ML20086E089

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Shroud Head Contact on Upper Support
ML20086E089
Person / Time
Site: Quad Cities  Constellation icon.png
Issue date: 07/03/1995
From: Behringer T, Deboo G
COMMONWEALTH EDISON CO.
To:
Shared Package
ML20086E084 List:
References
9389-64-DQ, 9389-64-DQ-R, 9389-64-DQ-R00, NUDOCS 9507110193
Download: ML20086E089 (16)
v • d • e


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COMMONWEALTH EDISON COMPANY

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, CALCULATION No. 9389 64-DQ PROJECT No. 9647-006 PACE No.14.1 j

REVISION No. O Quad Cities Unit 2 Shroud Head contact on Upper Support Safety Reisted 4

PREPARiED BY T. J. Behringer DATE: 7/r/g R

BY A.DeBoo DATE:

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1. Purooes and Ohiocuve i.

During the installation of the shroud head and separator assembly at Quad Cities j

Unit 2, two of the lifting rod extensions contacted two of the long upper supports i-that are part of the shroud modification hardware..An initial evaluation was j

performed (Reference _4) demonstrating that no damage of the hardware occurred, i.

A subsequent evaluation was performed (Reference 1) based on utilizing the 3

original design basis finite' element analysis (FEA) of the long upper support (LUS).

j The purpose of this calculation is to verify that the critical stresses calculated -

i based on interpolation of the results from the onginal design' basis analysis are i

representative of the a'ctual support configurabon, during the contact loading i

condition. This calculation also demoristrates that the critical stresses are less

]

than the ASME stress limits, and thus no damage or yielding of the LUS could l

have occurred as a result of the shroud head assembly contact.

l 1

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2. Methodoloav and Acceptance Criteria l

The original design basis analysis (Reference 5) was based on the bounding l-normal / upset loading conditions (P, =711,900 lbs. and P,= 102,500 lbs.) with j

conservative boundary support conditions (see Figure 1). This " revised analysis" l-(Referencesi 2 and 3) is based on the same finite element model (FEM) dith some modifications to simulate the actual conditions associated with the contact loading of the LUS. The specific details of the modeling changes are defined in section 6 i

of this calculation. The acceptance criteria for this calculation are the same limits l

as defined in Reference 1. Also included is a comparison of the critical section stresses from the top contact loading FEA versus the results of the analogous j-original design basis FEA (References 1 and 5). The results shown are based on j

an interpolation of an analysis performed for a Py = 102.5 K!ps. All results have been multiplied by 81.43/102.5 = 0.794 to obtain the equivalent results for an applied load of P = 81.43 Kips (Reference 1, page 13.2).

l 4 Assumptions f

There are no major assumptions that require verification, all key design inputs and assumptions are based on approved references or standard engineering practice.

Minor assumptions related to specific items are noted in the calculation.

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. CALCULATICN No. 9389 64-0Q PRCJECT No. 9647-008 PAGE No.14.2 REVISION No. 0 Quad Cuss Unit 2 Shroud Head Contact on Upper Support Safety Related 5

j PftEPARED BY T. J. Behringer DATE: 7/y/g REV1 D BY G. DeBoo DATE:

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4. Desian input Parameters 1.

Weight of shroud head and separator assembly = 141.9 Kips (dry weight, Reference 4) 2.

Buoyant weight of the shroud head and separator assembly = 141.9 x 0.9 =

127.71 Kips (Submerged weight, Reference 8, page 14) 3.

S,,, of X-750 at room temperature = 50,900 psi. (Reference 9) 4.

S, of X-750 at room temperature = 102,300 psi. (Reference 9) 5.

S, of X-750 at room temperature = 152,800 psi. (Reference 9) 6.

Preload on the 11e Rod = 14,400 / 0.9 = 16,000 lbs. (Reference 10, page 8),

neglecting the effect of any preload relaxation 7.

Impact Factor for the QC Reactor Building 125 Ton Crane = 1.15 (References 11& 12)

5. References 1.

Calculation No. 9389-64-DQ, Section 13, Rev. O.

