fbz s) + ( f xpcs/ Fms) + t ((fxges/Fas+fbygs/Fbys+fbzgs/Fbzs)"2+ = 0.299483 <= 1.0 <=== 4 (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' s Allowable shear stress for d' cts with Pittsburgh lock f1 longitudinal seamsFvyo (per (ksi)
EQ.3.5-3): 5 = 2.294724
,c, Fvzo (ksi) = 2.294724 .%
6 Maximum shear allowable (0.4*Fy): 13.2 W y Fvmo (ksi) = 3
'1' gei -
P Use shear allowableFvyo (ksi) = 2.294724 Fvzo (ksi) = 2.294724 F[h/ ':>
- W' d(-
ifs ,
*f '
Combined fvyo (ksi) shear-(fvydo+ftydo)+(fvygo+ftygo) stresses in Y-direction: p;t = 0.4 BOO 93 <=== s' fvyo <= Fvyo,OK 4: if' Combined shear stresses in Z-direction: ,* h, fvro (ksi) =(fvzdo+ftzdo)+(fvzgo+ftzgo) 0.359525 s 7' = <=== S
%' fvzo <= Fvzo OK +
kok
!?.* Maxitium in-plane shear stress = 0.480093 ,:n a*8
.A I'
.g gA$
4 + SSE: ' h, p.1 Allowable shear stress for ducts wit.h<Pittsburgh lock .s d,, .l,[ z{.,+
.t +
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( - PAO,stCT Deco FERMT ? - CCHVAC Duct Evaluat.icn c: 4319 9a rt 5 5_ f 7l oatt ous System Series so 76230.502 4 SututCT - { '7 va, 2 longitudinal seams (per EQ.3.5-1): *-
; Fvyn (ksi) == 3.325442 e,,
y Fvzu (ksi) 3.325442 gy Maximum shear allowable (0.52*ry): 17.16 ; 2 Fyms (ksi) = L g Uno shear allovables Fvys (ksi) = 3.325442 s 3.325442 Fvzs (ksi) = C
?,
t Combined shear stresses in Y-directions
,"; . fyys (ksi) =(fyyds+ftyds)+(fvygo+ftygs) 0.633966
=
fyys <= Fvys,0K <=== K ,
>U
, !- Combined shear Ivra (ksi) stresses in Z-directiont
=(fvads+ftzds)+(fvzgs+ftzgs)
. = 0.449756 <===
s fvzs <= Fvza,0K a. Maximum fn-plane shear stress = 0.633966 ksi f 4
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t # ' D l Duct Evaluation of 43:6 so N230.502 I b Gus#C f Systen Series 7 ! 4 1 s- ; s_ y.
- f f D. Overall Strecs Evaluations for Rectangular Ducts (Con't) 3 4316 - 3 5 E D.03 Duct String Analysis No.
4-- r 10 y i Duct Size: W (in) = 10 H (in) = Bare Metal Thickness: t (in) = 0.0478 3 L Bare Metal + Coating: = 0.0516 <=== Enter Value l- (, P- 5 s Section Properties (based on bare metal thicknesu): LI Gross area: Axg (in*2) = 1.912 j- O' E Effect. area (OBE) : Axeo (in'2) = 0.829775 N Effect. area (SSE): Axes (in'2) == 0.597476 Effect, moment lyyo (in*4) 17.02515
= 17.02515 of inertia (OBE): Izzo (in*4)
- hr[--0 Effect. moment Iyys (in'4) = =14.37405 Izzs (in~4) = 14.37405
_ of inertia (SSE) : Any (in'2) 0.956 l
![i- Effect, shear area:
j- Asz (in*2) = 0.956 P- N'k Torsional moment i fe of inertia: Ixx (in*4) = 47.8 [4- I Torsional section c- ', medulus: Sxx (in'3) =
=
9.56 60 L Stiffener or C.A. spacing:1 (in) 4
# W Effect. length: KLy (in) a 84 ifa !' KLs (in) = 102
[-- 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 y Modulus of elasticity: E (ksi) = 29000 b Yield strength: Fy (ksi) = 3.3 (ASTM A526/A527)
- i. Sa Ultimate strength: Fu (ksi) == 45 (ASTM A52G/A527) i Unit weight: w (1b/ft"2) 2.909274 17 N- Load Data: '
h[- C- - N is Inter, pressure: Po(in of v.g.) = 6.5 <=== Enter Valuo
!?- ,
Inter. prensure: Ps(in of v.g.) = 6.5 <=== Enter Value '
' Correlation factors: C1 = 0.84 <=== Enter Value "
e C2 = 1.27 <=== Enter Value 3 ' w" Panel vibration input (enveloped El. 677', 659' & 643'); P-x 4e---- 1 OBE (4% damping) using maximum of 3 directions: q .. S .* N.. y'.-
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? "C ".$02 Pf 40JCC7 ~ DECO FERM} L a 4, 76230 Y Duct Evaluation of 431A 1 ;
ty_ Systen Series ! /k, Sva/C1 L.h 1 : is ' 19 'N in gs) ==
$A a ACCons 1.86 kW ACConv in g's in g s = 2.1
% ACCovt = 2.1 ACComax in q's t,N 1- SSE (7% da:eping) using maximum of 3 directionst 6 in q's) = 1 52 ACCans in q's) = 1.52 ,.
ACCsev = 1.27 in gs) s; ACCsvt in g s) = 1 52 ACCsmax M f, 4316 - 3 TP Element Forces from String Ar.alysis No.
(enveloped t. in element coordinates) s [h i 15.2 <=== Enter Value t 6t , Dead load: fxd (lbs) == ad Fyd (lbs) = 14.3 <=== Enter Value N 52.2 <=== Enter Value-Fzd (lbs) = 0 <wa= Enter Value fe Mxd (lb-ft) = 65.2 <=== Enter Value I Myd (1b-ft) = 15 7 <=== Enter Value Mad (lb-ft) ' 7 p-., 4 Global soismic loads: 9 ODE: fxo lbs) = 620.1 <=== Enter Value 644.8 <=== Enter value e-Fy-; lbs) = 134.3 <=== Enter Value y f Fzo lbs) = 557.6 <=== Enter Value-Mxo (lb-ft) == 283 <=== Enter Value K.
# Myo (1b-ft) = 1315.3 <=== Enter value ,
o, Mzo (1b-ft) ti, Fxs (lbs) = 593.6 617 <=== <=== Enter Enter Value Value;
%s4 SSE:
Fys (Ibs) == <=== Enter Value 4 "' 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 , j; e . W 7,M iA) Internal pressure stress: y a Longitudinal tensile stress fxpts kai in duct
= 3.961502plato -
;J. per EQ. (3.6.1-1): fxpto kai = 3.961502 ..
y A -; Longitudinal compressive fxpcs stress(ksi) at duct corner
= 5.989414 ,
per EQ. (3.6.1-2): fxpco (ksi) = 5.989414 +
-a
{d
, j 4; p4 7-
~ .
fp Qg, j LB) Panel vibration stress: , 3;[Q 3& U4 -t 4! b -, . q ; y; * -
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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 i per EQ. (3.6.1-3): f xsts (kni) =1.337812 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 . i C) plate stresses due to dead load when combined with OBE: Axial tens. stress; fxdto (ksi) = 0.007949
- t Axial comp. stress: fxdco (ksi) = 0.018318 Bending stress: fbzdo(ksi)= 0.055329 c
fbydo(ksi)= 0.229777 Shearing streasus:
- Y-dir, ftydo+fvydo (ksi) = 0.014958 L Z-dir, f tzdo+fvzdo (ksi) = 0.054602 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: ('i, Y-dir. f tyds+f vyds (ksi) = 0.014958 I e Z-dir. ftzds+fvzds (ksi) = 0.054602 e .
- g. D) Plate stresses duo to global seismic loads
. b OBE: Axial tens. stress: fxgto (ksi) =0.324320 g Axial co.ap. stress: fxgco (ksi) =0.747310 Dending stress: fbzgo(ksi)= 4.635376 "'
- y. fbygo(ksi)= 0.997347 p ,
Shearing stresses: f tygo+ fvygo (ksi) =1.374393 e Y-dir, , l 0 ftzgo+fvzgo (ksi) =0.840397 i
- Z-dir. ( '
3 E, SSE: Axial tens. stress: fxgts (ksi) =0.310460 ( {- e Axial comp. stress: fxges (ksi) =0.993594 Bending stress: (bzgs(ksi)= 5.518692 8+ 3 , l 2; \ W, '
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,1 +
4 is fbygn(ks1)= 1.161258 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 1 E.1) Combined axial tension & bending strences o OBE fto=fxpto+jfxdto+fbydo+fbzdo)+(3843(fxgto+fbygo+ kal f bzgo) - 2 + f xsto* 2 )
- 0. 5= 10. 4 kai 19.8
' Fto (Allowable) = 0.6*Fy = Fto >= fto, OK <===
SSE: fts-fxpts+(fxdts+fbydn+fbzds)+((fxgts+fbygs+ kol 1 f bzgs)
- 2 + f xsts
- 2 ) '9. 5= 11. 4 24 41 koi 29.7 If Fts (Allowable) = 0.9*Fy = Fts >= ftu, OK <===
.b t"
E.2) Combined axial compression & bending stresses .' 4
- OBE: fxco(por EQ. (3.4.1-3)) == fxdco+fxgco 0.765628 kai
.( = Fac = 16.87824 kai Fao (Allowable) Pno (0.6*Fy) = 19.8 kai ,
[<; ~ im For fxco/fao Pbyo <= 0.15:
= Fbzo = 19.8 kai -
E/ For fxco/Fao > 0.15Feyo = 352.7291 kai
, Fezc = 239.2211 koi p' "', fxgo(using full area)== (Axco/Axq)*fxco 0.332269 koi t, .
Tbyo = 19.70134 koi
- , Fbzo = 19.77249 kai . , f. -
A,. 0.045361 <= 0.15 y-For this case, fxco/Fao = 19.8 koi
^ t-(
USE Fbyo = [@R '
~
Fbzo = 19.8 koi t
}lj n;. overall interaction coefficient (IC):
gi{s
'f n IC=(fxdco/Fao+fbydo/Fbyo+fbzdo/Fbro)+jfxpco/Feo)+
- 2+
5- ((fxgco/Fao+fbygo/Fbyo+fbzgo/Fbzo) 0.670314 <= 1.0 <===
@ (fxsco/Fmo)*2) 0.5
=
i g; OK . 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 1.019036 kai 'l* Q{-? 25.31736 kai
? Fas(A11ovable)= 1.5*Fao = N;
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> Duct Evaluation of 4316 so 76230.502 SUSXCT System Series _
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 i fxgs(using full area)==(Axes /Axg)*fxes 0.318410 kai Tbys = 29.68212 kai Tbzs = 29.67364 kai
!f; n
For this case, fxes/ Tbys Fan == 0.040250 29.7
<= 0.15 kai USE 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 <=OK1.0 <===
{(, (fxsco/Fms)*2) 0.5 n fcnafxpco+jfxdcs+fbyda+fbrds)+((fxges+fbygs+
~
, fbzgs) 2+fxsce*2)*0.5= 14.28818 kai
(. [* E.3) Cotabined in-plano, 4 hear strono c
.l P ODE Allowable shear stress for ducts with Pittsburgh lock longitudinal coams (por FvyoEQ.J.5-1):3.45)260 (kai) =
l 3.499260 E Fvzo (ksi) =
> Haximum shear allcwable (O.4*Fy): 13.2 9 D Fvmo (ksi) =
p ~ 000 shear allowables ,. p,6 Fvyo (ksi) = 3.499260 3.499260
. .ji -
y sis Fvzo (ksi) = ,
%3 Combined shear=(fvydo+f stresr.ostydo)+(f in Y-directions "i' f vyo (ksi) vygo+f 1.389351 tygo) h_ =
f yyo <= Fvyo,0K <=== s. , {d . Combined shear=(fvzdo+ftzdo)+(fvzgo+ftzgo) stressos in 2-direction: N fvzo (ksi) 0.895 W. = <=== 12 v fvzo <= Fvzo OK S Haximum in-plane shear stress = 1.389351 kol k: ye Sh
' SSE
, 4
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/ Duct Evaluation of 4316 so 76210.502 r,un;t e t System Series __
e I o longitudinal seams (per EQ.3.5-1): = 5.248890 Tvys kni)
- Fvro kai) = 5.248890 i' Maximum orcar allovable (0.52*ry):
Tvss (ksi) = 17.16 Use shear allovablet rvys (ksi) = 5.248890 Tvra (kni) = 5.248890 lt . Combined shear strouses in Y-directiont l
# fvyn (kni) = ( f vyds+ f tyds) + ( f1.386004 vygs+ f tygs) I
=
fvys <= Fvyn,0K <=== i; ' ' Combined shear stresses in 2-directiont tvzs (ksi) =(f vzdu+ f tzds)+ (f vzgs+ f tzgs) a
= 0.916652 <===
v , fvzs <= fvzo,0K
. i Maximum in-plano shear stress = 1.386004 kni i I i .h I k ,',b k.
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" Overal!, Stress Evaluations for Rectangular Ducts (Con't)
D. D.04 Duct String Analysis No. 4316 - 6 [ Duct Size W in) == 16 16 H in) o Barc Metal Thickness t in) = 0.0478 Bare Metal + Coatings = 0.0516 <=== Enter Value 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 b Effect. moment in*4) = 45.88151 Iyys (in*4) 4 of inertia (SSE): = 45.88151 Izza 1.5295 Asy (in*2) (in*2) == Effect, shear area:
', Anz ( 1.5296
%'( Torsional moment i
[ of inertia: 1xx (in*4) = 195.7888 f Torsional section F' modulus: Sxx (in*3) = 24.4736 A Stiffener or C.A. spacing 1 (in) == 30 i Effect. length KLy (in) = 168 [i KLz (in) 168 Radius of gyration ry (in) = 6.531972 , l [J. 4 rz (in) = 6.531972 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 Yield strength:
Fy ksi = 33 (ASTM A526/A527). ru ((ksi i i < Ultimate strength: = 45 (ASTM A526/A527) l , Unit weight: w (1b/ft"2) = 2.909274 i Load Data; y A<, <2 \ Inter, pressure: Po(in of W.g.) = 8 <=== Enter Value= 'S l W~ 14 <=== Enter Value. 7 k p Inter. pressure: Ps(in of w.g.) = Correlation factors: C1 = 0.92 <=== Enter Value
%e C2 = 1.27 <=== Enter Value Q t; pMs -
panel vibration input (enveloped 4 El. 6778, 659L 0 643J):.: y{ ll M. OBE (4% damping) using maximum of 3 directions: W M hk h g,(. Cm
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-i
ACCons (in g'sh = 1.9 ACCoeW f in qs3== 1.86 ACCovt fin g s) 2.1 ACComax din n's) = 2.1 SSE (74 damping) using maximum of 3 directionst .
ACCann in q's) = 1.52
; ACCnew in g' = 1.52 ACCnyt in g' = 1.27 ACCsmax in g' = 1.52
'e i Element Forces from String Analysin No. 4316 - 6 ,
+
h (enveloped & in element coordinates) S:
' Dead loads 243.1 <=== Enter Value rxd (1bu) == 0.7 <=== Enter value ryd (15s)
Tzd (1bs3 = 267.3 <=== Enter Value Mxd (1b-ft) == 77.5 <=== Enter Value Hyd (1b-ft) = 697.7 <=== Enter Value 1 Mtd (1b-ft) 19.8 <=== Enter Value N( r, Global noismic loads: ODE: Txo (1bs3 == 531.9 <=== Enter Value h9- ryo (1bs) 418.3 <=== Enter Value rzo (Ibs) = 195.1 <=== Enter Value Mxo (1b-ft) = 238.6 <=== Enter Value - Hyo (1b-ft) = 734.2 <=== Enter Value f Hao (1b-ft) = 1011.7 <=== Enter Value SSE: Txo (1bs = 1009.8 <=== Enter Value hi Fys (1bs = 638.8 <=== Enter Valua . E. ti Tzs (Iba = 312.6 <=== Enter Value
$ Mxa (1b-ft) = 384.3 <=== Enter Value p Mys (Ib-ft) = 1177.9 <=== Enter Value ;
- % Hza (Ib-ft) = 1623.3 <=== Enter Value.
- x. 'O hit [?
n; pp. h, A) Internal pressure stress: ; as N
- Longitudinal tennile strean fxpts (kni)in duct plate
= 4.558530 "i g4 L;
- per EQ. (3.6.1-1): fxpto (kai) = 3.139059
' ' Longitudinal compressive f xpcs stress (kni)at
= duct 6.292754corner l '*2 por EQ. (3.6.1-2): fxpco (kni) = 4.333266 .f m m.
B) Panel vibration stress:
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Duct Evaluation of 4316 so 76:30.502 svaxcf Systen Serios
-i .1a s L.
3 y 8~ ODE CASE fL 1,ongitudinal tensile stress in duct plate =1.144987 l per EQ. (3.6.1-3): f xsto (ksi) 1,ongitudinal compressive fxncostress (kni)at~1.580580 duct corner por EQ. (3.6.1-4): e SSE CASE
@p+ <.A t,ongitudinal tensile stress + a.
f xstsin(kni) duct plate t per EQ. (3.6.1-3): a0.923032 i.ongitudinal compressive stress f xscs (ksi)at=1.274186 duct corner h- por EQ. (3.6.1-4): shall be combined
? Note: The stresses calculated under B)via SRSS .
With those calculated under D) C) Plate stressou due to dead load when combined with OBE Axial Axial comp, tons. stress fxdto (kai) = 0.079465 jjp (, stress fxdco (ksi) = 0.285017 Dending stress: tbzdo(kci)= 0.0349c2 r
- fbydo(ksi)= 1 232693 Shearing = 0.038457 Y-dir,stresses:ftydo+fvydo (ksi) 9 Z-dir. ftzdo+fvzdo (ksi) = 0.212751 y
SSE:Axial Axialcomp. stress fxdts tens. stress: (ksi) = 0.079465 fxdcs (kni) = 0.396647 Bending stress: fbzds(ksi)= 0.041428 t byds (ka i) = 1.459829 p{1 1 Shearing stresces: 7
- /f Y-dir. f tyds+f vyds (ksi) = 0.038457 ; g
+
18 Z-dir. ftzds+fvzds (ksi) = 0.212751 ' y ' D) Plate stresses due to global seismic loads W ODEt Axial tons, stress fxgto fxgco (ksi) =0.173868 (ksi) =0.623616
,p Axial comp. stress fbzgolksi)* 1.787468
{;ls* : Dending stress: fbygo(ksi)= 1.297182
%- r dJ
% Shearing Y-dir,stresses:f tygo+f yygo (ksi) =0.390461 f tzgo+f vzgo (kai) =0.244541 c
(fh h.;;' Z-dir. 1 rde fxqts (ksi) =0.330086 -
~T SSE Axial Axial comp.
tens. stress: stress: f xqcs (ksi) =1.647613 .. Bending stress: Ibzgs(kni)= 3.396505 J., g,i O)' 7. g, % i V.i ik ' a e: dy; 'i g;
*= fto, OK <=== +
SSEt f tsa rxpts+ (f xdts+ f byds+ f brds) + ( ( f xgts+ kal f bygs+ fbzgs)'2+fxsts*2)*0,5= 12.39884 Fts (Allowable) = 0.9aFy = 29.7 kai Fts >= fts, OK <===
,?
E.2) combined axlal enmpression & bending stresses fxco(per EQ. (3.4.1-3)) = fxdco+fxqco E OBEt = 0.908634 kul Y4 = Fac = 16.85978 kai Foo ( Allowable) 19.8 kai Fmo (0.6*Fy) = G For fxco/Fao <= 0.15: 4 19.8 kai h;l Fbyo = Tbzo = l' For fxco/Fao > 0.15: Feyo = 225.7466 kol
., Fezo = 225.7466 kai N
fxgo(using full area)= (=Axeo/ Axg)
- f xco I: 0.253334 kai
' Fbyo = 19.77778 kai
@0 Fbzo = 19.77778 kni ,l g For this case, fxco/Fao = 0.053893 <= 0.15
[. t. USE Pbyo = Fbzo = 19.8 19.8 kas i kai 'k M: , . overall interaction coefficient (Ic)t g, Ic=(fxdco/Fao+fbydo/Fbyo+fbzdo/Fbzo)+{2+fxpco/Fmo)+
% ((fxgco/Fao+fbygo/Fbyo+fbzgo/Fbro) g (fxsco/Fmo)*2) 0.5
= 0.508434 <= 1.0
<=== l
,y > OK -
I f co= f xpco+ j f xdco+ f bydo+ f bzdo) + ( ( f xqco kai + f bygo+ -4 fbzgo) 2+fxsco*2)*0.5= 9.917025 . g # Js: ? SSEt fxes(por EQ. (3.4.1-3)) = =f xdes+f xges 4;- p0 + 2.044260 kai M M Fas(Allowable)= 1.5*Fao = 25.28967 kai
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v, . Fan (0.9*Fy) = 29.7 kai
! 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 h For this case, fxes/Fas = 0.080833 29.7
<= kai 0.15
- b- USE Fbys =
p Fbts = 29.7 kai y;
' overall interaction coefficient (IC):
- IC=(fxdes/Fas+fbyds/Fbys+fbzds/Fbzs)+jfxpcs/Fms)+ 2+
hk- ~ (fxges/Fas+fb (fxacs/Fms)'2)ygs/Fbys+fbzgs/Fbzs) = 0.544084 <= 1.0 ( 0.5 <=== p OK { e ten = f xpco+ ( f xdes+ f byds + f bzds) + ( ( f xqcs+ f bygst N. kai 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) :
Fvyo (ksi) == 2.477965
,, Fvzo (ksi) 2.477965 ..
4 Maximum shear allowable (O.4*Fy): Fvmo (ksi) = 13.2 h+ Use shear allowablat L Fvyo (ksi) = 2.477965 - r* ' . c Fvro (ksi) = 2.477965 6% '
'T N Combined shear stressen in Y-direction:
f y- fvyo (ksi) =(fvydo+ftydo)+(fvygo+ftygo)
= 0.428919 <===
; ;gh. r fvyo <= Fvyo,OM M Combined shear=(fvado+ftzdo)+(fvzgo+ftzgo) stresses in Z-directiont fvzo (kni)
,= f. = 0.457292 <=== ,k pm fvzo <= Fvzo OK J!' ks1 Maximum in-plano ahear stress = 0.457292 Q w ,h[
SSE 4 Nk/,,- ' i,. 3 Allowable shoor stress for ducts with Pittsburgh lock
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I c .curo. 5(v e =v cc w se i oy,o y , , gggggge i 70*** COMPUTATlON vw 0 h N a,,. '*t W 'w r . SHEET 4 ~4* 'D x Oh l l 5 , enostet orco rtMt! 2 - ccHvAc 5"' " O"O oJI can l, 1 Duct Evaluation of 0 16 i Supstcf System Series so 76230.502 , i j i l= , l7 1' longitudinal seams (por EQ.3.5-1)t ;-
;i 1; Fvys (ksi = 3.589175 '
4 k- Fvza (ksi)) = 3.589195 t' .v Maximum shear allowablo (0.52*Fy): i .-
'#! Fvas (ksi) = 17.16 Uno shear allowables
?
Fvys ksi = 3.589195 Fvzs ((kni))
= 3.589195 p Combined shear stresses in Y-direction
- 1 y fyys (ksi) =(fyyds+ftyds)+(fvygn+ftygs) l-G, = 0.644514 4
fvys <= Fvyn,OK <=== S* Combined shear stresses in Z-directiont ! I. - fvru (ksi) =(fvzdu+ftzds)+(fvzgs+ftzgs) ; i
= 0.605550 p OK <===
Maximum In-plano ahear stress = 0.644514 fvts <= Fvzakka !! Irl. e. i )[ f,
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SHEET 4/27/46 x PRO >tCT Deco TERMI 2 - CcHVAC Duct Evaluation of 4316 s>< t t [9 ts 17 p,,, 3,,, SututCT ' System Ser ies Jo 76230.502 ,
.4.
H. Overall Stress Evaluations for Rectangular Ducts (Con't)
! D.05 Duct String Analysis No. 4316 - 7 W (in) = 16 Duct Size
- H (in) =
= 0.0478 16 Bare Metal Thickness: t (in)
= 0.0516 <=== Enter Value Bare Metal + Coating:
Section Propertion (based on bare metal thickness);
- i. Axg in'2) = 3.0592 Cross area:
Effect, area (OBE): Axco in*2) = 0.843810 Effect, area (SSE): Axes in*2) = 0.606520 Effect. moment lyyo (in*4) = 54.33562 of inertia (OBE) : Izzo (in*4) = 54.33562 3 Effect, moment Iyys (in*4) = =45.88151 Izzo (in*4) = 45.88151 of inertia (SSE): 1.5296 Effect. shear area: Asy (in*2) Anz (in*2) = 1.5296
.( Torsional moment of inertia: Ixx (in'4) = 195.7888 v Torsional section*
i modulus Sxx (in~3) == 24.4736 Stiffener or C.A. spacing 1 (in) = 30
? Effect. length KLy (in) = 72 KLz (in) 96 (in) = 6.531972 Radlus of gyration: ry i rz (in) = 6.531972
/ Maximum of KL/r: (KL/r) max = 14.69693 p,. '
Y p Material Properties (use coated metal thickness for weight): s, Modulus of elasticity: E (kni = 29000 h Yield strength Fy (ksi)) = 33 (ASTM A526/A527) f P2 Ultimate strength: Tu (ksi) = 45 (ASTM A526/A527) ? >
*> Unit weights v (1b/ft"2) = 2.909274 .
J _; Load Data 3 g_ i ' . Inter. pressure: Po(in of v.g.) = 8 <=== Enter Value' 1 . Inter. pressure: Ps(in of W.g.) = 14 <=== Enter Valuo; - O. C1 = 0.92 <=== Enter,Value1 4 Correlation factors: 1.27 <=== Enter Value
- C2 = ,
f Panel vibration input (enveloped El. 677', 659' & 643'): OBE (4% damping) using maximum of 3 directions: s di
- 1
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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 i O SSE (7% damping) using maximum of 3 directionst ACCsns (in g's == 1.52 9 ACCsev (in g's 1.52 ACCavt (in g's = 1.27 ACCsu x (in g's) = 1.52 1 t-Element Forces from String Analysis No. 4316 - 7 . 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) =
,. Mxd Ib-ft) = 77.5 <=== Enter Value l' Myd Ib-ft) = 697.7 <=== Enter Value- ?-
O - Mzd Ib-ft) = 19.8 <=== Enter Value. ' L, bl
;y Global seismic loadst p
Fxo (Ibs) = 531.9 <=== Enter Value, OBEt 418.3 <=== Enter Value 2; Fyo (1bs) = W Fzo (1bs) = 195.1 <=== Enter Value fE . Mxo (1b-ft) = 238.6 <=== Enter Value Myo (Ib-ft) = 734.2 <=== Enter value
" Mzo (1b-ft) = 1011.7 <=== Enter Value SSE: Fxs 1bs) = 1009.8 <=== Enter Value b.' Fys Ibs) = 638.8 <=== Enter Value 7 Pzs 1bs) = 312.6 <=== Enter Value. .
X. Mxs 1b-ft) = 384.3 <=== Enter Value Mys Ib-ft) = 1177.9 <=== Enter Value ~
<ly f =
07 Mza lb-ft) 1623.3 <=== Enter Value $ L .$ - p4 IY
- t. 6.
[ M 's " A) Internal pressure stresst 41
-ll 3-Longitudinal tensile stress in duct plate fxpts (kni) = 4.558530 a
.) ;, per EQ. (3.6.1-1): fxpto (ksi) = 3.139059 M Longitudinal compressive stress J
per EQ. (3.6.1-2): fxpcs (ksi) at duct corner
= 6.292754 -
fxpco (ksi) = 4.333266 4 , .s -. n Pi D h. yJ* j D) Panel vibration stress: f r.
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% a t; 1 '; OBE CASE:
ae Longitudinal tensile stress in duct plate 1~ a; wo por EQ. (3.6.1-3): fxsto (kni) =1.144987 , Longitudinal per comp)ressive EQ. (3.6.1-4 : stress fxsco (ksi)at=1.580580 duct corner SSE CASE: s Longitudinal tenslie stress in duct plate l~ 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 N~; OBE: Axial tons. stress: fxdto (ksi = 0.079465 Axial comp. stress fxdco (ksi)) = 0.288098 Dending stress: . fbzdo(ksi)= 0.034982 fbydo(ksi)= 1.232693 w Shearing stresses 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
- i. fbyds(ksi)= 1.459829
[C R Shearing stresses: ^
.' Y-dir. ftyds+fvyds (ksi) = 0.038457 f
a Z-dir. f tzds+fvzda (ksi) = 0.212751 (y 2t.N
.g g 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 }
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, , ;r 3
. tbygs(kni)= 2.464574 4' Shearing stresses:
a: 4 Y-dir. ftygs+fvygs (ksi) =0.606057 Z-dir. ftzgs+fvzgs (ksi) =0.J92798 E) Overall stress evaluation: E.1) Combined axial tenslor t bending stresses l 1 ODE: f to=f xpto+ j f xdto+ f bydo+ f bzdo) + ( (f xgto+fkal bygo+ tbzgo) 2+fxsto"2)*0.5= 7.940031 19.8 kai
/ Fto (Allowabic) = 0.6*Fy = Fto >= fto, OK <===
j SSE: fts-fxpts+(fxdts+fbyds+fbzds)+((fxgts+fbygs+ ksl
;' tbzgs)*2+fxsts*2)*0.5= 12.39884 Fts (Allowable) = 0.9*Fy = Fts >= fts,koi 29.7 OK <=== ,
a,5 E.2) Combined axial compression & bending stresses ODE: fxco(per EQ. (3.4.1-3)) == fxdco+fxgco 0.918453 kai J = Fac = 17.08049 kai
*L( Tao (Allowable)
. Fmo (0.6*Fy) = 19.8 kai For fxco/FaoTbyo <= 0.15: = Tbzo = 19.8 kai For fxco/Fao > 0.15:
kai Feyo = 1229.065 2
.. Fezo = 691.3491 kai >
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:: - 4 For this case, fxco/Fao = 0.053772 19.8
<= kai 0.15 ,
t Tbyo = ' USE J S I" Fbzo = 19.8 kai , ,4
'S Overall interaction coefficient (IC):
D , d' f.. IC=(fxdco/Fao+fbydo/Fbyo+fbzdo/Fbzo)+(fxpco/Fmo)+ + ((fxgco/Fao+fbygo/Fbyo+fbzgo/Fbzo)*2+ <= 1.0 4' (fxsco/Fmo)*2) 0.5
= 0.508318 <=wa OK '
fco=fxpco+(fxdco+fbydo+fbzdo)+((fxqco+fbygo+ f fbzgo)*2+fxsco*2)*0.5= 9.926305 kai <.g
,f .
. b'
~
W fxcs(per EQ. (3.4.1-3)) == fxdcs+fxges L Mb' " SSE: 2.065716 kai ' Fas(Allowable)= 1.5*Fao = 25.62073 ksi ., , fig Q.. dQA,
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; SututCT System Series .., ,
,j~(()
, N Pas (0.9ery) = 29.7 kai ja For fxcs/ Fan <= 0.153 t
Tbys = Tbts = 29.7 kai b For fxes/Fas > 0.15 Foys = 1843.597 kai
- 1037.023 kai Feza =
fxgs(using full area)= =(Axes 0.409551
/Axg)*fxcs kai Fbys = 29.69340 ksi
[ Tbzs = 29.68827 ksi
- For this case, fxes/ Fan = 0.080626 <= 0.15 ,
': 29.7 kai 1 USE Thys =
29.7 t i Tbzs = kai
'l 1-1
'1 overall interaction coefficient (IC): ,
1 IC= ( f xdes/ Fas+ f byds/ Fbys+ f bzds/ Fbza) + ( f xpcs/ Fas) +
; :'t (fxges/Fas+fb (fxscs/Fms)'2)ygs/Fbys+fbzqs/Fbza)"2+
( 0.5 = 0.543879 <= 1.0 ox <=== a f xdes + f byds+ f bzds) + ( ( f xges+f bygs+
! t fes=fxpca+{2+fxscs*2)'O.5=
tbrgs) 15.82791 kai r ,(
. V ,
E.3) Combined in-planc shear stress l, l
.r, { -
OBE: [
~
r O Allowable shear stress for ducts Vith Pittsburgh lock r
' longitudinal seams (per EQ.J.5-1): = 2.477965 Fvyo (ksi) m 4
Fvzo (ksi) = 2.477965 Maximum shear allowable (0.4*Fy): 13.2
; }7h Fvmo (ksi) =
O # si . Use shear allowable: Fvyo (ksi) = 2.477965 e 2.477965 c,9 N.6 Y" Pvzo (ksi) = i. 4 *, vv. . l, Combined shear stresses in Y-directiont l [% f yyo (kui) =(fyydo+ftydo)+(fvygo+ftygo) 0.428919 y y = fvyo <= Fvyo,0K <=== ain O ta Combined shear=(fvzdo+ftzdo)+(fvzgo+ftzgo) fvzo (ksi) stresses in Z-direction: ;' c = 0.457292 <=== 9#* OK . . l' Maximum in-plane shear stress = 0.457292 fvzo <= Fvzok ks .y c w y b
; Q., 06:
SSE ( 113 , Allowable shear stress for ducts with pittsburgh lock , p(d . w M ;'bd l m% m; t?? - ) 4 3 gyg, g-v n, . gy y
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M K t t: longitudinal seaan (per FvysEQ.3.5-1):).589195 (ksi) == 3.589195 y e Fvzs (Kni) 4 h , W Maximum shear allowablo (0.52*Fy): 17.16 Fvms (ksi) =
~
1 i i ph } S' Use shnar allowable:Fvyn (ksi) == 3.589195 w
* > Fvzu (ksi) 3.589195 3
g Q- Combined shear stresses in Y-direction:= ( f vyds+ f tyds)i'.+ ( f yygs+ fvys (ksi) 0.644514 <=== y [, = fyys <= Fvys,0K h :# . y~ , Combined shear stresses in Z-direction:=(fvads+ftzds)+(fvzgs+ftzgs) fvzs (ksi) = 0.605550 <=== ' f r-: A' fvas <= Fvzs OK jy 0.644514 ksi Maximum in-plane shear stress = .,
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OATE 1 suaxcl CV& TEM-GEREG 80- 76230.502 o . f The data contained in this attachment are generated using - the STARMAP is a companion program of / STARMAP post processing feature. Q-.i STAROYNE vhich is used to perform the system string analyses, k" The purpose of the tabulated data is to present the forces and moments in the ductvork by each duct size for DL, OBE and SSE conditions. Maximum and ninimum values for each duct size are also 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
- prints the data in tabular form.
