ML20151U990
| ML20151U990 | |
| Person / Time | |
|---|---|
| Site: | Oyster Creek |
| Issue date: | 04/30/1988 |
| From: | CBI SERVICES, INC. (FORMERLY CHICAGO BRIDGE & IRON |
| To: | |
| Shared Package | |
| ML20151U944 | List: |
| References | |
| NUDOCS 8805020230 | |
| Download: ML20151U990 (102) | |
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L UPPER DRYWELL.
ANALYSIS
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Oyster Creek Nuclear Generating Station !
GPU Nuclear Corporation !
Parsippany, New Jersey esoso2o2so eso42s 7 Prepared By.
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Oak Brook, Illinois April,1988 Q
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UPPER DRYWELL ANALYSIS
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OYSTER CREEK NUCLEAR GENERATING STATION GPU NUCLEAR CORPORATION PARSIPPANY, NEW' JERSEY
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CBI Services, Inc.
Oak Brook, Illinois
]{ SUBJECT OFFICE April, 1988 REFEPENCE NO.
l 0YSTER CREEK NUCLEAR GENERATING O .0AK BROOK REVISION / 871135 STATION UPPER DRYWELL ANALYSIS MADE BY l VERIFIED BY MADE BY VERIFIED BY p CORRODED SHELL T/A D r?/4 y,/A O/Pg SHT_ OF L DATE DATE DATE DATE
'l2t/ss 1N/97 9 /83 'I/W/P l
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L Table of Contents Description Page No. Rev. No.
Section 1 - Introduction Cover Sheet 1.0 0 Introduction 1.1 1
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Introduction (continued) 1.2 0 Section 2 - Design Inputs Cover Sheet 2.0 0 Description of Applicable Load Case 2.1 0 Description of Thermal Gradients 2.2 0 l Acceptance Criteria 2.3 0 Acceptance Criteria (continued) 2.4 0 Section 3 - Analysis Technique Cover Sheet 3. 0 , O Analysis Technique and Computer Model 3.1 0 Upper Drywell Computer Model 3.2 0 Section 4 - Design Outputs Cover Sheet 4.0 0 Design Output - Description 4.1 0 Stress Plot - Membrane /Circumferential 4.2 0 Stress Plot - Membrane / Meridional 4.3 0 Stress Plot - Inside Surface /Circunferential 4.4 0 Stress Plot - Inside Surface /Meridiona. 4.5 0 Stress Plot - Outside Surface /Circumferential 4.6 0 Stress Plot - Outside Surface / Meridional 4.7 0 Section S - Evaluations and Conclusions Cover Sheet 5.0 0 0
Evaluation of General Membrane Results 5.1 1 Evaluation of Local Membrane Results 5.2-5.3 1
{ e Evaluation of Surface Results 5.4-5.5 1 Evaluation of Stiffener Attachment Welds 5.6 1 Discussion of Stress Evaluation 5.7-5.8 1 Conclusion 5.9 0 f
SUBJECT OFFICE REFERENCE NO.
+ OYSTER CREEK NUCLEAR GENERATING O OAK BROOK REWSION / 871135 STATION UPPER DRYWELL ANALYSIS MADE BY VERIFIED BY MADE BY VERIFIED BY TOC-/
~
CORRODED SHELL 7"JA ppH 73A % )4 SHT_ OF_
_- DATE DATE pATE DATE WloS 2/s/S2 4/C/80 t//7/f?
4 Pnnled in USA ,
GO 64 A AUG 87
Description Page No. Rev. No.
Section 6 - List of References Cover Sheet 6.0 0 References ,
6.1 0-1 f
Appendix A - Computer Input and Output for Drywell Shell A-0 All and Computer Program E0781A Description thru Rev.
I A-66 0 l
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SUBJECT OFFICE REFERENCE NO.
L OYSTER CREEK NUCLEAR GENERATING O OAK BROOK REVISION O 871135 STATION UPPER DRWELL ANALYSIS MADE BY VERIFIED BY MADE BY VERIFIED BY pc.{
r CORRODED SHELL 7/~A py>H SHT_ OF _
_ , p AJ E DATE DATE DATE
'/4/a8 1/WST Owed 19 USA GQ 644 AUG 47 r
4 SECTION 1
) INTRODUCTION i
SUBJECT OFFICE REFERENCE NO.
O .0AK BROOK REVISION O 871135 OYSTER CREEK NUCLEAR GENERATING.
MADE BY VERIFIED BY MADE BY VERIFIED BY /, o STATION UPPER DRYWELL ANALYSIS D/PH SHT OF _
T/A CORRODED SHELL D$TE DATE DATE DATE
~=
'/D/BS 2/3/88 ne w usa c,o m . o .,
Introduction The Oyster Creek Nuclear Generating Station utilizes a General Electric BWR NSSS end a steel Mark I pressure suppression type containment vessel system. The drywell part of the system is shaped,like an inverted light bulb.in which the spherical portion is 70 feet in diameter and the neck is 33 feet in diameter.
The spherical shell is embedded in a concrete base slab at a point 36' above the invert. A sand transition pocket subtends an arc of about 60". This sand
-pocket provides a transition which diminishes the severity of the abrupt thermal and mechanical discontinuities. The 33 foot diameter cylindrical portion includes a removable head which is attached by use of 96-2 1/2 inch diameter bolts. The cylinder is about 23 feet long.
A recent ultrasonic inspection of the upper drywell shell at elevation 87'-5" showed localized evidence of thickness reduction below the .64" design thickness. Subsequent core samples taken showed the local degradation to be due to corrosion. This report' provides an axisymmetric analysis of the upper drywell cylinder assuming a uniformly reduced thickness of .59". This thickness (
was arbitrarily defined for the purpose of a conservative analysis, while the minimum average reading of local thinned areas was .619". The work is performed under authorization of General Public Utilities Nuclear Purchase Order No.
PC-049122. Change Order No. 6 describes the work scope and, for purposes of this report, constitutes the project specification.
SU BJ E'CT OFFICE REFERENCE NO.
0YSTER CREEK NUCLEAR GENERATING O _QS BROOK REVISION / 871135 STATION UPPER DRYWELL ANALYSIS MADE BY VERIFIED BY MADE BY VERIFIED BY S HT_/, fOF_
CORRODED SHELL TJA O n l4 TJA ORij DATE i DATE DATE DATE
%iles ! zws2 4/slaa 67Mr
%.o ia usa **^^*"
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.This portion of'the report consists of an engineering assessment of the corroded configuration for the maximum design pressure loadipg condition' described in the referenced purchase order for this project.
SUBJECT OFFICE REFERENCE NO.
OYSTER CREEK NUCLEAR GENERATING REVISION O 871135 8 OAK BROOK STATION UPPER DRWELL ANALYSIS MADE BY VERIFIED BY MADE BY VERIFIED BY f,2 CORRODED SHELL 7g4 pgp SHT _ OF _
pAJE DATE DATE DATE 4/4/bb y/7/79 Pinted in US A GO 64 A AUG 87
i SECTION 2 DESIGN INPtTIS I
i OFFICE REFERENCE NO.
SUBJECT REVISION O 8.0AKBROOK 871135 OYSTER CREEK NUCLEAR GENERATING, HADE BY VERIFIED BY MADE BY VERIFIED BY 2.0 STATION UPPER DRYWELL ANALYSIS YJA sui _ OF_
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Cl?H DATE DATE DATE DATE CORRODED SHELL
'/2//aa 2/3/29 e,o m . .,
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l Description of Applicable Load Case The project ' specification consisting of GPUN Purchase Order No. PC-049122, Change- Order No. 6 describes the applicable load case to be the accident condition with 62 psig internal-pressure and an internal temperature of 175*F.
A previous study performed by CBI indicated that this loading case produced the 4
maximum circumferential stress in the upper cylindrical portion of the drywell.
(Refer to ref. 1 page 8.28) Since the corrosion is present in the region which
^
has a capacity margin factor of 1.00, a more refined analysis of this region is warranted.
In addition to the internal pressure and temperatures previously identified, the following loads are considered.
- 1. Gravity load from internal platforms and equipment supports.
- 2. Gravity load of compressible material.
- 3. Gravity leads on welding pads.
- 4. Seismic loads - OBE (.11g h/.05g V)
- 5. Reactor building displacements at the dryvell interface including an allowance for the interface gap .
OBE = .0390 inches SSE = .0680 inches SUBJECT OFFICE REFERENCE NO.
0YSTER CREEK NUCLEAR GENERATING REVISION O 871135 O OAK BROOK STATION UPPER DRYWELL ANALYSIS M ADE BY VERIFIED BY MADE BY VERIFIED BY 2, CORRODED SHELL /~./4 Og/g SHT _/OF_
DATE DATE DATE DATE
'/Li/aa 2/3/ ?2 am.co usa oc o. n o
The region under investigation included the region of the seismic ties. The offect of the earthquake is considered to be minimal in the region in question. .
The circumferential stress has been identified as the critical stress component.
It can be shown that the earthquake loads do not affect the circumferential stresses in the cylindrical portion of the drywell.
t Verious vertical dead loads, vertical and horizontal earthquake loads and.
displacement loads may have some effect on the vertical stresses, but will have virtually no effect 'on the circumferential stresses. It is, therefore, considered conservative to analyze the vessel for only the internal pressure of 62 psig for this project.
Description of Thermal Gradients The 175 F internal temperature vill have a minimal effect on the upper cylindrical portion of the drywell. The previously referenced CBI study (ref. 1) shows that the stresses in the sand transition zone are influenced only slightly by the presence of this temperature gradient. This effect is limited to the region near the embedment zone. There is no effect of this gradient in
- the upper drywell cylinder. For purposes of this study, the thermal gradient may be assumed to be negible.
l l
OYS CREEK NUCLEAR GENERATING g OAK B b K REVISION O STATION UPPER DRYWELL ANALYSIS MADE BY VERIFIED BY MADE BY VERIFIED BY g,g CORRODED SHELL 774 pgy SHT_ 0F _
DATE DATE DATE DATE Y21l88 .1/ 3 /8 Y 00 64 A AUG 47 Preted M USA
- s Acceptance Criteria The following table is a description of the acceptance criteria applicable to tensile and compressive stress allowables for the applicable load"case.
Allowable Stresses * '
Primary Stresses (does not include thermal effects)
Allowable Stresses Ref.
General Membrane 1.1 x 17500 = 19250 psi 1272N-5 5(g)(1)
Local Membrane ** 1.5 x 1.1 x 17500 = 28875 psi NE-3221.2 Local Membrane 1.5 x 1.1 x 17500 = 28875 psi 1272N-5
+ bending 5(g)(2)
Secondary Stresses (includes thermal effects)
Surface Stresses (P1+Pb + Q) = 3.0 x 17500= 52500 psi 1272N-5 ,
5.(f)
Surface Stress *** 3.0 x 23300 = 70000 Table NE-3217-1 1
!
- All actual stresses are either stess intensities per NE 3000 or unidirectional stresses per ASME VIII, and Code Case 1272N-5, whichever is greater.
- A local primary membrane stress is defined as one which i does not exceed 1.1 x 1.1 x 17500 = 21175 psi for a distance greater than 1.0 4 rt ~ Ref. NE 3213.10. The distance over which the' local membrane stress may exceed the general primary membrane stress allowable value is not explicitly defined in
' the ASME Code. Good engineering judgment should be used in determining whether configurations with stress patterns thus described are structurally sound.
- If bending moment at the edge is required to maintain the bending stress in the middle to acceptable limits, the edge moment is classified as P .b Otherwise it is classified as Q.
SUBJECT OFFICE REFERENCE NO.
OYSTER CREEK NUCLEAR GENERATING REVISION O 871135
$ OAK BRO _OK STATION UPPER DRYWELL ANALYSIS M ADE'BY ' VERIFIED BY MADE BY VERIFIED BY 2,]
CORRODED SHELL DA pgp SH T_ OF_
DATE DATE DATE DATE I/2.1/88 2I!J27 Pemted M USA GO 64 A AUG 87
. Note: For primary stress evaluation - loads may include (1) Internal pressure (2) Dead weight.of Steel (3) Dead weight of appurtenances (4) 11% Horizontal Earthquake -
OBE equivalent.J5) 5% Vertical Earthquake - OBE Equivalent essentially service Level A in 1983 ASME Code.
For Secondary Stress Evaluat' ion - loads may include all of above plus meridional thermal gradient.
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SU BJ ECT OFFICE REFERENCE NO.
OYSTER CREEK NUCLEAR GENERATING 8 OAK BROOK REVISION O 871135 STATION UPPER DRYWELL ANALYSIS MADE BY VERIFIED BY MADE BY VERIFIED BY g,4 CORRODED SHELL / /g Q,v)) SHT_ OF_
DATE DATE DATE DATE
'/tl)A8 2/3/83 NMed la U54 GO 64a evo 37
E t
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1 1
I SECTION 3 ANALYSIS TECHNIQUE f
SUSJECT OFFICE REFERENCE NO.
REVISION O 871135 OYSTER CREEK NUCLEAR GENERATING. O.0AK BROOK MADE BY VERIFIED BY MADE BY VERIFIED BY STATION UPPER DRYWELL ANALYSIS s NT3_, go F --.
TJA OCl4 CORRODED SHELL DATE DATE DATE DATE
'/tIlet A/3/ES co u , ,, ,,
m ie m usa
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Analysis Technique The entire drywell extending from the point of embedment to the top of the closure flange is modeled in the CBT Computer Program E0781A/B, Revision 0, dated 7/29/87. The model consists of 28 parts and is completely described in Appendix A. The spherical portion is described in parts 1 through 5. The knuckle transition joining the sphere to the cylinder is described in parts 6 and 7. The cylindrical portion of the upper drywell is the region which ir to be analyzed in detail in this' study. The model is shown in the figure below, wtad h i tuo im 9..
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SUBJECT OFFICE REFERENCE NO.
OYSTER CREEK NUCLEAR GENERATING O OAK BROOK REVISION O 871135 STATION UPPER DRYWELL ANALYSIS MADE BY VERIFIED BY MADE BY VERIFIED BY j,/
CORRODED SHELL g/4 p,p// sHT _ OF _
DATE DATE DATE DATE l '/tt)83 2/3/35 P.Me3 M USA GO 64 A AUG 87
A more detailed description of the upper dryvell cylinder along with the stiffening as described in the project specification is < included in the figure shown below. A description of the entire model is also shown in Appendix A.
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SUBJECT OFFICE REFERENCE NO.
O.0AKBROOK REVISION O 871135 0YSTER CREEK hUCLEAR GENERATING.
MADE BY VERIFIED BY MADE BY VERIFIED BY J , f, STATION UPPER DRYWELL ANALYSIS 73A i)#I/ sHT oF_ '
CORRODED SHELL DATE DATE DATE DATE
- /tllas .t /) /W co u .uc,.i sm.c m vs.
7' E
SECTION 4 DESIGN OtfrPtfrS
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SUBJECT OFFICE REFERENCE NO.
O .0AK BROOK REVISION O 871135 0YSTER CREEK NUCLEAR GENERATING, MADE BY VERIFIED BY MADEBY VERIFIED BY 4o STATION UPPER DRYWELL ANALYSIS 7/A Op# SHT._ OF _
DATE DATE DATE DATE l CORRODED SHELL
- /U/SB 2/1/S.7 _
l w a * .1
- .. us.
Design Output ,
Although the entire drywell was analyzed for the.62 psig and 175'F loading case, the plots. included in this portion of the report are directed at.. providing maximum' detail to the upper drywell cylindreial section. The plots cover the
. region between elevation 71'-10 3/4 and elevation 92'-3.
The plots include the actual calculated stresses in the upper dryvell cylinder.
as follows:
membrane stress-circumferential direction .page 4.2 membrane stress-meridional direction page 4.3 inside surface stress-circumferential direction page 4.4 inside surface stress-metidional direction page 4.5 outside surface stress-circumferential direction page 4'.6 outside surface stress-meridional direction page 4.7 All of the plotted stresses are less than the stipulated allowable stresses. Of particular interest is the circumferential membrane stress plot shown on page 4.2. The maximum stress is shown to be 21.422 ksi. The allowable local primary membrane stress is 28.875 ksi. The definition of a local primary membrane stress states that a local stress may not exceed 1.1 x 19250 = 21175 for a distance greater than 1.0 / Rt = 1.0 J 198 x .59 = 10.8 inches. The plot shows that there are two areas where the stress exceeds 21175, however, these regions are limited to 8 inches and 5 inches as shown. These lengths are less than the f
10.8 inch limit.
SUBJECT OFFICE REFERENCE NO.