2.

ANYSIS Output RUNID BKT12RFS.OUT Dated 7/1/95 (Case 4) 3.

ANYSIS Input RUNID BKT12RFS.INP Dated 7/1/95 (Case 4) 4.

GENE-771-111-0605, Rev. O, " Shroud Head Contact on Upper Support",

DRF# B13-01740, ohne 15,1995 5.

GENE-771-68-1094, Revision 4, " Shroud and Shroud Repair Hardhare Stress Analysis - Shroud Repair for H1 through H7 Welds for Comed Quad Cities Stations Units 1 & 2.

6.

GENE-771-70-1094, Revision 3, " Backup Calculations of Shroud and Shroud Repair Hanfware Stress Analysis for Comed Quad Cities Stations Units 1 & 2.

7.

ASME Section lit, Subsection NG,1989 Edition, NG-3200.

8.

GENE-771-69-1094, Revision 1, " Backup Calculations for Shroud and Shroud Repair Shroud Stress Report for Comed Quad Cities Stations Units 1&2 9.

GE DRF-B13-01740, Section N, "CMTR's for X-750".

10. GENE-771-68-1094, Supplement A to Revision 4, " Supplement A to Shroud and Shroud RepairHardware Stress Analysis", DRF B13-01740, April 1995.

i

11. June 29,1995, S. Eldridge - Determination of impact Factor for QC Reactor Building Crane.
12. Whiting Crane Handbook, Whiting Corporation,1979.

COMMUNWEALTH EDISBN COMPANY CALCULATION No. 9389 64-DQ PROJECT No. 9647-008 PA2E No.14.3 REVISION No. 0 Quad Cities Unit 2 Shroud Head Contact on Upper Supporf Safety Related P.REPARED BY T. J. Behringer DATE:

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6. Calculation j

The ' original design basis analysis model included the applied vertical (Y axis) and horizontal (X axis) loads as illustrated in Figure 1. The element restraint conditions for this original model are also illustrated in this figure. The revised 3

analysis model (References 2 & 3) incorporates several changes to represent the specific loading and restraint conditions associated with the actual contact loading condition (see Figure 2). The key differences are that the honzontal seismic loads 2

(X axis) were deleted as they were not present during the contact loading event.

The vertical load was relocated from the bottom of the LUS (original design basis load application point) to the top of the LUS (shroud separator assembly load i

contact point). The nadal restraint changes consisted'of the addition of horizontal (X axis) restraints at the nodes representing the upper contact surface with the shroud (nodes 709,710,711,712,673,674,675,676 see Attachment A). The addition j

of these restraints resulted in a tension / compression form couple (moment resistance) at the nodes in the upper inclined support point (Y axis, nodes 745-748, 729, 733, 734, 735, 693 and 697-699 ) as well as the upper horizontal contact i

surface with the shroud (X axis). Since these supports are actually compression l-only (one directional) restraints any nodes that had a resultant tension were l

released and the analysis was rerun until the final solution (compression reactions l

only) was obtained. The nodes that were released are as follows:

Top Horz. Restraint Surface 693,697,698,699 Outside row i

729,733,734,735 Middle row Top Vert. Restraint Surface 709,710,711,712 Upper row i

in the final analysis case (References 2 and 3) compression was eventually I

obtained in the last row of elements (see Figure 2, nodes 745-748 and 673-676).

l The stresses in the lower section of the LUS were substantially reduced as there was no horizontal seismic load and the stresses at the critical cross section are i

less than what was obtained using the original design basis analysis and loading conditions. Summarized below is a comparison of the element reactions and the critical section stresses for the original condition and the rowsed analysis condition.