S against the string analysis outputs by the checker, o The string analysis outputs are contained in the following N calculations:
,s m '
g; E DC-5763 CCHVAC Concern Resolution Task Duct String Analysis and Support Evaluation of [ it ( 2268 System Series
% J DC-5764 CCINAC Concern Resolution Task pk Duc.t String Analysis and Support Evaluation of
' 2848 System Series a
- E CClWAC Concern Resolution Task M DC-5765 Duct String Analysis and Support Evaluation of ,
2849 and 4126 System Series 4
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CCHVAC Concern Resolution Task Duct String Analysis and Support Evaluation of g' 4 t+ .. 2850 System Series
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T'-R 1 OF 9 8& DtCO ttuv&O STsttu 4316 1.2.3 iet Apr 12 14:37:31 19 % DC*SIO [ E ;
- $1AmmAP veralon 4.41
- Nedet 4 eeport : Etenant
[ % Ferent 1 $1AaDiet Der / Beam Element title : Peor 1 14*x14+ -4 h' *4 ' l ,' M output Set 1
- D00 LOAD (00 8i&M LLtMEu! L0A05 ') 9,*
tutAs tcasicW BEucluG 8tel#C C* ' Ax1At P v2 swtA8 v3 M1 M2 M3 8 TAM 1.744179D 2 1.470957b 0 stAMG 0.0 1.476710t+0 5.80%31t 1 8.393562D1 1.064550D1 e 1 JA 1.084550D1 3.522116t*1 1.854904 0 2 e' JS 100.0 1.476710D 0 5.80%31t 1 8.393562t*1 3.52211M *1 1.854904b 2 atAMG 2 JA 0.0 1.476710D 0 5.809631t 1 *1.787671t*1 1.084550t*1
" 1.T87671t*1 1.084550t+1 9.183669t*1 1.821361t*0
\ JS 100.0 1.47671M
- 0 5.8096314 1 9.183669t+1 1.821361t+0 stAMG 0.0 1.4 7671M +0 5.80%3ff 1 4.308971t*1 1.08455M +1 3 JA 1.064550t + 1 1.6429700 1 2.&38047D0
.ts 100.0 1.476710D 0 5.8c 4 31t 1 4.308971E
- 1 5.80 % 311 1 6.68%69D1 1.08455M + 1 1.642970D1 2.838047D0 6tAMG 4 JA 0.0 1.4767100 0 1.005 Mob 2 3.854732D0 JS 100.0 1.476710t+0 5.809631t 1 6.685469D 1 1.064550t+1 1.084550D 1 1.005660t*2 3.854732D 0 SEAMG 5 JA 0.0 1.476710t+0 1.4 M19% 0 7.947839D 1 7.947139D 1 1.084550t+1 6.082681t+1 3.11713M+0 A. JB 100.0 1.476710D 0 1.4 M 19M *0 4.066%0t+1 1.co4550t+1 6.082681t*1 3.1171330 0 stAMG 3- 6- JA 0.0 1.4767100 0 1.4 75199t + 0 1.66T3500 1 1.4M193D0 4.0M340E+1 1.084550t*1 2.049999D1
[ . Je 100.0 7 JA S0
- 1. 47671M
- 0 1.476710t+0 1.4751NDO 6.149856E v 1.084550D1 1.06M50t*1 2.049999t+1 3.946000t*1 1.667350 6 1 stAMC 4.381303t*0 J8 V: 0 1.4767100 0 1.4 M19960 6.149856( 4 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.
3.946000D 1 -8.543119D1 2,28880M *0
' J8 100.0 1.475200l+0 -1.4767110 0 6.8085146 1 8.563119t+1 2.258803t+0 stAMG 9 JA 0.0 1.4M200bo 3.4410578 1 3.9e1229D 1 3.M60000 1 5 1.457444f + 0 U 46 10'3.0 1.+ 7520000 3,441c578 l 3.96122W et 3.9460000 1 1.007210D1 1.00721061 1.457444b0 8tAMG 10 JA 0.0 1.4M200D0 3.4410571 1 -6.796244b o 3.946000D 1 J5 100.0 1.4 5200b 0 3,4410571 1 6.7962440 0 3.9460000 1 2.649862D1 6.257402t 1 3,946000t*1 2.649862t+1 6.2574021 1 stAMG J 11 JA 0.0 1.475200t*0 3.4410571 1 4.45487!b t 3.4410571 1 4.4548Mt+1 3.9460000 1 2.174768t
- 1 2.530737t 1 c J8 100.0 1.4 M 200D 0 1.4 520000 3.4410571 1 5.926267t+1 3.946000t+1 2.1747686 1 2.530737t 1 stAMG 12 JA 0.0 3.4410571 1 5.926267D 1 3.946000D 1 8.598641b1 1.199368t 1 JS 100,0 1.475200f *0 1
3.946000t+1 8.598841b 1 1.197368 0 1 6tAMG 13 JA 0.0 -1.4752006 0 7.6D0%t 2 5.383398b t 6.20550M*1 3.309453 0 1 p$ (. JS 100.0 1.475200 0 0 7.673034t 2 5.383398t*1 3.M6000t+1 6.205503t*1 3.3094534 1 atAMG lf 14 JA 0.0 1. 4 75200t +0 7.6730%t 2 5.9985136 0 3.946000D 1 4.844060E 1 1.4 52006 0 7.673034t 2 5.9985130 0 3.946000D 1 5.0058000 1 b JB 100.0 15 JA 0.0 1.4 5200t*0 7.6730%E 2 3.937813b t 3.M4000D 1 5.005300D1 -4.844060t 1 atAMG 7.67*,0%f 2 3.937813D1 3.94600001 -6.476862D1 7.081517t 1 J8 100.0 1.475200 0 0 1.4752000 0 7.673034t 2 8.901883D 1 3,946000t+1 6.4768621 1 7.081517t 1 atAMG 16 J4 0.0 7.337029b1 3 JS 100.0 1.4 M200E 0 7.6730 KI 2 8.9018a31 1 3.946000D ? 9.441189D 1 1.236859t+2 3,9460000 1 9.441189t+1 7.337029b 1 stAMG 17 JA 0.0 1.4M20060 3.643754t 1 7.046138t+1 1.21M15t +0 Je 100.0 1.4 M 200D 0 3.6437548 1 1.23M59D 2 3.9460000 1 0.0 1.915790t+0 8.027965t 2 -1.T30116t+1 1.421460t+1 8.215705t+0 4.863944t 1 s(AMG , (' 18 JA JB 100.0 1.9157W60 8.027965t 2 1.730116t+1 1.421460D 1 6.15725M*1 7.339769b t 1.4214606 1 6.157256b t 7.3397691-1 stAMG p* 19 JA 0.0 1.915790D 0 8.027965t 2 2.457950D 1 Ja 100.0 1.9157906 0 8.0279651 2 2.457950D 1 1.421460t+1 1.423063D 1 9.815593t 1 20 JA 0.0 1.915790(+0 8.027965t 2 9.21M9301 1.421460t+1 1.423063D 1 9.8155930 1 atAMG Q 8.027965t 2 9.217593t+1 1.421460t+1 9.101317t+1 1.048432t+0 . y Je 100.0 1.915790C+0 1.915790D 0 6.5260071 1 4.682442b 1 1.421460t+1 9.101317bt 1.0484320 0 stm 0.0 4 W 21 JA J8 100.0 1.915790t+0 6.5260071 1 4.682442t+1 1.421460D 1 2.6356M b 0 2.567691E 1 4 22 JA - 0.0 1.9157904 0 6.5260071 1 9.3%67600 1.421460D 1 2.635673 6 0 2.567691b 1 stAMG 9.33467M +0 1.421460D 1 -1.798462D1 1.698364t+0 Je 100.0 1.915790D 0 6.5260071 1 1.698364t+0 stAMG 1.915790D i 6.3260071 1 3.93260M+1 1.421460E*1 1.798462t*1 v 23 JA 0.0 1.048166t+2 3.139306t+0 3.932608t*1 1.421460D 1 E 24 JA Ja 100.0 0.0 1.915790b'1 1.475200t+0 6.5260071 1 1,391091t+0 1.643284E+2 9.032750t+0 1.135837t+2 5.1542231 0 stAMG g
$ Je 100.0 1.475200t +0 1.39109190 1.643284b2 9.032750D 0 2.779120t*2 6.547314t+0 6.54 5140 0 stAMG .t.
-1.475200t+0 1.661740t+0 8.2ST258bt -9.032750 0 0 2.779120t*2
- 25 ' JA. 0.0 1.475200D0 -1.M1740bo 8.287258t + 1 9.032750 0 0 -1.294044b 2 3.56M 75t+0 M Je 100.0 3.f 6947500 SEAMG
-1.4M200t+0 1.661740t+0 3.097081t+1 9.032750D 0 1.294044E+2 26 JA = 0.0 7+ Ja 100.0 1.475200t +0 -1.661740s 0 3.097081bt 9.0327506 0 7.39ue4bt -5.9495986 1 ^e 1.4M199t+0 1.146315b1 7.3966609 1 9.032747t+0 5.9495988-1 stAMG N 27 JA 0.0 1.661740D 0 7.396660D1 -2.144M401 2.192600E+0 ,
R JS 100.0 1.661740D 0 -1.4M 19990 1.1463159 1 > 1.4 M 1990 0 3.846953D1 T.396M0t + 1 2.144734t +1 -2.192600D0 SEAMG 7" 28 J4 0.0 1.661740D 0 5.451314E+0 J8 100.0 1.661740D0 -1.4M199DO . 8469530 1 7.196660D 1 6.353184D 1
-1,661740t+0 1.4751996 0 6.789734t* I.396660t+1 -6.353184t+1 5.451314t+0 stAMG 29 JA 0.0 8.586111t+0 Ja 100.0 1.661740 0 0 *1.4751991+0 6.789736i. 7.396660t+1 2.078137t+2 t ?, 2.078137D2 -8.586111t+0 SEAM 30 JA 0.0 -1.661740t+0 3.06099990 7.000432b . -7.396660D 1
$Q'1 J8 100.0 1.661740D0 3.060999t*0 F.000432D 1 3.060999D0 4.2844346 1 7.396660D 1 6.780510t+1 2.464114 b 0 7.396660t+1 -6.780510D 1 2.464114DO BEAMG
^*
31 JA 0.0 -1.6617400 0 wm Y
- asyg . . ;g
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l l '
~ m ATTACHMENNA@ ~
Of to CCWAC $111tM 43161.2.3 SHEET OF 9 .
%M6 9 Y -
. pri Apr 12 14:37:35 1994 MOD
$1AasuP versten 4.41 Report s Element p, Model 1
-. Fernet t $1AA0 fat Sar/ seam Element .
Title PecP 1 14+I14+ -- R Pi
% tutput set 1
- OtA0 LCAD (DL1 tLtutuI LOAD 5 <
8IAN R, ttupluG MuDinG intAA snot ites10s 4 . AdlAt af M2 M3 v2 V3
}il StAM P
7.39666M *) *1.788358O 1 3.6578 m +0 1 1.M1740D0 3.060999t*0 4.284434D) 3.65T88M*0 SumG Js 100.0 2.864317D1 7.3946M*1 1.788358O1 0.0 1.661740t 0 3.06099W+0 1.792038O 1 7.48413tt+0
. 32 /4 3.060999DO 2.864317D1 7.36660t*1 JS 100.0 1.661740t+0 T.39666M
- 1 l.792038t*1 7.484131E o stAMG JA 0.0 1.M1740t
- 0 3.060999D 0 +4.56t816t*1 7.494308t*1 *1.131038t+1 33 J8 100.0 1.M17&OD O 3.06099% + 0 4.561416DI 7.396660D 1 7.49430M*1 1.131038D 1 LEAMG
- 5. 53049t + 1 7.356660t*1 0.0 1. M17604 + 0 9.123543D0 3.069791t+1 34 JA 5. 53049t+1 T.396660D 1 4.730921D1 J8 100.0 1.6617400 0 e.123% 3D 0 7.396660D1 4.730921E+1 3.069791U1 8tAMG 1.661740D 0 9.123543DO 2.867301t+1 5.008544t+1 35 'JA 0,0 2.86001E*1 7.396660D 1 1.082394D2 J4 100.0 1.6417400 0 9.123%3D0 7.396660D 1 1.082394D2 5.008544t*1 M AMG 34 JA 0.0 1.M17&Ot +0 9.123%3D0 2.77644TD1 T.396660(+1 4.923985t+1 6.947297E*1 1.6617400 0 9.1235&3D 0 2.776447t+1 6.947297t+1 SUMG ss 100,0 4.923985D1 1.661740D 0 0.12354M
- 0 5.662195t+1 -T.396660t+1 8.886049D 1 31 JA 0.0 9.1235431*0 5.662195D1 7.39M60t+1 7.108179D1 8.886049D 1 StAMG JS 100,0 1.661740D 0 7.396660t+1 7.108179t+1
-1,661740t+0 6.41390Tt+0 2.155455D 1 38 JA 0.0 6.413907D 0 2,155455D1 7.396660D 1 3.605565D1 9.928309D 1 Ja 100.0 1.661740D 0 7.396660D 1 3.605565t+1 9.928309D 1 stAMG 0.0 1.661740t+0 e.613907D O -5.129330D1 1.097057t*2 39 JA 7.3966600 1 3.688917t + 1 JB 100.0 1.6617400 0 6.41390TD0 5.129330D 1 7.396660t+1 3.688917t+1 1.097057t+2 SEAMG 0.0 1,661740t+0 6.41390TD 0
- T.200044D1 1.538899t+2 1.201283D 2 40 JA 7.700044D 1 T.39666M *1 Ja 100.0 1.661740D 0 6.413907t*0 1.538899t +2 1.201283D 2 StAMG
, 9.406792t+1 7.396660t+1 0.0 1.66tT404+0 6.413907t+0 7.396660D1 3.067502D 2 1,305509D2 E 41 JA JS 100.0 1.661740D 0 6.413907t+0 9.406792t+1 3.067502t+2 1.305509D 2 stAMG 2
^ 42 JA 0.0 1.661740D 0 1.586874D 1 1.333380D2 7.39460t+1 1.234105D 2 1.087314D Z 4 1.661740 D 0 -1.586874t+1 1.313380t
- 2 T.39666M *1 1,087314t+2 stAMG JS 100.0 1.146455D2 T.396460D1 1.23410$t+2 JA 0.0 1.661740D 0 1.5 M874t+1 43 JB 100.0 1.661740D 0 1.586874D 1.58474D1 1 1.146655D2 7.396660D 1.137550 0 2 9.1905520 1 3.425451D1 0 d.42%51D
- stAMG 8.69118M +1 64 JA 0.0 -3.429050t+1 3.196190D 1 1.03931M*2 f 3.196190D 1 1.586874t*1 1.137550D2 2.540346D 1 1.039318D 2 StAMG JS 100.0 3.429050t*1 1.137140D 2 2.55880 m 1 1.339180D 1 1.1010021 1 t.586874D1 1.279104t*2 45 JA 0.0 1.586874D1 1.13T1406 2 6.014843D1 JS 100.0 1.339180D 1 1.101002t+1 3.803615E+1 atAMG 1,661740D 0 1.58687&t+1 5.5945334+1 1.2289000 2 1.279104D 2 to JA 0.0 1.228900D 2 6.5090371+0 3.600092t+0 1.584874D1 5.594533#*1 Je 100.0 1.661740D 0 1.586870D 1 1.661T&ct+0 8.539354D 1 6.509040D 0 1.2289000 2 3.600992D0 stAMG 47 JA 0.0 1,661740D0 8.5393% D1 6.509M OD O 6.215735t+1 1.3111731 13 JS 100.0 1.586870D 1 6.215785D1 atAMG 1.596350D 2 1.586874t*1 1.661740D 0 2.9309900 14 6.519037t +0 48 JA 0.0 1.461740D0 2.930990014 2.630535D 0 2.512021E+1 J8 100.0 4 596350D 2 1.586874t*1 1.919720t+2 1.586874D1 1.o6174cD0 3.164140014 2.63053$t+0 2.512021E+1 SUMG N 49 JA 0.0 1.M174000 3.1641400 14 2.828293b l4 3.441691E 14 J8 100.0 1.91072M
- 2 1.586874D1 2.618264D'1 7.330209t 1 SuMG iX 3.934771t+1 6.185730E+1 JA 0.0 1.124690t 1 1.1050060 1 1.142962t+2 4.855650E 1
/ 50 1.10500eO i 3.934771t+1 6.185D0D1 C; Ja 100.0 5.124690t-1 6.192940E*1 1.142592f+2 4.8556500 1 St.ueG 5.1240000 1 1.106242t 1 3.47434M*1 51 JA 0.0 0 5.126000E 1 -1.108242t.1 3.474343D1 6.192940E+1 3.645447D1 2.373845b 1 2.3738450 1 atAMG Ja 100.0 6.013398t+1 1.799160t*1 6.957341E*1 52 J4 0.0 4.405960t 1 2.840958t 1 2.062737t*1 6.6352821 1 b' 1 <
2.840958E 1 6.01339eD 1 1.799160E*1 Ja 100.0 4.405960t 1 2.062737t+1 6.6352820 1 suMG 4.605960t 1 2.840958D I 8.051076D1 -1.799160E+1 1.089956t+0 53 JA 0.0 1.799160E+1 1.414740t+2 Ja 100.0 4.405960t 1 2.840958D 1 8.051076D 1 1.414740D 2 1.089956t+0 suMG 2.840958D 1 *1.373586D2 1.799160t+1 54 JA 0.3 4.4059600 1 1.799160D 1 2.558937D2 1.326608t+0 4.405960t 1 2.840958e 1 1.373586t+2 1.3266080 0 suMG JS 100.b 9.72TT29t+1 1.799160t+1 2.558937t*2 55 JA 0.0 4.405960E 1 T.384903t 1 6.133917t+1 1.503728t 1 F 4.405960t 1 7.3849030 1 9.72T729D1 1.799160t+1 1.503728U 1 stAMG 0** JS 100.0 8.086587t+1 -1.799160D 1 6.133917t+1 56 JA 0.0 4.405960t 1 7.38490 M 1 2.7i1810E*1 4.5832336 1 7.38 903t 1 8.086587t+1 1.799 40E*1
-*. JS 100.0 4.6059606 1 1.7999001 2.)o1810D 1 4.583233D 1 BUMG 57 JA 0.0 4.4059600 1 7.384903e 5 5.053837t+1 1.799160t+1 -1.443036t+1 1.0734860 0 Ja 100.0 4.405960t 1 T.3849030 1 5.053837D 1 2.296190t+1 1.073486t*0 stAMG Ji* 2.1037980 1 2.947674t+ 1 -2.475540D 0 1.544612t+0 58 JA 0.0 8.3380606 1 2.967674D1 2.475540E*0 8.942020D 1 2.103798D 1
-8.3380604 1 2.532010t+0 S.941862D 1 1.544612t+0 stAMG Ja 100.0 h"" $9 JA 0.0 8.336730E 1 2.109063t 2.1090610 1 1 -4.433441D1 4.433441D1 2.532010D 0 9.864172t+0 2.014917t+0 -
W M Je 100.0 8.3367300 1 1 P1 top 1 14=x14= 5 W
~
Title
, OJtpJt Set 1
- OtAD (CAD (OL) value
-/
N ' t Set ' MAX / Mis saamary table set 10 44 34.2905
<fM p&m Minimum 1 seem tal A Aztet forte
@4 ; ... .
nm-
- u. w . NM Rw Vej ~
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be 9 k DECD CCmVAC $f$1tm 45161,},]
~
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+' stammAP version 4.41 8 el Apr 12 14:37:39 1996 esport : Element 4 =
M( meest i Forent 1 $1AR0 Tut Ser/Sean Element y
-(
1% ,
+
7[^ - Title : Peop 1 14*I14= 4 ~'
/ output Set 1
- DEAD LOAD (DL) 49 191.9T2
! masium 1 T Seen End A theer2 f orce minimus 1 48 44
*15.6687 31.9619 maaiaum hf **
1 . x nintam 1 54 *137.359 ' 4 Seem (M A Sheer) f orce 1 24 144.328
' maa lmas .,
&~ team EM A forcpe ulniman 1 46 122.89 )
M, - 1 10.6455 - W maala m 1 1 1 ei Seem (M A moment 2 minimm 1 42 25
+306.75 277.912
) )
maximm 1 5 O4 - minisus 1 45 +103.932 *
, *'y aN . . .
T Seas (M A moment 3 42 130.551
' maalma 1
[l% = ~ 49 *191.972 Deam EM 8 Aalet f orce minious 1 m
. ' menimm 1 44 34.2905 :P
%9 , 44 +31.9619 minimm 1 I 1
.- team trus 8 sheer 2 force 1 48 15.8687 h maa t sum minimue 1 24 -164.328 1
Seen EM S Sheer 3 Force maa t am 1 54 137.359 10.6455
> 1 minimm 1
$ )) seen K M 8 Torma maalam 1 46 122.89 ;
. A minimm 1 24 277.912 JO Seem E M 8 mesent2 manium 1 41 306.75 130.551
> K; , minimm 1 41 team (M e nament3 127.91 g$ 45 g
me stam 1
.4
.titte t P90P 1 14*I14' i pT4 f ; tht}ut Set 2
- Ost L0A05
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? 1.425654t+1 2.00278E+1 '
M 12 JA 0.0 4.1014500 2 1.484158D 2 2.080766E+1 2.237343E+2 1.484158E+2 1.425654 D 1 2.00270E+1 b Ja 100.0 4.101450E+2 2.237343t*2 stAMC 3.6971506 2 5.0123M
- 1 1.300664(+1 2.0632786 1 2.080766D 1 13 JA - 0.0 1.300664D 1 2.0632706 1 1.4 W 95t+1 1.314344t+2 C JS 100.0 3.697150D 2 5.8312360 1 1.4 W 95D 1 1.314344E+2 stAmc 2.042484t+0 2.063278t+1
,- 14 JA 0.0 3.3850600 2 4.91182SD1 2.00270E.1 1.278068t+1 1.325097D 2 JS 100.0 3.385060(+2 4.91182SE*1 2.042484t+0 1.325097D 2 BEAMG A. 9.557304D O 2.063278E+1 1.278068D1 0.0 3.211790E+2 4.44WOD1 u 15 JA JB 100.0 3.211790(+2 4.44 WOE +1 9.557304D0 2.00270D1 1.771669t +1 1.771669E+1 2.033796E+2 2.033796E+2 DEAMC i'
to JA 0.0 2.955320(*2 4.0025229 1 2. t 41172t + 1 2.00278D1 2.105262t+2 2.1411729 1 2.043270E+1 2.436924D 1
'- Je 100.0 2.955320D 2 4.0025221 1 2.063278t+1 2.436924t+1 2.105262t+2 stAMC 2.58798cD 2 6.653263D 1 2.97420?t+1 17 JA 0.0 2.974202f+1 2.06327DD 1 1.890944t+1 2.502673E+2 JS 100.0 2.587980C+2 6.6532 0(+1 1.105105t+2 EEAMc
( 2.880196E+1 1.28&39M
- 1 2.845726D 1 3.481194D1 ,d 18 JA 0.9 9.405320E+1 2.M5720D1 1.507225t+1 9.115167D1 J5 100.0 9.405320(+1 2.880196(*1 1.286396t+1 7 - N$dQs y'
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;~ 19 JA 2.8457?M +1 4.054360t+1 1.478620D 2 9.354890t*1 3.11TT34D1 1.3539?st*1 E JS 100.0 2.84572M *1 4.054360t+1 1.4786200 2 SumG 20 JA 0.0 1.03905M*2 4.655540D1 2.530514D 1 5.51450 D 1 1.771647D 2 2.84572M *1 Ja 100.0 1.0390%D 2 4.6555400 1 2.530574t +1 2.84572M+1 5.51450 D 1 1.T718471+2 MneG 0.0 1.293300D 2 1. W 613D 2 3.480859t+1 21 JA 1.574147t+1 1.25850M*2 Je 100.0 1.2933000 2 1.364613D 2 3.480859D 1 2.845720D 1 1.574147t+1 1.258506t+2 HANG' 1.145246 0 2 3.224640D1 2.84572M +1
+ 22 JA 0.0. 1.5245700 2 3.224640D1 2.M 572M + 1 8. MOM 4t + 1 4.120172t*2
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- 2 1.34524M*2 4.1201T2t+2 stAmG s
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- 1 2.845726t*1 8.M 0644t+1 23 JA 0.0 1.658140t+2 1.33799M*2 1.58015M+2 7.0540 1D 2 1.337993D2 3.302433D I 2.84572M *1 JB 100.0 1.658140D 2 1.971328t*2 1.235118t+3 SEAMG 6.43614M +1 24 JA 0.0 2.419910D 2 2.160C75D2 4.917165D 1 2.341854t+2 1.42475M+3 2.419910D 2 2.160075D2 4.917165E+1 6.0614M+1 Je 100.0 2.341854t+2 1.42475M *3 etAmG 25 JA 0.0 2.849970D2 4.642364D2 4.500065D1 6.43614M 6.436140t+1
*1 2.865845t*2 8.9601860 2 2.849970D ? 4.642 W t+2 4.500065t+1 8.96018M *2 SumG Je 100.0 6.43614M
- 1 2.845845t+2 3.117470D 2 4.500317D2 3.9195 T3D 1 26 JA 0.0 3.919573D 1 6.436140D 1 3.51543M
- 2 8.94T74M+2 Jo 100.0 3.119470D2 4.50031?t+2 8.94774M+ 2 SumG 3.850187t+1 3.5154321+2 6.436143D1 27 JA 0.0 4.4 *80D 2 3.221110D2 2.62585t*1 5.974472t+2 JS 100.0 4.4104800 2 3.22t110D2 3.850187D1 3.515440D 2 2.62585D1 5.974472t+2 SumG i 3.515432t+2 28 JA 0.0 4.179580D 2 3.445319e2 4.212741D1 3.5154400 2 6.M391?t*1 5.00722O2 3.445319D2 4.212741t+1
" Je 100.0 4.177580E*2 3.515432t+2 6.843917t*1 5.00722t+2 stAmc -
h 29 JA 0.0 4.042380D 2 3.519815D 2 4.550242t+1 1.12168M+3 4.042380D 2 3.51985D2 4.55024?t+1 3.515440D 2 1.640228D2 JS 100.0 1.640228D 2 1.12168603 MAMG 30 JA 0.0 3.40350E
- 2 1.318960D 2 3.011794 U 1 3.515432D2 1.076072D 2 8.7070780 2 1.318960D 2 3.011794D 1 3.515440t+2 Je 100.0 3.40350E+2 1.076072O 2 8.7070780 2 MAMG 31 JA 0.0 3.25490D2 !.326731D2 2.T3217tt+1 3.515432t*2 5.601180t+1 6.367321t*2 3.515440E+2 Je 100.0 3.275490D 2 1.326731t +2 2.732171D1 6.347321t+2 atAMG bf3 32 JA 0.0 2.936110D 2 1 W755D2 2.726011t+1 3.515432t+2 5.601180t+1 5.15639M+2 2.936110D 2 1.366785D 2 2.72601161 3.515440D 2 2.350584D1 Je 100.0 5.150 960 2 SumG R
33 JA 0.0 2.8552900 2 1.3778 W 2 2.873913t+1 3.515432 O 2 2.350584t+1 2.130507t+1 4.026340t+2 JS 100.0 2.855290D 2 1.3T7858t+2 2.873913D1 0.515440D2 2.130507F *1 4.026340D 2 SumG '
- 4. 839685D 1 1.621537D 1 3.515432t+2 4 34 JA 0.0 2.449960E
- 2 1,621537D 1 3.51544M *2 2.910193t*1 3.77451M+2 J4 100.0 2.449960D 2 4.889M5D 1 3.774516D2 MAnc 1.086891D 1 3.51543292 2.91019M*1 35 JA 0.0 2.31172M + 2 4.299664D1 5.111869E*1 3.648125D2 JS 100.0 2.31172M +2 4.299664D1 1.086891D 1 3.515440D 2
- 3. M8125 D 2 MAMG JA 0.0 2.0403900 2 3.187470D1 1.054574D I 3.515432D 2 5.111249D1 S 36 2.040390E*2 3.187470D 1 1.054574t + 1 3.515440E +2 6.208335t+1 3.48399M*2
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1.901260D 2 2.893442t+1 1.582160t +1 5 37 JA 0.0 1.582160D 1 3.515440E 2 7.96977M *1 3.3241ME+2 JS 100.0 1,901260D 2 2.893442t + 1 3.324164t+2 SumG t 1.320250D 2 4.290475D) 8.510741D1 3.515432t+2 7.969T7661 9 38 JA 0.0 8.510741E +1 3.5154406 2 6.09330M*1 2.94295M+2
# JS 100.0 1.320250(+ 2 4.2904 5t+1 2.9429580 2 tumG 3.515432t+2 6.0933080 1 39 JA 0.0 1.214160D 2 3.832235D1 8.468345D 1 1.980736D2 2.63198M +2 4'~ JS 100.0 1.214160E*2 3.&l223M +1 8.4683454 1 3.515440D2 9 8.TZ3960E*1 3.209675D1 8.5tS642t+1 3.515432D 2 1.980736D2 2.63196M*2 tuMG 40 JA 0.0 3.515440t+2 3.35395M+2 2.3059200 2 Ja 100.0 8.723960E+1 3.209675D1 8.515642E+1 3.304495D1 8.607797t+1 3.515432t+2 3.353953D 2 2.305920D 2 sumG 41 JA 0.0 7.681020E+1 4.740760D 2 2.0558ett+2 g JS 100.0 7.6810200 1 3.304495t*1 8.607797t+1 3.51544M+2 2.055881t+2 MAMG gp 42 JA - 0.0 4.510760D 1 8.908400D 1 t.075775D2 3.515432D 2 4.740760E*2 4.038383D 2 1.436422t+2 4.510760D 1 8.9084000 1 1.07577'D2 3.51544M+2
+, J8 100.0 4.0383&3D 2 1.436422t+2 suMG 43 JA 0.0 4.76353001 7.893653D 1 1.058563D 2 3.515432E+2 1.605509D 2 g 4,763530t+1 7.895653D 1 1.05856M+2 3.5154409 2 3.727844t+2 a' Jo 100.0 44 JA 0.0 1.121260t+2 5.156705D1 4.515302D 1 2.132209D 2 3.182383t+ 3.762347D 2 2 3.T27844t+2 sumG 3.646350t+2 4.515502E*1 2.132210E*2 C J8 100.0 1.121260E*2 5.156705D I 3.M6350t+2 SEAmG 1.2086300 2 4.378149D 1 3.sc4M eE+1 2.127400D 2 3.765041D 2 L 45 JA O.0 3.80604tt+1 2.127400D2 4.062564D 2 3.8665336 2 Ja 100.0 1.208630t*2 4.378'49D1 '
4.218365t+1 9.910458D 1 4.16T204t+2 3.866533E+2 2.2888 4D 2 SOMG .? 46 JA 0.0 1.059480D2 5.940352t+2 2.557386t+2 1,059480t+2 4.218365D1 9.910458D 1 4.16T200t+2 ~'
.' J8 100.0 1.180t30E+2 1.037170D 2 5.940352t+2 4.1672036 2 2.557366t*2 stAmG -
[ 47 JA 0.0 5.657870t
- 1 5.940350D 2 4.199651D 2 3 01T204t 12
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- 2 1.031521Di
(.- ** JA Ja 100.0 1.087550D 2 1.031521D 2 1.491515E+2 1.818700D 13 2.459896D 2 1.553946t+ 2 1.218661D13 2.45Va9M+2 1.782104t+2 1.782104(+2 SumG y%. W@ 49 JA 0.0 1.117430D 2 1.125776t +2 c
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- 1 1.1535734 3.799458E*1 12 2.897665t 2.200160(*2 stmG 12 i
10 JA 0.0 2.162660t+2 2.906015t*1 7.954992t+1
- ? 1.192414t 2 1.587066t*1 2.T77560(*1 J8 100.0 2.162660(+ 2 2.9046521*1 7.9549921+1 SEAMG 1.561370f
- 1 2.77898M *1 2.5M261t*2 St JA 0.0 1.977%M + 2 9.543075t + 1 2.778980(*1 2.228911t+1 4
9.503075t+1 1.561370t + 1 2.590261t*2 stAMG 48 100.0 1.977940t + 2 3.12645M +1 1.707724t*1 8.204323t+1 f.98504M*1 1.638580f*2 52 JA 0.0 1.948490(+2 3,126460f*1 1.&55341t + 1 8.2%323t.1 1.985049t*1 1.638580t+2 stAmG Jr. 100.0 1.94549C(+7 3.126458t+1 1.885341t+1 S.41987M *1 2. 378127t+ 1 1.324090E*2 51 Ja 0.0 1. 6732Kt + 2 3.12460t *1 5.158508t*1 8.4 n879t
- 1 2. 378127t + 1 1.324090t*2 atAmG JS 100.0 1.473280t
- 2 3.12645M *1 5.158508E+1 3.5875664+1 1.666386t*2 54 JA 0.0 1.0802M + 2 8.8391cas.1 3.126460t*1 7.954031t+1
- c. JS 100.0 1.69802Ct+2 8.55910N +1 3.587566(+1 7.954031E*1 1,6663864*2 stAmG tJ 1.007431t + 2 2.34388E +1 3.126458t+1 2 55 JA 0.0 1.53951M
- 2 3.126460t+1 4.879939E*1 1.0541422*2 JS 100.0 1.539510t+2 1.007431t + 2 2.343888t
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9.980013t*1 1,950680t+1 3.146458t+1 4 56 JA 0.0 1.518120(+2 4.620006(+1 1.3363621*2 9.980015t+1 1.950680t+1 3.12644M *1 1.518120(+2 1.336344t+2 stAMG
;, 57 JA 0.0 Js 100.0 1.490370t+2 9.8216711 1 1.225367t+1 3.126458t +1 4.620006t*1 4.440907t + 1 2.0264464*2 9,82t971t+1 1. 225367t+ 1 3.126460(+1 Js 100,0 1.490370t+2 5.317071t+1 1.104884t+1 2.026446(*2 stAmG 1.444860t+2 1.c2143M .2 7.308734t+0 3.766711t+2 58 Ja 0.0 1.02t43M +2 7.308734t +0 5.317070t+1 2.249874t+1 as 100.0 1.444860t+2 5.3167041 1 2.250727t+1 3.764711t*2 stheG p- 1,562030t+2 9.055772(+ 1 1.07779ef *1 59 JA 0.0 5.316710(*1 5.616553(+0 5.441864t*2 9.055T72t +1 1.077798t + 1 J8 100.0 't. 562030( +2 j h 14'1114
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; 2.783555t+2 3.604884(+0 2' JA 0.0 7.276230t+2 2.668620t+0 1.841992t+1 8.6758621*2 '
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- 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
'. 1.0200 m *3 u Je 100.0 6.304060t 4 7.112M7I4 1.438667t*1 2.400950D 1 1.784 6 2t*1 1.744954t d 8.00953M +0 2.40095M*1 1,784792t+1 1.0200134*3 SUMG 4 9 Ja 0.0 5.699700D 2 6.100960t*2 Je 100.0 5.6097000 2 1.744954D2 8.00953 e 4 2.400950D 1 2.967899D 0 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 l '..