OYSTER CREEK NUCLEAR GENERATING $ OAK BROOK REVISION d 871135 STATION UPPER DRYWELL ANALYSIS MADE BY VERIFIED BY MADE BY VERIFIED BY SHT4_,fOF_
CORRODED SHELL Q f)pg pAJE DATE DA"E DATE t/4/LS 2/4/ZI ,
Go 64& AUG $7 P med M US A
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Allowable Secondary Surface Stress = 52.50 Ksi
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~g g- Allowable I.ocal Primary Membrane atress = 28.875 Kel zx
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& gc "g Limit Index for Local Primary Membrane Stress = 1.1 x 19.25 = 21.175 Ksi h f E$ - [ ^ s [ O [ 'N t-
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' Elev. 92'-3 Scale 1" = 10 Ksi ,
1" = 30 in of Shell
- Eley, 88'-8M
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Elev. 84'-11-3/4 y
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Elev. 80'-6%
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30 40 30 20 10 0 .go _g3 Stress Ksl INSIDE SURFRCE STRESSES -SIGNR THETR RNRLYSIS OF OTSTER CREEK CONTAINMENT; INT PRESS OF 0.0620 KSI.
MAXIMA 21.136 SUBJECT OFFtCE REFERENCE NO.
O .0AX BROOK REVISION O 871135 OYSTER CREEK NUCLEAR GENERATING.
VE FE BY MADE BY VERIFIED BY fg STATION-UPPER ORYWELL ANALYSIS "^Dj
- j. BY AATE DATE DATE DATE CORRODED SHELL t/4/88 QH/N ma yo po r ..
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Scale 1" = 10 Ksi 1" = 30 in of Shell
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40 30 20 0 -10 -15 50 10 INSIDE SURFACE STRESSES - SIGMA PHI Stress Ksl ANALYSIS OF OYSTER CREEK CONTAINMENT: INT PRESS OF 0.0620 XSI.
MAXIMA 28.139 SUBJECT OF FIC E REFERENCE NO.
REVISION O 871135 O .0AK BROOK OYSTER CREEK NUCLEAR GENERATING.
MADE BY VER F EO BY MADE BY VERIFIED BY STATION- UPPER ORYWELL ANALYSIS ,, SHT F_
pATE DATE DATE DATE I CORRODED SHELL 2/4/98 .2N/J"I l
1 Elev. 92'-3 i H
Scale 1" = 10 Ksi 1" = 30 in of Shell
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0 10 .g3 50 40 30 20 10 OUTSIDE SURFACE STRESSES - SIGMA THETA Stress Ksi ANALYSIS OF OYSTER CREEK CONTAINMENT; INT PRESS OF 0.0620 KSI.
MAXIMA 22.061 OFF!CE REFERENCE NO.
SUBJEC1 REVISION O 8.0AKBROOK 871135 0YSTER CREEK NUCLEAR GENERATING, MADE BY VERIFIED BY MADE BY VERIFIED BY 4 SNT 4oF_
STATION- UPPER ORYWELL ANALYSIS 73A 01?H DATE DATE DATE DATE CORRODED SHELL 2/A/SS VW83 _
v Elev. 92'.3 Scale 1" = 10 Ksi l" = 30 in of Shell Eley, age.gy, 7
Elev.80'.IJ.3/4 x
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- a 50 40 30 20 10 0 10 .g3 OUTSIDE SURFACE STRESSES - SIGNA PHI Stress Ksi ANALYSIS OF OTSTER CREEK CONTAINMENT: INT PRESS OF 0.0620 XSI.
MRXIMA 14.777 SUBJECT . OFFICE REFERENCE NO.
O.0AKBROOK REVIStord C 871135 OYSTER CREEK NUCLEAR GENERATING, VER EO CY MADE BY VERIFIED BY STATION- UPPER DRYWELL ANALYSIS "^fE BY CORRODED SHELL DATE DATE
,J^pE O*)g, g
w 0964 at@of
i 3,4 ;
8: ..
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k r-I SECTION 5 i
EVALUATION AND CONCLUSIONS 1
i 4
SUBJECT OFFICE REFERENCE NO.
REvlSION O 871135 OYSTER CREEK NUCLEAR GENERATING 8 OAK BROOK STATION UPPER DRWELL ANALYSIS MADE BY VERIFIED BY MADE BY VERIFIED BY fo CORRODED SHELL TJA pg// _
S H7_ O F_
DAJE DATE DATE DATE lf4/db s?/vVE GO S44 AVO II
.~ Pnneed 6n USA
,3 Evaluation and Conclusions Evalust. ion of General Membrane Results
'The calculated membrane stresses in the region between. elev. 80'-6 1/4" and elev. 71'-10 3/4", as shown on the stress plots on pages 4.2 and 4.3, appear to have a substantial zone in which the local effects of the stiffeners are not present. Therefore, in this region, it is appropirate to compare the calculated stresses to the general primary membrane allowable, c) Per ASME,Section VIII, 1962 and Code Case Interpretation 1272N-5 s
Membrane stresses are compared to the allowable value of 19.25 ksi from Code Case 1272N-5. The calculated meridional general membrane stress in the cylinder model (using a uniform thickness of t = 0.590 inches) is 10.40 ksi. This value is evident in the stress plot on page 4.3 and is calculated using the formula S = PR/(2t). The calculated circumferential general membrane stress in the cylinder model is 20.81 ksi. This value is evident in the stress plot on page 4.2 for the above region and is calculated using the formula S = PR/t. The meridional value is less than the Code Caso allowable. The circumferential stress, however, is greater than the Code Case allowable. In th!s region, the calculated stresses exceed the general primary membrane allowable.
5,U BJ E CT OFFICE fg y. REFERENCE NO.
0YSTER CREEK NUCLEAR GENERATING @ OAK BROOK REVISION / mao 871135 STATION UPPER DRYWELL ANALYSIS MADE BY VERIFIED BY MADE BY VERJflED BY CORRODED SHELL 7 74 ggj4 -gp (jg// SH TMOF _
04TE DATE DATE DATE t/$/88 2/s*/ts' 4/f/88 y/r/27 s.u w ,,vss c,o us nua n
b) ' Per ASME,Section III, 1986 1 Membrane struus intensities are compared to allowable values from NE-3220.
These paragraphs of the Code consider both general primary membrane and local primary membrane classific :itit ns . The general primary membrarie v stress intensity is calculated for 9 s cylinder model using the femnula S =
PR/t + P/2 (reference Code paragraph A-2221). This value is 20.97 ksi and is evident in the stress plot on page 4.2 for the above region. The allowable value is 1.0 x Smc = 19.25 ksi. The calculated general primary membrane stress intensities exceed the general nrimary membrane allowable.
i Evaluation of Local Membrane Results The calculated shell stresses at all of the stiffeners, as well as the re;;1ons cdjacent to the stiffeners are influenced by discontinuity effects. The extent of these effects along the meridian is apparent when studying the stress plots.
I Tlie exact termination point, however, is very hard to identify. The stresses ,
shown on page 4.2, in the region between elev. 92' 3" and 80'-6 1/2", are evaluated as a local primary category of stress. A study of the circumferential l ctress plot indicates that the stresses in the entire region between elev.
92'-3" and 88'-8 1/2" and betwern elev. 88'-8 1/2" and 84'-11 3/4" are clearly l influenced by the adjacent stiffeners and should be compared to the specified local primary allowable criteria. By inspection of membrane stress values, the stresses in the region between elev. 84'-11 3/4" and 80'-6 1/2" are also affected by the adj acent stiffeners and are compared to the specified local l
SUBJECT OFFICE /.fg7 j REFERENCE NO.
f OYSTER CREEK NUCLEAR GENERATING O OAK BROOK.
REVISION
/PtMApr./ 871135 STATION UPPER DRYWELL ANALYSIS MADE BY VERIFIED BY MADE BY VERIFIED BY l
CORRODED SHELL ~qp d)Rh 77A OMN _ S H T[*_k F l DATE DATE DA,TE DATE t/.t/ss /wrf 4/S/88 WF/8f m . _ ,, oo m avo o
primary allowable criteria. In addition, the stresses in the portions of shell immediately below elev. 80'-6 1/4" and immediately above elev. 71'-10 3/4" are af fected by the adjacent stiffeners and are compared to the specified local primacy allowable criteria.
a) Per ASME,Section VIII, 1962 and Code Case Interpretation 1272N-5 Local membrane stresses are compared to the allowable value from Code Case 1272N-5 of 1.5 x 1.1 x 17.5 = 28.87 ksi. The. maximum calcu ' . ted local membrane stress is the circumferential value of 21.42. This stress occurs near elevation 90 feet and is shown in the stress plot cn page 4.2. This calculated local membrane stress is less than the local membrane stress allowable value.
b) Per ASME,Section III, 1986 Local membrane stress intensities are compared to allowable values from NE-3220. Note that the stress plot on page 4.2 shows the circumferential stresses along the height of the cylinder which are also the stress intensities. This is dua to the fact that 1) both the meridional and circumferential strasses are positive, 2) when this is the casa, the higher of tha two is also the stress intensity, and 3) the circumferential sttess along the height of the cylinder model is always greater than the meridional stress.
SUBJECT OFFICE gg y- I REFERENCE NO
[ OYSTER CREEK NUCLEAR GENERATING REVISION / 871135 O OAK BROOK / mot STATION UPPER DRYWELL ANALYSIS M ADE BY VERIFIED BY MADE BY VEgiED BY S
CORRODED SHELL 77 4 cpy 7yg vgg sayf3op_
DATE DATE DATE DATE
%l83 .t N /P2P Vr/S 8 y/c/72 Naled in USA GO 64A AUG 87
The highest local primary membrane stress intensity la 21.42 ksi and is located near elevation 90 feet. The next highest location has a value of-21.20 ksi near elevation 74 feet. These values are less than the allowable value of 1.5 x Sac = 1.5 x 19.25 = 28.87 ksi. In addition, these valuus are above the limit index of 1.1 x 19.25 = 21.17 ksi. This is permitted, however, for a distance of 1.0 x / (Rt)' = 10.8 inches provided that the regions are no closer than 2.5 x O R3 = 27 inches. These conditions are satisfied. At elevation 90 feet, the distac.ce is about 8 inches and at elevation 74 feet, the distance is about 5 inches. Both these distances are less than the required distance of 10.8 inches. Also these locations are about 190 inches apart which is greater than the required value of 27 inches. Therefore, the calculated local primary membrane stress intensities meet the local primary membrane allowao' Evaluatica of Surface Results l The calculated surface stresses in the region between elev. 92'-3" and 71'-10 3/4" are shown on pages 4.4 thru 4.7. All stresses shown are well below the specified allowables. ,
a) Per ASME,Section VIII, 1962 and Code Case Interpretation 1272N-5.
l
' Surface stresses are compared to the allowable value of 3.0 x 17.5 = 52.5
(
ksi from Code Case 1272N-5. The highest calculated surface stress is 28.14 L
ksi. This is a stress in the meridional direction and is located at the f
( bottom of the cylinder model where it joins with the thickened knuckle I SUBJ ECT OFFICE REFERENCE NO.
OYSTER CREEK NUCLEAR GENERATING 8 OAK BROOK REVISION / Sg)l 871135 STATION UPPER DRWELL ANALYSIS MADE 3Y VERIFIED BY MADE BY VERIFIED BY CORRODED SHELL 7]A Ogg rJA Ogd SHTfdOF_
DATE DATE DATE DATE W/as usvse 4Was Ws-M e.a.4i. usa oo s4a avo o
plats (see stress plot on page 4.5). This value includes discontittuity effects and is less than its allowable value of 52.5 ksi.
b) Per ASME,Section III, 1936 Surface stress intensities are compared to allowable values from NE-3220.
These paragraphs of the Code consider surface stress intensities comprised of both primary and primary plus secondary classifications of stress. A limit of 1.5 x Smc = 1.5 x 19.25 = 28.87 ksi is imposed on the surface stress intensities made up from local primary membrane plus primary bending stresses. In this analysis, there is no primary bending in the corroded cylinder and the primary surf ace stress limit is met by satisfying the limits for local primary membrane stresses. The surface stress intensities due to primary plus secondary classifications of stress are limited to a 3.0 x Sm1 = 3.0 x 23.30 = 69.9 ksi range. The highest calculated range of surface stress intensity is on the inside surface and at the bottom of the corroded cylinder where it joins the thickened knuckle plate (see stress plots on page 4.4 and 4.5). (Since the meridional and circumferential ,
inside surface stresses are both positive at this location, the surface stress intensity is the higher of the two.) This calculated value of 28.14 ksi is less than its allowable value of 69.90 ksi.
(
i
~
( SUBJECT 0YSTER CREEK NUCLEAR GENERATING OFF:CE 8 OAK BROOK REVISION I g- REFERENCE NO.
871135 ,
STATION UPPER DRYWELL ANALYSIS MADE PY VERIFIED BY MADE BY VERIFIED BY I
[ CORRODED SHELL 7,fA pgy y /4 PAW SHT.SIOF_
TE DATE DATE DATE f 88 A/s*/s2 4/3/3R 9'/s~/92
~, ., vs. co uuvo .,
Evaluation of Stiffener Attachment Welds Ti}e stress in the welds attaching the three stiffeners at elev. 80'-6 1/4, 84'-11 3/4, and 88'-8 1/2 is checked using an allowable stress equal to 0.55 x Sm/0.70711 on the throat of the fillet weld. The maximum weld stress is 13.7 ksi. This value is less than its allowable of 0.55 x 19.3/.70711 = 15.0 ksi.
Discussion of Stress Evaluation The stress plots and the preceding evaluation of the calculated stresses are cummarized as follows:
The stiffeners and the stiffening effect of the knuckle introduce geometric otructural discontinuities. The stress patterns reflect this effect, i.e., the ,
local primary membrane stress at the stiffener is reduced and the local primary membrane stress at some arbitrary distance away from the discontinuity is 4
greater than the general primary membrane atress.
l The ASME Code allowable stress criteria for local primary membrane stress should logically be applicable to stresses which are clearly the result of a geometric discontinuity. The limit of the effects of the geometric discontinuity varies, but generally depends upon the specific geometry. A study of the stress plot is recommended for making this determination.
I l
(
SUBJECT OFFICE Jgy-l REFERENCE NO.
f OYSTER CREEK NUCLEAR GENERATING O OAK BROOK REVISION / ewA 871135 STATION UPPER DRYWELL ANALYSIS MADE SY VERIFIED BY MADE BY VERIFIED BY CORRODED SHELL 7--g pgy g g// SHT b F
{ DATE DATE ATE DATE
~~ ,es.
W/ss usvn S/ss yMgr co . . .,
L The local primary membrane stress is logically made up of two components. The first is the general primary membrane stress and the second is a membrane stress due to discontinuity effects. The calculated stress is then the sum of the two components and is compared to the code identified allowable. In the area in which the discontinuity effects are present, tae Code allows the stress to be as much as 1.5 x the general membrane allowable. The index which is used to limit the extent of this localized effect is as follows: the distance over which the stre.ss exceeds 1.1 x Sm must be less than 1 x /E. The Code does not specify a maximum distance f t.- which the stress may exceed 1.0 x Sm while remaining below 1.1 x Sm. .
Good engineering judgment would dictate that when the membrane stress level stabilizes over some length of cylinder, then the local discontinuity effects
.cre no longer present.
In summarizing the effects of the above listed assessment, several additional factors should be considered.
- 1. A recent ultrasonic inspection of ti e upper drywell shell at elevation 87'-5" showed localized evidence of thickness reduction below the .64" design thickness. Subsequent core samples taken showed the local degradation to be due to corrosion. This report provides an axisymmetric analysir of the upper drywell cylinder assuming a uniformly reduced thickness of .59". This thickness was arbitrary clefined for the purpose of SUBJECT OFFICE REFERENCE NO.
f RFVislON / gyp AD() 871135 OYJTER OREEK NUCLEAR GENERATING O OAK BROOK ,.
STATION UPPER DRYWELL ANALYSIS M ADE BY VERIFIED BY M ADE BY i VERIFIED BY
{
CORRODED SHELL m 9.4H 71A O#H DATE SHT N OF _.
p3TE DATE QAJE C/ 5/8S . A/$~/88 4/flL6. 9N/E$
{ _ _ . _ _ _ _
s v a conservative analysis, while the minimum average reading of local thinned areas was .619".
- 2. The ASME Code allowable stresses are intended for use on new construction and are not necessarily applicable to vessels which have been in service.
New construction permits a .01 mill underrun on the thickness of the steel.
This permissible underrun is equivalent to a 1.67. overstress. This has not been factored into th1s analysis.
- 3. The allowable stresses are based on specified minimum mechanical properties. A separate assessment of stress levels based on actual properties obtained from CMTR's has been made by the GPUN staff. Refer to this assessment for further information.
- 4. The Code includes a factor of safety over the design strasses. This factor of safety may be found by dividing the minimum tensile strength of the material by the specified allowable stress. In this case, it is 70000/19250 or about 3.64. Using the calculated general primary membrane stress of 20.8 ksi, the minimum factor of safety would be 70000/20800 or about 3.37.