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COMMUNWEALTH EDISON COMPANY CALCULATION No. 938944-DQ PROJECT No. 9647-008 PACE No.14.4 REVISION No. O Quad Cities Unit 2 Shroud Head Contact on Upper Support' Safety Related

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PREPAR'ED BY T. J. Be nger DATE:

REVIEWED BY G. DeBoo DATE:

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76ffg Table 1 Summary of Critical Section Stress Results (Py = 81.43 Kips)

Stress Combination Design Basis FEA Revised FEA Model ASME Section ill-NG j

Model Stress Stress Results (Psi.)

Stress Limits (Psi.)

Results (Psi.)

P,,,

25,057 22,467 50,900 P,

13,871 16,262 N/A i

O 7,247-2,592 N/A

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l P,,,+ P, 36,695 37,498 76,350 li P,,, + P, + Q 40,342 37,831 152,700 l

i Table 2 Summary of Element Reactions (Py = 81.43 Kips) t i

Support Location Node Numbers Design Basis FEA Revised FEA Model

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Model Reaction (Lbs.)

Reaction (Lbs.)

Upper Horz. & Vert.

745,746,747,748 Rx = 15,657 Rx = 15,654 Restraint (Bottom Ry = 81,430 Ry = 81,430 l

Horz. Inclined Surface of LUS)

Upper Horz.

673,674,675,676 No Reaction as these Rx = -5426 Restraint (Upper nodes were load Vert. Shroud Contact application points Surface of LUS) l Lower Horz.

161,174,182,184, Rx = -6198 Rx = -10,228 l

Restraint (Lower 189,198,203,204, Vert. Shroud Contact 217,226,231,232 Surface of LUS) 4

COMMUNWEALTH EDISON COMPANY CALCULA11bN No. 9389-64-OQ PROJECT No, 9647-008 PA2E No.14.5 REVISION No. O Quad Cities Unit 2 Shroud Head contact on Upper Support.' Safety Related N

PREPARED BY T. J. Behringer DATE:

REVIEWED BY G. DeBoo DATE:

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s Figure 1 - Quad Cities UNIT 2 Shroud Long Upper Support - Free i

Body Diagram Of Design Basis Finite Element Analysis Reactions And Applied Loads

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.CALCuLAT12N No. 9389840Q PROJECT No, 9847-008 PACE No.14.6 s.

REVislON No. O Quad Chios Unit 2 Shroud Head Contact on Upper Support ' Safety Related 1',

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Figure 2 - Quad Cities Unit 2 Shroud Head Assembly Contact On Long Upper Support - Free Body Diagram Of Revised Finite Element Analysis Reactions And Applied Loads f

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.CALCULATlaN No. 9389-64-DQ PROJECT No. 9647-008 PASE No.14.7

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REVISION No. 0 Quad Cluas Unit 2 Shroud Head Contact on Upper Support-Safety Related PREPARED BY T. J. Behripger DATE:

REVIEWED BY G. DeBoo DATE:

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7. Summary of Results. Conclusions and Recommendations The conclusion of the original evaluation (Reference 4), though based on a simplistic approach remains valid. The methodology, results and conclusions as identified in Reference 1 are a reasonable approximation of the actual condition as the results of this evaluation are very similar to the more refined analysis results presented in this calculation. The maximum stress results as provided in Table 1 for the " Revised FEA Model" are well below the ASME stress limits as well as the yield strength S, = 102,300 psi. Based on these results it can be concluded that no damage of the long upper support would have occurred from the contact loading and therefore the hardware remains adequate to perform its original design function.- See Attachment B for the output listing of the nodal reactions and critical section stresses.
8. Attachments A.

Attachment A, Long Upper Support, FEA node number plots B. Attachment B, Reactions and maximum stresses from the FEA output (Reference 2). \\ t l i 1

3. COMMONWEALTH EDISON COMPANY CALCULATION No. 938944-DQ PROJECT No. 9647-008~. PAGE No.14.A.1 REVISION No. O Quad Cities Unit 2 Shroud Head Contact on Upper Support Safety Related PREPARED BY T. J. Behringer DATE: REVIEWED BY G. DeBoo DATE: TA YS sb wr r]G'av~7)* 7/%C a a Attachment A - Lona Upper Support Node Numbers Upper Attachment Point I I I le9Y V V WM 7oa 74T 7o3 hs - M7 W 709 ,54 88 "IG I / Mi "Il0 79g 782-735 gy b Tl 744 479 7% (o15 w7 m