- Je 100.0 5.149400D 2 1.512521t4 8.4094199 0 2.400950D 1 4. TTT797t+0 1.640510D 2 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 s Js 100.0 3.9635901 4 5.! W 33t+1 8.074673t+0 2.400950D 1 1.67521M + 1 2.913535D2
' 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 4 1 S JC 100.0 1.37!910D 2 6.94540$ D1 2.393501t*1 3.536750t+1 6.549630D 1 2.346835D 2
- 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 1,026909(4 Qy Ja 100.0
. 23 JA 0.0 1.974060tQ 2.14000D 2
- 1. 746T20D2 1.73876/1 4 3.9W487t+1 4.022267t+1 3.536750t +1 3.53475 71 + 1 1.066909t+2 5.3699390 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
@& G 25 JA 0.0 3.937900t*2 7.081358D2 5.0851434*1 8.02937M + 1 2.&39237t*2 1.87761?D3 8tAMG 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 e
; S- Je 100.0 6.730440t+2 4.3964521 4 4.801213D1 4.400010D 2 3.067406D 1 9.555999E*2
' - , 28 JA - 0.0 6.3M 310E*2 4.68651M 4 5.156445t*1 4.400027t+2 3.06740M
- 1 9.555499t*2 SEAMG
; h[q 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 j . g ^. JS 100.0 5.201970t 4 1.761343D 2 3.411854t*1 4.400030D 2 1.324728D2 1.091033D 3
- f. 31 JA 0.0 5.007020d 4 1. 763732t
- 2 3.255487t*1 4.400027t+2 1.324728D 2 1.091033D 3 suMG g 32 JS 100.0 JA 0.0 5.007020D 2 4.490820D 2
- 1. 768732t
- 2 3.255487t+1 4.400030(*2 6.919681t+1 ' 7.927423D 2 -
. 7 1.804270 0 2 1.28438M+1 4.40002M*2 6.919681t*1=1T.927423t*2 BOMG '
i a_ . J8 100.0 4.49c820t d 1.8042700 2 3.284382t+1 4.400030D 2 2.927978t*1 6.424002D 2
, V fL : 33 J4 0.0 4.367860t 4 1.8142634 4 3.375793D1 4.40002M +2 2.927978D 1 6.424002t*2. stAM4 s' JS 100.0 4.34786ct+2 1.814263D 2 3.375W3t+1 4,400030D 2 2.026591t+1 5.057627t*2
$g f (.
34 JA 0.0 3.M090Ct d 7.422492t*1 1.602450D 1 4.400027t+2 2.026591D 1. 5.057627D 2 suMG
~
[_, 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
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- tt00 CDvat $1tftM 4316 1.2,3 SHEET E OF 9 4
+- STAsnA# verstort 4.41 tel Apr 12 14:31:55 1996 soport : Element DC.-$T O -
Ni nedst- : D Fernet : 51At0 Tut ser/Seem Element
.1 tte -s Peo* 1 14 M14" .M. I
,c h66
! ' Output Set 6
- tst iLtutai LOA 05 stAe :
, ,, stM0lBG ';
1CR$104 SEMDlhG e AIIA4 satat setA4 M3 mr M2 v3 {j- stM P 3.540360D 2 V2 6.399215t+1 1.2426t2Dt 4.400027D 2 3.471638D1 4.8026000 2 4.809544t*2 - StAmc 1 35 JA 0.0 1.24261291 4.40003M
- 2 6.01121M *1 Je 100.0 3.540360D 2 6.399215D1 4.400027t+2 6.0112T3D1 4.8026000 2 stAmc 3.126950D2 4.428719D 1 1.201132t+1 4.708169t*2 36 Ja 0.0 1.20tt32D 1 4.400030D 2 7.889964t+1 Je 100.0 3.12695M *2 4.428719D 1 7.889964t+1 4.708169D 2 stueG 3.893066t+1 1.5'a312t+1 4.400027t +2 31 JA 0.0 2.914&30D2 4.400030D 2 1.013a29D 2 4.577022t+2 2.916830D2 3 89306M*1 1.54A3 tit +1 Ja 100.0 1.1027toD 2 4.400027D 2 1.013829t+2 4.5T7022D 2 stweG 38 JA 0.0 2.028350D2 5.625090t+1 7.91814M+ 1 4.164844t*2 LC2835cD2 5.625090t*1 1.102718D 2 4.40003002 4.166844t+2 stAMG JB 100.0 1.098173D 2 4.400027t+2 7.918146D 1
- 39 JA 0.0 1.McM002 5.14M94D t 4,400030D2 2.571386t+2 3.812938D 2 1.86(340D 2 5.140494D 1 1.098173t+2
.M Je 100.0 1.089813D 2 4.4000271+2 2.573386D 2 3.812938D 2 stAmG 40 JA 0.0 1.%3/70D 2 4.891959D1 1.0898t3D 2 4.400030D 2 4.338385D 2 3.322004D 2
~
0' 1.343770D 2 4.891959D1 s
*i- Ja 100.0 t.092248D2 4.400027D2 4.338385D 2 2.923246D 3.3220042 D 2 StAmG 41 JA G0 1.1839 70t + 2 5.1428 MD I
- Je 100.0 1.183970D 2 5.142879D 1 1.092248D2 4.400027D4.400030D 2 6.10657002 '6.106570t*2 2 2.223244E+2 stAnc 42 JA 0.0 6.165550D1 1.140377D 2 1.59254M +2 5.05315tD 2 2.137900E*2
- 1. 640377D 2 1.592544D 2 4.400030t+2 4 :- Je 100.0 6.165550D 1 4.400027D 2 5.053151D 2 2.11 M000 2 MAmG 6.296600D 1 1.022184D2 1.4 78157D2 2.232150t 2 43 JA 0.0 1.5 7515 7t + 2 4.4000300 2 4.735971t*2 as 100.0 6.246600D 1 1.0221 M *2 %.735971t+2 t!Anc 1.8295T2D 1 6.421501E*1 2.845123D 2 3.977837D2 k,, 44 JA 0.0 1.60391CD 2 2.845120E+2 6.723885E+2 4.929914t d Ja 100.0 1.6039100 2 7.3295T2D1 6.421501Dt 4.727112t+2 4.92M14D2 stAMG 2.839654D 2
= 45 JA 0.0 1.T371000 2 6.4236c8D 1 5.68459D 1 5.68%59t + 1 2.839650D2 5.205538D2 5.508M
- 2 Js 100.0 1.T371000 2 6.4236G8D 1 5.304093D 2 5.508299D 2 3.1k872t+2 stAMG 1.488490t * ? 6. 010325t
- 1 1.464384t+2 3.6410000 2 46 JA 0.0 1.66438&D 2 5.3M090D2 8.619048t*2 JB 100.0 1.4854900 2 6.0103251et 3.641000t+2 stAMG 1.6SO203D2 1.509442t+2 8.619047D2 5.3M092t*2 47 JA 0.0 1.583810D 1 1.680203D 2 1.509442t+2 8.619050D2 5.438542D 2 3.764144E 12 Ja 100.0 7.583810D1 5.438542t+2 BEAnc p- f 1.53515M+2 1.341915D 2 2. te t 500D2 2.2541211 13 8.619M8D2 2.307193t+2 48 JA 0.0 2.1615000 2 2.25417N 13 3.5753T2t+2
~
h 1.341915D2 Js 100.0 1.535150D 2 2.307193D 2 stAMG 49 JA 0.0 1.5502100 2 1.457482D T 2.258604D 2 1.113091t 13 3.5753T2t*2 1 48 100.0 1.5502106 2 1.457482t
- 2 2.2586M D 2 1.713090D 13 1.782864D12 4.702217D1 2.935129t*23.6957218 stAMG 12
; "a 1.515854D 2 1.781135D1 3.148720f +1 50 JA . 0.0 2.T96710D2 2.555Mit +1 1.188181D 2 1.515854D 2 1.781135D 1 3.148720E +1 Je 100.0 2.796710t + 2 3.149934t + 1 2.5535366 1 1.188181t+2 stAMG L et9320t+2 1.234530D 2 f.779958 0 1 3.364121t+2
- 51. JA 0.0 f.TM958D 1 3.14993M + 1 2.667219D 1 Ja 100.0 2.619320D 2 1.236530D 2 1.435391t+1 3.366121D 2 stAMG 1.124506D 2 2.062087t+1 3.So9857D 1 52 JA 0.0 2.538250D 2 i.169860 D 1 2.30$N1t+1 2.063913t*2 P Je 100.0 2.588250D 2 1.124506D2 2.062087t+1 2.063913D 2 stamG
~. 3.8698571+1 2.305791D1 T $3 JA 0.0 2.5tt7200 2 1 t618871+2 2.137118D ) 3.869660D 1 5.571932t*1 1.T3676'E*2 Js 100.J 2.511T20t+2 1.161887D 2 2.33717M
- 1 5.571932t+1 1.T36761D 2 stAMG M: 54 JA 0.0 2. 44500D 2 1.244375t + 2 3.239415D1 3.869857D 1 2.304374D 2
+
1.244379D2 3.239415D 1 3.869860D 1 8.058423D 1 Ja 100.0 2.344300D 2 8.058423t+1 2.304374t*2 stAMG
% 55 JA 0.0 2.220GYD2 1.3056a3D2 1.960875D1 3.869857D 1 5.874566t+1 1.3459t2DF Y Je 100.0 2.2200000 2 1.305683D 2 1.96087!C+1 3.869860D1 1.345962t+2 stAMG 3.869657t+1 5.874566t+1
' F' - 56 JA 0.0 2.207660D2 1.291044D2 1.414317t +1 1.670384t*2 1.291044D 2 t.634317D 1 3.869660D 1 5.674997D 1 Je 100.0 2.207660D 2 3,869857t+1 5.674997t*1 1.670364t+2 BEAMG 0.0 2.197880D 2 1.267158D 2 1.033599t*t 57 JA 3.869860D 1 5.475883t+1 2.525221t+2 2.197880E+2 1.267158D2 1.C335999 1
> JS 100.0 1.242168t+1 2.525221D2 stAMG 58 JA O.0 2.0735900 2 1.450G52O 2 6.276858DO 6.589245D 1 1.941569t*1 4.880791t*2 >y 1.450852 O 2 6.276858DO 6.589250D1 J ,
; ,f Q f Je 100.0 2.073590t *2 2.221080t+2 1.373735D 2 9.12t873t+0 6.588806 D 1 1.943038t+1 4.880791t+2 stAMG 4
p - 59 JA 0.0 5.L8095t+0 7.459466t+2 [ Js 100.0 2.221080D 2 1.373735D 2 9.121873DO 6.588800t+1 J .Z f e a title : Paw 1 14914* DOM
. TM '
M . output set 6 - sst V g 4 Q Set,. mAXAalM Stannery f able set 10 Value J@ Wt mint uun 6 42 61.6555 mmoG
/ce: Q . Seas Erd A Aalet Force maaloue 6 1 731.754 :M l
*M; d%h}.
~
MJ %: 'Seem traf A Sheer 2 Force 1. ulnimum Maslaum 6 6 37 8 38.9307 711.287 WMd.
' I g' . "- Dean Minisun 6 to 1.80284 - 1G
%g_ truf A Sheer 3 Force 225.86 man (sue 6 49 49 1.71309D13 . gGme Q.-[Q g} 'r. '
seem trus A Torque - Minimus mau(sum 6 6 47 861.905 M. . mN g $
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- N d K $6- ATLACHMENT MW 0(C0 C mv4C St51ta 4316 1,2,3 SHEE.T 9 OF _ $
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- fri apr 12 14137:59 1996 OC.-SW3
-$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 minimm 6 8 2.66842 *'
.+
f.1 + s Seem tnd A nament! 6 48 861.905 manimm g . Seen tnd A w t3 ulnimm 6 2 41.10T4 3
.gi manian 6 8 2000.92 ~
minimm 6 42 61.6555 Seen Erd 8 Amlet f orce 731.754 4 maa letse 6 1 ' 3e. minim m 6 37 38.9347
' Seem Erd a pear 2 f orce
~_ maelma 6 8 711.287 W. mintam 6 10 1.00284 f
Seem trd 8 Seer) f orce 225.86 h-e4 man imm 6 49 49 1.71349t 13 teen trd 8 foegd minimm 6 uesim a e 47 861.505 49 1.7828M 12 [/ been led 8 moment 2 minian maa t am 6 6 46 861.W5 minina 6 49 3.695 T21 12 e Seen Erd a moment 3 6 7 2000,92 men tam N'ti- Title Petr> 1 14*I14* value set to S. F irst >AX/ute sommery f acite 44 +34.2905 Seen Erd A AAlet f orce minisue 1 7 me: E nm 6 1 731.754 minleus 1 48 15.8687 Sees trd a peer 2 force 8 711.287 maalaue 6
+
minisue 1 54 *137.339 o Beam Erd A Deer) f orce 6 49 225.86 ma a lam
%; Seem trd A f orge m 6 nimm 1 46 d22.89
.C 6 47 &&1.905 maa t am
- g minisua f 42 306.75 j Seem Erd A moment 2 6 48 861.905 maalaus y iis minimm 1 45 103.932 been Erd A moment 3 gf s v. -
masimam minious 6 1 49 6 2000.92 191.972
*s ' heen Erd 8 Aslet f orce 6 1 T31.754 men isun L ulnimm 1 44 a31.9619 9 Seze Erd B n eer2 force 6 8 70. 287 maa tam
% minium 1 26 164.328 pgt . Seem trd 8 Sheer 3 f orce 6 49 225.84 manisue W mintam 1 1 10.8455 4 g
s e, Sean Erd & Torgae mas isus 6 47 861.905 minleus 1 24 277.912
$^, * . Seem tnd 8 moment 2 46 861.905 maafsue 6 gi minim a 1 41 130.551
%y 4een End a masent3 2000,92 ,, .4 mea tum 6 7 ge -n.."yl
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CHKT10Y SETE0 CDs E/ moymeen Engineers & GENERAL. l CALCULA 2-Constructors COMPUTATION Voto o - - - - E pF i SHEET PAEllM FIP4AL g g l X FERMI 2 - CCINAC SHEET of DATE OATE CT uvu r.vaLuatic7r or GT LututCT SVGTEM-GERIEC J 0- 76230.502 g 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 moments in the ductwork by each duct size for DL, OBE and SSE
- conditions. Maximum and minimum values for each duct si:e are also g p"esented, en Based on the commands issued by the preparer, STAR) TAP accesses the t
y working files saved by STARDYNE during the string The data are then analysis runs and spot checked prints the data in tabular form. against the string analysis outputs by the checker. 7 4 in the following 7 The string analysis outputs are contained eg k ., calculations:
~
DC-5763 CCINAC Concern Resolution Task 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 > E 2848 System Series k CCINAC Concern Resolution Task N' DC-5765 Duct String Analysis and Support Evaluation of 2849 and 4126 System Series
!?{E
{0% , , ,; ' ki DC-5766 CCINAC Concern Resolution Task 5 Duct String Analysis and Support Evaluation of yL NL{.7 ' 2850 System Series
*f $zw M' " ,
DC-5767 CCINAC Concern Resolution Task Z((E Duct String Analysis and '.upport Evaluation of Q 4316 System Series . , B
#% M s
i , jff
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-- ATTACHMENiew E OF O l $Le *tto 12reAt Sv51tu 4316 1,2.3 SHEET
'1 +
trl Apr 12 14:38:48 1994 S ete t : Itenant I 11AmA# version 4.41
'I, Model -
t-i 1 ma0m 4.y.. D-t 4 w 1 a L ifitte 1 Pew 2 19-319= 4OAD8 T* ;) twegut tot 1 + NA0 toad (041 *i4m t41ata1 MeluG YN g, ; frallow SteluG
" Ax1A4 tut A8 lutat m2 A3 M1 V3
- v2
' MM 2.979980E 1 5.2946511 2 1.1007tM
- 2 1.020440D2 3.735589t+12.194436D2 5.6455M 1 6.901800D 1 HmG 60 JA 0.0 1.1007?M
- 2 d.02044002 2.97v980D 1 5.2966518 2 1.02WOD 2 3.735589D4.16658M 1 5.66655M 1 stA'eG
*~ J8 100.0 t.724159D 1 1 0.0 2.97v980t + % 294451t I 1.020440D 2 8.62101t+1 61 J4 1. 724759t
- 1 4.16658M 1 timG 2.9 M 80D 1 5.2946511 2 1.02 m 00 2 4.621831E*1 Je 100.0 5.29 6510 2 6.472806D 1 3.1071240 1 2.979980D t 1.020440D2 4.33025M+1
- 62 JA 0.0 5.2946518 2 -6.47250M +1 4.D02!3t *1 3.1071241 1 DEAMG Ja 100.0 2.979980E 1 1.02%40t+2 f
63 JA 0.0 2.97998M 1 4.294651t 2 1.015975D21.02M4M *2 2.46497M
- 2 2.04819M 1 2.979960t 1 5.2966518 2 1.015975t +2 2.4M97M + 2 2.048193t 1 EtAMG Ja 100.0 0.0 2.9799800 1 *.kMuD2 1.407229D 2 1.020440D 2 3.480741t+1 1.11936M *1 6* JA 4.M6440 2 1.407229D2 1.02M4062 1.119369D 1 atAMG Je 100.0 2.979980E 1
- 4. t* mud 2 1.m195D1 1.02m062 3.480741U1 0.0 2.9799806 1 1,68419$t+1 1.02M40D2 1.0497100 2 8.16339M 2 65 JA 4.M M444-2 JS 100.0 2.979980t 1 1.0?M40D 2 1.049710D2 8.1633 h D 2 stAW.
M JA 0.0 2.979980t 1 4.M M44t 2 6.540688t
- 1 1.02M40D2 4.k817M+0 1.533286t 1 2.9799800 1 4.MM64E 2 6.540688D 1 4.048180D 0 1.02M45t+2 1.533286D1 StAMG J4 100.0 h'" JA 0.0 -4.MM40D 2 2.97M78D1 9.114456t+1 9.11445M +1 4.k8180t+0 1.188625D1 5.25825M 1 67 4.MM40D 2 2,979978D 1 1.1884255*1 5.25425M 1 EEAMG '
Je 100.0 1.592976D 2 4.048180D 0 1.146853t+0 4.M6,4M 2 2.97997M 1 4.M8180t *0 3.438625t+2 68 JA 0.0 2.97997M 1 1.5929 7M
- 2 1.14645 M
- 0 SEAMG Ja 100.0 * ,s.640s 2 1.118M4t*2 4.048160D 0 3.438625D2 S.24178M 2 1.480962t*2 1.002622D0 69 JA 0.0 4.MM40t 2 1,1tS664t+2 4.Ma184 0 1.002622D 0 stAMG 4.MM40D 2 8.241780D 2 4.044180D 0 1.480962t+2 Je 100.0 7.500617t+1 1
70 JA 0.0 4.MM40E 2 8.241780t 2 4.048180D 0 2.066770D1 8.171819D 1 Je 100.0 4.646440t 2 8.241780D 2 7.500617D 1 4,%8180D 0 2.066TTDE + 1 8.171819t*1 SEAMG
%P 71 JA 0.0 4.MM40t 2 8.2417806 8.24118M 2 2 2.431659D 2,431659t*1 1 4.048160t+0 9.728035t+0 7.141597t = 1 7.141597E 1 SEAMG C JS 100.0 4. MM40D 2 5.196179t+1 4.k8160D0 9.72803M+0 0.0 4.M6440t 2 8.24178M 2 4. k8180D 0 1.006612t*2 5.699235E 1 72 JA 4.64M4062 8.241780D 2 5.196179D1 5.699285 0 1 stAMG s , 1. JB 100.0 7,9290W D1 4.ks180D0 1.006612t+2 9.059002D 2 0,0 4.46440D 2 2.8064318 1 4.044180D 0 3.476784t+1
- 73 JA 4.M64401 2 2.80M31D 1 4. 781232t
- 1 4.k8180D 0 3.476784t+1 9.0590020 7.929099t + 1 2 8DMG .
Je 100.0 2.80M31D 1 3.887485 0 1 l
- M644Ct 2 1.16431M*2 74 JA 0.0 4.781232t+1 4.044180D 0 3.887485t 1 SEAMG Ja 100.0 4.M6440D 2 2.80643tD1 4.k8180D0 +1.164313D2 1.008409t+0 75 44 0.0 4.64M400 2 2.806431D1 3.34939001 4.044tS0D 0 4.247675D1 1.008409D 0 stAMG e 4.MM400 2 2.80M 31D1 3.349390D 1 4.048180t+0 4.247675f +1
% J8 100.0 2.80M31D 1 7.572655t +1 4.MM40E -2 4.k8180D0 1.373738D2 1.67493M +0 alAMG
- 76 JA 0.0 4.MM400 2 2.80o431D 1 7.572655D1 1.373738D2 1.67493M +0 JB 100.0 4.k818M +0 4.M64400 2 1.uM24D2 1.100112D 2 4.048130D 0 4.480244t+0 1.692409D 0
' 77 JA 0.0 1.446424D 2 1.100112D 2 J8 100.0 4.MM4002 4.M8180D0 4.480244D0 -1.692409D 0 stAMG 1.444 24D 2 8.77476491 4.M8160t+0 1.015189D2 1.709882t+0 78 JA 0.0 4.64440D 2 e 4.4M40D 2 1.u 64241 2 8.774764D1 1.015189D2 1.709882t+0 SEAMG J8 100.0 1.444424 0 2 1.772158D 1 4.048180D0 1.752681t+0 6 79 JA 0.0 4.M6440D 2 1.772158t*1 4.048180D 0 4.908075D1 R Js 100.0 4.64440t 2 1 uo4248 2 4.%8180D 0 4.908075D1 1.752681E+0 atAMG
-4.MM40t 2 1.4464241 2 7.225635D1 4.048180D 0 1.647258D2 1.7954810 0 t
80 JA 0.0 4.6444062 1.u6424D2 7.225635t*1 JB 100.0 81 JA 0.0 4.4 44002 1.24131200 9.845376t+1 -4.M8180D 0 1.647258D2 1.74.%8180D 0 9.7850400 1 1.515098t+0 4.64M40D 2 1.2413120 0 9.84537M+1 4.048180D 0 9.785040tet 1.515098t+0 stAMG W[ n J8 100.0 4,64M40t
- 2 1.241312D 0 1.725217D1 4.048180D 0 1.337867t+2 4.100751t+0
< 82 JA - 0.0 4.64 M40D 2 1.241312t+0 1. 725217t +1 1,337867t+2 4.100751t+0 stAMG JS 100.0 4.k8180D0 5.75666tt+0 2
4.MM40E 2 1.241312D 0 5.166573t + 1 4.M8180D0 4.486459D1 0 JA 0.0 5.7566 tit *0 stAMG 4.MM40Di 1.241312t*0 5.166573D1 4.048180D 0 6.486459D1 JS 100.0 1.241312f+0 7.624231t+1 7.411329D 0 E 0.0 4.64M400 2 4.044180D 0 3.676641t*1 i? k JA 1.241312t+0 -7.624231D1 3.676641t+1 7.4113290 0 SDMG J8 100.0 4.MM400 2 2.922904D1 4.k S180t+0 O 4.MM40D 2 8.608252t+0 6.364109t+0 1.634391t+1 85 JA 0.0 8.608252t+0 2.922904t*1 4.M8180t +0 N Ja 100.0 4.M6440E 2 4.M644402 7.739506D0 6.368210D 0 4.048176D 1.642394t+10 1.634391D 1 atMG q,
- 86 JA 0.0 8.608250t*0 8.6082500 0 4.44412 7.73950M+0 6.368210D 0 1.404762t+1 1.404762D1 1.642394t+1 StAMG Ja 100.0 5.081144t*1 6.368210t+0 1.647041t+1 t 8.6082500 0 4.6464440 2 b, $7 JA 0.0 5.08114*D 1 6.3682106 0 3.676355D1 8.608250D 0 4.MM4402 JB 100.0 88 JA 0.0 8.608250t+0 4.MM44E 2 6.924158D 1 6.368210D0 3.676383D 1 -1.647041D 1 J JS 100.0 -8.608250t+0 -4.4 M440 2 6.9241586 1 6.3682106 0 1.060054D2 1.651687D 1 6.368210D 0 1.06005401.137027t+1 2 *1.651687t+1 SEAMG Vf N:
89 JA 0.0 8.608250D 0 3.167140D0 9.457244t+1 6.368210D 0 -4.767482D 1 3.167140!*0 9.45T244t+1 1.137027t*1 luMG
~ ~
Ja 100.0 8.608250t*C 6.364210t+0 4.76748291 90 JA 0.0 8.608250D 0 3.167140D 0
- 2. 71934M + 1 yQA 6
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432n f&y ly
% {
j[#m hh h l I l
% ATTACHMENf 3 N M N Otto ttuvat Svitta 4316 1.2.3 Fel Apr 12 14:38:51 1994 l STMmAP version 4.41 modoi 1 eesort : ILement Ob"b"II) ; r.re.t i stAA0 m s.ri6. (i nt <
M ,i b
~
YW 3 * -fitte Pew 2 19-n19e + 1
+ Output let 1
- MAD LCAD (Ot) 10A0S
+
m etAe !Ltato1 ' g < AI14L tutAA latAs 10tt10m MuDinG MuefuG m7 m2 m3
* "p ', NAM -
JS 100.0 P 8.608250t+0 V2 3.16 T14M
- 0 V3
- 2. 71934M + 1 6.36821M +0 9.16641M + 1 6.2D6671*0 3.16714M +0 3.239552t+1 6.36821M+0 9.186418t*1 -6.223667t+0 StAMG 0.0 8.60825Ct*0 91 J4 1.077% 5t+0 3.239552t + l 6.368210t+0 + 3.92214M
- 1 as 100.0 8. 60825M
- C 3.16714M *C 3,16714M
- 0 6.2M449t*1 6.366210E+0 3.92214M +1 1.077065f+0 StAMG h 92 Ja 0.0 8.608250t*0 6.20ec33f+1 4.069537t+0 3.167140t*0 6.234449t
- 1 6.368210E+0 Je 160.0 8. 6C425M
- 0 6.206833t+1 4.069537t*0 stAMG 0.0 8.60825M
- 0 9.377424t 1 6.4492671+1 6.368210t+0 93 Ja 6.368210t+0 8,03114M *1 6.140073t+0 Ja 100.0 8.608250t*0 9. 3 77424t . t 6.4492eTt+1 6,1400T3t+0 stamG 1.36*030(*1 6.36821M +0 8.03114M + 1 94 0.0 8.608250(+0 9. 3 r7424t - 1 JA 6.3M21Cf *0 5.018007t+1 8.211545t+0 JS 100.0 8.608250t
- 0 f.37*424t t t.364030tet a.211545t+0 stAMG 9.3 774244 1 5.434325t*1 6.36&210E+0 5.018007t+1 95 JA 0.0 8.608250(*0 6.990902t+1 = 1.02820M +1
-8.608250t+0 9.377424t 1 5.434325t*1 6.36821M *0 JB 100.0 6.364209t+0 6.9809821*1 MAmG 0.0 9.618800t*1 8.608252teo 9.3774244 1 1.028210E*1 96 JA 1.02821M e l + 4.18045M +0 4.972677t+1 9.3774248 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 6.624990E+0 4.686340E*2 Je 100.0 1.087540t + 2 5.172657t .1 2.101649t*0 +3.652810t*0 3.652810t+0 6.624990t+0 A.686340E 2 SEAmG 98 Ja 0.0 1. 2 T2140(
- 2 7.01567tt+1 2.101649t *0 3.652810t+0 3.652310t*0 9.916970t+1 JS 100.0 t,272140t*2 T.015671t*1 - 2. t 0 t %9t
- 0 9.916970t+1 stAMG 2,230060t*2 4.01*%ot 1 2.1018 9t*0 1.T30560t = 14 5.165853t*0 99 JA 0.0 2.627061t*0 5.043211t+1 JS 100.0 2.230060t*2 . 01.5601 1 '2.101ket+0 1.73056ct 14
*~ 100 JA 0.0 3.0365 70t + ' 4.034569t + 1 2.10149t*0 1.3177005 14 2.627061t*0 -1.043211t*1 stAMG 3.036570t+2
- 034569t*1 2,101649t*0 *1.317700E 14 7.699397t 14 1.8818284 14 Ja 100.0 5.282670t+0 .t.387937t+1 1.229261t*2 8tAMG 101 0.0 1.06710cter a.1826 MT + 1 3.039f91t*0 JA 3.039301t+0 5.2826TW*0 9.581019t*0 3.544979t*1 JS 100.0 1.06710ct + 2 6.1826771 1 d
1.251400t*2 8.J2169ttet 3. 0.19391t
- 0 5.282670(*0 +9.581019t*0 3.548979t + 1 stAMG 102 Ja 0.0 3,039399t*0 5.282670t+0 5.232670t+0 7.801062t*1
[l i
* ' 103 Je 100.0 JA 0.0 1.251400E*2 8.02:00 t
- 1 2.236820t*2 - 3.173 744t
- 1 3.0393911 0 . 4.10T&30(+ 15 F.470824t+0 ?.801062t+1 8tAMG 3.96?180t+1 3.799239t*0 J6 100.0 2.286820t+2 3.173744 t + 1 +3.039391t+0 4.107U C( 15 p 104 Ja 0.0 3.093320t*2 3.173744t+1 3.019391t+0 1.337120E 14 3.799239t+0 3.96?180E+1 atAMG
' 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 g Set . NAX/mit $6mmary table let 10 Value d minim m 1 67 0.046464 Y Seem Erd A Aalet force 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 Seem trus A theer3 perce minimm 1 64 *140.TZ3 /
41 manimm 1 68 159.298 E h* . minian 1 96 10.2821 :, Qf M% Beam Eful A Tortam masium 1 60 102.044 A minimm 83 -133.787* Q j ,, Seem tesi A hemmat2 1 343.863 qK4 s sj Seem truf A 3ecasnt3 maaimm minimm 1 1 69 99 99.1692 , n .3ils M ( i
,1
- 1.- maaisus 1 101 122.926
~,
W team trus 8 &aul f orce minium 1 104 -309.332 maaima 1 67 0.046464 s s minimm 102 80.2569 M
'm k Seem tres e sheer 2 Force maalam 1
1 99 40.3457 J' < 68 *159.296 NH Coen trus e shear 3 force minimm maalam 1 64 140.723 kh M 3 .m Seen End 5 forsyn minim m 1 1 60 96
*102.044 10.2321 $m masisus C Seem truf 5 Moment 2 minim a 1
1 68 82 343.863 133.T87
. 4 T-D" w i . .
maaimm minim a 1 1 101 35.4a98 a, ,d 44 Sean End s momenti maaimm 98 99.1697 a: f+C.}41
$$ c ; . .