{
[
SUBJECT OFFICE
( 0YSTER CREEK NUCLEAR GENERATING 8 0AK BROOK { AEVISION(at
/ / S4 y y- l REFERENCE 871135 NO.
STATION UPPER DRYWELL ANALYSIS MADE BY VERIFIED BY MADE SY VERIFIED BY CORRODED SHELL 7pA pfpH yg, h//h sH TNOF_
D DATE PAJE DATE I
t/S,pTE83 .2/S/fS MS/&!) 9'N/ES e.a.o m vu ooou;ua u
Conclusion The acceptability of the upper drywell cylinder in the corroded condition becomes a matter of good engineering judgment. An analysis using Code design, rules and the hypothetical axisymmetric model described herein shows that a 40" long region of the shell near elevation 75'-0" exceeds the allowable for general primary membrane stress. The regions adjacent to this zone meet the allowables for local primary membrane stress. Good engineering judgment, consideration of the localized nature of observed thickness degradation, and other considerations presented in the Discussion of Stress Evaluations, support the conclusion that this condition does not compromise the structural integrity of the vessel.
SUBJ ECT OFFICE REFERENCE NO.
OYSTER CREEK NUCLEAR GENERATING REVISION O 871135 O OAK BROOK STATION UPPER DRYWELL ANALYSIS ' MADE BY VERIFIED BY MADE BY VERIFIED BY CORRODED SHELL 7CA DRH SHTNOF DAJE DATE DATE DATE 4/5/33 Ws-/gr Qw,teeja US A GO 64A AUQ 87 i_
s-P' SECTION 6
) LIST OF REFERENCES f
~
SUBJECT OFFICE REFERENCE NO~
OYSTER CREEK NUCLEAR GENERATING, O.0AKBROOK REMN O 871135 MADE BY VERIFIED BY MADE BY VER:FIED BY 4,0
[ STATION UPPER DRYWELL ANALYSIS 70A Dxs sta_ or_
CORRODED SHELL DATE' DATE DATE DATE I YEI/48 2/y/gg aae usa co u. .voii I
References
- 1. CBI Report - Drywell Modification Feasibility Study Oyster Creek Nuclear Generating Corporation '~
Parsippany, New Jersey Prepared by CBI Services, Inc.
Oak Brook, Illinois May 1987
- 2. Project Specification - General Public Utilities Nuclear Purchase Order No. PC-049122, Change Order No. 6
- 3. CBI Computer Program E0781A/B Documentation, "Program 781 General Shell of Revolution Stress Analysis, f
Part B - Users Manual." pgs 1-59, prepared by CBI.
- 4. CBI Fabrication and Assembly Drawings for Contract 9-0971. List of applicable drawings is ,
shown on Drawing 1, Revision 1 i
I
~
SUBJECT OFFICE REFERENCE NO.
REVISION O OYSTER CREEK NUCLEAR GENERATING $ OAK BROQE 871135 STATION UPPER DRWELL ANALYSIS MADE BY VERIFIED BY MADE BY VERIFIED BY 4,/
CORRODED SHELL 7 /4 Q;)g SHT_ OF_
[ ATE DATE DATE DATE E/4/89 2/4/f5 Prmted la USA GO 64 A AUG 87
(
6 Appendix A Computer input and Output for Drywell Shell A
and Computer Program E0781A Description SUBJErT OFACE REFERENCENO.
REVISION o 871135 0YSTER CREEK NUCLEAR GENERATING, 8.0AKBROOK MADE 8Y VERIFIED BY MADEBY VERIFIED BY A.O STATION UPPER DRYWELL ANALYSIS TJA gp SHT _ or _ 06TE DATE DATE DATE CORRODED SHELL ,l$ 1/89 2/3/38 hea usa w e.. m ., I
The Shells of Revolution Program is the Chicago Bridge & Iron Company Program E0781A/B, Rev. O, dated 7/29/87. The . program calculates the stresses and displacements in thin walled elastic shells of revolution when subjected to ctatic edge, surface and/or temperature loads with arbitrary distribution over the surface of the shell. The geometry of the shell must be axially symmetric, but the shape of the meridian is arbitrary. It is possible to include up to nine branch shells with the main shell in a single model. In addition, the chell wall may consist of four layers of different orthotropic materials, and the thickness of each layer may vary along the meridian. Program E0781A/B numerically integrates the eight ordinary first order differential equations of thin shell theory derived by H. Reissner. The cquations are derived such that the eight variables are chosen as those which f cppear on the boundaries of the axially symmetric shell so that the entire problem can be expressed in these fundamental variables. I l Chicago Bridge & Iron Company has extensively revised the Kalnins Program. The program has been altered such that a 4 x 4 force-displacement relation can be used as a boundary condition as an alternative to the usual procedure of specifying forces or displacements. This force-displacement relation can be used to describe the forces or some compatible combination of the two. In this i manner, it is possible to study the behavior of a large complex structure. ( f l SUBJECT i CFFICE REFERENCE NO. REVISION O OYSTER CREEK NUCLEAR GENERATING $ NAE MrOK f STATION UPPER DRYWELL ANALP is , MADE BY ' VERIFIED BYi MADE BY IVERIFIED BY j 4-/ ' r CORRODED SHELL l Og pgH l { l SHT _ OF _ j DATE '( DATE j DATE ' DATE l W//68 I a /f/M i GO W AUG$7 P m M m USA
f The ' Kalnins Computer Program CBI Computer Program.E0781A/B, Rev. O, dated 7/29/87 is employed to obtain stress and stress intensity values.of ring-stiff branched shells of revolution. The shell may have various meriodional geometries, wall constructions, boundary conditions, ring reinforcements, and types of loading, including thermal loading. Specifically, the program can be used to obtains
- a. Axisymetric stresses and displacements for a series of step-wise increasing thermal or mechanical loads,
- b. Displacements and stresses in symmetrically or nonsymetrically loaded shells.
It is also possible to introduce a "spring matrix" at the end of any part of the ) stress model. This matrix must be expressed in the form, force = spring matrix 4 x displacement. In this manner it is possible to model the restraint of the cand cushion in the transition zone at the point of embedment. In addition to the above changes, the Kalnins Program has been modified to increase the size of the problem that can be considered and to improve the accuracy of the solution. The Kalnins Computer Program was developed by Professor A. Kalnins, Assistant Professor of Engineering and Applied Science, Yale University, New Haven, , Connecticut. The program is described in the September 1964 Issue of the Journal of Applied Mechanics. The program is used on CBI Mainframe Computer IBM Model 4381. SUBJECT OFFICE REFERENCE NO OYSTER CREEK NUCLEAR GENERATING 8 OAK BROOK REVISION O 871135 STATION UPPER DRYWELL ANALYSIS MADE BY VERIFIED BY MADE BY VERIFIED BY A -L> CORRODED SHELL 77A Oje H SHT_ OF_ DATE DATE DATE Yo/as m /6 8 l DATE
,,- m. w . .. . ,
t Additional information about the program can be obtained from the User's Manual (Reference 3), ) f } f SUBJECT OFFICE REFERENCE NO. REVISION O 871135 OYSTER CREEK NUCLEAR GENERATING, 8 .0AK BROOK MADE BY VERIFIED BY MADE BY VERIFIED BY A .,,{ STATION UPPER DRYWELL ANALYSIS 7'JA O,qM sHT _ oF CORRODED SHELL DATE DATE DATE DATE
'/ft /AE 1/J/FS *ae u5' co u..voir
[
wud Q.-Tk - i
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d8r Compular- . P+oy mm Eo7.et A/c @ 5 $*Q t '. \ t \ \ s p r e. s t. H s ho Mademooc../ ad./ \A3 1 h4c dc u/ of 2.8
"'" @Q. y- --
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,a n ly \".1 6 -- ~ delade.1 mdel of caeradeJ 4e// re9 *el Odtnded b: 390* poet,- { tAra h
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60 1 A ':6 Y ' , g' " 4 EL,tV,GD Lokl i 4 ;4
- a N}
f,A% '" ' -- - Et.s v: 2'-3,, ' SUBJECT OFFICE REFERENCE >$O O OAK BROOK REVISION d 871135 OYSTER CREEK NUCLEAR GENERATING. MADE BY VERIFIED BY MADEDY VERIFIED BY A. STATION UPPER DRYWELL ANALYSIS CA prp sHT _ F_ CORRODED SHELL DATE DATE DATE D A'IE Us/b8 2/3/M n . us. co u. .uo .,
.t . )
w 4 g The stiffeners presently located inside the cylindrical shell are modeled as
' parts 9, 12 and 14. 'The outer and inner refueling bellovx seal rings are modeled as parts 17 and 19. The closure flange and removable head are also ,
included and make up parts 21 thru 28. The critical segments of the cylindrical shell are described as parts 8, 10, 11, 13 and 15. The thickness in these parts is described in the project sp'ecifications to be 0.590 inches.' s The Kalnins Program -' CBI Program E0781A/B plot options has been used and the results are shown on pages 4.2 through 4.7. A tabular listing of the stresses is included in the following pages. Plots of membrane stresses in the meridional and circumferential direction are presented first. These are followed by plots of the inside and outside surface stresses in both the meridional and circumferential directions. i
]
r SUBJECT OFFtCE REFERENCE NO. REVISION Q g71133 OYSTER CREEK NUCLEAR GENERATING O OAK BROOK STATION UPPER DRYWELL ANALYSIS CORRODED SHELL M ADE BY VERIFIED BY MADE BY TJ" A pg// VERIFIED BY A.[ SHI_ OF_ DATE DATE DATE DATE
%//a3 AN/M.T w . a usa co us avo n
f
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08Z Conpader bymm EO78/ A/6 lfoyer Drym// PfadAceridw/ PfedeI SUBJECT OFFICE REFERENCE NO. O .0AK BROOK REVISION O 871135 0YSTER CREEK NUCLEAR GENERATING. MACEBY VERIFIED BY M ADE BY VERIFIED P.Y A-G STATION UPPER DRYWELL ANALYSIS 73A DA g SHT_ OF_ DATE DATE DATE CORRODED SHELL
'[D AT ELtlSo
.:n/M oo unvo .,
L usa -
\ r 3
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.0.0000 0.9770 1.1540 0.0000 0.0000 0 0 0 0 0 0.29395f+05- 0.1000CE+00 0.00000E+00 0.00000E*00 0.00000E+00 0.00000E+00 0 C 0 0 0 0 0.29195t*05 0.30000E+00 0 00000E+00 _0.00000E+00 0.00C00E+00 C.00000E*00 0 0 01 0 0 0 J 420.093 ___. 0.000 ___ 44.420 42.000 2 2 1 1 0 0 _ , , , , , , _ , , , _ _ , , , _ _ _ , ,
0.0000 0.57f0 1 1540 0.0000 0.0000 0 0 0 0 0 0+23319E*05 0.30000E*C0 0.000C0E+00 0.C3000E+00 0.00000E+00 0.00000E+00 0 C 0 00 0 0.20275r+95 0.1000 0E
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-1.0000 3 2111 1 5625 0'0000
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- 0. 211'8 5C +a5 1.50000t+00 0.000C0E+0i __0.000CCE+00 0.00000f+00 0.C0C00E+00 0 0 0 0 0 0 0.2119%C+0*i 0.10000r+00 0.00000E+00' 0.00000C+00 0.00000F+00 0.0000CE+0C C C C C 0 0 1 148.000 tito.000 0.000 6 000 3' 2 1 1 2 0
-0.1750 0.0000 0.1750 0.0000 0.0000 0 0 0 C 0 1.2341556)6 0.sd350G d6 "5.5715dcr+OFO buo00F00 00000FFD0' O.'c0000E +00 0 C' O C 0 0 0.2M M%r.05 0. 3 000 0F + 00 0.000C0E_+00. 0.00000E+00 0.CC000E+00 0.00000E+00 0 C 0 C 0 0 1 118. M C 90.000 0.000 36.000 4 2 9 I O 0 0.0000 0.?950 0.%900 0.0000 0.0000~ 0 0 0 0 0 0.24395i.605 ) .100 00 r- 6 0 0 c.000CCE+00 0.00000C+00 0.00000E+00 C.00000C+00 C ~0 0 0 0 WmTii+as ' 3.1DJ0M+N F.650Y6r+00 5'.35565U5F'"0. 0Md O E7 00 ~ 0. C0 C 00C 0 +00 C C - 00 0 0 1 1 % .10 ^ 90.0u0 0.000 27.5C0 5 2 5 1 0 0
- 0. f>00 0 0.2950 0.5900 0.0000 0.0000 0 0 0 C C 0 23995E+,1% %'0000r e 00 0.00000E+00 0.00000t+00 0.00000F+00 0.00000C+00 C C 0 0 0 0 0.29395E*05 0.30000E+c0 C.000000+00 0.0001CE+C0 0.0J000f*00 0.00000E+00 0 0 0 C C 0 t 19C.000 180.000 0.000 o.000 3 2 1 1 2 0
- 0.1 f 5 0 0.0000 0.3790 0.0000 0.0000 0 0 0 0 0 SUBJECT OFFICE REFERENCE NO.
OYSTER CREEK NUCLEAR GENERATING REvlStON O ' 871135 O OAK BROOK STATION UPPER DRYWELL ANALYSIS MADE BY VERIFIED BY MADE BY VERIFIED BY A-7 CORRODED SHELL g ,p,pp SHT _ OF _ DATE DATE DATE DATE 2hlas 2N38
. us. 00 +.. .uo e
, .t 9 *. 0.21191t
- W 0.30000E*00 0.00000E+00 0.0000Cf+CO' d . 00010 r + ,10 0.00000E+00 0 C 0 0 0 0
- 0. 2311%r
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REVISION O 871135 OYSTER CREEK NUCLEAR GENERATI!!G 8 OAK BROOK STATION UPPER DRYWELL ANALYSIS MADE BY VERIFIED BY MADE BY ~ VERIFIED BY A.8 CORRODED SHELL ~K7A imp SHT_ OF_ QATI DATE DATE DATE z/ 1 /.se a h /9 7 : Prumed m USA GO 644 AMG E7
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- i. SPHEPE R= 420.000 T= 1.154 51= 52.000 SF= 67.000 LAYER 1 Z= 0.0000 TC 0.5770 Fa 20395. NUa.30 ALFA =.000000000 LAYER 2 Z= 0.5770 TO 1.1540 E= 28395. NU=.30 ALFA =.0000C0000 PART 4, MAIN SilE LL, 6 SEGMENTS S P H Li' E P= 420.000 T= 0.770 51= 67.000 SF= 113.000 L A YEk 1 Z= 0.0000 TO 0.3050 E= 28395. NU=.30 ALFA =.000000060~
LAYED 2 Z= G.38t0 TU 0.7700 Em 28395. NL=.30 ALFA =.000000006~
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F 1 P A F. T 5, MAIN SHELL, r, SEGMENTS SPHEhE 't = 420.000 T= 0.722 Sl= 113.000 SF= 146.717 LAYER 1 l= 0.0000 TC 0.3610 E= 28395. NU=.30 Alfa =.000000000 l tAYER 2 Z= 0.3E10 TO 0.7220 E= 29395. ,hu=.30 ALFA =.000000000
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AtlALYSIS CF CYSTE9 CREEK LCNTAIN"ENTi ItJT PRESS OF 0.0'20 KS!.
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PART 6, M A I t,- S b F.L t. , 5 SEGMEN T S n TOPalD F l= - 72.700 R0=270.000 T= 2.5625 51= 213.3 % SF= ?70.000 LAYER 1 ls -1 0000 TO 0.2o13 Em 28395. NU=.30 ALTA=.000000000 LAYEK 2 Z= 0.2813 TO 1.5625 E= 28395. N U = . 3'O ALFA =.650000C00
=
PART 7, HAIN SHELL, 1 SEG ME N T S CY L I NDE R R= 194.700 PHl= 90.000 T= 2.5625 51= 0.000 SFs 4.500 LAYER 1 Z= -1.0000 TO 0.2813 E= 28395. NU=.30 ALFA =.000000000 L A Y E P, 2 Z= 0.2813 TO 1.5625 E= 28395. NU= .3 0 ALFA =.000000000 PART 8, 'i A ! N SHELL, 10 SEGMENTS
" CYLINDE4 R= 173.000 P41= 40.000 T= 0.59C0 51= 0.000 SF= 103.47'O' L A Y t- 4 1 Z= 0.00J0 TG 7.2950 3 E= 283 % . NU=.30 SLFA=.000000000
~
LAYER 2 l= 0.2750 TO 0.5900 E3 23395. NU=.30 A W A=.000066000~~~ P A ?. T 9, ORANCH SHELL END, 3 SEGMENTS PLATE R= 198.000 PH1=100.000 T= 0.7500 51= 0.000 SF= 6.000 LAYER 1 Z= -0.3750 TO 0.0000 E= 28395. NU=.30 ALFA =.C00000000 LAYER 2 Z= 0.0000 TO 0.37'50 E= 28395. NU=.30 ALFA =.C0CCCOC00 PART 10, MAIN SHELL, 4 SEGMENTS
~ CYLiNJEP P= 198.000
~
PHl= 90.000 T = 0 . 5 'v 0 0 Sl= 0.000 SF= 36.000
~~ LAYEb 1 Z= 0.0000 TO 0.295C E= 28395. NU=.30 ALTA= 000000000 LAYER 2 2= 0.2950 TO 0.5900 E= 28395. NU=.30 ALFA =.000000C00
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Af1 AL YS IS OF OYSTEP Or,EEK CONTAINMEN11 INT PRESS OF C.0620 KSI.