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j i COMMONWEALTH EDISON COMPANY CALCULAU::N Ns. 938644-DQ PROJECT No. 9647-008 PACE No.14.A.2 REVISION No. O Quad Cities Unit 2 Shroud Head Contact on Upper Support"- Safety Related 1 PREPARED BY T. J. Beh inger DATE: REVIEWED BY G.DeSoo DATEj/W' f i Mu'w %4r }n V2Ge;% 7/2 f v 1 i j Attachment A - Lona Upper Support Node Numbers lmuer Section 1 t i l 4 1 i 1 l

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k / COMMUNWEALTH EDISON C(MPANY CALCULATION ND. 938944-DQ PROJECT No. 9847 418 ' PAGE No.14.A.3 i s j REVISION No. 0 Quad Cities Unit 2 Shroud Head Cented on Upper Support' Safety Reisted 1 PREPARED BY T. J. BehnnDer DATE: REVEWED G. DeBoo DATE: 'rA Mau 7AAr gy_ yf2)& 7/3/3 s' i V ~ y !j Attachment A - Lona Unoer SuDDort Node Nu@= Lower Sectkm i i 37 i l j 13 1 i es i i l 85 l l 42 i } 4 l $? N.g 14 2 its e i q 7s ~ ns j Q 'T .C,4 E i Quad Cities Shroud Repair -- long upper support -- bbkt-6 l i

COMBIONWEALTH EDISON COMPANY CALCULATION No. 9389 64-0Q PRDJECT No. 9647-008 ' PA2E No. 14A4 i j REVISION No. O Quad Cities Unit 2 Shroud Head Contact on Upper Support-Safety Related \\ PREPARED BY T. J. Behringer DATE: REVIEVyED BY G. DeBoo DATE: ? Tf M W. fren U. % yk-7fTbf 1 f u i l Attachment A - Long Upper Support Node Numbers Lower Sectkm i 1 1 w wn -= i 1 1 1 24 6 1 1 .i 1 14 213 i l 1ss si l 157 r i Y,! .[. as-1, ,= _ W ~ 21 g4(, q j 'g '._ p-BS

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COIMONW$ALTH EDISHN COMPANY CALCULATbN No. 938544 OQ PROJECT No. 9647-008 PA'lE No.14.A.5 REVISION No. O Quad CNes Unit 2 Shroud Head Contact on Upper Supporti Safety Related 1 PREPARED BY T. J. DATE: ' REVIEWED BY G. DeBoo DATE:bi 7l 8 f }rix ( 0 #En W3 TM ' ~ Q ' ~ u i Attachment A - Long Upper Support Node Numbers Upper Contact Point 1 8 6 i 2 .s...,, 376 l ) s 960 1 f - #; $67 Np-- O';g Q. %g =W 2 n um: hkh,h? a %c M d: s., i y q m = m q o i q= %g = l m Quad Cities Shrokr -- longu%er suQk-bbkNk se i i 4 0 w ,yw---- w w emv--,-m-wy-w -g-~<-.----g,e----,---p --avv -.-w aypp--w myw. w-we- -,

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( COMMONWEALTH EDISON COMPANY CALCULATION No. 935 64-DQ ' PROJECT No. 9647-008 PAGE No.14.8.1 j REVI8 ION No. 0 Quad Chios Unit 2 Shroud Head Contact on Upper Support ' Safety Reisted PREPARED BY T. J. B DATE: REVIEWED BY G. DeBoo DATE.fr YMr