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m 0 u - m M n 43,6 1.2.3 ATTACHMENT i+4~ SHEET. b 0F b
~
t< F Title 1 PACP 2 19'I19= DCdTD [ 1lhaput Set 2 + Cet 9EAs ttIatut LOAD $ 7 ICRSION HelWG HelBG AI1AL sataa $kEAA R3 at K2 P v2 v3 2 M41 e t. 2.641910D1 2.467699D1 5.26707M* 1 3.252691D2 StamG 0.0 2.205390D2 6.41678M
- 1 8.965429t+0 2.?M615E+2
? l- 60 Ja 6.4167S8D1 2.641910t*1 2.47700t +1 JS 100.0 2.205390D 2 2. 47699D1 8.965429D 0 2.2%415D2 SEAMG 7 61 Ja 0.0 2.108210t*2 6.270254D1 4.1498829 0 2.070988t+1 1.907760(*2 2.108210t+2 6.270254t 1 4.1498820 0 2.4770001 1.90T760D 2 4 TANG
<t 100.0 1.55374M*1 2.467699D1 2.070988D 1 62 JA 0.0 2.030490D2 5.971515D1 2.4677000 1 1.0491121 1 2.499693D2
+
2.030490D2 5.971515D 1 1.55374M*1 2.49969)(+2 M AmG f Ja 100.0 2.438515t+1 2.47699t + 1 1.049112t+1 63 JA 0.0 1.9982500 2 5.8A217M + 1 3.420009t+2 1.998250D 2 5.832176D1 2.438515D 1 2.467700D 1 5.9193821 1 3.420009t*2 atAmG JD 100.0 3.390029t*1 2.467699t*1 5.919382D 1 0.0 1.8961800 2 1.067916D 2 64 Ja 1.06791M
- 2 3.390029t+1 2.47700D1 9.193529D 0 1.362852D2 JS 100.0 1.896180D2 1.342852t+2 StAmG 0.0 1.8292200 2 9.638652t+1 4.972741D0 2.47699D1 9.193529D 0 2.754254D2 65 JA 2.979373t + 1 1.82922002 9. tJ8e 5M
- 1 4.97274tD O 2.46T7000 1 2.754254D2 StAMG as 100.0 1.59658M
- 1 2.47699t + 1 2.9793S D 1 1.??9060D 2 7.976849D 1 3.9579604 2 s4 66 JA 0.0 1.59+588D 1 2.4677%t + 1 2.04251?D 1 Je 100.0 1.799060D 2 7.976849D 1 3.957960D 2 DEAmG 7.430340D 1 1.79215802 2.20715M +1 2.042515D1 2.47696D1
" 67 JA 0.0 2.042510D1 2.9259371+0 2.914918D2
; Je 100.0 7.43034001 1.792158D2 2.20715M+1 d.8 JA 0.0 6.257240t + 1 1.78165992 3.834800D1 2.04251591 2.925937D0 8.28129?t+1 4.374578t* c.914918D 2 2 atAMG 6.257240D1 1.781659t*2 3.834800D 1 2.042510D 1 4.374)78t+2 stAxc Ja 100.0 8.281299D 1
[ 69 JA 0,0 5.666260D1 1.011456D 2 2.6aomD1 2.042515t + 1 3.589255t*1 2.922668c+2 J8 100.0 5.666260D1 1.011+ 3aD 2 2.6SomD 1 2.042510D 1 3.589255t+1 2.922668D 2 t!AMG 5.877390D1 1.001922t+2 1.803376D 1 2.042515D1 1.965965D2
- 70 ' JA 0.0 1.001922t+2 1.803376D 1 2.M2510E *1 5.58432M *0
(; Ja 100,0 5.877390D 1 1.965965D2 atAMG 71 JA 0.0 7.480600t+1 9.678843D1 5.937703DO 2.042515D 1 5.58632M *0 Je 100.0 7.480600D 1 9.678843D 1 5.937703DO 2.M251M2.625854t+0
- 1 2.625834D0 2.264087D 2.264087D2 atAmG 2
; 9.624529tet 1.251903D1 2.042515D 1 72 J4 0.0 8.126860D' 2.042510t+1 2.416938t*1 3.404004t*2 9.624529D 1 1. M 1903t + 1 3.404004D 2 SEAmo JS 100.0 6.126860D 1 2.042515t*1 2.416938D 1 1.026620t*2 7.484355t*1 1.904783D 1 2.750379t*2 73 JA 0.0 t .904783t + 1 2.042510D1 8.61244860 JB 100.0 1.028620t+2 7.486355D1 8.61244860 2.750379t+2 SEAMG 1.116400t+2 7.073323D1 1.150464D1 2.042515D1 2.506542t+2 N* 74 JA 0.0 1.150464t+1 2.042510D 1 2.816723D1 Ja 100.0 1.116400D 2 7.073323t+1 2.816T23t+1 2.506542t+2 BEAMG
> %v.* 5.916c 7to t 8.080401D0 2.M2515f+1 75 J4 0.0 1.351640D 2 2.042510D 1 1.151612t+1 2.524927D2 1.351640D 2 5.916071D1 8.080401t+0 2.524927t+2 stAnc s' JS 100.0 1.8193166 1 2.042515D) 1.151612t+1 76 JA 0.0 1.476970D2 5.324382t+1 2.902303t+2 J8 100.0 1.476970t+2 5.324382D1 1.8193166 1 2.042510D 1 3.377260D1 2.416143t+1 2.80854ff*1 2.M2515t
- 1 3.37T260D1 2.902303D2 stAMG I* 77 JA 0.0 1.760380D2 2.042510t +1 4.381282E*0 2.775091t+2 1.760380D2 2.416143D1 2.808541t+1
' ' Ja 100.0 2.312362t+1 2.042515D1 4.3812821+0- 2.775091t+2 atAMG
< 78 JA 0.0 1.828160D 2 2.90611661 2.903008D 1 2.581923D2 JS 100.0 1.828160D 2 2.90611M
- 1 2.312362D 12.042515t+1 2.042510D12.903008D 1 2.581923t+2 SEAMG 1
2.151300D 2 5.8T7409D 1 1.030511D 1 1.536172t+2 N 79 J4 0.0 1.030511D 1 2.042510D 1 4.512155t+' Js 100.0 2.151300t*2 5.877409D 1 (.512155t+1 1.536172t+2 6tAMG p 2.318570D 2 7.124806DI 1.960091D1 2.042515t*1 2.t?.i355t+2 80 JA 0.0 1.969091t+1 2.M2510t +1 8.140143t+1 J5 100.0 2.318570D 2 7.124806D 1 2.223355t+2 stAmG {; 7.01.192t*1 2.042515t+1 8.140143D 1 2.660870t+2 1.217099D 2 E 81 JA 0.0 1.217099D2 7.016192D 1 2.042510D 1 1.074432D2 2.172934D 2 W JB 100.0 2.660870t*2 1.074432t+2 2.172934t+2 atAMG 2.908520D2 1.157268D2 6.51 t T3M+ 1 2.042515D) 4.2 W 14 D 2
- 82 JA 0.0 1.1572680 2 6.51173M+1 2.042510D 1 2.423627t +2 Ja 100.0 2.908520E+2 2.M 2515D 1 2.423427t+2 4.255414E+2 StAMG 1.10380$D 2 6.519799t+1 83 JA 0.0 3.117760D 2 1.103805D2 6.519799t+1 2.042510DI 3.259784D2 5.64784M+2 Ja 100.0 3.117760D 2 3.259784t+2 5.647848D2 stAMG 1.089309D 2 6.63455M+1 2.042315 D 1 84 JA 0.0 3.192090t*2 2.042510D 1 4.107042E+2 7.059714t+2 3.192090E*2 1.089309D 2 6.63455M*1 7.059714D 2 SEAMG C,' JS 100.0 3.823410D 1 2.042515t +1 4.107042t+2 D 85 - JA 0.0 3.453450D 2 3.798435f+2 4.496900D 2 8.730234D 2 3.796435D 2 3.823410t+1 2.042510D 1 Ja 100.0 3.453850t+2 2.042517t+1 8 T30234t+2 BEAmG 0.0 3.8171806 2 3.518181t*2 3.796558D 1 4.496897D2 5.06507M+2 y
84 JA 3.511381D 2 3.79655891 4.4969000 2 2.879372t*1
?' J8 100.0 3.8171806 2 2.879372D 1 5.0650760 2 stAMG 87 JA 0.0 3.8691200 2 3.654895D 2 4.034280D 1 4.496897t+2 6.764705t+1 3.883396t*2 3.8691206 2 3.654898D 2 4.036280t+1 ~4.4969000 2
- JS 100.0 6.764705D1 3.883398D2 stAMG 84 JA 0.0 3.885760E*2 3.687326 6 2 4.199877D1 4.496897t+2 1.086597D 2 5.612793D2 3.687326D 2 4.199877t+1 4.4969000 2 JS 100.0 3.885760t+2 4.496897t+2 1.086597t+2 5.612793D 2 BEAMG 9r 0.0 4.010160t+2 1.070519D2 2.622733t+1 4.232029D 2 89 JA J5 100.0 4.010160D2 1.070519D2 2.622733D1 4.496900D 2 8.74063M 8.740636t+1
*1. 4.232029t+2 SEAMG '
1.004057E
- 2 1.47697M+1 4.496897t+2 90 JA 0.0 4.076490D 2 1.47697M + 1 4.496900t+2 7.242484D 1 3.439200t+2
* (( , JB 100.0 JA 0.0 4.076490D 2 4.136290E*2 1.004057D 2 9.342229D 1 1.549697t +1 4.49 M97t*2 7.262484t+1 3.439200t+2 atAMG 3.174464t+2 y,q 91 5.535724t+1 1.549697t+1 4.496900t+2 J# 100.0 4.136290D 2 9.342229t+1 YNj g, QEg g < ,
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- 2 8.93199N 1 2.013589tel 4.496900f*2 Je 100.0 4.166550D2 4.9319%t 1 2.013589D14.49689M*2 4.925375D1 3.402MSD2 StAmG 4.2662400 2 7.4849111 1 6,527827t*1 9.431513t*1 3.03026aD2 93 JA 0.0 6.5278221*1 4.4%9000 2 3.030268t*2 stAmG
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- 2 9.631513D 1 de 100.0 5.83003N *1 6.245195t*l 2.314943D2 3.0094841 2
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- 2 5.1300381 1 6.245195D 1 4.496897D 2 2.314943t*2 44 100.0 4. 7272 79D1 6.316185t *1 3.679613D 2 3.113287t*2 h
95 JA 0.0 6.369690D2 S.116181E*1 4.496900t*2 3.679613t*2 StAmG 6.389690D 2 4. 72727M *1 3.11328 4 *2 4.496900f *2 ) J8 100.0 4.4326336 2 3.64 7380t
- 1 96 JA 0.0 6.602 T70D 1 3.847380t
- 1 3.1132900 2 4.1762821 2 6.666543D 2 6.602770t*1 4.412633t*2 5.565840D2 3.588650D2 elAMG st 100.0 3. 375913D2 1.071505 0 2 2.434303D2 4.056131t
- 2 1.21443M *2 97 JA 0.0 6.690960E*2 6.690960D 2 3.375913D2 1.07150$D 2 2.436310D 2 96 JA Ja 100.0 0.0 6.7048200 6,704820D 2 3.3662002 2 3.W2DD2 1.149162D2 2.4M310D2 1.149162D 2 2.4M303D2 4.05413126 2.4 M302D 2 5.956251D2 stAMG Je 100.0 S.2555700 13 3.44545ce 2 5.956251t *2 1.s11982t*2 3.04303002 99 JA 0.0 7.1377300 2 2.408601021.349335t*2 1.349335t *2 a.655570D 13 7.1377308 2 2.4 W cit 2 1.815982D Z 3.048030D 2 BEAMG Ju 100.0 1.4527Nbi 3.588614t 13 100 JA 0.0 7.156970D 2 2.4344241 2 1.45278 4 *2 3.5686100 13 4.25502713.09522M 12 1.32509D12
*2 stAmc 7.156970D ' 2.438424D2 1.714434t*2 J8 100.0 1.20811t*2 101 JA 0.0 6.137030De 3.0118241 2 4.909127D 1 4.359198D1 1.024021E*2 1.2M811D 2 StAMG J8 100.0 6. f'17030D3.C=643182 3.0558248 2
2 4.202121t*1 4.909127D 4.3591980 11 4.3591900 1.024021t*2 4.35920?t*1 1 5.548714t.2 y 6.110770D2 4.359190t*1 102 JA . 0.0 e.150770D2 3.0as433D 2 4.202121D 1 103 JA Ja 100.0 0,0 6.520910D 6.520910D 2 2.2428521 2 2 2.2428521 2.f.307071+1 7.60&340D 2 2.810707t 13 2.761759t*1
- 1 7.808333D 2.761759D1 2.640836D 2.840a3M*
2 2 StAMG 13 6.1646 J4 100,0 2. 20940M *1 6.218794t
- 13 6.541980t*2 2. 2 72669t
- 2 6.218790 0 13 9.017101D 13 1.0587M *12 104 JA 0.0 2.277669t *2 2.20040M *1 Ja 100.0 6.5419400 2 Peor 2 19-s19*
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} Set = ulnima 2 100 715.697 Ei" Seen tral A Aalet f orce mealesa 2 2 77 24.1614
- 8+em tral 6 $heer2 f orce a n nimm mes team 2 96 443.2M
- 61 4.14988 S_ minimm 145.279 Dean trd 6 5heer! Force 100 mesiam minimm 100 3.58861D13 Y._E' " ' 86 449.69 Seem Erd 4 f orme maaleam 2 2 72 2.425&3 -
mir imm 556.584 Seem tid 4 moment 2 2 97 i men taes 121.444 96
- b. minimm 2 86 873.023
* ' I M # - Been Erd A moment! mealsam 2 69 56.4626 7 4>> u ln',eam 2
100 71?.697 M "' Seems trd 8 Aalet f orce mes esa 2 2 77 24.1614 N ulniemen 96 443.2&3 A 6eem tid 8 theer2 force menieus 2 2 61 4.14968
- minieue 145.279 Seem trd S Sheer) force 2 100 meslesm
.,qq minimm 2 100 3.56861t=13 449.69
.PP, . . Sees trd 5 forspe Mon teus 2 86 ^ "4
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. gtam P 60 JA 0.0 3.206550D2 9.88856FD 1 2.201819D1 2.08199M*1 4.349822t*1 4.269634D2 MAMS 3.206550D2 9.868547D 1 2.201819D 1 2.08200001 7.471215t+0 2.740722t*2
; J8 100.0 H: 61 JA 0.0 3.026850D2 9.596164t*1 3.472494D0 2.08199M *1 7.471215t+0 2.740722D2 MAmu 3.02685002 9.5961MD1 3.472494t +0 2.082000t*1 1.72821M
- 1 2.859037D2
~ 62 Je JA '.00.0 0.0 2.881650D2 9 055494t+1 1.295162D1 2.08199M*1 1.72821M +1 2.459037t*2 MANG JB 100.0 2.841650D2 9.055494t+1 1.2951621 1 2.08200001 8.87570M+0 4.079709D2 63 JA 0.0 2.82101002 8.952238t+1 2.C32334D1 2.081996D1 8.875706 0 0 4.079709t+2 MAnt 2.82101002 8.952238D1 2.032334D1 2.08200001 4.93751M +1 5.614880D2 Je 100.0 S 64 - JA 0.0 2.627180D2 1.755450D 2 2.842429t +1 2.08199M +1 4.937513D 1 5.614880D 2 stanc JS 100.0 2.627180D2 1. 55450D 2 2.842429D 1 2.082000D1 8.701669D 0 2.20682!*2 65 JA 0.0 2.498590D2 1.572144t + 2 5.174T11D0 2.081996t*1 8.701669D 0 2.263682t*2 StANG JS 1C0,0 2.498590D2 1.572144t+2 5.174771DO 2.0820000 1 3.011161t+1 4.447341t+2 64 JA 0.0 2.440820D2 1.277168D2 1.36M3M +1 2.08199M
- 1 3.011161t+1 4.44 D41t+2 stAmc I'" JS 100.0' 2.uC820D 2 1.2771680 2 1.366635t+1 2.08200001 2.770121D 1 6.371525t +2 67 JA 0.0 1.174470D2 2.427737D2 1.864188t+1 2.T70118t+1 2.081995D 1 6.371525D2 - MAnc Je 100.0 1.174670t
- 2 2.427737D 2 1.866188D 1 2,770120t*1- 2.534715E +0 4.515452D 2 68 JA 0.0 9.359440D1 2.412974t+2 3.211804h1 2.77111t(*1 2.534715D 0 4.515452t+2 stAnc JS 100.0 9.359440D1 2.412974E 2 3.211804D1 2.T70120D 1 6.940574t+1 5.25997M+2
$9 JA 0.0 7.502780D 1 1.213479D2 2.242091D1 2.T70118D 1 6.940574b t 5.25997M*2 8tAmc Ja 100.0 7.5027 sot +1 1.213479t*2 2.242091t+1 2.77012001 3.038944t+1 3.640166D 2 TO JA 0.0 7.607080t*1 1.191590t+2 1.5072T7t +1 2.T70110D I 3.038944t*1 3.64016602 etAmG
[ JS 100.0 7.607080D 1 1.19:590D 2 1.5072T7t+ 1 2.7701200 1 5.4150691 0 2.T2101862 5.tmung + 0 2.770118D1 5.415069t +0 2.721018D 2 stANG g ;; 71' JA 0.0 JS 100.0 9.954250t+1 1.1246&3D2 9.954250D 1 1.1246a3D2 5.081682t*0 2.7701'0D 1 2.541157D0 3.037090D2 7 72 JA 0.0 1.098190D2 1.116869D2 1.049941t+1 2.T70118D1 2.541157t+0 3.037W002 SEAmG J5 100.0 1.098190D 2 1.116869D2 1.04994lt+1 2.770120E+1 2.015620E+1 4.239397t+2 l 4.239;97D2 SEAmG F T3 JA O.0 1.446490t+2 1.131494t+2 1.5898090) 2.770118D 1 2.015620t*1
" Ja 100.0 1.446490D 2 1.131494D 2 1.5898090 : 2.770120D 1 7.535927t+0 3.303873t*2 g-(- 74 JA - 0.0 JS 100.0 1.588550t*2 1.062569t+2 1.588550D2 1.062549D 2 9.62817M+0 9.6281 ?M +0 2.77011801 7.535927D 0 3.30387M*2 atAmG 2.T70120t+1 2.378043D 1 3.19290E+2 b 2.378043t*1 3.197963t+2 stAMG
). 75 JA 0.0 1.968740D2 8.07418D 1 6.7911586 0 2.T70118D1 f 48 100.0 1.968740D 2 8.07418D 1 6.791158t+0 2.770120D 1 1.119280t+1 3.03633t+2 LI 76 JA 0.0 2.170840D 2 7.546397D 1 1.518699D 1 2.7701186 1 1.119280D 1 3.633633D 2 BEAmc . Je 100.0 2.17086 & 2 7.5 6397t+1 1.518699t+1 2.77012M +1 2.92236M *1 4.489849D 2
+
TT JA 0.0 2.626860D 2 3.651169D 1 2.557808D1 2.7701186 1 2.922346D 1 4.489849D 2 MAmc + J8 100.0 2.626560D2 3.653169D1 2.557808D1 2.77012001 5.868619D 0 4.31017M *2 73 J4 6.0 2.735 D00 2 4.397252D 1 2.184311t+1 2.770118D 1 5.868619D 0 4.31017M+2 atAMG y JL 100.0 2.735n002 4.397252D1 2.184311E+1 -2.770120t*1 2.957882D1 4.02838M+2 U 79 JA 0.0 3.254070D2 9.014889E*1 1.324032t+1 2.770118D1 2.957882D1 4.02834M+2 SEAmC - W JS 100.0 3.254070D2 9.014289t*1 1.324032D1 2.T101200 1 6.006371t+1 2.443391E+2 to JA- 0.0 3.521890t+: 1.096847t+2 1.921758t +1 2.T10118t+1 6.006371D1 2.443391te2 SEAmc f / Je 100.0 3.521890D 2 1.096M2t*2 1.921758t +1 2.T70120D 1 1.021954t*2 3.457964DI . ?- 81 JA - 0.0 4.0691706 2 1.895975t + 2 9.193560D 1 2.770188D 1 1.021954t*2 3.457964D 2 MANG
! Je 100.0 4.069170D 2 1.895975t+2 9.193568D1 2.770120E+1 1.441002t+2 3.188T78D2 82 JA 0.0 4.444580t+2 1.796834D 2 8.833M7D1 - 2.T10118t+1 1.441002t+2 3.188778t+2 SEAMC
- Ja 100.0 4.464580E*2 1.796834t+2 8.833347t+1 2.T10120t*1 3.2T1102t+2 - 6.450J63D 2
- 0.0 83 JA 4.798350D 2 1. 70442M
- 2 8.739942E+1 2.770118D 1 3.277102t+2 6.45026M+2 atA>G JS 100.0 4.79 0500 2 1.704426D2 8.739942D1 2.770120D 1 4.425484t+2 8.609107t+2
.f' 84 JA 0.0 4 .91685M + 2 1.678216D 2 8.7764806 1 2.770118t +1 4.425684D 2 8.609107D2 BEAMG Je 100.0 4.916850E*2 1.67821M *2 8.T164806 1 2.T10120t+1 5.57628M+2 1.07861M+3
{7 85 JA 0.0 5.33J930D2 5.158115D 2 5.118362t+1 2.770118t+1 5.576286t+2 1.07861M*3 stAMG t . Je 100.0 5.33393062 5.158115D2 -5.11a162t+1 2.7701200 1 6.104424t+2 1.207294t 3 4 to JA 0.0 5.1881606 2 5.436708D2 5.137540t + 1 6.10642M + 2 2.770121t+1 1.207294D3 MAnc Ja 100.0 5.1881600 2 5.436708D2 5.137540(+1 6.104420t+2 3.876810D1 6.541264D 2
. 87 JA 0.0 5.272020D 2 5.65390D2 5.31741M*1 6.1044200 2 3.876810D 1 6.541264E+2 stAmc e
JS 100.0 5.272020 0 2 5.653963t+2 5.317416 D 1 6.1044200 2 9.115217D 1- 5.635827t+2 t 88 JA 0.0 5.2990506 2 5.705673t+2 5.413866D1 6.104420D 2 9.115217D1 5.635827t +2 OIAnc ., Je 100.0 5.I9905M +2 5.7056 D D 2 5.41386M + 1 6.1044200 2 1.44 M18t+2 9.244835D 2 - M 89 Ja 0.0 5.503170D 2 1.653059t*2 2.674935t + 1 6.104420D 2 1.447518D 2 9.244835t*2 BEAMG Je 100.0 5.50317DD 2 1.658059D 2 2.674935D1 6.1044200 2 1.169364t+2 6.981564D 2
- 1. 90 Ja 0.0 - 5.613190D 2 1.54C804t + 2 1.98324M+1 6.104420t+2 1.1693o4E+2 6.981564t+2 ' MAmG
- .; Je 100.0 5.613190D 2 1.540804D 2 1.98324M.1 6.1044200 2 9.444830E+1 5.556509t+2 W- 91 JA 0.0 5.712950D2 1.42s75M
- 2 2.036729D1 6.104420D 2 9.4648300 1 5.556509D 2 stAmG 2.- Je 100.0 5.712950D2 1.428756 0 2 2.036729t+1 6.1044200 2 7.484T10D 1 4.T72220t+2' --.
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F 4iAN ItINtu? LOA 0$ Az1AL $m(O Sat AA ItallCas SteluG BENDluG stAm P v2 v3 MT m2 m3 92 JA 0.0 5.763590D 2 1. 367072D2 2. 308404 t + 1 6.10442M + 2 7.484710D 1 4.772220 0 2 stAMG
, J8 100.0 5.763590D2 1.367072D 2 2.308404t + 1 6.104420 0 2 6.81M37D1 4.6797286 2 93 JA 0.0 5.931140D 2 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 g Ja 100.0 9.445890t=2 4. 743844D2 1.604191t+2 3.4719900 2 3.471987t+2 8.436039t+2 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 s b{ 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 keimm 6 6 69 100 75.0278 1005.9 1' f.' = 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* seem End 5 forgae men imm 6 100 207.727 n minimm 6 100 5.228571 13 -
'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* ,_
' g ;t Fine 1 MX/ Min Summer 1> Tabte let 10 Veiue i 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[ l me czy , w : Jc . _
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O Title : PeoP 2 19*319* U"r *10.2821
minf aus 1 96
' team trus & terem to 610.442 .s monimum 6
'i _.~ 81 *113.787 11/
Deem truf a moment 2 minimm 1 ' maalaus 6 17 782.2 minisue 1 93 '99.169F M team truf A moment 1 6 8d 1207.29 f, maa t am ut n4mm i 104 +309.332 Seam truf 8 Aalet f orce 100 1005.9 maa t sun 6 min 6 sue 1 102 +80.2569 Seam trus a sheer 2 f orce 621.254 mea tsus 6 96 minlaun 1 68 159.298 team tid I LAeer3 Iorce 100 207.T27 man tase 6 Seem tid 6 tor pe m6nisue 1 60 *102.044 maalaua 6 $6 610.442 minisun 1 68 +343.843 Bese trad 8 moment 2 610.442 p mealsum 6 85
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PA[UM. F ed AL CD J SHEET I I X FERMI 2 - CCHVAC sHEU W OME-1 DATE ( N CE uuva z.vnvulus ut TM7 OV6TEH-GERIEC J 0- 76230.502 , iv
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W y 0.g attachment are generated using the 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 moments in the ductwork by each duct size for DL, OBE and SSE conditions. Maximum and minimum values for each duct size are also I l presented. b Based on the commands issued by the preparer, STARMAp accesses the I working files saved by STARDYNE during The datathe string analysis are then spot runs and checked prints the data in tabular form. against the string analysis outputs by the checker. following , y The r,tring analysis outputs are contained in the calculations: DC-5763 CCHVAC Concern Resolution Task Duct String Analysis and Support Evaluation of h 2268 System Series VE CCm?AC Concern Resolution Task D DC-5764 Duct String Analysis and Support Evaluation of o M 2848 System Series i CCHVAC concern Resolution Task e- DC-5765 Duct String Analysis and Support Evaluation of - & J d [p+' 2849 and 4126 System Series .a
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DC-5766 CCHVAC Concern Resolution Task 4 Duct String Analysis and Support Evaluation of jk _$r5; 2850 System Series Z. k*?
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@kV jS- , DC-5767 CCHVAC Concern Resolution Task Duct String Analysis and Support Evaluation of M: , 4336 System Series .v K, a; Q
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fri apr 12 14 MO:C2 1996 gg 3793 g $18AhAP Verstw) 4.0 pesert f iemient Mcdel : tg format 51 AActet ter/te.ma I L emem ( , iltle : P90P 3 10*110* Output let 1 DEAD LOAD (DL) (0AD5 h[".
*d W "
+1- ulat et4a sotaa ttImtaf tutAa V3 TCRL om mi StuolmG m2 stacing m3 k 1 SEAft 0.0 a
3.044360t 2 v2 7.137547t t 2.0155221+1 3.930880t 15 3.209238E 15 0. 1.5675171 0 etAmG h 105 JA JS 100.0 3.044360E 2 7. E3 75871 ' 2.015522t*1 3.930880E 15 1.6 8800E 15 A.031043E 1 4.031043E*1 1.567517t +0 StAMG M+ 0.0 3.MMot 2
- 5A3839t 3 3. 673 t T3r t 106 JA .
4.107659t.1 1.5511371 0 Je 100.0 3.0 4%0t 2 7.8&3239t 3 3.6731734-1 1.668800t 15 4.107659t*1 1.551137E 0 stAmG 107 JA 0.0 3.G+4360( 2 f.3019t't*0 -3.197319f*1 8.246880E 15 2.893415t*0 2.3999071 1 3.M360E 2 1.3019114 0 3.197t.9t*1 3.246880E 15
! Je 100.0 2. 893415E *0 -2.3899071 1 stuG 108 JA 0.0 3.064360f-? 135232f 0 . 5 31L33t
- 1 -3.625570( 14 2. 764339t *0
- 3. J5570t 14 6.524045t*1 Ja 100.0 -3.k4360( 2 -1.325282i 0 = L110314 1 2.764339t*0 stuG 0.0 3.%4360E-2 ' . 32527M *C . 481769n t 3.52843C1-14 6.1240431 1 109 J4 1.665805t.1 7.8571T71 1 k4 Je 100.0 3.044 Mot 2 1. 82529M
- 0 4.481769t*1 3.528430E 14 3.432063t*1 1.856850E 14 - 1. M5805E
- 1 -7.857177t1 1 EEAMG h 119 JA 6.0 3.Wh0t 2 - t 40534 71 0 2. 0476SM
- 1 7.%86721 48 100.0 3. M 360E 2 1.4053471 0 1.4 3200t
- 1 1.b68501 14 7.%86T21 1 St uG y 111 JA 0.0 3 % 4 % 04 2 1.035459t-1 ' . 780768f *0 2.00881M 15 2. 0476SM
- 1
- 9.850294t 1 015 39t ?SU6M*C 2.008810f 15 -2.477920t*1 Ja 100.0 3. N4360t - '
2.*?7920f*1 9.850294E 1 stAnc 0.0 3. 0 .h0E . S.3 M st 2.16 419t 1 5 . 5 3 7240( - t 5 1 030820(*0
, 112 JA 1.16 6toget 5.537240(-15 2.756130f 1 JS 100.0 - 3.M%0E 2 -8.336845E 1 1.030820E*0 stAmG 0.0 3.044 h0(-2 -f.728.'071 0 *.390269t*' -1.5543106 14 - 2. 756130E
- 1 5.987180E 1 O 113 JA Je 100.0 3.0=4360f-? t.778e07t.c . 390269t.1 1.554310E-14 2.2339Act 14 1.65850t*1
-1.6555634 1 5 987180C 1 8(Anc
% 114 Ja 0.0 3. 0-4 h0( 2 7.5"561M i 1. 43 M t*1 1.M T259t*1 4.686848t 1
; },
- 3. k4360f 2 7.5 7561M t -1.M3 M t+1 2.2339sof-14 JS 100.0 5.6868488 1 BEAMG 1 !,
JA 0.0 3. MM01 - 2 1.5982tu t . 69.334t *0 2.169100f 14 1.% 7250t*1 8.151300E 1 7 11$ JS 100.0 -1.044360( 2 1.59821M - 694 334 t
- 0 2.169100E 14 2. 09112 M
- 1 8.151300E 1 stAnc 2 281023tet 2.706860f 54 2. 09112M
- 1 0.0 3. M hof-2 9. 05 36M - 1 h
.e 116 JA Je it* O 3 044360E 2 9.40536M t 2.231023E*1 2,70d860( 14 2.543185E t 5 722991E 3
- 3. 073 h0( 2 1.541822f
4.734224E 2 3.646209t 2 stAMG
$ 117 JA .; 1.521430t*1 - 3 0 435M ' 3.073 %0E-2 1.236493tet 5.126371t 2 h-Y 118 Ja 100.0 JA 0.0
-1.52'430(*1 2.775920E-2 3.0 43554 2 1.424964t*1 2.5 31851 1 5.21519?f 1 3. 479660E - 15 1.191381t*1 5.765685f*1 3.309993t*0 SEAnc 1.569902t*1 4
2.795020E 2 1.4249644 1 5.215t92t*t 3.479860E-15
$ JS 100.0 5.765685f 1 1.5699021 1 SE4mc 0.0 2.795920( 2 1,12 7136E .1 e .135 701t a t 2.003950t-14 119 JA 5. 37445M
- 0
$~
JS 100.0 2.795920( 2 1.127136tet 2 .1357014 1 2.003950f 1+ 1.9773831 1
- 1. 97738.3 E .1 5 . 374456E
- 0 stAnc 0.0 2.795920t-2 8.9 b220(*C 3. 2 78 38f
- 1 5.82867t4 15 120 JA 3 270 38f*1 5.328670E 15 1 02566M a 2.80928)t*0 'd !