'Aul 11, t' A PI 5 FELL, 6 SEG"ENTS r, Y L I N D E / Ps 199.000 PH!= '3 0 . 9t 0 T3 C.5900 3!= 0.000 Sr= 27.500 LAYO' 1 !. = 0.0000 70 ') . 2 c 5 0 E= 20395. %=.30 All t. = . 00 0 00000 0 LAYUG 2 Z J . .' tH TC ).5909 E= 28195. f.U=.30 ALFA =.0010C0CCC PA;T 12, 3L /. h C H SHELL END, 3 SEGt4rhTS PLATd f: = 193.000 t'H I= 130 .0 0 0 T= G.7500 St= 0.000 ST= 6. COG LAVEa 1 Z= -0. 3 7 5 0 TC 0.0000 E= 29395. NU=.30 ALFA =.000000000
~ ~ ~
LAYEI 2 Z= 0.0000 TO 0.3750 E= 79395. Nt=.IO A L F A = . 00'iO 00 030 P Al: T 13 "AIN S'4E L L , 4 SEG'iENTS CYl l'PE R Rs 193.700 PHI- 90.000 T= 0.5900 51= 0.00n Sr= 44.750 L A YF ' 1 Z= 0.0000 TC 0.2950 Em 28399 NU=.30 Alfa =.0000C0000 LAYES 2 Z= 0.2950 TC d.5900 C= 20395. NL=.30 ALFAi.0000GOLOO PA.'T 14, f.FAhCh 5 FELL ENC, 3 SEGMENTS
~
PLATE h= 198.000 PHl: 10 0. E0 T= 0.5000 Sl= 0.009 ST= ~~~d.500 L AvW l := -0.2601 T P' O.0000 E= 2e?95. ht=.30 ALTA=.C00000000 LAYFL 2 '
.s 0. 01 T T, TC U.?S00 [= 2A395. NUs.30 AL F A= . 00 0 0 0 ~)C0 0 l
PM' 15 T ! t. SHELL, 6 SLCMENTS ( YLIVE! P= 19 R . V" P5t l = 90.00') T= C.6900 SI= 0.100 SFe 42.50C LAYfh ! != 0.0000 Tr.' O.."150 E= 283 % . hin. 3 0 Alfa =.0000"9000- - _ _ _ _ _ _ _
~
LAYE? ? Z= 0.2959 TO O.5000 E.: 23395. ?!L= . 3 0 t, L f 4 3 "0CCCJC00 w -_ - . - A-t 7 Ce s . o _I~}A $/Yd2 -__ - - OtCH D.I 16.7
/,NALYSIS Uf OY Sl ER CP.EEK Ct;NT A IN:1E NT 1 INT PRESS OF 0.0620 /.51.
PAhi 15, "AlF SHELL, 1 SEGHCNIS CYL INDER Re 10d.000 PHl= 90.M0 T= 1.2500 51= C.000 SF = 6.000 LAYE" 1 D 0.0000 TC 0.6250 E= 28395. NU=.30 ALFA =.000000000
~
LAY 4 2 /= 0.6250 TU 1.P500 Em 20395. liU=.30 Alfa =.000000000 PART 17, Sf'. A NCH S FEL L END, 2 SEGMLNTS PLATE R= 198.000 PH1= 0.000 T= ?.7500 S!= 0.000 SF= 16.3? i LAYER 1 Z= -1.7500 TO -C.3750 ti = 2 ti 3 95. NU=.30 AI.FA=.0000000d0~~ L I NE Aft FUNCT ION GE Nt:C ATOP FOR 2(1) S= 0.0000 7.0000 7.1250 14.375C FGEN= -1.'5000 -1.'5000 0.00000 0.00000 LAYr4 2 Z= -0.'.'53 TO 1.0000 Em 28 *$9 5. NU=.?O All- A= .00000000 0 LINEAR FUNCTICIJ GENERATOR FUH 2(?) S= 0.0000 7.0000 7.1250 14.3750 FGENs -0.3750] -C.57500 0.500C0 0.50000 PAsi I t; , fiAIN 5FLLL, 2 SEGHFNTS CYL,!NDER r = 100. M0 PH1= 90.000 T= 1.2500 51= 0.000 Sf= 16.000 t AY f.h ~ 1 l= 0.0030 10 0.6250 iTu 28395. NL=.30 ALFA =.00n000000 LAYER ? ?= 0.t250'TC 1.2500 f= 28395. "U=.30 ALFA =.CC00C0060 PART 14, SkANCH SFELL END, 6 StGHENTS PLATE ft= loh.000 PHM180.0C0 1= 1.00C0 51= 0.000 SF = 17.0C0 lAYER 1 /= 0.0000 T il C.f000 [= 28305. N l> = . 5 0 AtFAs 000000000 LAYft 2 2= 0.5000 Til 1.0000 t= 28395. NL=.30 ALIA=.000C33COC A - 18 Eevo _WA . C/c { es --.__ _ _ . ORH 2/ 2/SE' __
AN AL YS I S OF OYSTEF. CR FEK ( CNTA !f !!E NT) I fit PRESS OF C.0620 KS!. PART 20, Mn i t, SHELL, 1 SEG'lENTS
~
CYL I.'!D ER n= 19tl.000 Pil l = 90.000 T= 1.2500 51= 0.000 SF= 3.750 LAYEh 1 Z= 0.0000 TC 0.6250 E= 20395. NL=.30 ALFA =.000000000 L A YER 2 /= 0.6250 TO 1.2500 E= 28395. NU=.30 ALFA =.000000000 PART 21, M A lf: SFELL, 2 SLGMENTS C YL !NOFF l '. = 140.000 PHI = 90.000 T= 4.5000 51= 0.000 SF= 4.500 LAYER 1 Z= -2.2500 TO C.0000 Em 28395. NU=.2 0 ALFA =.C00000000
~
LAYER 2 Z= 0.0000 TC 2.2500 E= 28395. NU=.30 AL FA =.C00000000 PAhT 22, MAlti SHELL, 4 S EGM E f> T S , CYLINDER P= 198.000 PHI = 90.000 T= 1.5000 51= 0.000 SF= 20.500 LAYER 1 Z= 0.0000 TC 0.7500 E= 28395. tJU=.30 ALFA =.000000000 L A Y E r' 2 Z= 0. 7 50C TO 1.5000 E= 20395. f:U= . 3 0 ALFA =.000000000
~
PAhT 23, GE A t4Cll SHELL EtJD , 2 SEGMLt.TS DL AT E R= 108.000 PHl= 0.000 T= 2.2500 51= 0.000 SF= 5.500 LAYER 1 Z: ~ 1. 2 r,t)O TC -0.1290 E= 28395. NU=.30 ALFA =.000000000 < L A Y Ell 2 Z= -0.12 50 10 1.0000 E= 28395. NU= .3 0 Alfa =.000000000
~~
PA7T 24, vtIN Sid E L L , 1 SEGMENTS CYLINDER P= 198.000 PHl= 9C.ooO T= 1.5000 51= 0.000 Sf= 0.250 LAYER 1 Z= 0.0000 TO 0.7500 E= 23395. f: U= . 3 0 ALFA =.COC000000
~
tAYFP 2 Z= 0.7000 TG 1.5000 E= 28395. NU=.30 ALFA =.000000000
~l I?oV Q _
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CAH 2/3/ N _
- - - - - _ ~ _ _ _ _ _ _ _ _ _
~
ANALYSI5 CF nYSTEP r,R E F X CChT A INMENT; It!! PRESS OF 0.0620 KS1.
~ - PART 25, BRArdH SFELL END, 2 SEGMENTS t
PL A TE R= 198.000 PHI =180.000 T= 2.2500 51= 0.000 Sr= 5.500 L A Y E P. 1 Z= -1.2500 TO -0.1250 E= 28395. NU=.30 A L F A= . 0 0 0 0 00 C 0 O'~
- 1. A Y E R 2 Z= -0.1250 TU 1.0000 E= 28395. NU=.LC ALFA =.C00000000 PART 26, MAIN SHELL, 4 SEGMENTS CYLINDEP P= Ic8.000 PHI = 9C.000 T= 1.2500 51= 0.000 SF= 34.000 LAYER 1 Z= 0.0000 TC C.6250 f= 20395. NU=.30 ALFA =.000000000 LAYER 2 Z= 0.0250 r0 1.25C0 E= 28305. NU=.30 ALFA =.000000000 PART 27, " n ! f- 5 HELL, !G SEGMEhTS Ell IPSul u A= 150.000 B= 99.000 1= 1.108C SI= 90.000 SF= 162.864 LAYER 1 Z= 0.0000 TO 0.5940 E= 28396 NUr.30 ALFA =.00C000000 LAYER 2 ?= 0.5940 TO 1.1880 E= 28395. NU=."30 AtFA .000000000
' Ari 20, "AIN SHELL, 5 S EG';ENTS
~
SPUELE F. = 352,656 T= 1.188 SI= 162.964 SF= 175.C00 LAYEl: 1 Z= 0.0000 TO 0.5940 E= 28395. NL=.30 ALFA =.000000000 LA(FR 2 2= 0.5940 TC 1 1880 E= 26395. NU=.30 ALFA =.000000000 LOAC PARA'FTEPS OF FCUPIEF t' AR MON IC CCS 0 THETA b.C. START W 0.0000E+00 UI 0.0000F+00 P1 0.0000E+CO U2 C.0CCOE+00 B.C. END 0 0.00CCE+00 til 1. 0 9 32 E 4 01 P1 0.000GE+00 A 0.0000E+00 B.C. E*5 0 0.0000E+00 "1 0.On00E+00 H1 C.CCCCE4LO N 0.0CCOE+0C D.C. END A 0.000CE+00 N1 0.00COE+C0 M1 0.000CE+C0 N C.00COE+C0 B.C. END Q C . 000CF+ CO h1 0.0000E+C0 VI 0.00CCE+C0 t; 0.0000 5 +00 M.C. END C 0.0000L+0C PI O.0000F+"O "1 0 . 0 C C 'X + 0 0 N C.CCCCE+0C B p c, END o r,0qCCE4 00 F1 0.0000F+00 "1 0.0000E400 N C.00000+00 \ - C.C. CNC C n n900E-CD N1 0.00C0E+CC "1 0. 00CCE + C0 h C.0000E+70 A-20 2" o l ~RA 1/2/88 MM 2N5'--
- 3. 0. E rlD - 0 0. 0000E+00 til 0.00COE+00 M1 0.0000E+00 N 0.0000E+00
~
'PART 1 DSC C- 0.000 N1 0.000 M1 0.0C0 N 0.000
.g . F N= 0.062 PP= 0.000 PC= 0.000 TI= 0.C00 10= 0.000 ?
't t
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~
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=
_ A - '2 l 12ey. o 1
~
1d~A %/B8-my gz/r/
sANALYSIS CF OYSTER CF.CEK CONTAINPENTi INT PRESS OF 0.0620 KSI. r DART 2 DSC 0 0.000 N1 0.000 P1 C.CCO N 0.000 i' PN= 0.062 PP= 0.000 PC= 0.000 Tl= 0.000 70= 0.000 PART 3 D SC C C.000 N1 0.000 F1 0.000 A 0.000 ~~ PN= 0.062 PM= 0.000 PC= 0.000 TI= 0.C00 10= 0.000 PAPI 4 DSC 0 0.000 N1 0.000 M1 0.000 N 0.C00 Pt:= 0.062 PM= 0.000 PC= 0.000 TI= 0.000 TO= 0.000~ P A E1 5 USC C O.000 N1 0.000 M1 C.CCO N 0.000 PN= 0.062 PM= 0.C00 PC= 0.000 TI= 0 G00 10= 0.000 PART 6 DSC C 0.000 N1 0.000 M1 C.0CJ N 0.000 FN= C.062 PN= 0.000 PC= 0.000 TI= 0.C00 TO 0.000 pt F T 7 P SC C 0.000 N1 0.000 M1 0.000 N 0.000_ PN= 0.062'PM= 0.0C0 PC= 0.000 Tl= 0.000 1G= 0.000 P t.k l 6 DSC C 0.000 N1 0 . 0 1i 0 d.1 0.000 N 0.C00 PN= 0.002 PY= 0.000 PC= 0.000 T1= 0.000 TO= C.000' PAFT 9 CSC 0 0.000 N1 0.000 P! 0.0C0 N 0.006~ FA= 0.0C0 PM= 0.000 PCs 0.000 Tl= 0.000 10= 0.000 PAFT 10 DSC 0 0.000 N1 0.0C0 F1 C.CCO A 0.070~ Ph= 0.002 P"= 0.000 PC= 0.000 TI= 0.000 TG= 0.000' P tJ T 11 DSC ( 0.000 N1 0.000 N1 0.000 N C.C00 PN= 0.06? PM= 0.C00 PC= 0.C00 T!= 0.000 10c 0.000~ PAFT 12 OSC C 'O.000 F1 0.000 P1 0.000 N C . C'50 PN= 0.000 Po= 0.000 PC= 0.000 Tl= 0.000 TO= 0.000 T P6PT 13 DSC C 0.000 N1 0.000 M1 C.CCO N C.C00 F9= 0.05F PP= 0.000 PC= 0.000 TI= 0.000 1G= 0.000 PAM' 14 'SC C C.000 Al C.000 v1 C.0C0 N 0.005-l Ph= 0.0C0 5"'= 0.000 PC: C.000 T!= 0.C00 T0= 0.00C
- l. A-22 4%v. O p
l ___ 'TJA %/95 1/Wf8 ( DAW l
~~
AN ALYSIS OF OYSTER CREEK CONTAIN*ENT; INT PRESS OF 0.C620 KSI.
. PAhi 15 U SC C C.000 N1 0.000 *1 0.000 N 0.000 ?
E PN= 0.0f2 PM= 0.000 PC= 0.000 TI= 0.C00 10= 0.000~ PART 16 DSC 0 ^ 000 P.1
. 0.000 F1 0.0C0 N 0.C00 Pf'= 0.0f>? t'M= 0.000 PC= 0.000 TI= 0.000 TG= 0.000
~
PART 17 CSC 0 0.000 N1 0.000 F1 C.000 N C. COO "f:= 0.0C0 PF= 0.000 PC= 0.000 TI= 0.C00 TO= 0.000 PAP,T 18 DSC Q 0.000 til 0.000 F1 C.000 h C.000 PN= 0.062 PF= 0.000 PC= 0.000 TI= 0.0C0 T0= 0.000
~
FAFT 19 DSC 0 0.000 N1 0.000 M1 0.000 N 0.0C0 PN= 0.000 FM= 0.000 PC= C.000 T!= 0.000 T0= 0.000
~
PAPT 20 DSC 0 0.000 N1 0.000 91 C.0C0 N C.000 FN= 0. 06 ? P f'= 0.000 PC= 0.000 T1= 0.000 TC= 0.000 P A f, T 21 DSC Q 0.000 til 0.000 91 C.CC0 N 0.000 P!l= 0.062 P"= 0.000 PC= 0.000 T!= 0.000 TO=~~~ C.000
~
P A P.T 27 DSC C C.000 N1 0.000 P1 0.000 t- 0.000 TN= 0.062 Pri= 0.000 PC= 0.000 TI= 0.000 TC= 0.000
~
PAET 23 PSC C 0.000 N1 0.000 M1 C.000 N C.000 PN= 0.000 PP= 0.000 PC= 0.000 T!= 0.000 10= 0.000 P A l:1 24 DSC C 0.000 N1 0.000 .Y1 C.0C0 N C.000 PN= 0. C( 2 P A' = 0.000 PC= 0.000 TI= 0.000 T0= 0.000 PAPT 25 000 C C.000 N1 C.030 M1 0.000 N 0.000 PB = 0.000 P f' = 0.000 PC= 0.000 TI= 0.000 T0= 0.000 D A .V T 20 DSC 0 0.000 N1 0.000 F1 0.000 f. 0.000 of = 0.06? PM= 0.000 PC= 0.000 Tl= 0.000 T0= 0.000 P t. r. T 27 DSC C 0.000 N1 0.000 41 0.000 N 0.000 PN= 0 . 0 ( 2 P L' = 0.000 PCr 0.000 TI= 0.000 T0= 0.C00 A-28 Dw. o
~Z2A 2b/SS ORP 2/3/67
ANALYSIS GF OYSTEk CREEK CONTAINMENTi INT PRESS OF 0.0620 KSI. PAAT 20 DSC C 0.000 N1 0.000 P1 0.000 N 0.C00 PN= 0.062 fra 0.000 PC= 0.000 Tl= 0.000 T3= 0.000 INPUT ELAPSED CPU TIME IN MINUTES = 0.0194 EQUtTIONS EL AP5EU CPU T IME 16. M INUT E S= 0.1986 SOLUT10N E L AP5FO CPU TIML lh FINUTES= 0.2030 1 l . l l 1 j- _ , A-24 4'ev. o
'T2A % /82 CX91+ 2/3/88 ..