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i u Attachment B - Loan Unoer Support Nodal Reactions For Revised FEA Model 1 I i bkt12rfs.out NODAL FORCES STOREDREt SELEMNTS REACTK)NS STORED FOR 2NEllCHOPS 1 FOR LOAD STEP = 1 ITERATIN= 1 SECTION= 1 j TNE. 000000E+00 LOWCASE-1 TITLE = Quod Citas ShroudReper-long igper esport - bbkt-12 ) PRINT REACTK)N FORCES 79tPGE j 1 ANSYS. ENGNBIBIGAPMLYSIS SYSTEM REVIS10N 44 A137 38339. NETWORK MAY1,1990 ANSYS(R) COPYRIGilp)1971,1978,1982.1983.1985,157,195.1990 SWANSON ANALYSIS SYSTEMS. INC AS UNPUBUSHED WORK. 1 PROPRIETARY DATA.talAUTHORIZED USE, DISTRIBUTK)N OR DUPUCAflON IS PROHIBITED. ALL RIGHTS RESERVED } FOR SUPPORT CALL SLNutt MERSON PHONE SUPPORT PHONE TWX SUPPORT FAX Qad Cites Shroud Reper-hug spur separt - bbkt-12 206736 JUL 1,1995CP= 960 " POST 1 REACTIMEEELETDIG- ,1 LOAD STEP 1 ITERATlalk 1 SECTION= 1 TIME- 00000E+00 'LOWCA!E= 1 TE FOLLOWING X,Y.Z FGEIS AE N G.0BAL COORDINATES N00E FX FY FZ 1 nnnnnnnnr.00 m. m a 161 9525.6110 (IMEIE 00 nannnnnnF+00 174 20474 338 .N AIIIIIIE+00 182 21240.210 . N HEIRIIE+00 184 9378.1771 A m R EIIIlOE+00 180 194 16883 00 M AIIIIlODE+00 198 134 40985 .nnmunanr+00.lE RIDODE+00 210 226 90813 enemmanF 00 AEXIIIE+00 204 324 82996 .N ARIDtIlOE+00 217 11491 070 m asennnnnr+00 226 -25422.48g .anummes.W AIEllutE+00 231 -252E3774 00 m samanonr+00 232 11298.356 _ ON AllIlOOODE+00 673 1286.4686 .namummar+00 AIlOOIIlOE+00 674 -2171 2817 ,N (IIIIIIl0E+00 675 2151 2886 .nnummes.80 nnnnnnnnr+00 676 1240.9800. _ nnannes.g.nnnnnrw.00 745 3292.6977 17t1988 A BOODIE+00 746 8500 8306 340t114 nnnnnnnrL OO 747 8580 8020 34t3M AIIIIlODE+00 748 3292.7057 17125 E annertmnr+00 TOTAL.3668446BEM M 2 M 894E 4

l 1 i COMMONWEALTH EDISON COMPANY i CALCULATION No. 9389 64-DQ PROJECT No. 9647-008 PAGE No.14.B.2 REVISION No. 0 Quad Chios Unit 2 Shroud Head Contact on Upper Support Safety Related PREPARED BY T. J. Bep DATE: REVIEWEDAY G. DATE: Tf. WM 1VtJ'~