Ja 100.0 '2.795920t 2 8.95 220(*0 2.809289t*0 EtAMG 5,258 45E *0 0. 1. 02566M * ' JA 0.0 2.795920t 2 1.42987M *0 5.311571E*0 121 0. 1.945894t*1
-2.795920( 2 1.42957M
- 0 -5.258445t*0 g
W 122 J8 100.0 JA 0.0 2.7959201 2 3.03516*t*0 1.111939t*1 1.1119391+1 c. 0. 1.945894t 1 -5.311571t*0 SEAnc 7.10542?t 15 2 .122434f - 15
=.
2.795920(-2 3.0P18.E 0 O viite A IN.0 reon 3 10 iio-
%- Output Set 1 DEAD LOAD (Ot) ID Value N M Set MAX / Nim Summary table minimm Set 1 118 0.027959 N! ' Seesa End A AAlet forte t 11? 15.2143 [
DU maa s sun - minima 1 118 14.2496
'@ , Beems tral A Sheer 2 f orce 119 11.2714 me n isus 1 g- Beems End A shear 3 f orce minisun 1 118 -52.1519 W, menisue 1 109 44.81 77 j- id, minimm 1 108 3.625571-14 dMd Seen End A forwe me a le. m 1 117 0.030734 ,O i 4 M.f minimm 109 65.2404 hM Seem . , (M A moment 2 1
Mh;
- mea tma 1 107 41.0766 < jf minisam 1 122 5.31157 l Mre*, , Seem tnd A Moment 3 i 119 15.e99 max imm QM p4yg c < BeJa End B Amtet force minisam 1 1
117 118 15.2143 0.027959 me n iaue y miniaun 119 11.2714 '+ Q[2; y A;, Sosu EM S Sheer 2 force maa ttem 1 1 118 14.2496
.l g & g' ..
miniu m 1 109 -44.8177 5 l pr Seem fnd 8 Sheer) Force 118 M.1519 -l 1j maaimm 1 M miniaun I 117 0.030734 Seen End 8 for we 108 3.6255't-14 g . .' maaimm 1
.5 '
minimum 1 106 41.0766 T Seen End 8 Moment 2 j i, ww.mw ,g maa tam 1 108 65.2404 t.N-@
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tri Ar 12 lu40:06 i m seport 1 tienent oc-syn
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[ s-g title a Per 3 10*t10* A Outsmit let 1
- DEAD LOAD (04) minious 118 *15.699
); seem trui e nament3 1
5.31157 i ,"; manimum 1 121
.11tle Pew 3 10*E10'
,Q[.. Output let 2 = CSE 4040t 6tAe i4EuEu1
{j , stuoleG lutAA latAN TCstlica steluG ulA4 R3 P v2 v3 ut m2 C M AA 105 JA 0.0 2.281530t*2 4.030591t*1 5.193237t+0 1.152003t 14 2.093015t 148.061183t*1 1.038647t+1 1.655167t 13 stAmG 2.281530t+2 4.030591E
- 1 5.193237t+0 1.152000t 14 8.061183t+1 EtAMG Jt 100.0 3,97 6 3tet 1.872070t+0 3.613319t 16 1.03364 71+ 1 106 Ja 0.0 2.510000t*2 1.24899SE*) 1.6327671+2 2.510000t*2 3.97 & 3tet t . S T2070t + 0 3.6133201 14 JS 100.0 1.248998t+1 1.632767t+2 BEAMG 3.907352t*1 7.893246t+0 6.400450E 14 107 JA 0.0 2.88333M
- 2 7.893246t+0 6.40045M 14 1.021205t+1 2.165091t+2 J3 100.0 2.f43330t
- 2 3.9073521 1 1.021205t+1 2.16509tt+2 stAnc
(' 108 JA 0.0 3.037'50t*2 3.89773M
- 1 1.102912fet 1.297789t 13 2.695998t + 2
=
- 3. 03715M
- 2 3.897739t
- 1 1.102912tet 1.297790t 13 2.016248t + 1 2.695996t+2 StAms JS 100.0 1.556899t
- 1 1.8633cM*13 2.016248t+1 109 JA 0.0 3.93534M*2 2.27978et
- 2 3.455037t+1 3.935340t*2 2.2 79754t
- 2 t.556899t+1 1.863360E 13 4.16802M *0 Ja 100.0 1.393929t+1 9.k2TT9f 14 4.16802M
- 0 3.455037t+1 stAMG 110 JA 0.0 4.03637M+2 2.2TT211t *2 2.269762t+2 1.393929t*1 9.64278M 14 1. 27476M +1 J8 100.0 4.05637M
- 2 2.2T7211E*2 2.269762t*2 stAMG t t t9139t + t 1.610a57t 14 1.274769t+1 111 Ja 0.0 4.4313&M *2 2. 261775t
- 7 7. T2175 M
- 2 t.tf9139t+t 1.610860E 14 3.919 789t
- 1 J6 100.0 . .+ 3138M
- 2 2. .'6175 t * ? 7.T21758t+2 BEAMG 1.228142t+1 2.125687t 14 3.919759t
- 1 JA 0.0 4.70101Ct 2 2.247503t*2 1.315305t+3 til t.228142t+1 2.125690E 14 6.597604t+1 J5 100.0 4. 70101M
- 2 2.247503t
- 2 1.315305t+3 stAMG 5.435300t*2 2,1835e9t*2 4.6286tt+1 1.8785511 13 6.597604 t +1 Q 113 JA 0.0 4.642561tet 1.878550C-13 5.454538t+1 1.273438t*3 48 O J.0 5.435300t*2 2.18358vt*2 5.454538t+1 1.273438t+3 stAMG W 0.0 5. 71418M
- 2 2.159171t
- 2 + 538887t*1 6.786921t 14 1.0433Nt + 3 114 Ja 4.538837t+1 6.726920t 14 1.704756t 1 JS 100.0 5.714150t*2 2.15417tt 2 1.043399t+3 EFAMG 4,50119TE+1 8.196640t 14 1.704756t*1 115 JA 0.0 5. 885690t
- 2 2.112496t*? 8.839697t+2 4.501197t+1 8.196640f 14 8.529686t+1 JS 100,0 5.885690t*2 2.11249M
- 2 8.839692t*2 atAMG
-3 0.0 6.201050s 2 1.95615M
- 2 4.49014t*1 1.215221t 13 8.5 N68M
- 1 8.396118t+2 3 116 JA JS 100.0 6.201050t*2 1. 95615 SE
- 2 4.490104t+1 1.215220t 13 1.259558t*2 6.402543E+2 staxG 5.576320t+2 1,891404t 11
- 6. 27896M
- 2 8.863805E+1
.117 Ja 0.0 1. 74 7770t
- 2 5.57632M
- 2 4.309570t+1 9.301316t+2 6.275969t*2 8.563803E+t Je 100.0 1. 74 7770t
- 2 1.04T800t+3 stAMG JA 0.0 1. 73081M
- 2 6.448189t*2 1. 343414t
- 2 1.81150M 12 2.82968vt + 2 3.212390t+2 118 1.091191t*2 JS 100.0 1. 73961 M
- 2 6.44818 M
- 2 1.343414t + 2 1.8115004 12 3.212390t*2 stAMG 1.Sf3104tal 4.881519t 13 1.091191t+2 JA 0.0 1.222220t*2 5.217201t+1 2.74039t+2 119 1.81310 stet 4.881520t 13 9.454545t+1 JS 100.0 1.2S822M*2 5.2172011 1 2.764039t+2 stAmG 1.371589t
- 1 1.84761M 13 9.454545t+1 JA 0.0 1.224960t*2 5.*16-65E+1 2.287262t+2 120 1.57tS89t+1 1.6476201 13 7.896502t*1 JS 100.0 1.224940t 2 5.41663t 1 7.896502t+1 2.2872621+2 StAmG L JA 0.0 1.02318M.2 6.340563t + 1 2.182795t+1 4.906365t 14 1.179174E+2 121 4.106642t+1 JB 100.0 1.023180t*2 6.3405< e t 2.182795t + 1 4.906360f .14 1.179174t+2 StAMG 2.346653t+ 4.0647911 16 4.106642t+1 122 J4 0.0 9.045870(*1 6.738 t e tt e t
+ 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 minisun 2 122 FO 4587 seem EM 4 Aalet f orce 2 116 620.105 %"
han isus
% Seam End A Sheer 2 f orce minious 2 108 38.9774 "
masisue 2 118 644.819 L {et wy; ;Some End A Sheer 3 Force NNaus 2 106 1.87207
-$Gf , Beam End 4 fortpe maalsue Minimes 2
2 118 105 134.341 1.1521 14 W
'7 DW menisue 2 117 557.632
= minisue 2 105 2.093021 14 ^
$+aan EM A moment 2 f maalaus 2 118 282.969 C .
minisun 2 105 1.65117t.13
- Kf '
Does EM A noment3 maalaus 2 113 1315.31 i
% minious 2 122 90.4587 pf team EM 5 hiet force maalmJa 2 lie 620.105 M y- utnisun 108 38.9774 7' ; Seem (M 4 Sheer 2 f orce 2
644.819 h manimum 2 tla y i ninluur 2 106 1.87207 ' Seems End B Sheer 3 f orce p maatsus 2 118 134.341 f M k N{ W% hs yMW W W +L "-
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y ATTACHMENiE $n~ DICO ttavAt $ttttu 4316 1,2,3 pel Apr 12 14:40:10 199o SHEET $ OF T j"
~876amAP vercian 4.41 leadet toport tienent QG]Q ,
? Ft+eet $1Aa0fut ter/8ean Element h . Title : Peor 3 10*s10a . 6 s - thstput Set 2 + OSt 105 1.152t.14 j, , fp^ (
~
team EM 5 Terem . minimm 2 nomiam 2 117 557.632 E-minima 2 tN 5.811M .13 toen E M S enament2 116 125.956 masimm 2
-Of '
minium 2 122 3.217kt 12 5l~ seen (M e moment 3 2 112 1315.31 mes t am T I title t Peor 3 10* 10a h Cutput let 4 * $$t L0A05 8 TAN tLiaieI 10ellom stuolnG StuottG aslAL Set Aa SMA8 N2 143 gr v2- 1/3 #7 P p MAM 0.0 2.1980000 2 4.099140t+1 4.430953D0 1.498109t 14 2.721389E 148.1982800 1.804241t 13 8tAMG 74 105 JA 1 b J8 100.0 2.1980000 2 4.0991400 1 4.43095300 1.4981900 14 8.86190M +0 8.861907t+0 8.1982800 1 StanG 4.013853D 1 t . 81347M +0 3.68S437t 14 7 106 JA 0.0 2.415M00 2 3.68844M 14 1.108205D1 1.651527t+2 2.41566CD 2 4.013853t+1 1. 81147M +0 1.651127D 2 StAmG
. JS 100.0 6.43308D0 6.973581t*14 1,108205t*1 107 JA 0.0 2.771460 6 2 3. 953353D 1 2.181795t*2 JE 100.0 2.T714606 2 3.953353D1 6.643308t+0 6.973580E 14 9.879538t +0 2.181795t*2 SEAmG 108 4A 0.0 2.9180900 2 3. 967103t
- 1 9.239869E*0 1.845373f 13 9.87?538D 0 2.71313M* 2 Je 100.0 2,918090t*2 3.967103D1 9.239869D O 1.84537M 13 1.792T72D 1 2.71313M +2 alAMG 2.29658+D 2 1.406587t+1 1.9405891 13 1.792772t +1 109 JA 0.0 3.774530t+2 2,2965890 2 1.406587t+1 1.940590t*13 3. 74593M *0 4.570320t*1
- JS 100.0 3.T745300 2 4.570320 0 1 stAnc 3.88W70D 2 2.N2517t *2 1.281861D 1 1.21694M 13 3. 74593M +0 -
110 JA 0.0 1.281861D1 1.2169500 13 1.2114866 1 2.326387t*2 J8 100.0 3.8899700 2 2.292517t*2 2.326387t*2 BEAMG 111 J4 0.0 4.2476406 2 2.2705T71+ 2 1.075913t*1 2.2312390 14 1.21148601 7.78425 M
- 2 Ja 100.0 4.2476400 2 2.2 7057?D 2 1.075983f+1 2.2312300 14 3.762248 1 7.78425M
- 2 St AM.
1.15 3 702t
- 1 3.1980391 14 3. 762264D 1 112 JA 0.0 6. W 800t+2 2.M14bt*2 1.3220790 3 j c 2.2516M D 2 1.153702t + 1 3,19804DE 14 6.336983D 1
< Ja 100.0 4. W 800t+2 6.336983t*1 1.322079D 3 stAMG ,. 113 JA 0.0 5.205t50t+2 2.937925f+2 4.385423D1 2.4378090 13 1.268030E*3 }; I 114 Je 100.0 JA 0.0 5.2051500 2 2.93M25D2 4.38%23D1 2.43?B00E 13 5.26342M
- 11.2680300 3 stAMG 5.4711?M + 2 2.906557D 2 4.307533D1 7.7539118 14 5.263426019.930184t+2 1.74128 4 Ja 100.0 5.47117M + 2 2.90655 7D2 4.30M33D 1 7.753910 0 14 1.7412SM
- 1 9.930184t+2 StAmG y
115 JA 0.0 5.6%M002 2. 8*539 7t + 2 4.276515 9 1 1.1347121 13 8.751695t+2 Ja 100.0 5.6MM00 2 2.8453971 2 4.276515t+1 1.134710D 13 8.10182901 8.751695t*2 stAMG 116 JA 0.0 5.9355406 2 2.43024D2 4.257928D 1 1.403442t 13 81.195853t+2 101829f*1 9.010085t*2 2.43024D2 4.257928t +1 1.4034900 13 JS 100.0 5.935540(*2 3' 1 112 JA 0.0 2.2651002 6.009562D 1,304075D2 2 1.304075D2 5.7808500 5.780852t*2 1.864380D 2 6.340396t+1 9.6424730 112 7.013797D2 StAmG JB 100.0 2.2675100 2 6.009862 0 2 1.0911440 3 StAMG 118 JA 0.0 2.3612606 2 6.169588D 2 1.28299M*2 f.7299378 12 2.781M9t+2 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 3.912997t*2 2 stAMG e
7.785009 0 1 1.877510D 1 4.753630t 13 9.9965800 1 O JB 1C4.0 1.783880t+2 9.996560t*1 3.912997D 2 atAmc 120 JA 0.0 1.702690E+2 8.0125470 1 1.96247'D1 1.797178f 13 8.309045t+1 3.1934900 2
%m Ja 100.0 1.7026900 2 8.012587t+1 1.962473t+1 1.797170 0 13 2.301348t+1 5.10415M 14 8.309045t*1 3.19349002 stAMG E 121 JA 0.0 1.442950 0 2 8.92T264f + ' 1.63295402 JS 100.0 1.4429506 2 8.92T264t*1 2.301348t*1 5.1041600 14 4.303558t+1 a 1.632954D 2 StAMG
.. 122 J.4 0.0 1.2893500 2 9.331165t*1 2.45917M+1 3.996531t.14 4.30355801 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" R t d thatput set 6 55t Value ad set ID pgd let &luR/ Min Sammary Iobie MMimm 6 122 128.935 "
mo' hyg %. Seem
- EM A Aalet force Maalma 6 116 593.554 W '
team (M 6 Shear 2 force m i ni == 6 107 39.5335 W
,s.
JW maa lam 6 118 616.969 . rA ulnimm 6 106 1.81348
@_ 5ees EM A sheer) f orce 117 130.408 , ^ ,'
M aa l == 6
@6 . - -
Seen EM A Tortpm minim m 6 105 1.498190 14 ' *w uasiam 6 117 578.085 {W$ w, [s g
' team EM A moment 2 minium 6 105 2.721398 14 1> --N.
naulam 6 118 278.176 'J f "EJ i [V Seem EM A moment) Minimm maala m 6 6 105 1.80424t 13 113 1322.08
,28. m y
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t, 3 yfe , masima 6 lie 193.554 k
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l _ ATTACHMENT c-s@rfe
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. OtCO Cfevat 575114 4316 1,2,3 Fri Apr 12 14:40:14 1996 saport : Element
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N-6f: ~fitte : PecP 3 10=x10= 107 39.5335 JM - [ Owepwt let 6
- sti minimm a 4 1 F -[ 118 616.999 '
i y Seem tid e Sheart force maatam 6 1.81348 f 6 106 i: f minim m 130.408 (% 2A . , team Erd a sheer 3 force mas tam 6 117 105 1.49419t=14 i minimus 6 578,085 D~ Dean trd 8 forgue maalaus 6 *17 t h minleue 6 122 5.l?l19t*13 I~ team trd I feoment2 6 114 119.585 maalmun e - 6 122 3.17641t 12 minimum 1322.03 i Seen Erd 8 masent3 Natam 6 til
^
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fitle t PeQP 3 10"X10* let i 10 118 0.027959 firel NAX/plu Summary f ebte win 6mm i 116 620.105 teen truf A Aalet f orse maaloue 2
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~- a 6nimm i 118 118 14.2496 6&4.819 S'_ team trd A theer2 force mant sm 2 118 52.1519 minimm t 118 134.341 ,
2 Sean trd A Shear 3 f orce masisue 108 3.625571 14
- k. 1 minimm 117 518.085 Seeuntid A forspe mestam 6 65.2404 1 109 eI", .
minim a 114 212.969 been Erd A moment 2 man t am 2
, i 122 5.31157 alnlam 1322.08 Q Seem trd A moment) mea tma 6 113 g minisue i 117 *15.2143 p '.
116 620.105 Seen Erd 8 Aslet force aaaisue 2
, ; 119 11.2714 1
th minim m 644.819 2 118 f Seem trd 8 theer2 force maalma 109 44.81TT 1 gu- minimm 134.341 2 118
$ tea sres C Sheer 3 force maatsus 0.030734 1 117
%. e: Seen Erd 3 Tonym ministan maatsue 6 117 578.085 '
-! minima i 106 41.0766 h
.s seem truf 5 moment 2 mantman 2 116 125.956
*15.699 4
1 118
- minious 112 1322.08
; seem trd a moment 3 maatsam 6
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I h i eu . l ATTACHMENT d l ru- IL ' #a g
- mwer ~
C HK n Inf M QEu N w -u awase m enu GENERAL. cAtcuuTO4 SET M DC- 5773 k [drIR$Y" 14 pf g R?F' s Enginecis & COMPUTATION 00
'o 3 g$4 pg FINAI.
Constructors - _-PAEUM. .. A . SHEET ,e p , X __ *
- oATE
, FERMI 2 - CCHVAC ~. SHEri OF DATE s.
h, PRCUECT_ puvT LvALUATAvH vt_ %4 - J o. 76230.502 p:t TV ;4 .. sueutCT _ . cys9tg_ssnyt; ~;; - : I b the g; . are generated using t b T he data contained in this attachmentSTARMAP is a companion lyses. program of L STARMAP post processing f eature.STARDYNE which is used to perform the 7 9 the tabulated data is to present the forces and A E The purpose of ductwork by each duct size for DL, OBE and SSE moments in the conditions. Maximum and minimum values for each duct size are 4 presented.
- g ' ., P accesses the lysis runs and l Based on the commands issued by the checked preparer, STARM
,' in tabula.r form.
prints the dataagainst the string analysis outputs by the checker. Q contained in the following W The string analysis outputs are
?!I R calculations:
y
- 7'* s .DC-5763 CCHVAC Concern Resolution TaskDuct String Analys ,
- 2268 System Series gg .
- b y
- k. ' DC-5764 CCHVAC Concern Resolution TaskDuct String Analy y? 2848 System Series '
A> y s e; y DC-5" 65 CCHVAC Concern Resolution TaskDuct String Analys 2849 and 412d System Series IM - h' e 4D DC-5766 CCHVAC concern Resolution Tasknuct String Analysis .. 35 k 2850 System Series E' 4y .; . hN DC-5767 CCHVAC Concern Resolution TaskDuct String Analy 4316 System Series ,: ' gk
![,.'
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ATTACHMENT W M w& W .4
. g Q- OF W '
' 0100 ttu/aC 1151tu 4316 6 & T N*M D i thw Apr 18 12:49:02 1996
- N . '
Stae w version 4.41 4 aeger : [tsesnt Model :S u _ formet 1 Staa0fut Ber/Seem tie *wat -4 y (.;1;*
~
title 1 Pt0P 3 16*t16* , , 4 ", p - Outsut let 1 DEAD LCAD (Mt tLtatut L0A05 , at 8iAm a. ' ' ~ [;- StuothG SatAt $NE AR Tot $!CN $tlCl4G ARIAL su V3 af m2 P v2 M Mt
- 1. 95118M
- 1 2.15764M *0 1.349383t*1 1.737938t 1 SEMG 4 61 JA DJ 2.90799:( 4 ' . 4* %0 A t . 2 2.612947tel J.2251571 1
-2.90798;t.2 .*360ht 2 1.98118M *1 2.157M0t*C Je 100.0 1.063407t*1 6.60C884 1 SEAMG 62 JA 0.0 6.45870ct.t 1.01984t.1 4.509343t*y 1.29894M
- 1 5.509163t*0 1.298940t*1 2.1465871-1 1.664068t*0 JS 100.0 6.45870CE 1 5.019t%t 1 3.225157E 1 SEAMG 0.0 7.43600ct 2 4. 90799?t 4 0,01824*t 1 2. 61299M
- 1 4.157639t *0 63 JA 1.420638t*1 3.0434081-1 7.436 mci d ?.9ml?t 4 '9.018243t*1 2.61299Ct+1 JB 120.0 9. 98826;t
- 1 2,612MCE
- 1 1.420 384*1 3.0434081 1 st 4MG .
M JA 0.0
- 43609C( 4 L 90 587t 2 1.1M331t*2 2.861659t 1 JS 100.0 7.4360 N 4 2.9079521 2 -9.988269t*1 4.61299Ct
- 1 1.166331t*2 2.861659t*1 6tAMG 7.436@0E 2 2.617t321 1 1.059312t*2 2.612 N04+1 65 44 0.0 2.5395031 0 5.806720E 1 48 100.0 T.43609M 4 2.617&I2! 1 1.059312t*2 4.612990t*1 2.539503t*0 5.806T20t*1 StAMG 7.43409Cid 2.4171L12t 1 - 8.84 7069t
- 1 2.612990t*1 66 JA 0.0 1.C20690t*2 8.751781t 1 7.4360901 2 4.6178321 1 8.547c691 1 2.612990t*1 J8 100.0 2.63 450t 1 S.907958t*1 2.53924M*0 8tAMG 67 JA 0.0 1.7635t2t'? 1.8.0 % f 1 2.92967M*0 1.96111M*0 JS 100.0 l.7635 ?:(
- 3.54ht 1 4.92967M *0 4.0,44!LE *1 8.468507t*1 8.468507E*1 1.96311M *0 stAMC 5.763510( 1 3.840864t 1 2.621031t+1 2.634450t*1 58 JA 0.0 4.53444 1 1.386957t*0 5.76351M 1 3.84G86*t 1 2.621031t=1 2.63445 M
- 1
- J8 100.0 2.6 W 50t*1 4.53696M*1 1.384987t*0 SEAmG 3.0 5.7635tX ? 1.84 N t 1 4. 94 9095 t
- 1 69 4A 5.76351C1 1 5.bO86*t 1 *,9+9095t*1 4.6 W 5M*1 2.L M f+1 8.108571t 1 A JS 100.0 2.634450t*1 2. M t*1 8.108571t 1 &EAMG 70 JA 0.0 1,763110t 1 3.840%t 1 6.159552t*1
; 2.63445Ct+1 8,517389t +1 4.9091321 1 Je 100.0 5.76351C1 1 3.840864t 1 6.59552t*1
- 0. D. 2.392184t*15 BEAMG 71 JA 0.0 2.431360t*2 4.454554t 1 4.617797t = 1 4.45455 4 1 2.617797f 1 0, 1.3088991 1 2.2272T7E 1 p Ja i00.0 2.431340E 4 1,308899t 1 2.2272TTE 1 EtAMG 72 44 0.0 t 90331M *2 . 414554r-1 4.6177971-1 1.78113M 15 1.596067t*0 t 2.61T797t 1 1.781130t 15 9.3 m 671 1
,;t Ja 100.0 1.90331C1 4 i 4541141 1 1.14529Ct*1 1.942758t+1 SEAMG 1.3 m 34t 1 6.50874M 1 1.15985Ct+0 l4 73 JA 0.0 7.227890t*1 1.259193t*1 1.966864tet 7.227890t*1 1.3m34 1 6.50874M 1 1.159850t*0 i JS 100.0 1.15985W 0 1.2591934 1 1.966864t*1 stAMG s
0.0 1.T64230t*1 1.3 m 344 1 6.5C874M 1 7 ' 14 JA JS 100.0 1.7M 23M
- 1 1.3 m 344 1 6.50874M 1 1.159850(*0 1.335151t*1 1.335151t*1 1.982940t*1 1.159853t+0 stAMG 6.50875ct- 1. 3 m 341 1 . 6998511 1 1.9829 M *1 75 JA 0.0 1.389998t 1 9.990953t*1 6.50875 C5.1.3'1m 344 1 4.6998518 1 1.98294M*1 JB 100.0 1.98294CE*1 1.389998t*1 9.990953t 1 SEAMG T6 Ja 0.0 6.50875M 1 1.3 m 34f 1 4.540627t*1 1- 4.540627t+1 1.98294CE*1 3.660311t+1 9.302186t 1
- Je 100.0 6.508750t 1 1.3 m 34t 1 6.50875M .1 1.1308371 1 5.53033M
- 1 1.98294Ct 1 3.660311t 1 9.302186t 1 stAMG D T7 JA 0.0 t.982940t*1 4.793593t +1 7.9824411 1 JS 100.0 6.508MCt 1 1.13:5871 1 5.53033M*1 1.98294ct.1 2.793593t*1 7.982441t 1 SEAMG TS Ja 0.0 6.50875CE 1 1.13*8871 1 3.331870t 1 S 48 1Go.0 6.50875M 1 1.13G887t 1 3.33187CE*1 1.982940t*1 1,982940t*1 8.344489t+1 6.09838M 1 6.09838M 1 SEAMG
- 6.508750t 1 1.1308871 1 4.066599t*1 8.344449t+1 "1 '9 JA 0.0 1.98294CE*1 5.9327684 1 4.T78638t 1 J5 100.0 6.5C8 MCt 1 1.130887t 1 2.066599t 1 5.932770f*1 1.982940t*1 -4.778638t*1 SLAMG f 80 JA 0.0 1.130890t 1 4.5C874M 1 3.877812t
- 1 2.542490(+1 2.817069E 1 1.130490E 1 6.5C874M 1 3.8778328 1 5.932T70t+1 JS 100.0 B 81 JA 0.0 1.130490t 1 6.5C874M 1 8.888291t*1 5.932770t+1 2.54249ct.) 2.817069t*1 SEAMG 1.040627t*0
=0
^
6'" . 6.50874M 1 8.888291E*1 5.932T70t*1 1.290424t*2 Ja 100.0 1.130490E 1 1.290624t+2 1.040627t+0 stAMG 2.42141CE 1 1.269527t+2 5.932 TTCt +1 82 JA 0.0 6.82171CE-15 2.851580t*) -8.329932t 1 6.82171CE 15 *2.12141M 1 1.269527t
- 2 5.932770t*1 JB 100.0 5.932770t*1 2.85tS80t*1 8.3299521 1 ftAMG 0.0 -6.8217101-15 2.62161CE 1 8.7720511 1 83 Ja 5.932T70t.) 6.288896t*1 5.598235t 1 J8 100.0 6.82111Ct 15 4.62ta1M 1 9.772051t *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 14 _ 3.077906t*1 2.988*40t*1 4.032144t+1 -1.494918t 1 JS 100.0 8.302860t 2 1.1555Ct 1 4.032144t 1 1.4949184 1 stAMG .
1.17515CE 1 4.9142 Tit *0 2.98804M *1 85 JA 0.0 8.3028601 2 4.71T7721 2 h'M ~ JS 100.0 8.302S604 4 1.15 55CE 1 -4.9142?1t*0 2.98804CE*1 4.854302t+1 1.819441t*1 2.381550t*3 SLAMG 1.13C544 3 1.136343t *2 2.98804M
- 1 64 JA 0.0 6.3?25605 4 1.428254t +2 4.266931t 3 8.302360t 2 1.33014 4 3 1.1363431 2 2.98804Ct+1
+ JS 100.0 1.33C5444 3 1.382109t
- 2 2.988040t*1 1.428254t *2 4.266931t 3 stAMG 87 JA 0.0 8.302860E 2 3.846945t* 2 6.5953844 3 lt JO 100.0 8.30286CE 2 1.33054 4 3 1.382109t*2 4.98804CE*1 1p 2.2M666t*2 7.2338808 12 5.240121t+2 3.T79547t 2 BEAMG 88 JA 0.0 0. 5.03939M 2 2.116546t-3
- 0. 5.0.1939M 4 2.294666t*2 7.233880E 12 6.864745t+2 ON 48 100.0 6.864745E+2 2.116544t 3 BEAMG .' t 89 JA 0.0 5.55112M 15 1.039396t 2 2.672868t
- 2 3.538500t 12 0. 5'-
5.551120E 15 5.039396t 2 2.6T2868t*2 3.538500t 12 6.977C05t+2 JS 100.0 0. BEAMG1 ~$ 90 JA 0.0 0. D. 1.468943t+2 5.934920E 14 -6.9TT005t*2 0.
$ . Ja 100.0 C. D. 1.468943t*2 5.936920t 14 3.428038t+2 0. s m& , '
91 JA 0.0 0. O. 1.090633t*2 6.294960t 14 3.4280384*2 SEAMG [
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ATTACHMENT D M hp SHEET % or,,,1 ( , Otto 00mva0 $ttitu 4316 6 8 7 3 D (- 7'/"O - ;. . TV, Thu Apr 18 12:49:06 1996 ,.' **- A' 4 81AhmAP vertf ort 4.41 Report t tLtaent h *y M [3 leadet t p N Forset . t 51AA0tht ter/ teem tienent k.. t PROP 3 16N16" v;SU fitte ~~ thstpaat let 5
- OLAD LOAD (DL) LOADS 8 tam (Ltuttl '
[ latAA toasicM sinolmG SthotnG b 6 aulat satae at m2 m3 e vi v3 7.461723t*1 0. . [e- StAm JS 100.0 0. O. C. 1.09063312 6.294960t 14 4.56965M*1 *T.327470E 15 T.461723D1 0, et A#eG . 92 JA 0.0 6. 2.279671t*0 0. N' JS 100.0 0. O. 4.56965M
- 1 T.327470E 15 2.279671t *0 0. StAAec l' 0, 0. 4.206035t*0 8.570920t*14 0.