' ANALYSIS OF OYSTER CREEK CONTAINMEbT; INT PRESS OF 0.0620 KSI..
COCI!D S PHI S THET A S SHEAI S1-52 S I- 5 3 52-S3
'I PART 1 y
FACES=-1 .___L. ?u 10.0 7.543F+C1 7.62PE+00 0.000E+CD 1.780E+01 7.62SE+00 2.54 3 E +01 36.0 1.171E+01 3.512E+00 0.000E400 9.194E+C0 3.512E+00 1.171E+01 36.0 -2.013E+00 -6.040E-01 0.000E+00 1.409E+00 -2.013E+00 -6.040E-01 40 ? 8.642E+00 9.703E+00 0.000E+00 1.Ge0E+00 8._6 4 2 6 + 0 0 9.703E+00 j 40.2 1.127E+01 1.040E+01 0.000E+00 8.699E-01 1.040E+01 1.127E+01 i 40.? 1. 3 9 0F + 01 1.110E+01 0.000F+00 2.800E+00 1.110E+01 1.390F+01 l ' l 40.2 8.653E+00 9.714E+00 0.000E+00 1.062E+00 8.653E+00 9.714E+00 40.2 1._U 7E + 01 1 041F+01 _,0,0 0 0E + 00 8.619E-01 1.041E+01 1.l_27E+0_1 40.2 1.389E+01 1.110E+01 0.000E+00 2.7S5E+00 1.110E+01 1.389E+01 44.4 1.111E+01 1.14 8E + 01 0.000E+00 3.63aE-01 1.111E+01 1.148E+01 44.4 1.120E+01 1.153E+01 0.00CF+00 s 2.571E-C1 1.12SE+01 1.153E+01 44.4 1 144E+01 1.159E+01 0.000E+00 1.504E-01 1.14 4 E +t i 1.159E+01 cofT ?
. FACES =-1. 1. P.
Q. 44.4_ _ l ._1 12 E + 01 1.149E+01 0.000E+00 3. 6 4 8E- 01 1.112E+01 1 149E+01_ 44.4 1.12EE+01 1.154E+01 0.000E+00 2.640E-01 1.123E+01 1.154E+01 44.4 1.143E+01 1.15 9E + 01 0.000E+00 1.611E-01 1.143E+01 1.159E+01 46.2 1.137E+01 1.131f+01 0.000E+00 5.169 E-0 2 1.131E+01 1.137F+Cl 4E.2 1.128E+01 1.129F+01 0.000E+00 9.569E-03 1.128E+01 1.129E+01 44.2 1.120E+01 1.127E+C1 0.000E+00 6.883E-02 1.120E+01 1.1?lE+01 46.2 1.13 7E + 01 1.132E+01 C.000E+00 5.240E-02 1.132E+01 1.1375+01 48.2 1.120E+01 1.130E+01 0.0COE+00 1.294E-02 1.12 8E + 01 1.130E+01 49.2 1.119E+01 1.127E+01 0.000E+00 7.828E-02 1.119F+01 1.127E+01 52.0 1.!?9E+01 1.12 5E 4 01 0.000E+00 1.016E-02 1.128E+G1 1.12?!+01 S?.0 1.128E+01 1.129E+01 0.000E+00 6.590E-03 1.129F+01 1.128E+01 52 0 1.12CE+01 1.12 7F + G1 0.0 JOE +00 3.006E-G3 1.127E+01 1.128E+01 PAPT 1 FACES =-1. 1. 2. 52.0 1.110E+31 1. ! ? c r. + 0 ] 0.0n0E +oo 1.09CE-02 1.12 3E + 01 1.130E+01 52.0 1.128E+0t 1.12EE+01 0.000E+00 2.234E-03 1.12ME+01 1.129E+01 3 92.J 1.127E+0) 1.120E+Cl 0.000E+00_ 6.489E-03 1.127E+01 1.129E+0L A-2K Aev. o
~7 % f /t/BS DRH 213/72
Af.' AL Y S I S Of OYSTER CR EEK CONTAINAENT; INT PP.ESS OF 0.0620 KS!. COORD 5 PHI S THETA 5 SHEAP S1-52 51-S3 S2-S3
=
PART 3 FACES =-1, 1. ?. 59.5 1.109E+01 1.105t+01 C.000E+00 4.143E-02 1.105E+01 1.109E+01 59.5 1.12SE+01 1.111E+01 0.000E+00 1 714E-01 1.11 ] E + 01 1.128E+01 59.5 1.148E+01 1.117E+01 C.000E+00 3.014E-01 1.117E+01 1.149E+0! 59.5 1.094E+01 1.10BE+01 0.000E+00 1. 3 8 5 E- 01 1.094E+01 1.10SE+01 SC.5 1.128F+01 1.119F+01 0.000E+00 9.340F-02 1.1145+01 1.128E+01 5 9 .~ 5 1.162E+01 1.130E+01 C.000E+C0 3.263E-01 1.133E+01 1.162E+01 ( 7. 0 1. 914 E + 0 ! 1.631E+01 0.000E+00 2.824E+00 1.631t+01 1.914E+01~ 67.0 1.12 7E + 01 1.385E+C1 0.000E+00 2.58SE+00 1.127E+01 1. 3 8 5 E + 0_1_ 67.0 3.390E+CO 1.139E+01 0.000E+00 7.994E+00 3.398E+00 1.139E+01 PART 4 FACES =-1. 1. 2. (7.0 3.971?+00 1.334"+01 0.000E+00 4.363E+00 9.973C+00 1.334E+01 6'.a 1.6G9F+01 1.564E+01 0.000E+00 1.?43E+CC 1.564E+01 1.689E+01
. 67.1 2.48CE+0! 1.795h+C1 0.000F+00 6.8489+00 1.795E+01 2.480E+01_
74.7 2.001E401 1.776E+01 0.000E+00 2.251E+00 1. 7 7 6E + 01 2.001E+01-74.7 1.690F+11 1.692E+01 0.100E+00 9.510E-02 1.652E+01 1.690E+01 74.7 1.379F+C1 1. 59 7F + C1 0.000F+00 2.091E+00 1.379"+01 1.587E+01
~
74.7 1.700E+01 1.692E+01 0.000E+00 8.084E-02 1.692E+01 1.700E+01 74.7 1.691F+01 1.689E+01 0.000F+00 1. 0 2 0 E-0 2 1.609E+01 1.691E401_ 74.7 1.CS2L+01 1.686E+C1 0.000E+00 4.443E-02 1.6C?E+01 1. 6 6E+01 82.3 1.994E+01 1.776E+01 C.000E+00 2.181E+00 1.776E+01 1.994E+01 S2.3 1.69CE+01 1.684E+01 C.000E+00 6.184E-0? 1.684E+01 1. 6 9 0 E + 0_1_ S2.3 1.387E+C1 1.503E+01 0.000E+C0 2.057E+00 1.387E+C1 1.593E+01 82.3 1.A?7E+r1 1.693E+C1 0.000E+00 5.325E-02 1. 6 0 7E + 01 1.693E+01 82.3 1.691E+01 1.694E+01 0.000E+00 2.803E-02 1.691E+01 1.694E+01' 82.3 1. 6 94r + C1 1.695E+01 0.000E+00 2.792F-03 1.694E+01 1.695E+01 90.0 2.0ger+0! 1.776E+01 0.000E+03 2.246E+00 1. 7 7 6E + C 1 2 . C 0_0_E + 0 1 9 G. 0 1. 6 91 T + C 1 1.693E+01 0.000E+00 3.091E-02 1.683E+01 1.691E+01 70.0 1.391F401 1.SiOE+01 0.000F+00 2.085F+00 1.331E+C1 1.590E+01 96.7 1.687E+C1 1.(93E+01 C.000F+00 5.106E-02 1.687F+01 1.672E+01-
~ '
90.0 1.691E+01 1.694E+01 C.00CE+CO 2.724E-07 1.601E+01 1.694E+01 V u A-24 I?cv. o W4 t/tlBB _ CUT H 2/3/88
ANALYSIS OF OYSTEF CREf K CLfiTAIN4Et.i; TNT PRESS OF 000620 KSI. COCRD 5 DHI S THETA S SH E W SI-52 51-S3 S2-53 PAFT 4 _ F AC ES = -1. 1. 2. _ 90.0 1.694F+C1 1.695F+0) 0.000E400 2.594E-03 1.694E+01 1.695E+01 97.7 7.006E+01 1.775E+01 0.0000+C0 2.306E+00 1.775E+01 2.C06E+01 97.7 1.691E+C1 1.682E+01 0.000E+00 9.705E-02 1.682E+01 1.691E+01 97.7 1.376E+C1 1. S S 8E + 01 0.000E+00 2.112E+00 1.376E+01 1.580E+01 97.7 1.6S7E+01 1.092E+0! 0.000E+00 5 . 2 8 t. E- 0 2 1.697E+01 1.692E+01 97.7 1.691F+0) 1._6 9 4 E + 01 0.00fF+00 2.760E-0? 1.(91E+C1 1.694E+01 97.7 1.694E+01 1.595E401 0.0COE+00 2.335E-03 1.694E+01 1.695E+01 105.3 2. 009E + 01 1.775E+01 0. 000E + 00 2.347E+00 1.775E+01 2.009E+01 105.3 1.C9PE+01 1.681E+01 0.000E +00 1.102E-01 1.681E+01 1.692E+01 105.3 1.374E+01 1.587F+C1 0.000E+00 2.126E+00 1.374E+01 1.587E+C1 105.3 1.664E+01 1.693E+01 , 0.000E+00 8.14 5E- 0 2 1.6E4E+C1 1.693E+01 105.' l . 6 41F + 01 1.694E+C1 0.000E400 3.670F-02 1.691E+01 1.694E+01 105.3 1. 6 0 75 + C 1 1.696F+C1 0.000C+00 8.041E-03 1.6969+0) 1.697E+01 113.0 2. i t! 9 E + 0 ] 1.865E+01 0.0C0E+00 3.216E+10 1.F65F+01 P.188E+01
- 11 3.0 1. 6 9 ?E + 01 1. 720E + 01 0.000E+00 2. 7 02 E-01 1.693E+01 1.720F+01 111.C 1.107Et01 1. 5 74E + 01 0.000E+00 3.775E+00 1.197E+C1 1.574E+01 P A r.1 5 fnCc5=-1. 1. 2.
113.0 1. 53tE + Cl : . 716E + C 1 C.000E+00 8.369E-01 1.632E+01 1.7165+01 117.0 1.SO4E+01 1.769E+01 0.000E+00 1. 4 7 8E- 01 1. 7 6 9E + 01 1.004E+01 113.; 1. 9 7 5t + 01 1.822E+Cl 0.000E+00 1.535E+00 1.322E+C1 1. 4 7 5E +01 119.7 2.00ZE401 1.S10E+C1 0.000E+00 1.914E+00 1.610E+G1 2.002E+01-I l_1. 7 1.005E+01 1.752E+01 0.000E400 9..'51E ^1 1.752E+01 1.60*E+01 119.' 1. 0 0 7E + 01 1.694E+01 0.000E+00 0.639E-01 1.607E+01 1.694E401 119.7 1.805E&Cl 1.0C6F+01 0.007E+01 1.306E-02 1.005c+C1 1.8C6F+01 115.7 1. 603E + 0 ! 1.RC5E+01 0.000E+00 2.423E-02 1.803E+01 1.005E+01 l !!o.7 1. 0;E+Cl 1.RCSE+01 0.30,0E+00 3.540E-02 1. 8 01 E + 01 1.PCFE+01 l'6.5 1.799E+01 1. 3 0 8E + 01 0.000E+00 1.905E+0D 1.308E+01 1.999E+01 126.5 1.80bE+01 1. 7 51E + 71 - 0.Or0E+00 5.269E-01 1.751E+C1 1.SC5E+01 l 1.694E+01 0.000F+C0 1.611E+01 1.694E+01 176.5 1.011E401 9.271E-01 A-27 Ru o 77A 7/t/4L___ MM 2/3M8 _ l
ANALYSIS Cf OYS1CR CLIEK CCF T AINf!ENTI INT PRESS OF 0.0620 KSI. C0fW D S PHI S THETA S SHEAFS 51-52 51-53 S2-S3 par 7 5 _ FACES =-1. I. 7, _
!?6.5 1."P0F+01 1.BJ5F+0! 0.000E+00 E.113E-02 1.800E+01 1.805F+01 126.5 1. 80 3E + 0 ! 1.80tE+01 0.000E+00 2.862E-02 1.802E+01 1.806E+01 1 2 /> . 5 1 300E+01 1.907E+01 0.300E +00 6.516E-03 1.8C6E+01 1 . 0 0 7 E _+ 0 1 133.2 ~ 2. 0.01E + 01 1.80SE+01 0.000E+00 1.932F+00 1.003F+01 2.001E+01 133.2 1.605E+01 1.751E+C1 0.000E+00 5.494E-01 1.751E+01 1.805E+01 L_ 134.? 1.610E+D1 1.693F+01 0.000F+00 8.336E-Cl 1,610E+01 1.693E+01 133.2 1.POCE+01 1. 8 0 6E + G 1 C.000E+00 6.168E-02 1.300E+01 1.306E+01 133 2 1.003E+01 1.807E+01 0.000F+00 4.1A4E-02 1.803E+01 1.8C7E+01 13?.2 1. 8 0 6F + 01 1.808E+01 0.000E+00 2.202E-02 1.806E+01 1.803E+01 140.0 2.040E+01 1.775E+01 0.000E+00 Z.654E+00 1.775E+C1 2. C4 GE + 01 140.3 1.807E+01 1.7C6E+C1 3.000E+00 1.013E+C0 1.706E+01 1. E 0 7 F + 01_
140.0 1.574E4C1 1. 6 3 7E+ 01 0.000E+00 6.285E-01 1.574E+C1 1.63 7 E +01 140.0 1. 02 EF + 0! 1.776F+01 0.0f0E+03 5.?00E-01 1.775E+01 1.828E+01 140.0 1.534E+01 1. 7 5 7E + 31 0.DCP +00 3.699E-01 1.767E+01 1.904E+01 14^.0 1 79 0E +ol 1.75cE+C1 C.000E+0C 2.097F-01 1.7F9E+C1 1.780r+01_ 14 0 . 7 - ', . 7 0 3 E + 0 0 2. 22 7E+ 01 C.000E+00 2.697E+01 -4.703E+00 2.227E+01 14(.7 1.74'E+01 2.E85E+01 0.000E+00 1.138E+01 1. 7 4 7E + 01 2.885E+01 146.7 3.964E+C1 3.644F+01 0.000E400 4.206E+0C 3.544E+C1 3.964E+01 P A i: T 6 FALES -l. 1. 2. 213.4 2.067E+00 2.522E+31 C.000F+00 2.316E+01 2.06 7E +00 2.522E+01 21 3. 4 4. 91 CF 4 00 2.576E+01 0.0COE+30 2.085E+01 4.910E+00 2.576E+01 213.4 7.753E+00 2.629E+01 0.0CCE+00 1.854E+01 7. 7 53 E+ CO 2.629E+01 22 4.7 2.33CE+0' 2.330E+01 0.000F+00 2 . 0 9 6 F + 0 '1 2.33GE+C0 2.330E+C1' 2?o.7 ' .9019 00 2.336E+01 0.000F+00 1.945E401 3.001E+00 2. 3 56 E +01 224.7 S.464E+(0 2.342L+Cl 0.0000+00 1.795E+01 5.464E+CC 2.342t+01 229.7 2.33EE+0C ?.330E+01 0.000E+00 2.C96Ft01 2.33eE+00 2.330Et01 224.7 3.901E+00 2.336E+C1 0.0uoE+03 1. 94 6E + 01 3.9CIE+00 2.336E+01 224. 7 9.4e6E+0C 2.342F+C1 0.000E+00 1.795E+'l 5.4^4E+00 2.342E+01 230.0 ' 446E+0c 2.004E+C1 0.0 3CE + 00 1.460E+01 5.446E+00 2.004E+01 236.1 1.124E+00 1.903F+01 0.000E+0D 1.590E+0! ?.124E+CO 1. 90 2E + 01
?36.3 8.020E-O! 1.000F+01 C.000E+0C 1.720E+01 8.020E-01 1.800E+01
[ _ A-28 (!c v. o u l T~.l& Y2/0? OA'N 1/J M 8 l c l
ANALYSIS OF CYSTEP CREEK CONTAINVENT; [NT PRESS OF 0.0670 KSI. CO CI' O S PHI S TFETA 5 SHEAP. 51-52 51-53 52-S? P4hT 6 ___ _ FACES =-1. L. 2. _ 23f.0 5. 4 4 5E+ 00 ?.004E+Cl 0.000F+00 __1.460F+01 S.445E+00 ?.004C+01 236.0 3.124E+00 1.902E401 0.000E+C0 1.590E+01 3.124E+CC 1.902E+01 P36.0 8.0??E-Ol 0.000E+00 1.720E+01 8.0 22 F- C l 1.000E+01 1.9}0E+01 24).3 6.057E+00 1.503E+C1 0.000E+00 9.773E+00 6. 0 5 7E + CO 1.583E+01_ 247.3 2.061E+00 1.466E+01 0.000E+00 1.200E+01 2.661E+00 1.466E+01
?47.1 - 7. ? 41 F- 01 1. 34 8E + 01 0.000E+00 1.422F+01 -7.341F-01 1.348E+0!