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7/N5 o Attachment B - Imo Unoer SW Crhl Se% Stresses For Revised FEA Model Y bkt12rfs.out PRINT UNEARIZED STlWWRulDI A SECTION, NSOE NODE = 14 OUTSE N00E = 770 1 ANSYS ENWEERING APMLYSE SYSTEM REYtSON 4 4 A137 3833 NETWORK MAY1,1990 ANSYS(R) COPYMMflC)1971,1978,1982.1983.1985,1987,1989.1990 SWANSON ANALYSIS SYSTEMS, NC AS UNPUBLISHED WORK PROPRETARY DATA-LNAUTHORIZED USE, DISTREUTON OR DUPLICATION IS PROHEITED. ALL RGHTS RESERVED. FOR SUPPORT CALLERMTITRSON PH0fE SUPPORT PHONE TWX SUPPORT FAX Ouad Cnies Shroud Aquer-leigisprapport-12kt-12 20.6736 JUL 1.1995CP= 1.020 - POSTI LSEMEZED STIEBS USTING-NSOE N00E = 75 OUTSEE NODE =. 770 LOAD STEP 1 ITERADON= 1 ECTIOS 1 TIME =.00000E 4 toad CASE.1 I THE F,OLLOWNG X,Y25NEEEENE N G.0BAL COORDINATES. " MEMBRANE " SX SY SZ SXY SYZ SXZ 4 i 4963 2038E.05 2BL 8167. BIO 2 708 9 j SIG1 SG2 SaGB B SE j 6411. -2167. N 2E4.2511E.05 i " BENDNG" WEDEC= CENTER 0=0UTSOE SX SY SZ SXY SYZ SXZ l 1 5885. .142E4 elo 52 487.5 995 6 C 003)E+00 000E4 AIRE 4 EIEE+00.El0tE+00.0000E+00 i 0 5085. .142E4 315 M2 487.5 55.6 j SIG1 SG. SD S._8E t I 6147. 1020. 14EE4 347E4N179BE+05 C 0000E+00 00054 ERE4 EBOE+00 0000E4-j 0.1432E+05 103L 4147. 20E4.17HEa " hEMBRAPERIS EMIBEB" hoEDE C= CENTER SOUTSOE SX SY E BlY SYZ SXZ L i 1005E+05 3467E4 -Est. 2 88. 1438. 1704 i C 4053. l! .2030E4 23RL SIST. 050.2 70BA 0 1021. 4 100. 13 3. 8F87 42.7 38.7 SIG1 SIG2 SEI 5 SE i.tir7Ea -3m 3GE 05 #20E+O 417BE+M C 6411. 2167. 21BPE4 2E4 2511E+05 0 3716. 1354 1EIE4.141E4.1275E 05 j " PEAK" l=MEfXlENTEROGUTSOE SX SY SZ WY SYZ SXZ 1 2054 1026. Elf.8 -441.1 3131 115J5 i C 2056. 1033 -227.4 4401 3152 315 1 0 -2050 1339 227A -440.6 Il73 3147

~ COMMONWEALTH EDISON COMPANY CALCULA110N No. 938964DQ ' PROJECT No. 9647-008 PAGE No.14.B.3 REVISION No. O Quad C5ss Unit 2 Shroud Head Contact on ' Upper Support ' Safety Related PREPARED BY T J. Bearinger DATE: REVIEW $D BY/)w,00.%.DeBoo& 7/$lkS G. DATE: TCSI S .W3l1f~ s v Attachment B - Lana UDoor SuDDort Critical Section Stresses For Revised FEA Model bkt12rfs.out SIG1 SIG2 SIG3 5 SE I 1088. 269 0 2151 3M 2R24 C 2160 -209 3 -1154. 3E 2B30 0 1100 25 5 21st @ 2937. " TOTAL" 19EE C4NTER O OUTSOE SX SY SZ SXr SYZ SXZ l 8894. 3364E+05 3 4. 5127. 1404 2020. C 70m 21E+05 2M 8808. 983 7 393 8 O 3000. 5061. -E2. EDE. -429.0 27.96 SIG1 SIG2 SIGS 5 NGE. TEMP 1.1159E+05 3185. -RIE4Q252E+051.G7E+05 0000E+00 C.1117E 05 -2383. -JBE4 E9E;05 3231E-05 0 2502. 1102. ' -1EE4.t313E+05.1178E+05 0000E+00 PRINT UNEARIZED STMES TWERGI A SECTION I J INSEE N00E = 15 GliSOE NODE = 189 1 ANSYS ENGINEBMG AllALYSIS SYSTEM REVISION 4 4 A137 38339 NETWORK MAY 1,1990 [ ANSYS(R) COPYRIGHIlC)19ft.1978.1982.1983.1985.1987,1989,1990 SWANSON ANALYSIS SYSTEMS, INC AS UNPUBUSHED WORK PROPRIETARY DATA LatAUTimlZED UFE. DISTRIBUTION OR DUPLICATION IS PROHIBITED. ALL RIGHTS RESERVED 2 FOR SUPPORT CALLSl#REIPERSON PHONE SUPPORT PHONE TWX SUPPORT FAX 1 Ouad Cibes Shroud Raper-lag gpar mapsi-t6kt-12 20 6736.IUL 1,1995 CP= 1 110 POSTI LNi4RIZEDSTRESS USTING ~ INSDE N00E = 15 GJTSIDE NODE = 189 LCMD STEP 1 ITERATDe= 1 SECTION= 1 l TIME =.00000E+00 1o40 ORE =1 THE FOLLOWING X.Y,ZSTEEEES ARE IN GLOBAL COORDINATES. i " hEEMifWE" 4 i SX SV SZ Sur SYZ SXZ 611.4 -4143 34 5 BL -WF2 3 800 SIG1 SIG2 SWE E SIDE { 124 38.07 25E 4G8. 3 88. " BENDING" l=8eEEC= CENTER O OUTSOE SX SY SZ ERY SYZ SXZ l 645 3 1567. 5LE IK 561.8 4459 C 03X)E 00 0000E.00 03E+0D.0000E.00.0000E+00 0000E 00 0 4453 1567. 41.19 438. -561.8 34 50 SIG1 SIG2 SKB 5 SIGE t 3270. 80.23 -4lI21. T3f. ED1. C 0000E 00 0000E4 EM-00.0000E+00 0000E+00 0 4021. 4023 4DO. T291. 6331