93 JA 0.0 C. O.
- 206035t *0 8,570920t.14 1.64002tt 12 JB 100.0 1.294690tel 3.117368D 1 2.151903t 1 etAnc 94 JA 0.0 1.61016Ct t -.13431st 2 2.0 0862 D I F.294690t*1 T.210746D1 1.2&2565E 1 Ja 100.0 -1,61016ct 1 6.3343131 2 2.040862DI F.210746t*1 1.252565t 1 stamG
. 4.134318t 2 3.572086t*1 7.294690t*1
- 95 JA 0.0 1.6101608 1 4.617819D 1 4.132267D2 JS 100.0 1.610160t 1 4.334318t 2 -3.572086D 1 7.2946900 1 5.197097t*1 4.1322671 2 stAseG 0.0 S.302 %0t+2 1.446060D 1 5.516570D 1 5.119060D1 2.438813t*l 3.095033D2 96 JA 5.$ toltet.1 5.119060D 1
% S.302S60t 2 1.4460605 1 6.430296D 1 3.602644t 2 ELAmG J5 100.0 5.119060E*1
- JA 0.0 8.302560t 2 6.90634?t 2 1.76T296D t 5.L417t3D1 1.236455t 2 91 4.906342t 2 1.767296t
- 1 5.119060t*1 8.302460D2 5.236455t 2 stA#eG Ja 100.0 9.33777;t 2 2,411574t 2 4.7M64M 1 7.7510J0D1 5.029484t*0 98 JA 0.0 .75589pt 7.751030D1 a .988716D O 3.9668501 3 i _
9.337770t 2 2.411574t 2 5.958716D O 3.956850D 3 stamG ( C JS 100.0 2,411574I 2 5.661363D I T.51030t*1 49 JA C.0 9.337770t 2 7.751030 D 1 1.19559M*2 4.4390860 2 9.3377701 2 2.4115 7.D 2 5.e41363t*1 JB 100.0 2.988J40t*1 4.5%302D1 4.11TTT21 2 StAMG e 0.0 8.302540D 2 1.1555CD 1 l .06604 7t *1 4.498242t*1 S.644109D 2 h 100 JA JS 100.0 8.302560D 2 1.1M550D 1 1.066047D 1 2.933040D 1 1.15550D1 1.191366D 2 2.938040t*1 4.498.242t e t 8.M 4109D 2 atAmG 101 JA 0.0 8.302860D 2 1.191366 D 2 2.98sc4U+1 5 ?%37D0 1.255869D 1 5.302860t 2 1.1 55500 1 ' s 71*0 1.255569D 1 atAMG 45 100.0 (/ - JA 0.0 S.30256M.T 1.155508 1 1.25240M
- 2 2.980040D 1
- 4. 53D 1 2.137532t 1 102 J6 100.0 8.30286ct 2 f.15550t t 1.222409t*2 2.968040D1 6.w sDI 1.313642O 3 8tAmG 0.30286ct 2 t *305440 3 6.48tMIDI 2.983040D 1 1.819441D1 2.381550D 3 113 JA 0.0 1.330%403 6.44t?9tt*1 2.948040D 1 3.096033t 2 atAmG 48 100,0 8.302860t.2 2.438813D 1
;_ 1.446060t t 6.to2995D I 5.119060D 1 7.913413t 2 4 114 JA 0.0 9.302S60t 2 5.119060D 1 3.865351t*0 8.302860t.2 1,446060t 1 - 6.162995D s 7.913413D 2 BussG
~
Ja 100.0 1.7080618 2 5.119060D 1 3.865351t*0 115 JA 0.0 8.302860D 2 1.44060t i 1.274325D 1 O 8.302860D 2 1.4460600 1 1.703061D2 5.119060D1 5.318337tet 1.274325D 1 4tAseG 1.792talt*2 5.119060D1 5.318387t*1
'~
Ja 100.0 8.302860t 2 e.446060D 1 4
" 116 JA 0.0 1.4460CD t 1.M21818 2 5.119060D 1 1.87595D2 2.35487DD I 48 100.0 8.302860D 2 1,078609D 2 7.711274t 4 etAmG L 8.302860D 2 4.906342D 2 l.8a7723! 1 5.119060D1 3.602644t 2 12T JA 0.0 4.906342t 2 5.50T72501 5.119060 D 1 6.430298D1 J5 100.0 t.30286M 2 S.449105D1 4.935000t.) stAMG 5.132N001 -3,8909 GD I 4.382396D1 1.0514G0D1 8.84T373t*0 3.330267t*1 12$ J4 0.0 h
4 JS 100.0 5.832090D 1 3,890949D1 4.392396DI 1.405695D1 l.05t490D 1 1.0514900 1 B.84T373D 0 3.33026TE 1 stAMG 5.83209M 1 3.890949D1 1.159853D 0
- 129 JA 0.0 3.890949D 1 !.405695t*1 +1.051490D1 *2.102364D 1 5.&320900 1 4,
[W JS 100.0 18tle : Peop 3 16*n16* 7
% ? ,0utput Set 1 OtAD LOAD 10L3 la itenue
Q,F set A*f
- h. -',Nt L " Set MAX /mlu $6ssary table
^ leen EM A Aalst f orce mintam 1 80 71
% 11309 243.136 '
!V mealam 1 M
ulniam 1 80 0.65087 8een truf A sheer 2 f acce men tam 1 71 0.44546 ' ( , Minimm 1 89 267.281 m a V teen EM A theer3 Force mealam 1 116 179.218 7 u @?if R,
- ninfase 1 75 19.8294 '
An . . Seem (M A fortpe 98 TT.1103 *ZJ maaina 1
- A 1-Y - minimm I 90 691.701 W' M
$ F M' ? Seen EM A momemt mea f am 1 65 116.433 RW M
*F ,
Minima 1 67 -2.53925
'9.6686
*- W
- seem EM A moment 3 mes tam 1 74 243.136 N
4 <* Minleum 1 71 - g6
%9AM i teen EM S AAlet f orce maalam 1 60 0.11309 JM4
' "g "Wg-ulnimm 1 71 0.44546 -
bJ: 5 o . Some EM e thear2 f orce
~" maalam 1 80 0.65087 179.218 MIntius t 116 .J
! Sese trut 8 Sheer) Force 267.28T maalam Nintam 1
1 89 98 TT.5 t03 fQ 4
. Seas truf a fortwo menima N 19.8294 A W,sp minimm 1
1 116 18T.596 dv , 7m% %. u t I[ [, *, -E- Seem trui 5 maamt2 sv 3 hl hgh J N}} + [ "[& 'jy m u
?
%_Q&%_y a Q ,Ly
,,h0h ~lhk .
gP , . ATTACHMENEi@ SHEET 4 OF N
- tc0 00mvAc sv$1t= 4316 6 s 1 DC.6 D3
% , i4 12:49:30 i996 stA = e m on 4.&i geport 3 ((ement model 1-Format $1Aactat ter/Sean Eleavet 3
s f fille s P90P 3 16 116* i< _i _ V' - htsut let 1
- CLA0 LOAD (St1 $s,
~
resisue 1 39 697.701 h* o team ind 4 acaent3 m1M aus 1 74 19.8294 - " ~
" me n t eum 1 67 1.96312 # title : Pe0P 3 16*t16+
b Dutsut let 2
- 048 @,_
", etAu (Ltataf L0A0$ ,-_:--
;n etheleG StielmG AstAt intAt thtaa 104$10m
{p{- f HAM P v2 v3 at m2 m3 1.250959(4 6.60402M
- 0 5.085057t*0 1.34978M*0 6.027569t.1 stAmc
# 61 JA 0.0 3.0304308 4 1.115318t+2 3.030433*2 1.2509501 4 6.604920E.0 5.085040t+0 1.6713815 1 Ja 100.0 1.030564t 2 StAJeg 4.7060 0t*2 4.6762tSt*1 2.452649t*0 6.g588M*0 1.19561&t 1 0 62 J4 0.0 6.g5 EsM + 0 1.481048t+2 4.T06*4M*2 4.676215t*1 2.452291 0 1.072389t*1 Ja 100.0 1.085061t*0 3.115338( 4 stAmG g4 1. 6713 7M
- 1 63 JA 3.0 1.60736M
- 2 3.201578td 2.21034M
- 1 2.280372td Je 100,0 3.201575t
- 2 2.210366t*1 1.67135M +1 1.5022334 1
' 1.407360f 4 2.280372t *2 ltAnc g 1.42818M*2 3.222969(4 2.438754t*1 1.67137M
- 1 1.502233t*1 JA 0.0 2.968775t *2 1.&231$0t*2 3.222969t*2 2.438754t*1 1.67138M *1 2.97716M *1
*
- JS 100.0 2.97716M+ 1 2.968775t*2 atAMG
. 65 JA 0.0 1. 7064 Mid 4,183360td 2.85532M*1 1.67137H +1 4.18336M 4 2.855320t+1 1. 67138M
- 1 4.532008t*0 3.10713M +2 Ja 100.0 1.7064001 4 2.486303t*1 1.671375t+1 4.53200SE*0 3.10111M 4 StAMG So JA 3.0 1. 7565 0M
- 2 4.15 2111 t
- 2 4.15211114 2.484303t*1 1.6713SM*1 3.102537t*1 7.330!67t 4 Ja 100.0 1.7565Mf +2 7.535945t+2 stAnc '
2.2658Nt*2 9.3779e31 1 1.3392561+1 2.626131t+1 2.6549791 1 67 JA 0.2 6.+1500tt+1 6.338523t*2 Ja 100.0 2.265890t*2 9.3779434 1 1.389256t+1 2.626130t+1 9.4508331 1 1.509921t+1 2.626131t*1 4..A 001t*1 6.338523t+2 stAac P 68 JA 0.0 2.33849Cl*2 5.746889E*1 5.19265M*2 Ja 100.0 2.3354GCt*2 9.6508338 1 1.509921t*1 2.626130t*1 IJ 9.4484448*1 1.307125t*1 2.626131t*1 5.7&&83M
- 1 5.19265M*2 stAmc 69 JA 0.0 2.41190M 4 7.70769M +1 4.142927t + 2 f^ Ja 100.0 2.41190Cf 4 9.448444t*1 1.5071M t*1 2.626130t+1 9.405681t*1 2.120149t*1 2.626131t + 1 7.707695t+1 4.142927t+2 atAnc 70 JA 0.0 2 A494201 2 2 ,26130t+1 9.044899t*1 3.618a5M 4 JS 100.0 2.46M23 4 9.401681t*1 2.120349t+1
- p. 1.2350708 4 2.850971t*2 5.64230M +1 5.1243084 13 5.6470ME 13 3.061645t*12 stAMG i 71 JA 4.0 2.921155t*1 1.425485E 4 d JB 100.0 1.23507M 4 2. 850971 E
- 2 5.8423091 1 1.12431M .13 2.61910M +2 5.523230t 1 1.080232t*12 2.921155t+1 1.425485t4 stAmG
'4 72 JA 0.0 1.1801108 4 f.011677E*3 2.81910M 4 5.523230t*1 1.080230t
- 12 1.991884t+2
*: 48 100.0 1.1803108 4 6.492465t+1 8.195870E+1 2.385819t*2 1.564333t+2 2.8814591 4 stAmG
'3 JA 0.0 9.001790t+1 k'
^
JS 100.0 9.001790t*1 6.492465t+1 a.195870t*1 2.355820td 1.962119t*1 1.82813M*2 1.8281164+2 SumG 3.4094T3t*1 9.030214t+1 2.335819t*2 7.982119t+1
'" T& JA 0.0 8.840160t*) 9.503740t*1 9.03021&t t 2.385820t 4 1.277 tom 4 E Ja 100.0 8.849160t*1 S . 4094 T3 t e l 9.3 % CE*1 9.117254t+1 8.840100t*1 9.503741t+1 1.277166( 4 2.38561M
- 2 StAMG 75 JA 0.0 1.96179M4 9.3 % 0t+1 9.117254t*1 6.84010M +1 9.50374M +1 2.963536t +1 JB 100.0 2.96353M +1 1.961796E 4 stues 76 JA 0.0 1.022980t*2 1.052T71t *2 8.919983t*1 9.503741t*1 M -
9.503740t+1 2.992M5t+1 1.9031421 4 M Ja 100.0 17 JA 0.0 1.022980t 4 1.052T7184 8.919983t
- 1 1.22243Ct d 9.066749t*1 1.836709t+1 9.503741t + l 2.9922558 1 1.903142t+2 MAms l~ 1.836709t*1 9.5037&M +1 1.585913t+1 2.053438t*2 Ja 100.0 1.222430t 4 9.066740t+1 7 78 44 0.0 1.277400t+2 9.524842t*1 1.544490t+1 9.503741t+1 1.585913E+1 2.053438( 4 stAms 1.544490(*) 9.503740t + 1 2.407081t+1 3.038&O9t + 2
,7 ~ 48 100.0 1.277400t
- 2 9.5248421 1
- 9. 99537M *1 1.31605M *) 9.503741t+1 2.407081t+1 3.038409t4 StAmt 79 JA 0.0 1.41485M*2 3.98376M
- 2
@^ 1.484850t*2 9.99537M*1 1.316058t+1 9.503740t + 1 2.97431M + 1 t Ja 100.0 9.503740t*1 3.95376M
- 2 SEAmG 0.0 9.998640t*1 1.661554t d 1.498362E+1 2.974317t + 1 30 JA 8.25318tt*1 3.513827t *2 Ja 100.0 9.99864M + 1 1.4615 Sat
- 2 1.496542t+1 2.974324 1 2.974317t.1 8.255111t 1 3.513827t*2 SEAMG 41 JA 0.0 1.000310( 4 1.532215t 4 2.4140921 1 t.
1.532215t*2 2.616092t*1 2.97432M*1 7.713160t+1 3.890 4 8t+2 Ja 100.0 1.00031M
- 2 7.713160t+1 3.890648t+2 StAmc
@p , 82 JA 0.0 5.319080(4 1.329731t *2 3.&O1641t+1 2.974317t*1 2.974320t
- 1 5.910100t+1 3.009894t*2
*M Ja 100.0 5.31908M*2 1.329731t 2 3 &01641t*1 3.039994t+2 atAMG; 1.306864t*2 2.598567t*1 2.974317t
- 1 5.910100t 1 P 83 JA 0.0 JS 100.0
- 5. 311590t
- 2 5.311590t*2 1.306864t+2 2.598567t+1 2.974320t*1 4.5491223+1 2.614038t+2 i 1.180071t + 1 1.482878t+1 2.817654E 1 1.3091'4b 2 BEAmG 84 JA 0.0 3.191300t*2 4.342993t+1 1.6096530 1 6.047247t+1
,"' JS 100.0 3.191300( 4 4.342993t*1 1.180071t*1 1.482f +M+ 1 1.609653t 1 6.0&T247t + 1 StamG
( '. , 85 JA 0.0 3.173020E *2 4.444817t*1 9.3914048 0 1.48257tt +1 9.3914044 0 1.4825300 1 1.215294t*1 2.1M418t+1 .-
"A" Ja 100.0 3.173520b2 4.4448171 1 ,w
' 86 JA 0.0 1.655750D 2 2.12371861 6.190431b 1 1.&82878bt - 4.368994t+0' 4.266301b 0 stAMG 3.102499t+1
~
1.655750t4 2.123718D1 6.190431t+1 1.4828800 1 8.60080161 3.102499D 1 atAnc . G: Ja 100.0 8.600801t+t 1,6159905 4 6.&23320t+1 1.682878 6 1'
%A 87 JA 0.0 JS 100.0 2.086502t+1 1.615990D 2 2.086502E 1 6.423320D 1 1.482850b 1 1.979811D2 6.M8110t + 1 BN ' 8.640717t+1 2.905591 6 12 2.752236t+2 1.267357t+2 timeG 's
- 1. . 88 J4 0.0 5.02092001 7.397476t *1 1.421062t+2 b l;
^ Je 100.0 5.020920tel 1.397476t*1 8.640717t+1 2.905590 0 12 3.352293b2 O . ,a Ah:k p ,
4e, ~ .
+ sfh, l &' '"
WOkh -
_ n. ATTACHMENY Y , $h I
- OECO CCnvAt 191114 4316*6 & 7 SHEET T op 41 Oc.-57D .
thy Apr 18 12t&9114 1996 6 y St&BRAP Vertien 4.41 Report : Element M- Model 3
. 4
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,formet STAA0fut ter/ team itement M '
/ i O." *
.18tte : P90P 3 16*E16* d G, 4$c/
- N MM* L tutsut Set 2
- Ost StAm 1tIat#I e0 ADS i
+ }h*. ', ; r
- Sut at thtAt foestou t%lhG Stu0 gag AntAL st3 h ^g G v2 v3 mi m2 t&; - StAM P 1.421M2t+2 BEAMG
' 0.0 4.3448%t*1 7.609602t*1 9.242253t+1 8.761757t*13 3.352293t+2 1.434942t+2 7% 89 JA 9.242253t+1 8.76176M *13 3.389864t+2 4.34480ct *1 7.609602t*1 JS 100.0 0.0 2.698000t+1 2,711921t*1 6.518958t+1 3.06590t*14 3.389884t+2 1.436942t*2 atAMC ' 90 JA 6.518958t +1 3.06M904 16 1.81930M
- 2 7.897279t +1 MAMG JS 100.0 2.698000E+1 2.71592tt*t 1.819306t+2 7.8972Mt +1 2.010180t*1 2.'95099 1 1.576952t +1 4.05CSul 14 91 JA 0.0 4.0508?ct 14 4.429689t*1 2.026945t*1 2.010150tal 2.375094*1 5.576952t +1 JS 100.0 4.489689t+1 2.026945t*1 MAMG 0.0 8.433610t
- 0 1.237415t*1 2.7&2912t+1 5.1684TTL 14 y 92 JA 1.23?&15t+1 2.742982t *1 5,188480t 14 1.476195t*0 6.823556t 1
~
JS 100.0 8.438610t*0 1.476195t+0 6.82355M 1 taAMG 0.0 7.747810t 1 1.258958t+0 2.T23607t+0 8.032943t*14 - i
% 93 JA 2.723607t*O 8,0329&M 14 1.837587?I2 1.2486064 12 JS 100.0 7,76787 ( 1 1.258958t+0 3.027864t+1 1.74681M
- 2 StAMG I 94 JA 0.0 2.273960t
- 2 S.0147371+1 1.13 t elm + 1 2.277363t +1 2.168977t+1 5.359649t+1
$.014T371* 1.13161M +1 2.2773608 1 h Je 100.0 2.273960t*2 2.1689TTt*1 5.359649t+1 SOMG 7.502123 fat t.349790D 1 2.277363t*1 95 JA 0.0 2.221520t*2 1. 79600M
- 1 1.47557M*2 2.22152;t*2 7.502123E.1 1.349790 0 1 2.277360t +1 1.45570D 2 5tAMG
=5 JS 100.0 2.6059448 1 1.2T3195D 1
- 96 JA 0.0 2.01685Cl*2 1.1334&aD 2 f .69146M *1 9.689453t+0 9.M 9893D 1 2.60595CD 1 JS 100.0 2.016850D 2 ' .13348-D 2 f .691460( *1 2.6059648 1 3.36668CD 1 4.201351D1 stAMG 9.122&T0D1 6.2 T7952D 1 t.354512t+1 Of JA 0.0 1.354512t*1 2.605950D1 3.695907t+1 6.1934T3D1
". Je 100.0 9.122470t*1 6.277952D 1 1.289677t + 1 4.449791t *1 8.062724t+0 6.193473D1 MAMG
- 98 JA 0.0 1.101 AICD 2 2.836919D 1 4.449790D 1 3.385105t*1 3.004393D1 1.10161Cl*2 2.136919D1 1.2896TT!*1 48 +00.0 3.004393t+1 MAMG h 99 JA 0.0 1.177550D 2 3.663949D 1 1.82339M+1 1.823396D 1 4.449791D1 3.385105t*1 4.449790 0 1 ' 489949D 1 7.651791D1 JS 100.0 1.177150D2 1.64394Gt*1 3.69299CD 0 l a328781*1 1.215294D 1 2.1M61SD 1 StANG 0.0 3.159610D 2 .5056221 1 3.369874t+1 i 100 JA 3.15961;D2 4.505622D 1 9.69299CD0 1.482S80D 1 1.249722D I
, r JB 100.0 1.482578D 1 1.249722t*1 3.369874t+1 stAMG 3.054760D2 5.4C2987D I 3.02955M *1 9.430302t+0 4,693546D1 101 JA 0.0 0- 3.054760 0 2 5.402957D1 3.02955H+1 1.482&s0D1
$ Je 100.0 5.491312D 1 3.221936D 1 1.432378D1 9.439302D0 4.69354M+1 SOMG
'l IC2 JA 0.0 3.04631CD2 t.482330D 1 2.734230t*1 8.419445 D 1 5.498312D1 3.22193M + t JS 100.0 3.04431CD 2 1.&S2878D 1 4.495102D 1 1.704767t+1 SOMG
'j- 0.0 1.729sacD 2 2.475047D I 5.828649D1 4.266301t+0 113 JA 5.828649t+1 1.&82180D1 4.3M994t*0 Jt 100.0 1.72964CD2 2.4750471*1 9.689453t*0 9.M9893t+1 SOMG d- 116 JA 0.0 2.00240002 1.137397t
- 2 f.816841tet 2. 605964 +1 1.12591M
- 1 6.M 2515t + 1 j 1.13739 7t
- 2 f.816841D1 2.605950D I JS 140.0 2.002400D 2 1.125916D 1 6.752%15D1 SEAMG 1.21441tD 2 4,260479D1 2.605644t*1 7 115 JA 0.0 1.755650D2 1.957237t+1 5.151390D1 Ja 100.0 1.755650t*2 1.214411 0 2 4.240479D 1 2.60595M *1 T 1.957237t+1 5.151390D1 MAMG N? - 116 JA 0.0 1.T3646002 1.220893D 2 4.434335U1 2.605944D1 5.054826t+1 1.070790D 2 D JB 100.0 1.736460D 2 1.220893D2 4.434335D1 2.60595CD) 3.291898t+1 1.919258D 1 SUMG 6.502392t*1 1.694093 D 1 2.605944t*1 127 JA 0.0 8.20347M+1 g
y 48 100.0 8.20347CD 1 s.502892D 1 1.394093t+1 2.605950D1 3.366680D 1 4.20135 tD 1 1.950506D 2 8 &S8141D1 9.191974t+1 3.62&898D 2 SEANG JA- 0.0 2.M531CD2 9.339417t*1 S 128 t.950506D 2 8,88814M *1 3.242550D 2 2.310967D2 "J # J8 14J.0 2.8453tCD2 9.33941TD1 8.888141D1 3.242550D 2 2.310967P 2 stAMG m 0.0 3.040780D 2 1.043614D2 1.929514(+2 X 2.38581M* 2 b 129 JA JS 100.0 3.040780D2 1. 043614 t
- 2 1.929514*2 8.83814C01 7.342149D 2 U
Title : Peor 3 16's16*
- Output let 2 DM value
_O hh . Set MAX / Min Summary table let 10 *9 minisus 2 93 0.77679 P Ni. ' Seem tid A Aalet f orce 82 531.908 h? O Y, Seem Erd A Sheer 2 Force maa tous Minious mea tsue 2 2 2 93 65 1.25896 418.336 i v. Dys Seem trd A theer) Force m woue 2 62 128 2.45269 195.051 4 maniaun 2 + sg C; 90 3.06759t*1&;
"I' team trd A fortpe minisue 2 b *4 ;;
' mesisue 2 73 ? 238.582 ,
T1 5.64707t 13 . j p','* Seem trd A sument2 minisue 2 meslaus 2 90 338.988 .I M minteus 2 71 3.06165D12 " ' " *
.~
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 paaleum 2 62 531.908 0"N '
93 1.25496 7 Sean Erd a sheer 2 Force ulnimm 2 jQ mealsus 2 65 418.336
- [p g 4 ;
1 %*6x 9
%k 74 Q$9,Jf ynsv _ I
N ggp r ATTACHMENT V " 9ms ttC0 C: vat 5151tn 4316 6 61 SH W 0 -OF N
~
thw Apr 18 12:49:18 1994 DC.-3 M h $1ARAM Vet alon 4.41 aecort a fleasnt a- , ( Model t g_ v_ _ , f ormat t $fM0 tut $sr/ teem Element P90P 3 16 116" ' [* ' Iltle tuttnat Set 2
- 088 62 2.45269
. minious 2 -O e tems tras S Shear 3 f orce 128 195.051 mesisue 2 C minisus 2 90 3.06T59t*14 Y ~ . Seen Ersi e fortpe 73 238.582 maa taue 2 W 'V minisue 2 93 1.83759 0 12 Q'q. *
. team End 8 Momenti nos tous 2 129 T34.215
.g .Q
;i Seen ind 8 mmment3 minteue 2 93 1.24461D 12 1011.68
% WM c 4' maa true T2 #
title : PacP 3 16*116 Outpat let &
- 551
{p_ 8taa t41 min 1 L0a0$ 10A 510ei stM0thG StuoluG A lA4 sutAt IntAA M3 kI P V2 V3 M7 M2 1.117401t+1 9.534323t *1 htAMG fb atAM 0.0 4.784180D 2 1.92tt9sD2 0.595883t + 0 8.15196800 4.69241M
- 2 FI' '
61 JA Je 100.0 4.7&4183 2 1.921896D2 8.595883D 01.011323t*1 0.151970D 01.946162D 2.5971MD1 1 1.656822t+2 StAMG 62 JA- 0.0 7.12 7D M *2 ?.7N8101 3.560317D0 1.836786t
- 1 2.55026tt+2 7.79ta tt*1 3.560317t+0 1.011320D 1 at 100.0 7.12 TMCD 2 2.597159D 1 8.151974t+0 4.69241M*2 ttAMG 63 JA 0.0 2.133570D2 5.063$ 1D I 2.03t52$t+1 1.659916D I 3.49080M .2 J3 2.597160D 1 Nf" JS 100.0 2.13357M
- 2 5.06354802 2.031525 D 1 2.597159t*1 1.65991M
- 1 3.490806D2 atAMG 2.168760t*2 5.09560?p 2 2.222553t+1 4.760603D 2
# ' 64 JA 0.0 2.591160D 1 2.944760D 1 d- Je 100.0 2.168760D2 5 .0WO ?t
- 2 2.222553 9 1 2.597159t+1 2.944760D 1 4.760603t+2 StheG
' 65 JA 0.0 2.640060t*2 6.387T44D 2 3.056911tel 7.270539t*0 4.644605D 2 JS 100.0 2.640060D 2 6.38T7+4D 2 3.056911Dt 2.591160D1 7.270539t+0 4.644605t+2 stAMG r 2.591159D1
*. 66 JA 0.0 2.724780D 2 6.33456302 2.7935032+t 3.745391t+1 1.109039D 3 Ja 100.0 2.7247801 2 6.334543D2 2. M3503 D t 2.597160D1 4.290548 1 3.177159D 1 1.1315371 3 stAMG 3.5C97002 1.49+ 7s5D 2 2.221&37t+1 9.505003t+2 W- 67 JA A.0 1.494765D2 2.221837t+1 4.290760t+1 6.062682D 1 3.567770D 2 9.505003t*2 atAMC rife 7
- 68 JA Je 100.0 0.0 3.69049002 -1.491495t+2- 2.264259t+1 - 4.290754t+1 3.69049CD2 1.491495D 2 2.264259t+1 '4.290760t+1 6.0626821*l 9.10T238t+1 7.832209D 2 - t" 7.832209t*2 SEAJeG '
?WJ O- J8 100.0 4.290754t*1 9.107238D 1 69 JA 0.0 3.61419CO2 1.468273D2 2.413789DI 4.290760D 1 1.232226D 2 6.3M52902 T' Je 100.0 3.61414Ct*2 1.44927tD 2 2.413789 D 1 4.290754D1 1.232226D 2 6.3795290 2 StAMG V 70 JA 0.0 3.910960D 2 1.443334t* 2 2.604935 t + 1 1.423407D2 5.692247t+2 1.441334D 2 1.604935t*1 4.290760DI Ja 100.0 3.9109600 2 1.13998;D 2 4.576129D 2 1,018979D 2 8.2749071 13 9.416251t*13 4.8008190 2.288064b 2 12 SEAMG 71 JA 0.0 5.059897t+1 JS 100.0 1.819980E
- 2 4.576121D2 1.011979D 2 8.274910D 13 2.288064E+2 StAMG 72 JA 0.0 1.81201CD 2 4.5110MD2 9.52895M
- 1 1.624978D12 5.059897t+1 1.623248D3 JB 100.0 1.81201CD2 4.52300*D 2 9.5239166 13.84332 1.624980D 12 3.43903tD2 M
- 2 2.657849D 2 4.680513t+2 SEAMG T3 JA 0.0 1.403750D2 1.059473D2 't.302581D2 1.355844t+2 2.944992t+2 i Je 100.0 1.403750 0 2 1.C89* T3D 2 1.30258tD 2 3.843330D 2 1.355844 D 2 2.944992E+2 SEAMG 3.843326t+2 74 JA 0.0 1.39698CD2 1.391475D2 1.487306D2 1.537418D 2 1.196950t*2 1.391475 t + 2 1.48730M + 2 3.84333cD2 2.012528D 2 3.843321t+2 st#e4 N[ '
- Jt 100.0 1.39666M+2 1.5374189 2 2.012528D 2 1.5554500 2 1.503058t + 2 3.10752M*2 75 JA 0.0 4.8235i9t+1 N: Ja 100.0 1.555450D 2 1.50305402 1.396666D 2 1.537410D2 1.537418D 2 4.823529t+1 - 3.10752M*2 StAMG 1.740850t*2 t .724476D2 1.402118t*2 X n' 76 JA 0.0 1.402118t+2 1.537410D 2 4.905502D 1 2.992850D2 JS 100.0 1.740850t*2 1.T24476D2
,d/ 2.143730D 2 1,483142t*2 2.473209D1 1.537418D 2 4.905502t*1 - 2.992850D 2 St#eG '
3.241143t*2 77 J4 0.0 1.531410D 2 2.502026D 1 l' JS 100.0 2.143730D 2 1.488142O 2 2.473209D 1 3.241143D 2 LtAMG 4 1.560734D2 2.260606D I 1.537418D 2 2.502026D1 78 JA 0.0 2.2522901 2 1.537410D2 2.51?O7M+1 4.881094D 2 0, 2.25229CD 2 1.5607321 2 2.260606D I 4.881094D 2 St#eG Je 100.0 1.537418D 2 2.517076D1 D 79 JA 0.0 2.52059X*2 1.631445C+2 2.010574D1 4.086TT8t*1 6.438180t*2 JE 2.520590D 2 1.637445t*2 2.010574 D 1 1.537410D 2 6.438180D 2 SE#eG y
<=
J8 100.0 So JA a.0 1.638010D 2 2.610915D 2 2.049790t+1 4.086782t+1 4.086 Mot +1 1.537418t+2 1.329435t 2 5.685760t+2 J8 100.0 1.638010D2 2.610951D2 2.049790t+1 4.086782D1 1.329415t 2 5.685760D2 SEAMG w 0.0 1.638760t*2 2,745495D2 2.591860D1 6.582749t+2 31 JA 4.036790D 1 1.164721D2 1.638760D 2 2.743495t+2 2.591840t*1 6.582749E*2 BEAaeG Je 100.0 1.164721t+2 82 JA 0.0 1.009770t*3 2.381678t*2 3.59t T43t+ 1 4.0867821 1 9.444381D1 5.091635D2 1.009770 0 3 2.341478D 2 ,3.591743D 1 4.08679Ct+1 Y ' JS 100.0 1.008350D 3 2.342956D2 3.046613D 1 4.08679CD 1 4.086782D i 9.444381t+1 5.091635t+2 stAMG 4.58141M+2 2 83 JA 0.0 3.046613t*t 7.029585t+1
' ' ~ Ja 100.0 1.008350D 3 2.342956D2 1.652638D1 4.170111t+1 2.210T33t+2 SEAMG '
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E- giae iLtn(4i L0A0$ 5tu0 lug 8tuolhG t (; anlat Sat aa tutAt 1045104 v3 mi m2 K3 SEAM P V2 Ja 100.0 8.3025604 2 2.13191 4 2 2.60879tf*1 1.119060(*1 S.373246t*1 -8.0207082 2 1.248705t*1 5.119060t*1 S.3732461 1 8.020708t 2 atAsoc U 122 JA 0.0 8.302860E'2 2.13191 4 2 2.1319191 2 1.24870$t*1 1.119060t*1 7.12454't*1 5.88878/4 2 I J8 100.0 S.302860t 2 2.'3191H 2 2. 25640M
- 0 5.119 N t.1 7.124541t*1 5.8887E51 2 atAMC y 123 2A 0.0 S. 3:2M01 2 Ja 100.0 8.3023601 2 2.13151PI-2 2. 25640M *0 5.119 E t*1 7.0102214 1 -4.822829t 2
'. 2.t319 ut 2 2.513925t*0 1.119 N t*1 7.010221E*1 4.822829t 2 BEAmd 124 .i A 0.0 S.302S%'t 2 i at 100.0 8.302560E 2 2.13191;t 2 2.813925t*0 5.119060t 1 -7.080569t*1 4.289649t 2 2.13191M 2 1.552143t*2 5.11906M *1 7.08056M *1 4.28964M 2 st w 125 'A 0.0 8.302360t 2 Ja 100.0 8.302 Social 2.1319ut 2 -3.552143t*2 5.119 N tat -1.5960931 2 3.7568691 2 5.119060t*1 1.596c93t
- 2 3.7568691 2 'at AMC 4 126 JA 0.0 8.302560E 2 *. M65*2t 2 0.899777t
- 1
*.906342t 2 L S997T71 1 5.11M60t*1 1.078609t*2 7.711274E 4 JB 100.0 9.302560t 2 f.. s title . Pt0P 2 17.5* DI Antite Y cutsut let 1
- Ot AD LCAD (Ctl mat /mit 5 rnary foote $tt 10 d*Lwe 2 let
- Seem trw$ 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
Been trul A %Acer2 f orce m iriina 1 60 0.50199 h 50 0.71964 a; maninus 1 I I' lean Erd A Sheer) f orce minina 1 til 278.395 I ' me n ina 1 125 355.214 Is team Erd t 'ornse m inium 1 53 -12.9894 E $1.1906 S_ I me nina 1 117 Y Y,5 M Seen Erts A Namnt2 . Minium 1 104 *125.044 d meninn 1 '118'" " 234.252 - , A '- 1~{. minina 58 0.42M3 i- ** Beam trd a navnc3 1 48 0.37655
; manian 1 Sean E rd 8 A s t e t f or c e minina 1 53 0.64587
'I men ina 1 103 0.083029 8eam fed t thear2 force mini an 1 50 0.21964 t masina 1 60 0.50199 teen Erd a sheer) f orce minina 1 125 355.214 i ,
ma sina 111 278.345 h mintam 1 117 51.104 A Seam Erd B f or@e 1 ' 9, man ina 1 53 12.9894 1-g ;N 8een tre a manent2 minina 1 117 103 234.282 125.0 4 y ma n ina 1 60 0.66009 1 gs seem Erd 8 m e ts min nm 1 m an ina 1 57 0.42S43 q_ 7_ 1 ** fitte : PeoP 2 17.5" OI Amitta (. A%5** QJtput48et.1ACSt%%,,,,_., 8 TAN ,ti,t',Mt4i t0A0$ 4*. 3 g antat satAa sataa Ica$1cm stuotu; stuoluc [ Mt m2 K3 y( SEAM P W2 V3 3.679138t*0 2.041113t*2 SEAJeG I Q- 45 JA 0.0 1.714950t*2 1.8758062 2 2.221213t*1 1.085057t = 0 7;n Je 100.0 1.714950t*2 1.875806t*2 2.2212t3t*1 5.085060(*0 1.0444721*1 2.T79907t*2 2.779907t*2 stAMC f 46 JA 0.0 1.742080t*2 2.325022 1 1.521701t*1 5.085C57t*0 1.044472t*1
=
e JS 100.0 1. 742080t
- 2 2. 32502M
- 1 3.521701t *1 5.085060t*0 2.254518t*1 2.917240t*2 0.0 1.994610t*2 1.125535t*1 5.0850571 0 2.254518t*l 2.91720X
- 2 stAMG (6
47 JA J8 100.0 1.99461CE*2
- 5. 662674t
- 1 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 w
* .;B 100.0 2.112740t*2 2.7319251 1 4.7926564*0 5.08506M*0 1.2464T7t*1 3.001225t*2 f 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 5.085060t*0 1.296489t*1 2.822380t+2 *
( ,1 JS 100.0 2.144850t*2 2.1549 75 t
- 1 7.711105t 1 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 2.650189t*2 stAMG -
53 JA Q.0 3.590470t
- 2 4.655760t*1 1.7730381 1 6.645830t*0 1.135128t*1 4 42
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tutAt tutAt 104510N SIM0luo ulat M2 "3 P V2 V3 MI i StAm 1.760265t 1 2.81138M+2 C 3.590470t
- 2 4.655760t*l 1.TT30381+1 6.6458 W +0 J8 100.0 6.M5880E*0 1.760265t+1 2.81138M
- 2 SEAMG
$6 JA 0.0 3.663250t*2 2.447496t*1 3.57300&t 1 3.573004t*1 6.M5880t +0 f. 757675t e l 2.920139t*2 JS 100.0 3.663250s 2 2.a&T&86t*1 J
1.7760951 1 6.645880t+0 1.75765t+1 2.920139t+2 BEAMG 15 sa 0.0 3.9 tit &M*2 a.094056t+1
- 1. 776099t + 1 6.M5880t
- 0 6.879418t
- 0 3.172690t+2 48 100.0 3.911160t*2 6.09&O%E 1 i
6.784382t*0 6.9 5880t*0 6.8794 tat *0 3.172690t 2 SEANG 56 JA 0.0 4.0073 Mt *2 3.15729M
- 1
&,7843821*0 6.64558M +0 9.71668M +0 2.921534E+2 43 100.0 6.C07390t*2 3.157290t *1 2.559678t*0 6.645880t+0 9.716686t*0 2.921534t*2 stAMG 57 JA O.0 4.0J2850t+2 3.2022341 1 2.684345t+2
-- -Jg 100.0 -- 4.032850t*2 3.202234t+ L,2.559678t*0 . 6.6&S850t*0 1.116391t+1 9.45%29te t 1.89462M+1 ' ' 6.645880t*0 1.11639tt+1 - 2.684345E+2 ?tCAMG v-W-.