24 2 6.057E+00 1.563E+01 0.000E+00 9.773E+00 6. 0 5 7E + 00 1.583E+0! Z_.3 2 . /. 61 E + 0 0 1. 4 6 6F + 01 C.000E+00 1.200E+01 2.061E+00 1.4665+01 247.2 -7.140E-01 1.348E+01 0.000E+00 1.422E+01 - 7. 3 4 0E - 01 1. 34 3 t +01 755.7 4. 54 5E+ CC 1.23CE+01 0.000E+30 7.752E+00 4.545E+00 1.2300+01 258.7 ?.*SCE+00 1.162E+01 C. 000E + 00 9.173F+in ?.450E+CO 1.16?C+01 253.7 3.55EE-01 1.095E+01 0 000E+00 1.059E+01 3.552E-C1 1.C95E+01
?Sr.7 4.695F+a0 1.?iOE + C l 0.000E+00 7.752F+00 4.54SE+00 1.23nF+01 25E.7 2. 4 5 0E + t'0 1.162E+01 0.000E4C0 C.173E+00 2.450E+0C 1.162E+01 2 r. C . 7 3.56CE-01 1.095E+01 C.000E+00 1.059E+01 3.560E-01 1. 0 9 5 E LO_1
?70.0 ?.4,SE+00 1.014E+'l 0.000E+00 6.473E+00 3. 6 6 9E + 10 1.014E+01 271.0 2. 39 5E + 0 C 9.759E+00 C.00GE+00 7.364E+00 2.395E+C0 0.757E+00
?70.0 1.l???+00 C.377r+0C 0.000F+00 3.255E+00 1.120E+00 9.377E+00
'P A h T 7 FACES =-1. 1. 2.
0.d" 3.6SLE+00 1.C14E+01 0.000E+00 6.473b+00 3.068E+00 1.014E+01
. 0,0 2. 39 5E + 3 0 9.759E+00 0.000E+C0 7.364E+00 2.3CSE+00 9.759E+03 -
[~ 0.0 1.123E+0u 9.377E+00 0.000E+00 4.254E+00 1.123E+C0 9.377E+6d' 1.1 3.673E*00 1.003E+01 0.000E+00 5.257E+00 3.673E+00 .l .0 03 E +51~ 1.1 2.Ps5E+10 9.646E+00 C.000E400 7. 2 51E + 00 2. ? 9 5E + 0 0 9.646E+01 1.1 1.1185+00 9.263E+00 0.0JJE+03 B.149E+00 1.110F+00 9.263E+00 ' 2.3 3.t05E+00 0.903E+0C C.000E+0) 6. 29 7 + 00 3.605E+00 9.903E+00~ 2.3 7.399E+0C o.540E+00 0.00CE+00 7.]44F+00 ?.?95F+0C 9.540E+0C 2.3 1.lBiE+CO 4.'77E+C0 C.000E+00 7.991E+00 1.!P6E*00 9.177E+00 1.4 3.46?d+0' 9.760E+0C 0.000E+00 6.293E+00 3.4 6 7E+ CO 9.760E+00
- 2. 4 ?. ? 9 5E + C C 9.4 3 8E+ 0 0 0.00nF+00 7.043F+00 2.395F+00 9.438E+00 3.. 1.324E+00 9.117E+0C 0.000E+00 7.793E+00 1.324E+C0 9.!!7f+00 l A - 29 Ece o
[ Ts)A A$> - DJPN 213/8s i
ANALYS!S OF OYST EC CREFK CONT A INMENTl INT PRESS OF 0.0620 KSI. CDCHO 5 PHI S THETA S SHEAR 51-52 51-S3 52-S3
,' PtVT _! _
EACES=-1._ lm__2_. _ 4.5 1. 2 E EE + C O 9.601F+00 0.000E400 6.343F+00 3.256E+00 9.601F+00 4.S 2.395C+00 9.342E400 0.000E+00 0. 9 4 7E + 00 2.395E+C0 9. 44 2E +00 4.9 1._5 3 2 E + 00 9.033E+00 0.0000+00 7.551E+00 1.532E+00 9.0P?E+0C
~~
PAPT 8 FACES =-1. 1. 2. 0.0 2.814E+01 1.707E+01 0.000E+00 1.107E+01 1. 7 0 7E + 01 2.814E+01
- 0. 0 1.040E+0) 1.174E+01 0.000E+00 1.341F+00 1.040E+01 1.174E+01 C. 0 ~ 7. 3 3 3E + 00 6.424E+00 0.000E+00 1.376E+01 -7.333E+00 6.424E+00 1.0 2.41CE+01 1.593E+01 0.000E+00 8.253E+00 1. 59 3E + 01 2.416E+01 1.9 .
1.04CE+01 1.179E+01 0.000f+00 1.391E+00 1.040E+01 1.179E+01_ l.0 - 3. ? 74 E + 00 7.ob1E+00 0.000E+00 1.104E+Ci -3.?74E+00 7.661E+00 2.1 2.072E+C1 1.517E+01 0.000E+00 5.968E+00 1.517E+01 2.C72F+01
? ,, 1 1.040E+01 1.207F+01 0.000E+00 1.671E+C0 1.040C+Cl 1.2075+0) 2.1 3. 94 9E-02 0.080E+00 0.000E + 00 8. 8 91E + 0 0 0. 9 4 0E- 0 2 E.9e0e+00 3.1 1. 7 7 3F + Cl 1. 47 ?f + 01 0.000E+00 3.006E+00 1. 4 7 3 E + 01 1.773E+01 3.1 1.040E+01 1. 2 5 3E + 01 C.000E+00 2.124E+^0 1.049E+01 1.253E+01 3.1 3.174E+00 1.033E401 0.000E+00 7.255F+00 ?.074E+00 1.033E401 4.1 1.520E+0) 1.454E+01 0.000E+00 6.592E-01 1.4 5 4 E + C1 1,520r+01 4.1 1.040E+01 1.310E+01 0.000E+00 2. 700E & 00 1.040E+C1 1.31CE+01 4.1 5.604E+00 1.166F+0] C.000E+0C 6.060E+GO 5.604E+00 1.166E+01 5.2 1.310E+0! 1.457E+01 C.003E+00 1. 4 72E + CO 1.215E+01 1.457E+01 6.2 1.040F+01 1. 3 7 6E + 01 0.000E+00 3.357E+00 1.040E+01 1.376E+Cl 5.2 7.711E+00 1.295F+01 0.00CE+00 5.242E+00 7.711E+00 1.295E+01 l 6.? 1.130E+0] 1.475E+01 0.000E+00 3.377F+00 1.13BE+01 1. 4 7 5E + 01
( 6.2 1._C 4 CE + C 1 1.440E+01 0.000E+00 4.059E+00 1.040E+01 1. 4 4 6 F + 01__ J
!.2 9.430E+00 1.417E+01 0.000E+00 4.740E+10 9.4306+00 ' 417E+01 7.2 1. 0 C 1 f + 01 1.5C6E+01 0.000E+00 5.056E+73 1.001F+01 1.5C6E+C1 7.2 1.040E+01 1.510F+01 0.000E+00 4.777E+CO 1.040E+01 1. 518 6 +01 7.2 1.03CE+01 1.530E+01 C.000E+00 4. 499E + 00 1.0POE+01 1.53CE+01 d.3 d.945E+0C 1. 54 6t + 01 0.000E+00 6.511F+00 d.945E+00 1.546E+01 I R.3 1.04?E+01 1.589E+C1 C.0CJE+C0 5.490E+0C 1.040E+01 1. 5 30 F + 01 9.3 1.136E+01 1.633E+01 0.00]E+00 4.469E+00 1.106E+01 1.67?F+01 9.3 P.15 4E 4 C0 1. 5 91r + 01 C. 600E + 0C 7.753E+01 0.154E+CO 1.591E401 9.3 1. 9 '. 0 E + 01 1.65CE+01 0.000E+00 6.178E + 0 C 1.040E+01 1.658E+Cl l A-30. ney. o B
N & 'l.lb8 -- - l DRH 2J3/88
ANALYSIS OF OYSTER CREEK CONTA INME Nii INT P?ESS OF 3.0E20 KSI.
~
COC9D S PHI S THETA 3 SHfAR S1-52 51-53 S2-S? PAFT C races =-I m t. 2, 9.3 1.265E+01 1.726E+01 C.000F+00 4.604E&OO !.263E+0) 1.726E+01 1 Q, 3 7,595E+00 1.639E+01 0.000f +00 0.795E+00 7.595E+00 1.639E+01 10.3 1.040E+01 1. 7 2 3E + 01 0.000F+00 6.630E+00 1.040E+01 1.723E+01 i n,_d 1. 3 _lD 01 1.808F+01 0.000E+00 4,864E+00 1. ' 21F102 1.lG8E+01_ 10.3 7.60CE+00 1.639F+0! 0.000E+00 3.793E+00 7. 6 COE + 00 1.637E+01 10.3 L,040E+0J 1.723E+01 0.000E+00 6.031E+00 1.040E+01 L.723F+01 10.3 1. 3 21 E+ 01 1.808E+01 0.000E+00 4.869E+00 1.321E+01 1.808E+01 11.4 7.22CE+C0 1.689E+01 C .'00 0 E + 0 0 9.651E+00 7.239E+00 1.689E+01 11.4 1.040E+01 1.794E+01 0.000E+00 7.436E+00 1. 0 4 0E + 01 1.784E+Cl 11.4 1.3579+C1 1.879E+01 0.000E+00 5.222E+00 1.357E+01 1.9775+01 12.4 7.041E+00 1.738E+01 0.000E+00 1.034E+01 7.041E+C0 1.738E+01 12.4 1.C40E+01 1.939E401 0.000E+00 7.999E+00 1.040E+01 1.3?9E+01 12.4 1.3765+01 1.940E + C 1 C.000E+00 5.636E+00 1.3766+C1 1.940E+01 13.5 6.917E+00 1.766E401 0.000E+00 1.088E+01 6.977E+00 1.706F+01 13.5 1 0 4 CE + 01 1. 8 89E+ C 1 0.000E+00 9.486F+00 1.040E+01 1.800E+01 13.5 1.383E+01 1.992E+C1 C.C0CE+00 6.087E+00 1.363E+C1 1.992E+01 14.5 7.018E+00 1. S 31E 4 01 0.000E400 1.130E+01 7.011E+00 1.031E+01 14.5 1.qqns+n! 1.o33E+01 C.000E400 E.925E+00 1.040E+01 1.933E+01 14.5 1.379E+01 2.0 34E +01 0.000E+00 6.556E+00 1.?7?E+C1 2.034E+01 1E.5 7.14 CE + C O 1.873E+01 0.000E+00 1.159E+01 7.140E+0C 1.873E+01 15.5 1.040E+01 1.971E+01 0.CCOE+00 9.309E+00 1. 0 4 0E + C 1 1.971E+01 15.5 1.367E+01 2.069E+01 0.000Et00 7.025E+00 1.367E+01 2.069E+01
~
16.6 7. 2JE+0? 1.912E+01 C.000E +00 1.179E+C1 7.323E+00 1.912E+01 16.6 1.040E+01 2.004E+01 0.000E+00 9.63SE+00 1.040E+01 2.CC4E+C1 16.5 1.34SE+01 2. 09 7E + C 1 0.000E+00 7.462E+00 1.348E+01 2.097E+01 17.6 7. 54 9 E + n 0 1.946E+01 0.000E+00 1.191E + 01 7.543E+0C 1.546E+01 17.6 1.040E+01 2.032F+01 0.000E+00 9.916E+10 1.04^F+01 2.02?E+01 17.6 1.326E+01 2.118E + C 1 0.000E+00 7. 917E + 00 1.325E+01 2.118E+01 18.6 7.80CE+00 1.977E+01 0.000E+00 1.197E+01 7.CCOE+00 1.977E+01 l 1c.6 1.040E+01 2. 0 5 5E + C 1 0.000E+00 1.015F+01 1.040E+01 2.05 5E +01 18.6 1.201E+C1 2.133E+01 C .000E + 00 d.324E+00 1.301E+C1 2.133E+01 19.7 e. ]^ 7E + 0 0 2.003E+01 0.000E+JO 1.10?F+01 d.067F+00 2.003F+01 10.7 1.040E+01 7.0 74E + C1 0.000E+00 1.033E+cl !.04"E+Cl 2.074E+01 1.274E+D1 2.144E+01 0.CJOE+00 8.697E+00 1.274C+01 2.144E+01 1 19.7 A-RI nev o e NI _i-[83__ _ M YY l
~
ANALYSIS OF OY Sl ek CREEK UIN T A IN'iEN T ; INT PLESS OF 0.0620 KSI. CCCR0 5 aH1 S THETA S SHEAR 51-52 51-53 S2-S3 PA:T S _ __
- 1. '
_ IACEJ=-1. . ,)
?0.7 S.313E+00 7.026E+01 0.000E400 1.19 3E + 01 3.330E+00 2.076E+01 20.7 1.040E+C1 7.008L+01 G.000E+00 1.04aE+01 1.040EtC1 2.C88E+01 20.7 1. 24 79 + 01 2.150E+01 0.000E+00 9.035E+00 1.247E+01 2z160E+01 20.7 E.343E+00 2.027E+01 0.000E+00 1.172E+01 8.343E+00 2.027E+0!
20.7 1.040E+01 7.099F+01 0.0COE+00 1.048E+01 1.040E+01 2.088E+01_ 20.7 1.246E+01 ?.150E+01 0.000E+00 9.039E+00 1. 2 4 6E + 01 2.150F+01
~
21.7 8.610E+00 2.046E+01 0.000E+00 1.18SE+01 8.610E+00 2.046E+01 21.7 1.040E+01 2.100E+01 C.000E+00 1.060E+01 1.040E+01 2.100E+01 21.7 1.220E+01 2.154E+01 0.000E+00 9.340E+00 1.220E+01 2.154E+01 22.9 3.065E+00 2. 0 6 2E + 01 C.000E+0d 1.176E+01 c.P66E+00 2.062F+01 22.8 1.140E+01 2.108E+01 0.000E+00 1.06SE+01 1.040E+01 2.100E+01 22.3 1.194E+C1 2.154E+01 0.000E+00 9.603E+00 1.194E+01 2.154F+01 23.0 9.133E+30 2.075E+01 0.000E+03 1.164E+01 E.10CE+CC 2.075E+01 2'.S 1.04CF+D1 2.ll4E+01 0.000E+00 1.074E+01 1.040E+01 2.114E+01
'23.8 1.17 0E + 01 2.153E+J1 0.000E+00 9.831E+00 1.170E+01 7.153E+01 24.1 9.33IF+3G 2.035E+01 0.000E+00 1.152E+01 9. 3 31E + 0 0 2.096E+01
?4.? 1.04^E+01 2.113E + 01 0.000E+00 1.077E&01 1.040E+01 2.118E+01_
24.3 1.14EE+01 2.190E+01 C.000E+00 1.0C2E+01 1.19 9E + 01 2.150E+01 29.9 9. 5 3 4 E+ 00 2.094E+01 0.000E+00 1.140E+01 9.534E+0C 2.094E+01 25.9 1.0405+01 2.12 0E + 01 0.000E+00 1.079E+C1 1.040E+01 2.120E+01 25.c 1.12 7E + 01 2.146E+C1 0.000E+00 1.013E+01 1.12 7E + 01 ?.146E+01 26.9 9. 7169 + CO 2. 0 9 9E + 01 0.000E+00 1.128E+01 c.716E+00 2.000E+01
?6.9 1. 0 4 0 E- + 0 ) P .120E+ C1 0.000E+00 1.060E+01 1.040E+01 2.120E+01 26.0 1.10cE+r1 2.141E+01 0.000E+00 1.032E+01 1.109F+01 2.141F+01 27.9 9.37tEtCD 2.103E+01 0.000E + 00 1.116E+01 9.876E+00 2.103E+01 27.9 1.040E+C1 2.119E+01 0.000E+00 1.079E+01 1.040E+C1 2.119E+01 27.1 !.397E+01 2.12 5 E + 01 0.000E+00 1.042E+01 1.093E+01 2.135E+01 2 t' . C 1.001E+01 2. l C 61 + C 1 0.000E+00 1.104E+01 1.001E+01 2.1C6E+01 29.0 1.040E+01 2.11?E+01 0.000E+00 1.077E+01 1. 0 4 0E + 01 2.118E+01 29.0 1. C 79E F C 1 2.129E+C1 0.000E+00 1.050E+01 1.079E+01 2.129E+01 30.0 1.u13L+ul 2.107E+01 0.000E+00 1.094E+01 1. 013E + 01 2.1C7E+01 30.0 1.040F+r1 2.119E+01 0.000E*UD 1.075F+01 1.043E+01 2.115F+01 30.0 1.007r+01 2.123E + 01 C.000E+00 1.056E+C1 1.0L7E+01 2.123E+01 31.0 1.02?C+31 2.108E+01 0.OOOF +C0 1.034E+01 1.023F+01 2.1CSE+01 J ?1.0 1.040E+01 2.113E+01 0.00CE+00 1.072E+01 1.040E+]l__2.113E+01_ _
A-32 12c: v. o
- .- T /A 0 h l 08-- -
0VN 2/3/8f I
3
' ANALYSIS:CF CYSTEF CREEK CCNTAINMEN1; INT PRESS GT 0.0^20 KSI.