e 4 COMMONWEALTH EDISON COMPANY \\ l CALCULdTION No. 9388 64-DQ ' PROJECT Noi 9647-008 PAGE No.14.B.4 REVISION No. 0 Quad Cities Unit 2 Shroud Head Contact on Upper Support Safety Related _ PREPARED BY T. J. Bp=ku; 7/VtC m (3. AM)% 'T/3/9S~ er DATE: REVI D BY G. DeBoo DATE: 'K!AL v - Lona Upper Support Crtlical Section Stresses For Revised FEA Model i bid 12rfs out l - MEMBRANE Pt.US BENDING" l=N50E C= CENTER O 0UTSOE SX SY SZ SXY SYZ SXZ l 2ILS -1572. 16.60 1185. 374 5 3829 C 411.4 4 143 34 60 -2211. -187.2 4.899 0 -1457. 1510. 45.79 5807. -740 30.89 3G1 SIG2 SIG3 St SE I 8423 50.31 2214. 3057. 27 4 C B4 38.07 -2546. 4479. 3808. 0 SE22. -115.8 4786. ,1171E 4.1014E 4 " PEAK" l=lNSOE C= CENTER O OUTSOE 4 i E SY SZ SXY SYZ SXZ i I 154 513.8 149 -708.3 -453 33.59 i C.22.76 J16.6 - 113 0 378.9 218 7822 O 4 17.6 1989. 98.73 -451.3 1016. 4401 3 01 SIG2 - SIG3 SI SE i 13 5. 119.1. 4146 1723. 1500. C 1712 1351 547 1108. 1089. f 0 2en 44B8 830.5 3283. 3071. " TOTAL" !alNSIDE C= CENTER 0 0UTSOE SX SY SZ SXY SYZ SXZ l E.3 10E 1ES 476.5 48.39 -4 899 C 441 J20.7 78 38 1832. 31.56 4192 o -2174. 3552. 184 5 4 058. 1785. 33.12 3G1 SIG2 SG St SE TEMP j i 31.1 167.9 1267. 1858. 180. .0000E+00 C 1277. EOB 2813. 3890. 3488. O 838. 294.8 4700. .14E9E+05.1307E 4.0000E+00 ABFEN00lMERED ON FILE 18 4 PROELEM TERMINATED BY ltelCATED ERROR (S) OR BY END OF INPUT DATA - "RLNCOMPLETED CP= 11100 TIME 206736 i ) e i ,,,,.y ..r_., y._, .. w.. m_.,,, ,,.,}}

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