58 JA 0.0 4.137MM
- 2 6.645880t+0 7 4537tM+1 1.964339t*2 Ja 100.0 4.13 766M
- 2 9.45%29t*1 1.894626t+1 4
3.455530tet 6.645880t+0 2.451710t*1 1.964339t+2 stAMC ! 59 JA 0.0 4.505750t
- 2 8.5577:41 1 6,M588ct
- 0 1.6493501 1 1.231912t+2 J8 100.0 4.505 750t
- 2 8. 55 770&t
- 1 1.455530t*1
*.508787tel 6.047841t*0 6. M5880t
- 0 t .M9350E
- 1 1.2319121 2 6tAMG
< 60 4A 0.0 4.652220t*2 1.19561&E 1 1.03056&t 2 4.652220E*2 *.50875'l*1 6.047841E*0 6.4588CE*0
, Ja 100.0 2.734230t*1 8.419445E+1 BLAMG
'A 0.0 3.03MSM *2 5. 579829t
- 1 3.30&814t*1 1.4828781+1 103 0.757753t+1 3.037980t +2 1.5 M829t + 1 3.394814t*l 1 &82880t.1 3.540505t 1 Ja 100.0 9.757753t*1 atAMG 6.633847t*1 3.63196M +1 1.4828788 1 3.540505t*1 h' 104 JA 3.0 2. 941720f *2 1.809355t+1 6.527219t + 1 2.941720E*2 6.633847t*1 3.631968tel 1.482880t+1
, . Je 100.0 1.807355t*1 6.527219t+1 StAMG 2.93572M
- 2 6.585679t 1 3.517155t+1 1.&82578t + 1 L 105 JA 0.0 4.958602t*1 2.9357'0!*2 6.58H79tel 3.517155t+1 1.482880E+1 1.069717t+1
! E Ja 100.0 1.069717t+ 1 4.9586 N *1 SEAMG D M M W -'- 1064 JA , 0.0 -2.513390(+2 6.771515t+1 5.312523t+1 1.482878t*1 2.513390t*2 6.7715151 1: 5.312523f+1 i'1.482880t+1 " 1.882413t*1 ' 0 3.8%205:+1,. ~ : ;gg i - / 107 JA Ja 100.0 0.0 2.406070t
- 2 1, T78914 1 3.714211t+1 1.482878t+1 1.882413t+1 3.434205t+1 atAMG
~(- 3.714211t+1 1.482880t+1 3.012899t+1 2.654057t+1
- Je 100.0 2.4069 70t
- 2 1.T78916t*1 1.678068t ) 1.5042604 1 1.487878t+1 3.012899t+1 2.654057t+1 stAMG -
JA 0.0 2.389&30t*2 108 2.423538t+1 3.504260tet 1.482880t+1 6.341527E*1 c ( JS 100.0 2.38943M
- 2 1.678058t*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 Je 100.0 2.375510t*2 1.6256995 1 3.3587625*1 1.482880(*1 8.0022871 1 2.719024t+1 I 1 &S2878tet 8.0022871 1 2.719026t*1 ntANG x
110 JA 0.0 2.3M3 70t
- 2 ' . 60 7721t
- 1 3.290649t*1 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+1 112 JA 0.0 1. 745810t
- 2 2.592235t*1 5.770275tet 1.482878t+1 8.80162M +1 3.612529t+1 SEAMG O 1.&82880t+1 6.495102t 1 1.704767t +1 E st 100.0 1.745810t*2 2.592235t*1 5.770275tel 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 p 1.2246 8t*2 4.611601tel 2.605050tel 6.182025t*1 1.292645t+2 g J5 100.0 1.718860t*2 118 JA 0.0 1.519050t 2 8.486238t*1 5.410813t+1 2.60594&t+1 6.182025t+1 1.292645t+2 stAMG-4 2.60595M*1 3.513T39t+1 8.768885t+1 k 119 JA Je 100.0 0.0 1.519050t*2 8.6862381 1 5.410813t+1 1.506980t*2 8.4491231 1 5.294115t+1 2.605944t+1 3.513739t+1 8.768485t+1 B4AMG M 5.294155t*1 2.605950t*1 2.237926t*1 6.730190t 1
- 6. Jo 100.0 1.106080t*2 8.449125t*1 120 JA 0.0 6.895100t*1 8.621267t*1 3.78264M
- 1 2.60594&t+1 2.23792M+1 6.730190t+1 stAMG
! 2.605950t+1 2.801&55t +1 5.014649t+1 i, J8 100.0 6.895100t*1 8.6212671+1 3.782&4M +1 5.052470t') 3.034%2t+1 6.601162E+0 2.60594&t+1 2.801455t+1 5.014669t+1 REAMG
% 121 JA 0.0 h
tr 122 JA JB 100.0 0.0 Ja 100.0 1.052470t 1 3.034%2t + 1 6.601162t*0 2.605950t +1 4,785470tal 4.781470t*1 2.983023t*1 2.983025t*1 3.65169+t+0 3.65 %94 t +0 2.60594&t+1 2.605950t 1 2.2232664 1 1.979411t+1 3.533514t+1 2.22326M a l
- 533514t+1 stAMG 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 e 1.9754311 1 4.654506t+1- stAMG S, 124 JA 0.0 4.493560(*1 2.949911E*1 2.194869t*0 2.60594&t+1 J8 100.0 4.493560(+1 2.949911tel 2.196869t*0 2.605950t 1 2.001554t+1 5.245206t 1
@ 2.60594&t.t 2.001554t*1 5.2452064+1 stAMG f 125 JA 0.0 6.021590(*1 7.210919t** 8.5276634 1 6.164411t+1 ' JS 100.0 6.021590t*1 ?.210919t*1 8.521663t*1 2.605950t+1 3.980227t+1 Q- 6.164611t+1 stAMG 126 JA 0.0 7.95481f1 1 6.564910t+1 2.0944344 1- 2.605944t+1 3.980227t+1 . .
1.919258t +1 ?t' JS 100.0 7.9548101 1 6.564910t*1 2.094434t+1 2.605950t*1 3.291898t+1 c. title P40P 2 17.5" Oluatite , , , . Out:4; Set 2 - Cet . . 94 *D M. -Set MAX / MIN Swsnery table let 80 Value 5een EM A Aalen Force minisue masisue 2 124 60 44.9356 4 5.222
' ,#<$ N-2
% ,' Reen Erd A Shear 2 Force Minisue 2 110 16.0TT2
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minium 2 49 0.nm seem and A sheer) f orce 125 85.2766 m.una 2 5.08506 l 2' tems EM A f orcpe min 6 mm 2 &S 117 26.0594
- menina 2 teen tems & amenti " t ain8 2 'I i j
menina 2 111 3*'.
&S 2 *042 l 2 109 24.2354 i g ggaun,nt) m inina 310.632
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h4 St#64 *. w- _. . 4,. ' ~ JS 100.0 2.687890t 2 2.84311SD 2 2.2&&502t*1 8.151970E+0 1.008031D 1 4.185314D 2
- 3. 740304 t
- 1 3#3736D1 8.151966t*0 1.008031t 1 4.185314t+2 SFAmG ,
66 Ja 0.0 2. 718240E
- 2 3
as 100.0 2.71824N +2 3.740304D 1 3.083736t
- l 3.151970D0 2.03507&D 1 4.3953*2t + 2 !
l
&7 'A 0.0 3.105780D 2 8.905734D1 1.647156D 1 8.15196M + 0 2.03307& D 1 4.395392D2 SEAMG
', J8 100.0 3.105780D2 P.905734D 1 1.47156t+1 8.151970D 0 1.0331DD1 4.782388D 2 il La J4 0.0 3.294060D 2 4.42991291 4.25925600 8.1519680 0 1.033173D 1 4.782388D2 ntAMG f 4.4299121 1 4.2592560 0 8.151970t+0 1.311258D 1 4.483481t+2 ;
; JS 100.0 3.294060D 2 '
4 4.570815D1 1.112925t*0 8.151968D 0 1.311258D1 4.483481E+2 eDMG )- 49 JA 0.0 3.345510D 2 as 100.0 3.345510D2 e .5 7081tD 1 1,11292500 8.151970D0 1.373457t+1 4.210492t*2 l
- 1.02462&D2 1.719482t+1 3.151968D O 1,373457D1 4.210492t+2 stAMG 50 JA 0.0 3.56192002 s 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 ~
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 ' 1.636592D1 1.011323t+1 1.518827t+1 4.011855D 2 atAnc ; U~ 53 JA 0.0 5.&00290D 2 7.403140t+1 4.235978D 2 1.822017t+1 N JB 100.0 0.0 5.4002900 2 7.401160t+1 5.504160D 2 e 016213t*1 1.636592t+1 3.140161t*1 1.0113200 1 1.011323D1 1.822017t.1 4.255978D 2 stAsos 54 Ja , - . 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 t JS 100.0 5.876410D 2 9.71&T39t+1 1.593488t+1 1.011320D 1 1.112714t+1 4.750413t+'
56 JA 0.0 6.025060D 2 4.915697D 1 5.440827t+0 1.011323E+1 1.112714t+1 4.750413D 2 BEAMG < l 4 1.41451st+1 4.3679710 2 M JB 100.0 6.025060D 2 4.915697D 1 5.440827D 0 1.011320t+1 4.367971t+2 stAMC-57 JA 0.0 6.064560t+2 5.045079t
- 1 4.149610D 0 1.011323E+1 1.414518D 1 '
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
( 1.429751t
- 2 1.690209D 1 1.011320D 1 2.696644D 1 2.952591t+2
! & J8 100.0 6.223020t*2 2.696446t+1 2.952591t+2 BEAMG
+M- +
59 JA 0.0 6.80897Ct*2 1. 298870t + 2 3.043195 D1 1.011323D 1
.' J8 100.0 60 JA 0.0 6.808970D 2 1.2988?ct 2 3.043195 D 1 6.034504t*0 1.011320t+1 2.387717t*1 1.011323D1 2.387717D1 1.845978t+2 1.845978t+2 etAMG-l Q7 ~
Ja 100.0-7.042020t+2 7.042020t+2 7.508723D 1 7.508728t+1 6.036504 0 0 1.011320D1 1.946162D 1 1.656822t+2 .. 0.0 5.755630D2 9.351465D 1 1. 52638D 1 3.182864D1 1.410686D 2 8tAMG'
+03 JA 3.194333t*1 g(.
y.,. JB 100.0 104 JA 0.0 5.755630D2 5.572570t *2 9.351465t+1 1.108148D 2 3.194333D1 3.523607t+1 1.632640t+1 1.652638D 1 3.914044D1 3.914044t+1 1.635368t+2 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 1.65263SD 1 2.2751599 1 1.095265t+2 BEAMG ll i ; 105 JA Ja 100.0
-1.0 5.561140D 2 5.541140t*2 1.1003&SD 2 1.100388D 2 3.433285t+1 3.433285t+1 1.6526400 1 1.566511D1 8.327159D 1 .
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- 1. ' MAm 1.652638D1 1.566511t*1 8.327159D 1 StamG 106' JA 0.0 4. 75 T710D2 1.130515t*2 *.891621t*1 1.652400 1 1.847585t *1 6.416573t*1 j J8 100.0 . 75T710D 2 1.130515D2 4.891621D 1 6.414573t*1 HAMG 2.901440D 1 3.85 746CD 1 1.65263M *1 1.867585f*1 107 JA 0.0 4.55520CD2
- 1. 452MCl* 1 3.450958D1 4.399734D 1 JB 10C.0 e.555200t*2 2.901&&0t.1 3.857460D 1 1.b52638D1 3.&50958D1 4.199I)4D 1 StAMC 108 JA C,0
- 521810D2 2.TM171t*1 3. 70329 )t
- 1
- 3. 703293D 1 1. 65 %3t
- 1 6.96&347t+1 3.859009D1 ,
481M 0 * . 52 t s t 0D 2 2 '35171D1 6.968347t*1 3.859009t*1 MAMG
. .*S5320t *2 2. 6.8.*81t
- 1 1.5 9 7502D 1 1. 65263tD1 109 JA C.0 J8 100.0 e.49532Ct*2 2.M87811 1 3.597902D1 1.652McD 1 $.742353D 1 4.269775t*1 4.68173M
- 2 2. 519121t
- 1 3.1491&5 t
- 1 i.65263M*1 8.T&2353D1 4.269775t
- 1 StAmG 110 JA 0.0 1.6526400 1 9.622307t*1 4.195M8D1 J8 100.0 4.481730D 2 2.61912tt*1 3.549165D 1 1.65263St*1 9.622307t.1 4.195M891 atAnc 111 Ja . 0.0 3.531712D2 t .100397D2 6 4 8214t*1 5.709969D 1 g
3.5317t;t*2 ' 100J9?!*2 o M8214t*1 1.652 MOD I 9.921908D 1 J8 100.0 . 1.652635D 1 9.921908 u t 5.709969t*1 stAmG 24 0.0 3.N60 Ttt * *.126325Di s.154339t*1 til 6.554336D1 1.652M cD 1 1,021079D1 2.679219f 1 Ja 100.0 3.2964T;D2 *.126121D1 1.37563M .2 StAp4 2.! sit 65t.2 4.207776D 1 2.815SeCD1 5.0674 7t*1 it? Ja 0.0 3.25710Ct 2 6.0779948 1 2.28C8T2D 2 3.25700CD2 2,*64761t*2 . 20TT7 A
- 1 2.855340D1 1 J8 100.* 6.0TT994D 1 2.2808T2t*2 stAmG 1.456T33t*2 5.0443e591 2. 855 5.C01 h 118 44 0.0 2. t T71 T*.D 2 t aS6733D 2 5.k4349t ) 2.85584091 3.614882t*1 1.551485D 2 P 48 100.0 2.3 T7170t *2 0.0 2.854172D 2 1. &8104 TD 2 e.068642t*1 2.85554CD1 3.614882D 1 1.551485D2 StAmc L 119 JA JS 100.0 2.854170D2 1. 48104 TD 2 4.448682t*1 2.85584cD 1 2.446178D1 1.193130D 2 3.7&O141D1 2.S$1840t*1 2.446178t*1 1.193130D 2 etAmG R 120 JA C.0 1.236480D2 1.508343t*2 8.8375094 1 t.504343D 2 3.760141D 1 2.8516ACD 1 2.659055t*1 Ja 100.0 1.286480D 2 8.837509t*1 HAmG 121. JA 0.0 9.25199001 5.5823T21 1 6.2671321 0 2.855&e00 1 2.659c51D 1
_* 6.267132t*0 %~2.85564091 2.145TT7t*1 6.019889t+1 .. h% e 'Jo 100.0 9.251990t *1 s - 5.582372D1 r 122 JA 0.0 8.720280DI S.506998D 1 4.01T325t*0 2.855840D1" '. 2'1457TTD1* E019889t*14 MAm8 hMir$ 5.5069918 1 4.017325 D 0 2.8516409 1 1.922356D 1 6.227289D 1 J8 100.0 8.720280D 1
$ S A69577D1 3.0807510 0 2.855840t*1 1.92235M
- 1 6.22T2899 1 84AmG 123 JA 0.0 S.328320t*1 8.21092M
- 1 5.4MSTTiet 3. 080751D0 2.853S4Ct ) 1.91452t1 1 44 1CC.0 S . 32!U 2001 A
- 5. 45 T9404 1 3.0998105 0 2.855540t*1 1.914527D 1 8.21092M *1 SEAMG 124 44 0.0 8.13514CD 1 1.935724t*1 9.34922TD1 44 100.0 S.13514*D1 5. 45794CD1 1.099810D 0 2.85554001 2.85554001 1.935Ti&E*1 9.349227t
- 1 5tAMG t25 Ja *0 ' 10270 t.2
, ' E 931!!.2 5 465681t*1 t .098349D 2 3.550034t 1 J8 1G0.0 1.1CJ T0;D 2 ' fS931SD 2 f.*65681t*1 2.85154 01 1.098349t*2 SEAMG 1.20T504t 2 2.066616D1 2.35534CD1 3.550084D1 S
126 JA 3.0 1.4TT57CD2 2.85584ct+1 3.2566&SDI 3.055049D 1 L J8 100.0 1.4TT570D2 1.20T50*r*2 2.066616D 1 1 litle : Peer 2 17.5 a OIAmitte t'y
- k. cwipui Set 6
- sst Velue
~
h' MAX /mlu $mery table $tt IV
@\v $et minimm 6 124 81.3514 s
** Seem tid A &alet f orce -
(gf
' maalam 6 60 110 704.202 26.1912
*x 4'
Sees Erd A Deer) f orce minim m 6 I'. 6 45 284.312 maa t an
?
49 1.11293 , g
% , Some trul A Deer) Force minim m 6 >
7 masimm 6 125 74.6568 F minim m 6 45 0.15197
% Seen Erd A f oro.e 28.5554 maalan 6 11T 4 <
6.22303
- team Erd A moment 2 minisue 6 45 + 'Y h9); i' maa tam 6 112 99.2191 +
no m 6nieue 6 109 38.5901 p~j
' Sean Erd A moment 3 48 478.239 t
i' mo nimm 6 minima 6 124 81.3514 T* team ind e Atlet force 60 704.202 a> maaimm 6 y minteam 6 110 26.1912 i Se m Erd 8 Shear 2 forte 6 45 284.312 & maaimm D'?' minimm 6 49 1.11293 . ,h h Seen trd 8 shear) force menteue 6 125 74.6568
*d '
Seen trd a tercpe miniaun 6 45- 8.15197 3 J ap,!
.X2
~"
;f . . , maatsue 6 117 28.5584
=( -
minimm 6 51 6.94435 *N e, seem tre 8 moment 2 99.2191 men t am - 6 til Wh A - 4 s minlaue 6 112 26.7922 3 E Seem trd a masent3. meaimm 6 47 478.239 . V 4; % og ;3 y"*
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ATTACHMENT D Mhie u
- etco c:=nc sesta= 4316 6 4 r SHEET h Of h OC.- 9 73 .u.
ime , , ., 2 ir.5 omita el rinet w / mis s m e, tebie set to vetve
, h 7
se erd a anset force u tnina 1 6 tos 60 o.ca3c29-704.202 - m.n ian 0.5019' minina i 60
.: A sem and a sheer 2 sorce maniam . 6 45 264.312 /a l' % miairus 1 111 *278.375 h/ Seem (nd A Shear) force 125 355.214 masinum i k ,.
seem End a forcpe minian 1 53 12.9994 a meninn - 1 11T 51.1906 minina 1 104 125.044
< Seem (rd a moment 2 118 !}4.282 useinn 1 min 6an 1 58 0.42843 team tre a met 3 48 478.239 mon ian 6 6 m inina ' 53 0.64581 f Seem (rd 8 Anlat force 60 704.202
, monisue 6 16 a 6aina 1 50 0.21964 ' Beam trd 8 Sheer! Force .
) 2"y .
ass ina 6 45 284.312 (. team (rd 8 theor3 Force minian 1 123 111 35),214 273.3M masine 1 d sia m e ' 117 51,1906
' Seem tre e f ores e Ill 28.5) $.
[.
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minian 1 117 234,282
' team Erd a moment 2 12! ,eh4
< y mas tne 1 10] '~ Vf. g m ininD 1 60 +0.660C9 Beam trd 8 Marent3 47 475.237 ustlap & r jj h} -, ' i; - 279 i; - , y' - c.' 8 R?e? ; 4.*- . _ g:#ey$m NN
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- 1 ATTACHMENT E~ i W.
s l 3 Kswr ts= va CAN S weri Q 1L HEV I E*' GENERAL j f 3syynseems Engineers & _
~ ~
Constructors COMPUTATION O E E g PREUM. FINAL Voto qg SHEET { ,
~**
X ll I FERMI 2 - CCINAC __ W
~
NECT _ WE DATE uuu t. AUUATIOt7 Ur.WTG. , SUnJECT - SVGTEM-GERIEC l J1 76230.502 j p p t n , I The data contained in thic attachment are generated using the 1 , 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 y b calculations:
- f
, MN 'DC-5763' ^^ =- -
- CCiWAC-Concern-Resolution ,TasL Duct String Analysis and Support u.aluation of t ; b (..
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 E 2849 and 4126 System Series
'[
B c DC-5766 CCIWAC Concern Resolution Task Duct String Analysis and Support Evaluation of
$ R j 2850 Systen Series -
- w j._ DC-5767 CCitVAC Concern Resolution Task i %
Duct String Analysis and Support Evaluation of -- 4316 System Series s; .
! 6 ~
/,Qi f- 6 'I s ,j, if.
l ,-
'. '(4 .,
i (*;'; j M e ,y1 Q,;y-- E /j- 1 p 6 . ,' l
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7 ~ y . hfy. *
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j $p7 j - 4 / -t +
. !o wa,s ATTACHM,ENT4M@"
*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) L0A05 ttAa ttimieI
? '3t 104110e StuDitG Stuotte AIIAL SutAt lat At h
C DEAm P v2 v3 1.98t185tet mi 2.157640t*0 m2 1.3493&3t*1 m3 1.7379381 1 atAaeo 0.0 2.N7584 2 7.*36094t 2 2.412987t = 1 3.2251576 1 61 44 2.F 79act 2 -7.43609 t-2 1.98tt85tet 2,157640t*0 6.6008864 1 MAMG Jt 100.0 1.509363t*0
- 1.29894M
- 1 1.0M407t*1 62 JA 0.0 6.458700( 1 4.01989e4 1 1.293940t*1 2.146587t 1 -1.664068t*0 6.458700t 1 5.0198964 1 1.509363t*0 JS 100.0 9.018243t*1 2.612990t*1 2.157639t*0 3.2251571 1 atA>G O Ja 0.0 1.4 %790t*2 2.9079821 2 5.4206381 1 3.043408( 1 s t, +7.43609M 2 2,907982t 2 3.018243tet -2.6129901 1 JS 100.0
? .4 3Wct 2 2,9079s?f 2 9.9&a249tet 2.612990f*1 1.4206344 1 -3.0434081 1 stAMG 64 Ja 0.3 2.612990t*1 1.166331t*2 2.861659f 1 1.436090t 2 2.907961t 2 0.0&M69t*1 2.861659t 1 atAmG 1 JS 100.0 2.612990t+1 1.166331t*2 i
65 JA 0.0 7.4%090t 2 2.617852t t 1.0593121 2 2.539503t*0 1.806T20t=1 1_ 1.4 % 0901 2 2.6171325 1 1.059312t*2 *2.H2990t*1 JS 100.0 2.539503t
- 0 5.80672CE 1 StAmG
@ 66 JA 0.0 7.436090t 2 2.617K321 1 - 8. 84 7069f
- I 2.612990tet 2.6129908+1 1.020690t*2 8. 5 17818 1 P
Ja 100.0 4 7.4%09Ct 2 2.61783?t t 8.S47069t*1 2.6344501 1 8.907958t*1 2.13924M*0 StanG
%.70510t 1 3.84086*( t 2.929676t *0 1.96311M *0 67 0.0 8.468507t *1 3.540A6.t t 2.929676t *0 2.634450t*1 4 JA JS 100.0 4,7051M 1 8.4685071 1 1. 94311M *C StAmG 3,54C8ME t 2.62103tt*1 2.634450t*1 f4 4A Q.0 5.7631104 1 4,536960t*1 1.386987t*0 3.8408c t 1 2.62103ttet 2.63445M
- 1 x 4.ft351M 1 1.386987t*0 6(AMG Je 100.0 1 %086 t 1 *.940095tet 2.6b5M*1 4.5 3696C(
- 1 69 JA 0.3 5, *6t 41 1 2.6b501 1 2. 5866Mt
- 1 S.1085711 1 i.7M510t 1 3,kC86*[ 1 *.4 9045tet 4.1081714 1 StAmG
' ' JS 100.0 6. 759552t
- 1 2.634450t*1 2.886682t*1 70 0.0 5.705tM 1 3.8408648 t 8.517349t*1 4.909132t 1 JA 3.840864t 1 6.759512t*1 2.634450tel Je 100.0 4 .76351M 1 0. O. 2.392184t 15 StAmG
'T 11 JA 0,0 2.4313M
- 2 4.4545541 1 2.61TN71 1 0. 1.308899t 1 2.227277t 1 2,43 t hM 4 4.4545544 1 2.6tT797t 1 JS 100.0 *4N
- 2 4 t ??37t 1 1.781130s 15 -1,308899t ? - 2.2272T71 1 StamG 1.5 96067t
- 0
*.*5 15,6 1 2.st T?97t 1 1.78113.1 15 4.377%'t.i 72 aA 0.0 1. 4C3310f * ?
st 100.0 -1,9033106 2 1.14529M*1 1.942 58t*1 DEAmG 1.37534t 1 6.504746t 1 1.159850t*0 T3 Ja 0.0 1.227644 1 1.159850t*0 1.259193t*1 1.9668645 1 Ja 100.0 7.2278408 1 1.3T75341 t 4.5087465 1 1.966844t*, 4E7mG M, 1.377534t t 6.504746t 1 1.15tJ50t*0 1.259193t<1 1.98294W 74 JA 0.0 1.76423 4 *1 1.159850t*0 1.335151t*1
-1.764230fet 1.3T534t.1 6.50874M t 1.1598531 4 W mG F Ja 100.0 4.69995tt t t.982940t+1 1.31515tt+1 0.0 t.5085Ct 1 1.3T55 4 1 1.389998t*1 9.N 09531 1 D 75 JA 1.375341 1 4.699511t 1 t .98294M +1 JS 100.0 0.5045Ct 1 1.982940f*1 1.389998t*1 9.990953t 1 ttAmc 0.0 6.5085 0t
- t 1,375345 t 4.5406??t*1 9.302184 1 3.660311t*1 76 JA 4.540627t*1 1.982940t*1 JS 100.0 6.504 5CE ? ?.37534t.t 3.660311t f 9.30218M
- stA40
.130887t 1 5.530334t*1 1.9329 0t*1 TT JA 0.0 6.504504 1 1.9829ectet 2.793593t*1 7.982441t 1
/
6.50*501 1 1.130887t f 1.530338t e t 7.9824418 1 StAMG
- Ja 100.0 6.50a5*t 1 1,1305871 1 3.331870t e t 1.9829 0t*1 2.793593t*1 6.0983E3t 1 D TS JA 0.0 1.1308371 1 3.331870t e t 1.982940t*1 0.344489t*1
'* Ja 100.0 6.50650t.1 1.982940t*1 8.344489t*1 6.0983831 1 StAMG
- 508750t 1 1.1308871 1 2.066599tel 6.7756381 1
' is 79 44 0.0 . 1.130887t 1 2.066599t+1 1.982940t*1 5.932768t*1 Je 100.0 6.50850t 1 5.932770t*1 1.982940t*1 4.T786384 1 stamG
.* 1.1304?Ct 1 6.5087465 1 3.877&32!*1 2.617069t 1 1
80 JA 0.0 6.56874Al t 3.8778322*t -5.932 77Cl
- 1 2.542490f 1 Ja 100.0 1.130890t 1 5.922770f*1 2.54249M
- 1 2.817069t 1 st AmG -
O.0 1.130890t 1 6.50874M 1 8.88829ttel 1.040627t*0 31 JA 8.888291t*1 5.932770t*1 1.290624t*2 Ja 100.0 1.13C890t 1 6.5087461 1 1.040627t*0 alAMG 1.269527t*2 5.922770t*1 1.290624t*2 82 JA 0.0 6.821710E 15 2.621610t 1 2.851580t*1 8.329952t 1 2.621410t 1 1.2(9527t*2 5.93277M *1 Ja 100.0 6.821710(-15 5.932770t*1 2.85155M*1 8.3299125 1 StAMG 6.82171M 15 2.621610t 1 S.772051tet 5.598235t 1 83 JA 0.0 2,621610t 1 8.TRc5 tt e t 4.932770t*1 6.283596t *1 Ja 100.0 6.8217108 15 2.984040t*1 1.077179t+ 1 3.4463315 1 SEAmG 84 JA 0.0 8.302860t 2 1.15550f t 3.077906t al 4.032144t*1 1.4949182 1 1,155501 1 3.077906t
- 1 2.983040t*1 Ja 1FJ.0 - 8.302860E 2 2.988040t*1 4.012144t*1 1.4949181 1 stAMG n
8.30286M 2 1.15550t f 4.91427tt*0 4.TITTT2C 2
+ 85 JA 0.0 4.914271t*0 2.983040tel -4.654302t*1 J8 100.0 8.302860t 2 1.17555W 1 1.8194411 1 2.181550C 3 stAmG
- 1,1363431*2 2.988040t*1
&& JA - 0.0 - 3.30256M 2 - 1.330544t
- 3 2.983040t*1 1.428254t*2 4.266931t 3
-r JS 100.0 6.302860t 2 1.330544t 3 1.136343t d 1.428254t*2 4.266931t 3- 8(AMG
& 1.330544t 3 1.382109E*2 2.985040t*1 6/ JA 0.0 8.302860t 2 3.8469454 4 6.595384t 3
%' 8.302t40t 2 1.330544t 3 1.382109t*2 4.988040t*1 3.T795471 2 atAmG Ja 100.0 0, 4.039396t 2 2,29466M4 7.233850t 12 5.24012*1+2 4 - 88 JA O.0 2.29466M*2 7.233880t 12 6.86474M
- 2 2.t1654M 3
" Ja 100.0 0, 5.0193961 4 6.864745t
- 2 2.11654M 3 stAMG 39 JA 0.0 -5.5511201 15 4.039396t 2 2.672864t*2
- 2.672868t3.5385001
- 2 3.53850ct 12 0.