COORD S PHI S THETA S SHEAR 51-52 S1-53 S2-S3 PART 8
. FACES =-1. 1. 2.
21.0 1 067E+01 2 .116 F + 01 0 . 0 00 F '+ 00 1.060F+31 1.057E+01 2.118E401 31.0 1.024E+01 2.108E+01 0.000E+00 1.084E+01 1.024E+C1 2.1CPE+01 31.0 1.040E+01 2.113E+ 01 0.000E+00 L.072E+01 1.040E+01 ?.113E+01_ 31.0 1.057E+01 P.118E+01 0.000E+00 1.061E+01 1.097E+01 2.118E+01 32.1 1.03?E+C1 2.10 7 E + 01 C.000f+00 1.075E+01 1.032E+01 2.1C7E+01 32.1 1. 04 0E + 01 _ 2. l l0E+ 01 0.000E+00 1.069E+01 1.040E401 2_._L10 E t 01 32<1 1.049E+01 2.112E+01 C.000E+C0 1. 0 6 4 E +~ 01 1.049E+C1 2.112E+01 33.1 1. 03 7E + 01 2.106E+C1 0.000E+00 1.068E+01 1.039E+01 7.106E+01 33.1 1.04DE+01 2.lO7E+01 0.000E+00 1.066E+11 1.040E+01 2.107E+01 33.1 1.04?L+01 2.107E+01 0.000E+00 1.065E+01 1. 0 4 2E + 01 2.107E+01 34.1 1.044E+01 2.105E+01 C.000E+00 1.061E+01 1.044E+01 2 .10 5 E + 01
'4.1 1.040F+01 2.104E+01 0.000E+00 1. 0 6 3E + 01 1.040E+01 2.104E+01 34 1 1. 0? 70 + 01 2.102E+01 0.000E+00 1.066E+01 1.017E+01 2.102E+01 35.2 1.040E+C1 2.103E+01 C.000E+00 1. 0 5 5E + 01 1.049E+01 2.103E401 35.2 1.040E601 2.100E+01 0.000E400 1.060E+01 1.040E+01 2.100E+01_
35.2 1. 03 3E + 01 2.098E+01 0.000E+00 1.065E+01 1.033E+01 7.098E+01
~
36.2 1.051E+0) 2.101E+01 0.000E+00 1.050E+C1 1. 0 51E + C l 2.101E+01-36.2 1.040F+01 2.048F+01 0.000F+00 1.057F+01 1.040E401 7.09PE+01 36.2 1.C30E+0i 2.094E+01 0.000E+00 1.064E+01 1.030E+01 2.094E+01 37.2 1. 05 3E + C1 2.C98E+01 E.~000E+00 1.046E+01 3.053E+C1 2.098E+01 37.7 1. 04 CE + 01 2. 0CSE + 01 0.000E+00 1.054E+01 1.040E+01 2.095E+01 37.2 1.020E+01 2.091E+01 0.000E+C0 1. 0 63E + 01 1.02SE+01 ?.091E+01 3d.3 1.154E + C1 2.096E+01 0.000Et00 1.042E+01 1.054E+01 2.09tE+01 36.2 1.040F+01 2.092E+01 C. 0 0 0F + 00 1.052E+01 1.040E+01 2.092E+01 38.3 1.027E+01 2.098E+01 0.000E+00 1.061E+01 1. 0 2 7E + 01 ?.C88E+01
~
39.3 1.054E+C1 2.094E+C1 0.000E+00 1.040E+01 1.054L+01 2.094E+01 1 37.3 1.0*0E+01 ?.090E+01 0.000E+00 1. 04 9E + 01 1.04CE+01 2.090E+01 3 9. "$ 1. 0 ? 6f + 01 2.086E+01 0.000E+0C 1.059E+01 1.0?6E+01 2.086E+01 40.4 1.054E+01 2.092E+0! 0.000E+00 1.038E+01 1.054E+01 2.092E+01-40.4 1.040E+01 2.069E+01 0.000E+00 1.047E+01 1.040E+01 2.CC8F+01 40.4 1. 0 2 6E + 01 2.083E+C1 0.000E+00 1.057E+91 1.025E+01 2.083E+01 l 41.a 1.054L401 2.090E+01 v.000E+00 1.036E+01 1.054E+C1 2.090E+01 \ 41.4 1.C40E+01 2.086E+01 0.030E+00 1.345F+01 1.043F+01 2.086E+01 41.4 1.02 7E + 01 2. 0 9 2E + 01 0.000E+00 1.055E+01 1.0275+01 2.092E+01 ] N A -32 Ee v. o h _ 88 OMt ;2/3/7d' l 1
ANALYSIS OF CYSTEL CR EEK CON 7AINMENT; INT PRESS OF 0.0620 KSI.
~
C00a0 S nHI S TFETA S SHEAR SI-52 51-53 52-53 PWT a _ __ fares =_1. 1. 2. 41.4 1.054Fe01 ? . 09 0F+ 01 0.000E+00 1.076E+01 1.354E+01 2.090E+01
,1.4 1.040E+01 2.085E+01 0.000E+00 1. 04 6E + 01 1.040E+0L 2.086E+01 41.4 1. 0 ? t E + 01 2.002E+01 0.000F+00 1.095F+01 1.026E+01 2.08_2E+01_
42.4 1. 3 5_4 E + 01 2.^33E+Cl 0.000E+00 1. 0 34E+ 01 1.054E+01 2.083E+01_ 42.4 1.040EF01 2.784E+01 0.000E+00 1.044E+01 1.040E+01 2.084E+01 42.4 1.027F+0) 7.780E+01 0.000E+00 1.053E+01 1.027E+01 7.080c+01 4 ?. 6 1.053E401
?,087E+0J 0._000E+00 1.034E+01 1.053E+01 2.017r+01_
43.5 1.04CE+?! 2.083E+01 0.000F+00 1.043E+01 1.040E+01 7.003E+01 43.5 1,028E+01 2.0 77E + C 1 0. 0 00 E + QO 1. ^ 5 ] E + 01 1.029E+01 2.079E+01 44.E 1.052r+01 7.08sE+01, 0.003F+0C 1.033E+01 1.052F+Cl 2.085E+01 44.5 1. 04 0E + 01 2.0 92E+ C1 0.0002+00 1. 0 'e l E + 01 1.040E+01 2.082E+01 44.5 1.0?9E+01 P.078E+C1 0.000E+00 1.050E+G1 1. 0 2 9E + 01 2.078E+01 45.c 1. 0;lE + Cl P.084E+01 0.000E+00 1.033E+01 1.051E+01 2.084E401 45.5 1.040F+^1 2. Cele +01 0.000E+00 1.040Eini 1.040E+01 2.081E+01 45.6 1.030E+01 7.077F+01 0.000F+00 1.048E+01 1.03CE+01 7.077E+01
, 46.o 1.050E+01 2.083E+01 0. 0 0 0E + 00 1.033E+01 1.050E+01 2.033E+01 46.o 1.040E+01 2.030E+01 0.000E+00 1. 040E + 01 1.040E+C1 2.08CE+01 46.6 1.031E+01 2.077E+01 0.000E+00 1.046f+01 1. 0 31E + 01 2.077C+Cl 47.6 1.749:+01 7.092E+01 C.000F + 00 1. 0 3 3E + 01 1. 0 4 4E + 01 2.032E+01 47.6 1.04CE+01 2.079E+C1 0.000E+0C 1 039E+01 1.040E+01 2. 079E +01 47.6 l_._C 31 E + 01 P . 0 7 7E + 01 0.000E+00 1.045E+01 1.031E+01 2.077F+01_
48.6 1.048E+01 2.081E+01 0.000E+00 1.033E+01 1. 0 4 9E + 01 2.CRIE+01 2.079E+01 43.6 1.040E+01 2.079E+01 0.000E+00 1.038E+01 1.040E+01 4 3. f> 1.032E+Cl 2.076F+Cl 0.000E+00 1.044E+01 1.03?E+01 2.076E+01 49.7 1.040E+01 2.001E401 0.000E+00 1.033E+01 1.048E+01 2.081E+Cl 4?.7 1.040E+01 2. 0 7 eE + 01 C.000F+00 1.03BE+01 1.040E+01 2.078E401 4'.7 1.'33E+C1 2.0 76E + C 1 0.0CCE+C0 1. 04 3E + 01 1.033E+01 2.076E+01 l l 53.7 1. 04 7F & C 1 2.080E+01 0.000E+00 1.033E+01 1.047E+01 2.0SOE+01 50.7 1.]40E+G1 2.0 7 9E + 01 0.00CE + 00 1.038E+01 1.040E+C1 2.073E+31 3 50.7 1.014E+01 2.076E+01 0.000E+00 1.042F+01 1. 034E + Cl 2.076E+01 [ 61.7 1.046F+c1 7. 0 80F + 01 C.OCOE+00 1.033E+01 1.046E+01 2.000E+31_ S 1.7 1.040E+01 2.070E+01 C.000E+00 1.030E+01 1.040E+C1 2.078F+01 I 51.7 1. 614 E + C 1 2.076E+G1 0.00CE+00 1.042E+01 1.C34E+C1 2.C76E+01 l 51.7 1.c;7t+01 2.080E+01 0.000E+00 1.033E+n1 1. 0 4 7E + C 1 2.080E+01 E 1. 7 ! . n c f, E + 01 2.C78E+C1 0.000E+00 1.C38F+01 1.040E+01 ?.076F401 A-34 Dev. o
'7J" A */2/K9 ORM .2/.?/ J'8 _
ANALYSIS CF CY S T E P CF.EEK CO NT A INPE NT t INT POESS OF 0.0620 KSI. CHORD S PHI S THETA S 5 HEAR $1-$2 51-53 52-53 PAPT 8 _, FACFS=-1. 1. ?. ___ 51.7 1.734c+01 2. 0 76E + 01 0.000E+00 1.042E+01 1.034E+01 2.076E+01 52.d' 1.047E+01 2. OS OE + 01 0.000E+00 1.033E+01 1.0470+01 2.080E+01 52.8 1.040E+01 2. 0 7 8E + 01 0.000E+00 1.038E+01 1.040E+01 2.078E+0l~~ 52.8 1.034E+01 2.076E+01 0.000E+00 1.042E+01 1.034E+01 2.0765+01 57.C 1.046F+C1 2.0SOF+Cl 0.000E+00 1. 0 34 E + 01 1. 04 6 E + 01 2.060E+01 53.S 1.04GE+01 2.078E+01 0.000E+00 1.038E+01 1.040E+01 2.078E+01 5?.8 1.034E+C1 2.076C+0] 0.000E+00 1.042E+01 1.034E+01 2.076E+01 54.3 1.046E+01 2.080E+C1 C.000E+00 1.034E+01 1.046E+C1 2.080E+01 54.A 1.04CE+01 2.078E+01 0.000E+00 1.03eE+01 1.040E+01 2.078E+01 64.A 1. 03 4F + C1 2.077F+01 0.000E+00 1.04?F+01 1.039E+01 2.077E401 55.0 1.047E+01 _ 2.ORIE+01 0.000E+00 1.036E+01 1.047E+01 2.061E+01 55.9 1.04CE+21 2.079E+C1 C.000E+00 1.03RF+01 1.040F+01 2.079E+01 55.9 1.034E+C1 2.077E+0! 0.000f+00 1.C43E+C1 1.0345F01 2.077E+01_ 56.7 1.067F+01 2. 9 81 F + 01 0.000F400 1.014E+01 1.047E401 2.081F+01 St.o 1.040E'01 2.0 79E+ C1 C.000E+00 1.034F+01 1.040E+01 2.079C+11 5( .9 1.03sF+C1 2.077E+C1 0.000E+30 1. 04 3E + 01 1.034E+01 2.077E+01 5 ?.9 1.04 7E + 01 2.082E+01 0.000E+00__1.035E+01 1.047E+01 2 . 0 8 2 E + 0_1_ 57.9 1. '4 ]F + 01 2.08CE+01 0.000E+00 1.039E+01 1.040E+01 2.0BCE+01 , j' 57.9 1. .' 3 4 F + 01 2.078F+01 0.000E+C0 1.044E+01 1. 0 3 4 E + 01 2.078E+01 59.0 1.047r+01 2.082E + C1 0.000F+00 1.035E+01 1.047E+01 2.092E+01 59.0 1.040E+C1 2.060C+01 0.000E+00 1.040E+C1 1.040E+01 2.080E+01 69.0 1.033E+C1 2.n78E+01 0.000F+00 1.045E+01 1.033F+01 2.078E+01 60.0 1.04PE+01 2.083E+01 0.000E+C0 1.036E+01 1.04dE+01 2.083E+01 6L.0 1.04DE+C1 2.081E+01 0.000E+00 1.041E+01 1. 0 4 0E + C 1 2.C81E+01 60.0 1. 03?E + 01 2.079E+01 0.000E+00 1. 04 6 E+ 01 1.033E+01 ?.079E+01 61.0 1 04 0E + 01 ?.094E+01 0.000E+00 1.036E+01 1.040E+01 2.084E+01 61.0 1.04CF+C1 2. 0 3?E + 01 0.000E+00 1.042E+01 1.040E401 1.032F+01 01.0 1.033E+C1 2.090F+01 C.000E+C0 1.047E+01 1.033c+01 ?.080E+01 62.1 1.04CF+01 2.085E+01 0.000E+00 1.037E+'l 1.04SE+01 2.085E+01 62.1 1.04 CF4 C1 2.0E3F+C1 0.CCOE+00 1.043E+01 1.040E+01 2.083E+01 02.1 1.032E+01 2.0 PIE +Cl 0.000E+07 1.048E+C1 1.032F+01 2.081E+01_ l l 62.1 1 049E+C1 2.066E + C1 0.000F+00 1.037E+01 1.049E+01 2. 086 E +C 1 c2.1 1.040d+91 2.001F+r1 C.000E400 1.043E+01 1.040E+C1 2.083E+01 (. 2.1 ? . 0 81 E + M 0.000E+0C 1 049F+01 1.032E+01 2.001E+01 I 1. 0 3 2 E. + C 1 l A-M Rev. o B [ NM _!dO _ ORM V3/18 r t . _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ . _____ __ _ _ _ _ _ _ _ _ w
+
;4NALYSIS Of Ov3TEP CGEEK CONTA NMENTI INT PRESS OF 0.0620 XSI.
COCR0 5 PHI S TFETA S SHE4P. 51-52 SI-53 52-53
- PAFT ?