- 12 6.97700$t
- 2 0. SEAmG Ja 100.0 - 5 *511204 15 5.03939M 0. 4 6.977005t*2
^
. ./-
90 JA 0.0 0. 1.468943t*2 5.9 %9201 14 3.428038t*2 0. - O. -1.4689431 2 4 .936920E 14 b(" 91 JS 100.0 JA 0.0 0. 0, 0, 1.0906331 2 6.294960t-14 3.428038t*2 0. 8(AMG - r.L
. e,r
- i . 79' 5J g3 sy
~-
w~ mf Y m, m&& M ,; Q_
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J' 0(C0 : wv&C STittu 4316 6 4 7 SM[{
- y '2.4 thw att 18 12:491M 1996 ) b S W.
[ . 51AanAP version 4.41 g , Report a (Lemen t Formet $1 Anovut ter/ seas tienent a .3 ( N' litle t P40P 3 16*s16' ' (
~
Output let 1 Ot AD LOAD (CLt t0A0$ ( g(An tttatui f - w 1CallCet StkO1NG S!W0 lug SutA4 ( [ astA4 p SMEAR v2 v3 #f #2 "I 0. y 4 gg An
-1.090633D 2 6.2949601 14 7.461723b t Jo 100,0 c. O. 0. SEAMG 0.0 c. 3. 4.56945CE
- 1
- 7.32747CE
- 15 7.461723D1 I 92 JA 0.
Je 100.0 c. O. 4.569650D1 7.327470t
- 15 2.279671DO 0. Stan0 D O. 4.206035t*0 8.570920E 14 2.279671D 0 r 93 JA 0.0 3. 0.
L 0- 4,206035Do .s.57c920t 14 1.640021t a 12 F ' Jg 100.0 3.117368t.1 2.151903D 1 StAMG 1.alG igt - t .,33+315t 2 2.040862D 1 7.294690t.1 94 JA 0.0 2,0 0862D 1 1.2946900 1 7.210746t+1 1.282565t-1 E JS 100.0 1.6101gt.1 . 3343tH 2 1.282565D 1 SEAMG
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- 63 JA 0.J 3.49080M + 2 5.063548D2 2.0315258 1 2.5971 M D 1 1.65991M
- 1 Je 100.0 2 13357CE *2 1.65991M
- 1 3.49080M+2 BEAMG 64 JA 0.0 2.168760D2 5.09840?D2 2.222553D1 2. 597150t *1 5.098607t*2 2.222553D1 2.Se7160t+1 2.944760 D 1 4. 760603D 2 Je 100.0 2.168760D2
- 6. 38774*D 2 3.056911D 1 2.597159t+1 2.944760t+1 4.760603D2 SEAMG 65 JA 0.0 2.640060D2 2.591160D 1 7.27053M +0 4.644605D2
- Je 100.0 2.640060D2 6.387744 t
- 2 3.056911t +1 6.334563t*2 2.N3503t*1 2.597159t*1 7.27053M *0 4.M460$D2 8tAmG 64 JA 0.0 2.724780D 2 1.109039t*3 a.336563D 2 2.793503tel 2.5971MD1 3.745391D 1 Je 100.0 2. T24 730t *?
1.131537t +3 atAmc 3.56797ct.2 2.221837t+1 4.290754t*1 3.177159D 1 67 JA 0.0 5 . 494 765 D 2 6.062682t+1 9.505003t+2 i: as 100.0 3.54797; D2 1.494765D 2 2.221837D 1 4.290760t+1 1.491495D2 2.2M25M
- 1 4.290754D 1 6.062682t+1 9.505003D2 BEAMG 6.8 JA 0.0 3.69049CD2 1.491495D2 2.264259D1 4.2907Mt *1 9.107238D 1 7.8322090 2
- as 100.0 3.690490D2 3.8141900 2 1.469275D 2 2.+13789D 1 4.290754t+1 9.107238D 1 7.832209D 2 StAMC 69 JA 0.0 1.232H M +2 6.379529t+2 4.290760D 1
- i ..*' Je 100.0 3.814190t*2 1.469275t*2 2.413739 D 1 0.0 3.910960D 2 1.443334D 2 2.604935D1 4.290754D 1 1.23222M +2 6.379529D 2 stAMG 70 JA 5.692247t*2 as 100.0 3.910960D2 9 443334t *2 2.604935t*1 4.2907M D 1 1.423407t*2 z >
71 JA to 1.839980D 2 4.57M 29D2 1.0119ND2 8.274907t
- 13 9.416251013 4.8008196 12 BEAMG r 40 160.0 1.839980D 2 4.5 76129t
- 2 1.0119 Nt*2 8.274910D 13 5.059897D 1 2.288064D2 72 JA 0.0 1.812010D 2 4.523009t 2 9.52395M + 1 1.6249781 12 5.059897t*1 ' 2.288064t*2 BLAMG 1.812010D 2 4.5230N O 2 9.525956D 1 1.6249504 12 3.439031D 2 1.623248D 3 Ja 100.0 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 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 i 1.537418t+2 Ja 100.0 1.396980D 2 1. 391475 t
- 2 1.48T30M .2 3.843330D 2 2.012528D 2 O 1.5f 3058D 2 1.396666D 2 1.53741M
- 2 2.012528D 2 3.M3321t*2 BEAMG 75 JA 0.0 1.555450D2 Je 100.0 1.555450t*2 1.50305S4 2 1.396666D 2 1.537410D 2 4.823529t+1 3.10752M+ 2 5 4 76 JA 0.0 1.740850t*2 1.7244764*2 1.*02118D 2 1.137418D2 4.823529D 1 3.10526D 2 SEAMG 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 1 1.637465 t
- 2 2,010574D1 4.046T78D1 6.4381806 2 h- Ja 100.0 2.520590D2 1.537410t+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 JS 100.0 1.009770D 3 2.381678D2 3.591743D 1 4.086790t+1 9.444381t+1 5.091635D 2 W: 4,086782t+1 9.444381t + 1 5.091635D 2 StAMG i4 83 JA 0.0 1.008350t*3 2.342956D 2 3.046613D 1 '
Je 100.0 1.00a350t*3 2.34295M
- 2 3.046613D 1 4.086790t+1 7.029585t+1 4.58141M*2 84 JA 0.0 6.047230D2 7.298355D1 1.5319521*1 1.652638D 1 4.170111t+? 2.210733t*2 SEAMG Q. 2.049954E+1 1.025966t+2
- , f .. JS 100.0 6.047230 0 2 7.298355Da 1.531952D 1 1.652 Mot + 1 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 .
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- 2 2.244626D 2 8tAmG 5.123340D1 *.250244D t
- 41026. D 1 4.11069M 14 1.233379t*2 90 JA 0.0 7,010264 D I 4.1106900 14 1.99709H + 2 Jo 100.0 5.123340t
- 1 4.250244D1 0.0 3.817220D1 3.740560f*1 6.0997M D 1 5.2808060 4.97945M*1 14 1.997093D2 1.233379D 2 BLAmG 3.168864D1 91 JA 3.81722001 3.740560D1 6.099764t*1 1.28081CD 14 3.168864 tat stAmG JB 100.0 3.04168M*1 6.48162M .14 4. 9 7945M
- 1 g 0,0 1.602450D 1 1.934480D1 1.M5198D0 1.06785M *0 92 JA 1. 93448M *1 3.0416aM
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2.268460D 1 2.585169t*1 9.130815t*1 4.296050t*2 1.511513D2 1.4132 7tD 1 9.130815t*1 stAM J8 100.0 2.268461D I 2.585169t*1 95 JA 0.0 4.197370D 2 ' 4t245tD 2 ' . 1.M480M k480M **11 2.268.t4t*1 2.074H4Dt 2.800347t*2 4.197370t
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Ja 100.0 6.458700t 1 5.01989M 1 9.110383t*1 2.135328 1 H AMG 1.1 555Ct 1 1.3576f2t*2 2. 98804M
- 1
+ 103 JA 0.0 8.302S60t 2 1.250441E*2 2.431419t 1 1.1755504 1 1.357612t*2 2.9880*0E+1 JB 100.0 3.3028Wi 2 2.953040t
- 1 1.250441t + 2 2.4514195 1 BEAmG 0.30286M 2 1.51808et 1 t .422565t
- 2 1.6723771 1 104 Ja 0.0 2. 98804M + 1 5.391587t*1 6.30286M 2 1.518084t 1 1.422565t+2 1.6T23T71 1 6tAmG
~ Ja 100.0 1. 371562t +2 2.984040t+1 5.391587t+1 105 JA 0.0 8.302860E 2 1.5180848 1 1.962683t+1 1.29285M 1 i
1.5*S0848 1 t . 371562 t + 2 2.98804M
- 1 1,292856E 1 "AMG JR 100.0 8.3025606 2 1.962683t+1 e 8.3028601 2 +1.516084t 1 2.t52442t*2 2.98304M
- 1 9.13335M 2 O} tre JA 0.0 2.152442t + 2 +2.988040t*1 7.343787t+1 JB 100.0 8.302860t 2 1.5180&t 1 7.343787t+1 -9.1333Mt 2 SEAMG
@ 2.988040t+1 101 44 0.0 8.302860t 2 3.057310E 2 1.029071t +2 2.988040E+1 2.9469275 1 6.076044E 2
% 8.302860t 2 3.0573101 2 - 1.029071t + 2 2.988040t +1 6.076046( 2 stAmG
- J5 100.4 8.930628t*1 2.946927E*1 8.302860t 2 3. CST 310t 2 g 108 JA 0.0 2.98804M *1 1.18775*.t
- 2 3.018736t 2 JS 100.0 8.302860E 2 3.05T310t 2 - 8.930628t
- l 1.18755t + 2 3,018736t 2 StAMG 3.057310t 2 7.91056M+1 2.98804M +1 109 JA 0.0 8.302860E 2 1.583284t+2 1.490081t 2 7.910563(+1 2.988040t+1 JS 100.0 8.302860E 2 3.05T31M 2 1.583284t*2 1.490081t 2 stAMG 110 JA 0.0 0.302860E 2 3.05731M 2 7.400530t+1 2.988040t+1 y 1.768297D . 7.25754M 3 2.988040E+1 Ja 100.0 8.302860t 2 3.0573101 2 7.400530E+1 ?J37540t=3 stAmc p 111 JA 0.0 8.302860E 2 3,037310t 2 2.783951t+2 2.988040t+1 1.768297t+2 1.072309D 2 A.837340t 4 F 2.988040t +1 9 Ja 100.0 8.30286M 2 3.0573 tot 2 2. 783951t *2 2.988040t*1 1.072309t +2 2.857340t 4 stAmG '
112 JA 0.0 48.302860s 2 1,330544t 3 5.389743tel 6.680784t+1 1.3&l*421 3 ,. 2.988040E+1 Je 100.0 8.3028604 2 1.330544t 3 5.38974M*1 5.119060t+1 1.875975t *2 2.358870t 1 StAMG 8.302060t 2 +1.446060t 1 1.867384t*2 2.720385t 1 117 JA 0.0 5.119060!+1 -2,342821t+2 M JS 100.0 8.302860t 2 1.446060t 1 1.867384t+2 5.119060t*1 2.342821t+2 2.720385t 1 stANG t
- 8.302860t 2 1.70512M 1 2.151119t+2 1.867824t 1
. . 118 JA 0.0 2.151119t+2 5.119060t+1 1.267261t +2 Ja 100.0 8.302860t 2 1.7051234 1 1.26726)(+2 1.8678241 1 stAMG 2.100116t+2 5.119060t*1 119 JA 0.0 8.302860E 2 1.705123t 1 1.119060E*1 7.4223195 1 1.441543t.1 44 100,0 8.302860E 2 1.705123t 1 2.10011M +2 1.441543t 1 atAMG' 1.423887t+2 5.119060t*1 7.422319D 1 -
.;b 120 JA 0.0 8.3028604 2 1.705123t-1 1.098204t*2 1.015263t 1 1.TM123t-1 1.423887t+2 5.11906M *1 R Je 100.0 *8.302860t 2 5.119060t*1 1.098204t+2 1.015263E-1 stAMG 8.302860t*2 2.1319191 2 2.608791E*1 121 JA 0.0 ,,qhf V dIn e s;@
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' ATTACHMENT MW SHEET ..M 0F._.1 1 .
- lto t; mea 115ftn 4316 6 & 7-
- the apr 18 12:47:55 1996 StAanA* version 4.41 Report i t iemnt
. Model forset : StAA0f at Ser/Seem (Leaent
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' DEAM 5.11D06cD I +8.373246D1 8.020708D 2 46 100.0 6.302860t 2 2,1319191 2 2.60879tt*l 8.0207084 2 stAMG 1.248705D1 5.118060tel 8.373246tal 0.0 8.3028ME 2 2.1319 t er -2 122 44 S.302864t 2 -2,131919t 2
- 248705D 1 5.119060tel 1.124541DI 5.688788E 2 Je 100.0 i 488788D 2 atAmG 7.124541t*1 123 JA 0.0 S.10286 4 2 2.13191002 2.286400D0 5.119060D1 7.010221D1 4.32282tt 2 48 100.0 8.302840 0 2 2.t319196 2 2.286400D 0 5.119C60D1 1.010221D1 4.822829D 2 BE An'*
0.0 9.30286002 2.1319t&t 2 2.81);25t*3 5.119060D1 124 JA 1.080569tel 4.289849D 2 J8 100.0 8.302860t 2 2.13 trt902 +2.813925t*0 5.119060D 1 7.080569D1 4.289649t 2 atAMG 125 JA 0.0 8.302560t 2 2.131914t 2 3.552145D2 5.119060D t 1.596093t*2 3./56869D 2 Je 100.0 8.302860t 2 +2.13191902 3.5 tit 43D2 5.189060t*1 1.596093t*2 3.756869D 2 atAMG 126 JA 0.0 8.30286 4 2 4.906342t 2 6.879777D1 5.119060D 1 1.078609t*2 1.711274t 4 4,906342O 2 6.999777t*1 5.11906M
- 1 JS 100.0 8.302560D 2 title
- Pa0P 2 17.5* OIAmitta T OJtgut let 1 DE AD LOAD (04) 10 Value
,L MAX /uts $wsmery f ebte let Set 103 0.083029 Seem End A Aslet f orce mnimm 1 maalan 1 53 0.64587
- Q =Mine 1 60 0.50199 s+ Some End A Sheer 2 Force 1 50 0.21964 maa tam y mint am 1 111 278.395 Seen trd a Saeer3 f orce 125 355.214 man ian i a f naim t $1 12.9894'
[$ team trd A forcpe 51,1906 f5' team Erd A Mumient2 maalan minism 1 1 i 117 104 118 125.044 234.282 Y N' leam trd A moment) maa f am minimm 1 58 0.42343
'eas t ase 1 &8 0.37655 J 3y Bema trd 8 Aalet Forte mininst t 53 0.64557 1
maa 6nsa 1 105 0.083029 mininse 1 50 0.219M team trus 8 theori f orce f 60 0.50599 maume e+ seem trus t Shear 3 Force nintam i 125 355.214 ' maalma i ill 278.395
#f ' Seem truf 5 tercpe minim a 1 117 51.1906 6:
manina f 53 117 12.9894 234.232 4 minim m 1
'7 Seem tid e acaent2 103 125.044 maaima 1 1
6 , mintam 1 60 0.66009
% Seem Erd a nament3 maninn 1 57 0.42543
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- Osi (OA0$ l-y 654m tttuiu1 A4 n sim0 lng S(N0lue M SutAt SNEAR toastou b '
$ 9tAft AxlAL P V2 V3 NV m2 3.679138D O M3 2.06til3t*2 speeG 1.714950D 2 1.575806D 2 2.221283t*1 5.085057t*0 1 45 JA 0.0 1.085060f*0 1.0444T2t*1 2.779907t*2 Je 100.0 1.114950D 2 1. 57580et
- 2 ?.221283t*1 3.5217015 1 5.0850571*0 1.044472D1 2.77V907t*2 BCAMG 46 JA 0.0 1. 742080D 2 2.32502CD 1 2.254518D1 2.917240D 2 1.742050E*2 2.325020D1 3.521701D1 5.08506M*0 Ja 100.0
+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; 48 JA 0.0 2.112740D 2 2.781975D1 4.792656D O 5.0850571 0 8.7226410 0 3.196320D 2 SumG 1.246477D1 3.00122SE*2 .
.l ;
Ja 100.0 2.112740D 2 2. T51425t *
- 4.792656D 0 5.085060D 0 N. 7.711105t=1 5.0850571*0 1.2464TTD1 3.00)225t+2 StAMG *
@ 49 JA 0.0 2.144850D 2 2.134v75 t
- 1 1.296489t*t 2.822380ta2 JS 100.0 2.144850D2 2.8349 75t
- 1 7.711105 D 1 5.085060D0 1.29M89f*1 2.8223800 2 stAMG f
Q 50 JA 0.0 2.279380D2 6.606325D 1 1.955040 D 1 1,955040D I 5.082057t*0 S.085060D 0 2.898503D I 2.400221t*2-Ja 100.0 2.279380D2 6.606325D 1 2.400221t+2 stAMG 4: 51 JA 0.0 2.767270D 2 5.935523D1 3.375495tet 5.0850571 0 2.898503D1
. Je 100.0 2.767270D 2 5.935523D1 3.375495Eal 5.045060D0 6.303418D0 1.994575D 2
*f e=
\' 52 JA - 0.0 2.959740D2 1.259479D2 5.153902t*0 5.085057t*0 4.3.33418D0 7.349780t*0 - 1.994575t*2 St.AMG 6.027569t*1 Je 100.0- 2.959740D 2 1.259479D2 5.153902D 0 5.085060E*0 3.590470D2 4.65576cD1 1.773038D 1 6.645530D 0 1.13512sD t 2.650189D2 stwG 53 JA 0.0 ,
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n= . ATTACHMENTMM p .& 4 Dit0 t D at ttttta 4116 6 6 EkW !' -- QF D the asar 18 12:4T159 1996 STAand versten 4.41 4esett t ttamont modet 8 f6tuot t $1&A0thi 86f/$ees (tecent X
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- tot 4(Aa tt(ateI t0605 a h
7 Antal thtH tut At 1cas10e at Nie ttG m2 MuottG m3 e il v3 2.8 t t 38M
- 2 L' H AM 4.6HfMi*l 1. TT303M
- t 6.k%85M
- 0 1.160265DI 2.81138M *2 8 TANG J8 100.0 3.5906 ?M
- 2 6.M58.50t*0 1.7602Ht+1 2.66 F69M O 3.5 T300&D 1 2.920139D2
$6 Ja 0.0 3.M3250t*2 6.645880D0 1.5765t *1 2.66749M*1 3.5T3004t*1 2.920139D2 SIAmG 48 100.0 3.2125M
- 2 6.kS t.8M *0 1.757675t *l
,f, 6.C9405M e l I.776099D 1 3.172690t*2
$$ la 00 3.911140f*2 1.T76099f*1 6. 64588M
- 0 6,87961N *0 3,911160t*2 6.094056t*1 6.87941M
- 0 3.1T260t*2 SEAMG 3
i 48 100.1 3.157290t*l 4. T86382t
- 0 4.M5880t*0 2.9215%t*2 le da 0.0 6.00T390D 2
* . T54382t
- 0 6.645880D0 9.Tt668M *0
. 00T3 Mt*2 3.11F29CD 1 s8 100.0 ST 44 0.0 e . 032850D 2 3.202234tet 3.Nf 2MD t 2.S$96TH+0 6.64588M
- 0 2.5196T8DO 1.1163 tit *1 6 H5880t*0 2.684345t*2 2.684345t*2 StamG 9.T1M86D0 2.9 J4 100.0 6.0328%D2 1.1163 tit *1 4.137t&t
- 2 9.45 H9t*1 1.894626D I 6 M1880t*0 2.45371Drot 1.964339t*2 58 Ja 0.0 9,*5 D itt*1 1. 89&MM
- 1 6. 4588M *0 1.964339t*2 etano se 100.0 . 13 % Ol*2 6,k5850D 0 2. 4HFl0t *1 8.H. 0 O t 1.4 HUM e t 1.231912t*2
- 19 Ja 0.0 C50575002 8.H TT06t e t 3.45553M 6.Hl880t*0 1.kt350t*t e t 6 H1840D0 1,H9350F *1 1.231912t*2 HAuG J8 100.0 6.5057501 2 6.H T841D0 4.45H2:D2 4 $08787Di 6.047841t*0 6.645 t.80t *0 1.19561&l*1 1.0305Mt*2 60 44 0.0 8.6196458 0 $tAmG I +
48 100.0 4.652H0f*2 4.108787t*1 1.194814 0 1 1.482878tet 2.n4230tel 3.03fv8ct*2 LS Fi929t a t 1.5405058 0 9.M T53t
- 1 106 44 0.0 3.384816t*1 1.6t2880D 1 3.03480D2 6.579829fet 1,68 378D1 3.54050 Met 9.T57MM e l StamG 48 100.0 6.63384Tret 3.63ttset.1 104 sa 0.0 2.941720s*2 1.682880tet 1.809355t d 6.12T219tet 2,961TED 2 6 613847t*1 3.6319t.M
- 1 6.527219Dt M AMG 48 100.0 t.482878D1 1.809355t*1 2.935TMt*2 oS856Mid 3.512155Dt 1.069787t d 4.954602t*1 3
105 JA 0.0 1.482880D t 4.958602t*1 H AMG J8 100.0 2.93572M42 6.5856Mt e t5.112523Dt 3.51Fl55t d 1.48187H +1 1.0H117t e l 0.0 2.113!?Of *2 6.T?iS11t*1 1.842&I3D 1 3.8M205t*1
*f6 J4 J4 100.0 2.5133*cD2 6. Tf t515t d Lil2 2!t d 1.48tft80D 1.682878D 1 t
1.8824t3D1 3.834205t*1 Stamo 2,406910t*2 1. T7891M
- 1 3.Ttuttt*1 3.012899t*1 2.654057t*1 107 Ja 0.0 1.T7891M 4 3.7142titel 1.482880tel 9 J4 100.0 2.&O6910t*2 1.48287M d 3.01899t*1 2.654057tel StAMG
*E 0.0 2.329430t*2 1.67808M
- 1 3.$04260tet 1.482880tet 6.341527t e t 2.423538D 1 H ANG 108 Ja 1.678088t d 340460t*t 6.341527t+1 2.4353M *1 J8 100.0 2.3894 W 2 1.48287M el 2.37H t0D 2 1.62569vD 1 1.356T62tet 1.482880D 1 8.00H87td 2.71902&D1 i 109 JA 0.0 1. 625699t
- t 3.358?Mt*1 2.719024t*1 HAmG
- J8 100.0 2. t T55 t-D 2 1.482878t*1 8.00 n 87tet Stet 2 1.60TTitt*1 3.29049tet 8.820616t d 2.93650M*1
..h 110 JA 0.0 2 iFDD2 1.6JTT21t*1 3.290649t *1 1.482880tel 8,820416t*1 ' 2.936506t*1 StAMG J8 100.0 1.4828784 4
;=
. 111 JA 0.0 440D 2 6 1084$D) 1.2244T8t*t 1.&82880f*1 8,80162 Met 3.612529t*1 t> s440D2 6.70845t e t 7 2244T8Dt 8.801MM
- 1 3.612529t*1 StANG J8 100.0 2.$ 94435D1 1 TT02TH 1
- 1. 6828TM
- 1 112 J4 0.0 i.T&5810t*2 1.4828800 1 6.495102DI 1.70676TD1
- 1. TT02 T5t
- 1 1.0 TOT 90t*2 6fAMG J4 100.0 1. F&$810D 2 2.192235t*t 4.611601D1 2.60594&8 4 S.0548?M*1 1.71&S608 2 1.22&h8t*2 lif Ja 0.0 1.H&848t*2 6.6116M D 1 2.605950D1 6.182025td 1.292MSD2 1.292645t*2 StAMG 6@, - J8 100,0 1.11886M*2 2.605944tet 6.1820251 4 t.519050D2 0.68623 tdt 5.4108tM*1 8.766885tet V 118 Ja 0.P 5.&t0813t*1 2.W910D I 3.513739D1 J4 100.0 1.lt9050t*2 8.68438D 1 2.6v5944t e l 3.$13T39D1 8.F64885t d SEAMG 119 JA 0.0 1.5M980D2 8.4491230t 5.294tl5t*1 1.D41554*) 2.605950D1 2.23792M *1 6.T30190t*1 1.506980D2 8.4491231*1 J8 800.0 8.t.2 tutt e 3.T8264M 4 2.60$M4D t 2.23792M 4 6.T30t90D 1 S p 120 JA 0.0 6.8951000 1 6,895100 0 1 8.62126 Trol 3.782&&6D1 2.605950D1 2.801455D1 5.014469D)
J8 100.0 121 JA 0.0 5.052470D 1 3.0M56201 3.034562t d 6.601162D 06.6011M 2.605950D 0D2.2232MDI 0 2.60594&D1 3.53351st*12.801455DI J8 100.0 5.05247M O 3.653694t*0 2.605944tet 2.223266( 4 3.533514t4 SEAMG 4.T854T001 2.983023D1 1.9T9411D 1 3.6455T1D1 tu JA 0.0 3.65M94t*0 2.605950D1 3.6455T1D1 8tAMG s8 100.0 4.7854Mtd 2.983013D1 2.159u.TD 0 2.6059641 4 1.979411t*1 2.957729t*1 4.654506D 1
}/-
c6 fu JA 0.0 4.58968M e t 4.589650td 2.95TT29D 1 2.tl966Tt*0 2.605950D1 1.97543tf*1 1.975431D1 6.654506D1 StAMG
),
1*' J8 100.0 2.949911t
- 1 2.19486900 2.60594&D ) 5.24520M*1 0.0 4.4.*3%CD 1
% 124 JA 4.493560tF,210919t*1d 2.94991184 2.194869D0 2.605944t*1 2.605950D1 2.0015545 4 5.245206td2.001154D1 H AMG -
y A J8 100.0 8.52TM314 3.980U7t d 4.1M 6 t it *1 125 JA 0.0 6.021$9M O 8.5H663D1 2.605950D t
,, 6.0215900 1 T,210919t*1 3.980227D1 6.146118 4 H AMG
~
J4 100.0 6.564910D 1 2.0944MD 1 2.6059+4D I 1.919258D 1 126 JA 0,0 7.95&J1M H 2.605950D 1 3.291898t*1 6.$6491001 2.094434tet , JS 100.0 T.956810D 1 ;p h title Pe0P 2 1T.58 Otamitte Output let 2
- CSE 10 Vetue +
MM/u(8 sonnery table let 44.9356 . h~ Set 124
%{(,(), ,
2; Sees truj & &alet f orce ulnieus maaleue 2 2 60 465.222 j e~ 2 110 16.Orn mieu. g 8. tr.: 6 v .r2 t m e t< W Q,2
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' 2 109 24.2354 ,s i j go trug i siament3 s t atan 48 319.632 !
m *s tna 2 nietan 2 124 44 M356
- seem teus 8 Aalet f orse 60 465.N2 masina 2 8 t nian 2 00 16.0U2 leen trui 8 Shearl f orte 41 187.581 mestan 2
,; #laima 2 0 0.UlH i team traf I theer) fo'te 85.2766 M. mas tne 2 ili
ntan 2 45 $.085% o lean trwl 6 fortue 11T 26.0595 me.6nn 2 s tat *in i 11 4.303'2 team tro 8 manent! 110 88.2M2 y a s s ina 2 mininn 2 112 I T.04 U team truf a manents 4T 319.632
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9~ title a te0P 2 17.l* OlAuffit h -- tutsut let 6 a lit ttIatui LOAD $ + g4 etAm Int aa satas toal10m simotes titolhG ! Antat at m2 8L3
- I y* gga P v2 2.S.3118t*2 V3 2.244502t e l 4.15196M *0 6.22303M*0 3.1729MW2 StAssG el JA 0,0 2.8379Et 2 4.1853Mt*2 4 e
- 2. 843116t
- 2 2.244502t*1 8.11197M*0 1.0080311 1 4 JS 100.* 2.687890t
- 2 3.083 T3M
- 1 8.11196M
- 0 1.006031t*1 4.185314t*2 etAseG 46 JA 0.0 2.71824M*2 3.740304tal 3.083T3M *1 8.151970t*0 2.035074t*1 4.395392t*2
' . J8 100.0 2.71824M*2 3.T40304t*1 4.395392t*2 6tAsee 8.905 m tal 1. M T1$M
- t 8.15 t hM
- 0 2.035014t*1 47 sa 0.0 3.105 78M
- 2 1.033173t*1 4.T8238M*2
. Ja 100.0 3.1057S0t*2 4.905734tet
- MT1SM*1
. 8.151HM
- 0 3,294ket 2 4.42991M*1 4.25925 M
- 0 8.151968t*0 1.033173tel 4.T8236At*2 6tAseG 48 JA 0.0 1.31125M*1 4.483481t*2 JB 100.0 3.294MCtel 4.42991M*1 4.2$925M*0 8.111970E*0 3.34511M
- 2 4.570416t*1 1.112925t*0 9.111968t*0 1.3112584*1 4.483481t*2 StAmo O 49 JA 0.0 1,373457t*1 4.2104921*2 Ja 100.0 3.34111CE*2 4. 57081M
- t 1.112925t*0 8.15197x*0 10 JA 0.0 3.56192M.2 1.02662.I 2 1. 71948M
- 1 8.tli9t4t*0 1.3T3417t*1 4.21049M
- 2 atAsoc 2.61442M*l 3.$%272t*2 JB 100.0 3.161920t*2 1.0244248 2 1. T1968M
- 1 8.1$197M
- 0 6.355600t*2 9.420S31t*1 2.956109f *1 8.15196M*0 2.6M420t'l 3.5MIT2t*2 StA#eG
, 11 JA 0.0 JS 100.0 4.*15600t*2 9.420131t*1 2.956109E*1 8.1119fM
- 0 6.948145t*0 2.98TT88t* 2 l 4 6.948345t*0 2.98TT8M*! stA#ec t - 52 JA 0.0 4.M8A50t
- 2 1.835567t+2 T.875459t
- 0 0.11196M
- 0 4.Ma&S0tel 1.8855671 2 7.875459t*0 8. tS 197M *0 1.117401t*1 9.134323tet h 53 JA JS 100.0 0,0 5.400290t*2 T.40316M
- 1 1.6Ml92tal 1.011323t*1 1.11882Tt*1 4.011855t*2 MApeG
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- 1 4.41275M
- 2 Stase0
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- 2 9. 714 T39t
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. A- JB 100.0 6.064580t*2 5.M5079t e t 4.14961M *0 1.011320t*1 .
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- 1 2.952591t*2
, 59 JA 0.0 6.8089 fot
- 2 1.2988T0f*2 3.H3195t*1 1.011323t*t 2.69664Hel 2.952591t*2 StAreG
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60 JA 0.0 T.042020t*2 T.508728tet 6.036SMt*0 1.011323t*1 2.38Uttt 1 1.845978t*2 st Apoc " , JB 100.0 T 0420201 2 T.508T2St*1 6.014504t*0 1.011320t*1 1 k6 h2E*1 1.656a22t*2 103 JA 0.0 5.T5%&30t*2 9.311465t*1 3.19433M*1 1.65263N *1 3.1&2864t*1 1.410686t*2 stAsec JB 100.0 S . 75563M
- 2 9.351461t*1 3,194333t*1 1.612640t e t 1stuo44t*1 1.635368t*2 1M JA 0.0 5.54570t*2 1.10848t*2 3.523607t*1 1.65263M
- 1 3.9% % 4 *1 1.635368t*2 ofAmo ~
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$ 54570t *2 5.561 H M *2 1.108u8t*2 3.523607t*1 1.65240t *1 1.1003&St*2 3.433285t*1 1.65263M *1 2.271159t*1 2.275159t*1 1.095265t*2 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 - -
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