FACES =-1. 1._,2. . 84.3 8,. 4 4 5 F + 0 0 2.022E+01 C .000E +00 1.137E+01 8.P45E+C0 2.072E+01, U4.0 1.04CE+01 2.069E+01 0.000E+00 1.028E+01 1.040E+01 2.069E+01 84.3 1.1'4F+01 2.115E+01 0.000f+00 9.193E+00 1.196E+01 2.115E+01_ 35.9 8.695E+00 2.004E+01 0.000E+00 1.13SE+01 e. 6 6 5E + C0 2.004c+01_ 85.9 1. 04 0E + C1 2. 0 5 5 F + 01 0.000E+00 1.015E+01 1.040E+01 2.055E+01 85.9 1.21?E+01 2.10 7E + C 1 0.000E+C3 3.947E+00 1.212r+01 2.107 F +01' 06.9 8.539E+00 1.933E+01 0.003E+00 1.12 9 E + 31 - 8.S39E+00 1.9R3E+01 86.9 1. 040E + 01 2.039E+01 0.000E+00 9.937E+00 1.049E+01 2.039E+01
?(.9 1.227E+01 2.095E+C1 0.000E+00 9 . 6 8 2 E_ + C 0 1.227E+01 2.095E+J1 E7.9 E.41/F+C0 ,
1.960E+01 0.000c+00 1.11RE+01 8.416E+00 1.960E+0!
?.7.9 1.04 E+rt 2.020E+01 C.0COE+00 9.773E+C0 1.041E+01 2. 02 0 F +01 07.9 1.?39E401 2.079E+01 0.000E+00 8.402E+00 1.239E+01 2.079E+01_
_jB9.0 E.32(E+CO 1.935E+0! 0.000E+00 1.102E*01 S.326F+00 1.935E+01 c 9.G 1.040E+01 1.997E401 0.000E+C0 9.557E+00 1.040E+01 1.S97F+01 0-.0 1.?43E+01 2.054F+01 0.000E+01 8.113E+00 1.243E+01 2.059E+01 09.3 C.26TE+00 1.007E+01 0.000E+00 1.079E+01 E. 2 33E + CO 1.907E+01 k 90.0 1.04GE+01 1.971E+01 0.000E+00 9.305F+00 1.040E+01 1.971E+01 90.0 1.252F+C1 2.034E+01 0.000E+00 7.321E+00 1.252E+01 2.034E+01 91.1 8.301E+00 1.P78E+01 0.000E+00 1.043E+G1 0. 3 01E + C1 1.37dF+01 71.1 1.040E+C1 1.941E+01 C.000E+00 9.009E+00 1.040E+01 1. G4 IE +01 91.1 1.251E+01 ?.004E+01 0.000E+C0 7.537E+30 1.251E+C1 2.004E+01 02.1 8.395f+0J 1.848E+Cl 0.000E+00 1.008E+01 8.095F+00 1.648F+Cl_ 92.1 1. 04 0E + C1 1 908E+C1 0.000E+00 S.677E+00 1.040E+01 1. 90 8 E +01 72.1 1.241E+01 1.968E+01 0.000E+00 7.271E+30 1. 2 41 E + 01 1.968E+01 97.1 2.584E+CJ 1. 317E+ 31 0.000E+00 9.585E+00 0.504E+00 1. 617 E +0_1_ 91.1 1.040E+01 1.972E+01 0.000E+00 A.312E+13 1.040F+01 1.871Et01 93.1 1.2?2E+01 1.926E+01 0.000E+00 7.039E+00 1.222E+01 1.926F+01 l g 73.1 6.509E+C? 1.317E+01 0. 000E +00 9.5015'00 J.539E+00 1. 817E + 01 93.1 1.040E+01 1.872E+01 0.030E+0C S.313E+00 1.040E+01 1.872E+01 l 93.1 1.222E+Cl 1.92LE+01 0.000E+00 7.04?f+00 1.222r+01 1.926E+01 94.2 3.0s4t+0^ 1.787E+31 0.0COE+00 3.975E+03 3.894E+00 1.787E+01 l E 94.? 1. 0 4 0h + 01 1.832E+01 0.000EF00 7.918E+01 1.040F+0] 1.832F+01 98.2 1.191E+ol 1. 8 7 7E + 01 0. L' O C E + 0 0 6 862E+00 1.191E+01 1.877E+02 05.2 0. ? 3 5E + ? U 1.756E+;1 0.0 00 C +00 0.246E+00 9.214E+00 1.750F+01 F 7S.2 1.04CC+O! 1. 7 9 0F + 01 C.000E+00 7.4cAE+00 1.04QE+01 1.790 Ef01 A-se Osi. o Ih_ &- -- wu war l
AMA(YSIS CF CYSTEF CD.F E K CCNT A lf'"E NT ; INT PR ES S O F 0.0620 KSI.
~
CLOPO S PHI S TWFTA 5 SHEAR SI-52 S1-53 52-S3
. DALT 9 FALES=-1. 1. 2.
I ? .1 l '. 04 c F + 01 7 . 0 8 ,7 F + 0 ! 0.000E400 1.03dE+01 1.049F+01 2.087E+01 63.1 1.040F+C1 2.084E+Cl 0.000L+00 1.044E+01 1 040E*01 2.084E+01 63.1 1.072E+C1 2.062E4G1 C.000E+00 1.050E 4 01 1.032E+01 2.082E+01_ 64.2 1. 04 9E + 01 2.088E+01 0.000E+00 1.039E+01 1.049E+01 2.088F+01 64.2 1.040E+01 2.086f+C1 C.000E+00 1.045E+C1 1.040E+01 2.086E+01 A4.? 1.r32E+01 7.083E+01 0.000F+00 1.091F+01 1.032F+01 2.093F+01 65.2 1.048E+01 2.090F+C1 0.000E+00 1.041E+01 1.048E+C1 2.040E+01 65.2 1.*40E+01 2.0870+01 0.000E+00 1.047E+01 1.040E+01 2.087E+01 A5.2 1.Cf2F+01 2.085E+01 0.000E+C0 1.052E+01 1.03?E+01 2.0PSE+0_1_
/.6.7 1. 0 4 SE + 01 ?.091E+01 0.000E+00 1.043E+C1 1.048E+01 2.091E+01 n6.2 1.De0E+01 ?.G34F+01 0.000E+00 1.04SE+01 1.040E+Cl 2'. C E G E + C 1 66.? 1. 0 3 3F + 01 2.086F+01 0.000F+C0 1.054E+01 1.033E+01 2.006C+01 6 7. :. 1.047E+01 2.092L+0! 0.000E+0C 1.046E+01 1. 0 4 7E + 01 2.092E+01 f, 7. 3 1. 04 CE + C) 2. 09C E + 01 0.CCCF+0C ~1.050E401 1.040F+C1 2.090E+01 67.3 1.034E+01 7.0F 8E + C1 0.000F+00 1. 0F 5 E+ Cl 1.034E+01 _
' 008E+01 65.3 1.045E+61 2.094E+Cl__C.000E+00 1.049E+01 1.045E+01 2.C94E+C1
^
E S.? 1. 04 CE + 01 2.092E+C1 0.000E+CC 1.052E+01 1.040E+01 2.092F+01 e8.3 1.036E+01 2.091E+L1 0.000E +00 1.05cE+01 1.C36E+01 2.091E+01 60.3 1.f43F+rl 2.045F+C.1 C.000F+00 1.052E+01 1.043F+01 2.095E+01 69.3 1.040E+01 2,,094f+Cl 0.000E+00 1 054E+Cl 1.040E+01 2.C94E+01 69.3 1.03rE+0i 2.643E+01 0.000E+00 1. 0 5 6 E + 01 1.02eE+C1 2.093r+C1 70.4 1.040E+01 2.096F+01 0.Or0E+00 1.056E+01 1.040E+01 2.096E+01 79.4 1.040E+01 2.076E+01 0.0CCE+00 1. 056E + 01 1. 0 4 0 L- + 01 2.096E+01 70.4 1.041E+01 2.096E+Cl 0,000E+00 1.055E+01 1.041E+01 2.096E+01 71.4 1.036E+0) ? .0 9 7E + 01 C.000E+00 1.0610+01 1.036E+01 2.007E+01 71.4 1.04CE+0i 2.09eE+G1 0.000E+00 1.058E+01 1.040E+C1 2.090E+01 l 71.4 1.046E+01 ?.099E+01 C.000E+00 1.055E+31 1_. 0 4 5 E + 01 2.099E+01 72.4 1.031E+0! 2.007E+ni 0.300E+C0 1. 0 6 6E + 01 1.031E+C1 2. 0 9 7 E 4 0,1 7?.4 1.04CE+C1 2.100E+01 0.DonE+0C 1.060E+01 1.040E+C1 2.100E+C1 72.4 1.0SOE+01 2.103F+01 0.000E + 00 1.053E+01 1. 0 5 0 E + 01 2.103E +01 72.4 1.032E+C1 2.")7E+01 0.000E+00 1.066E+01 1.031E+01 2.097F+01 72.4 1.040E+01 2.100E+01 0.0CCE+0D 1.060E+C) 1.040E+01 ?.lC0F+01 72.4 1.049E+P1 2.103E+01 0.000E+CD 1.054E+01 1.049E+C1 2.lC3E+01 l 73.6 1.0?(C+C1 2.0 9 7E + C1 C.00CF+00 1.072F+01 1.C26E+01 2.397E+01 73.$ 1.740E+01 2.102E+01 C.000[+CO 1.061c+01 1.040E+01 2.102E+C1 A -3 & Mo
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A!!ALYS15 OF OYSTER CREEK CONTAINMEN1; INT PRESS OF 0.0520 KSt. C0090 S PHI 5 TFETA S SHEAP SI-52 51-52 S2-53 PART C . F_A C E S = - 1, 1. 1 __ 73.5 1. 05 6F + C 1 2.106F+01 0.000E+00 1. 0 519 t_01 1.055E+01 2.106E+01 74.5 1.019E+01 2.097F+01 0.000E+00 1.07dE+31 1.019E+01 2.097E+01_ 74.5 1. 04 0E + 01 2.103E+ 01 0.000E+00 1.063E+01 1.040E+01 2.103E+01 74.5 1.362E+01 2.110E+01 0.000E+00 1.04SE+C1 1.062E+01 2.110E+01_ 75.5 1. 01 CF + 01 2.095F+01 0.000F+00 1.085E+01 1.010E+01 2.095E+01 75.5 1.040E+C1 2.104E+C1 C.00CE+00 1.064E+01 1.040E+01 2.104E+01 75.5 1.070E+01 ?.112.E+0L_ 0.000E+00 1.043E+01 1. 0 70E + C1 2_.113E+01 76.6 1. 001 C + QJ 2.093F+01 0.000E+00 1.092E+01 1_. 0 01 E + 01 2.093E+01_ 70.6 1.040E+01 2.105E+01 0.000E400 1.065F+01 1.040E+01 2.1CSE+01 70.6 1. n P C F + 01 7.117F401 0.000E+00,_!.037F+01 1.080E+y1 2.l!7E+01 77.6 9.901E+00 2.090E+01 0.000E+00 1.100E+C1 9.900E + 00 2.090E+01 77.6 1.040E+01 2.10 5 E + 01 0.000E+00 1.065E+01 1.040E+C1 2.105E+01 77.6 1.091E+91 2.120E+01 0.000E+00 1.029E+01 1.091E+01 2.120E+01_ 73.6 9.77aE+00 ?.09;E401 0.000E+00 1.108E+01 S. 7 78E + CO 2.085E+01 78.6 1.040E+^1 2.1C4E+01 0.000E+00 1.0n4E+01 1.040E+Cl 2.1C4E+C1 78.6 1.10 3E + 01 2.123E + 01 C.000E+00 1.020E+01 1.103E+01 2.123E+71 7s.7 4.643E+00 2.079E+01 0.000E+00 1.115E+01 9.643E+10 2.079E+01 77.7 1.040E+01 2.102E+01 0.000E+00 1.062E+01 1.040E+01 2.102E+01 79.7 1.11tE+Al 2.1267+01 C. 000E 4 00 1.009E+ft 1.115E+31 2.125E+01 B0. 7 9.496E+10 2 . 0 72 E
- 01 0.000E+09 1.122E+01 9.496E+C0 2.072E+01 80.7 1.040E+01 2.099E+01 0.000E+00 1.059E+C1 1,040E+01 2.099 E +01 80n7 1.131E+01 2.126E+01 0.000E+00 4.952E+00 1.131E+01 2.126E+01 81.7 9. 3 3 9E + 10 2.062F+01 0.000E400 1.128F+al 9.3 39E +00 2.062E+01 01.7 1.040E+01 2.094E+C1 0.000t+00 1.054E+01 1.040E+01 2.094E+01 91.7 1.147E+01 2.126E+01 0.000F+00 9.795E+00 1.147E&O1 2.126E+01 62.3 9.175E+0E 2.051E+01 C.300F+00 1.133E401 9.175E+00 2.051E+01 82.3 1.040E+)1 2.090E+01 0.000E+00 1.048E+01 1.040E+C1 2.0SSE+01
,3 ? . 9 1.1636+91 ?.125F+01 0.000E+00 9.616F+00 1.163F+01 2.125E+01 R2.9 9 . 1 S O E '+ 0 0 2.051E+01 0.000E400 1.133E+01~ 9.1SOE+C0 2. 051E + 01 9 ?. d 1.04CF+01 2.088E+01 0.000E+00 1.043F+01 1.040E+01 2.088E+01
$2.S 1.163E+01 2.12 5E + 01 C.000E+00 9.620E+00 1.le3E+01 2.125E+01 83.9 9.012E+20 2.C39E+01 0 000E +00 1.137E+01 3.212E+00 2.038E+01
[ A3.6 1.04CE4C1 2.079E+C1 0.000F+00 1.039E+01 1.04]E+01 2.079E+01 83.6 1.17CE+01 2.121E+01 0.000E+00 9. 418E + 0 0 1.17 9E + C 1 2 121E+01 p A-37 /2ev. o l . . . 1 m w as { on .yyn
ANALYSIS CF OYS1EC CPEEk C0hTAINMENT; INT PRESS OF ).0620 KSI. cod 55~ S PHI 5 THETA 5 SHEAR 51-52 51-S3 52-S3 PAkl E _ FACES =-1. 1. 2. 95.? 1.14'E+0! 1.822E+01 0.000E+00 6.751F+30 1.147E+01 1.822E+01 96.2 4.037E+00 1.732E+01 0.000E+00 7.388E+00 9.937E+00 1.732F+01 96.2 1.040E+01 1.746E+01 0.000E+00 7.061F+00 1.040E+01 1.746E+01 96.2 1. 0 0 7E + 01 1.760E+01 0.000E+00 6.735E+00 1.037E+01 1. 7 6 0 E + 0_1_ 97.3 1.072E+01 1.712E+01 C.CCCF +00 6.393Etq0 1.072F+Cl 1.712E+01 97.3 1.040E+Cl 1.702E+01 0.00CE+00 6.616E+00 1.040E+C1 1.7C?E+01 07.3 1_. 0 0 0 E + C l 1.692E+01 0.000E+00 6.840E+00 1.008E+01 1.692E+01 99.3 1.172E+01 1.697F+01 0.000E+00 5.25PM+0C 1.172E+01 1.697E+01 95 3 1. 04 0E + 01 1.659E+Cl 0.000E+00 6.177E+00 1.040E+01 1.658E+01 00.1 9.001E+00 1.5199+0! 0.000E+00 7.096E+00 0.041E+00 1.619E+01 99.3 1.294E+C1 1 692F+01 0.000E +0C 3.983E+ 30 1.294E+01 1.692E+01 99.3 1.040E+01 1.616E+01 0.000E+00 5.70004CO 1.040E+01 1.61dE+01 05.3 7.865E+00 1.540E+ql 0.000E+00 7. 53 7E + 00 7.965E+00 1.540E+01 1a0.4 1. 4 4 ?F + 0 i 1. 6 9 9E + 01 0 000F+00 2.572E+00 1.442E401 1.699r+01 130.4 1.040E+C1 1.579L+01 C.000E+00 5.3e6e+:0 1.040E+C1 1.57se+01 100.4 6.184F+00 1.45BE+01 0.000E+00 0.1990+00 6.364E+C0 1 . 4 5 8f + 0_1 101.6 1.61CE+01 1.721E+01 C.CCOE+00 1.035E+00 1.610E+01 1.721E+01 101.4 1.04GL+Cl 1.543E+Cl C.000E+00 5.079E+00 1.047E+01 1.548E+01 101.L 4. 6 2 7F + C O 1.37Gr+01 0.000f-+00 9.122F+00 4.527E400 1.375E+01 172.4 1.n23E+01 1.762E+01 0.000E+00 6.092E-01 1. 7 6 ? E + C 1 1.623E+01 102.4 1.040E+0! 1 527E+C1 0.000F+00 4.660E+00 1.040E+01 1.527E+01 102.4 2 . f. 7 8F + 0 0 1.202E+C1 0.000E+00 1.035E+01 2.578E+00 1.292F+01_ 103.5 2.05aF+01 1.825E401 0.000F+GO 2.3?5F+00 1.626E+01 2.058E+01 1P3.5 1.14CE+r1 1. 51 G E + 01 0.000E+00 4.769E+00 1.040F+01 1.51CE+01 103.5 2. 2 5 'E- 01_1. 214E + 01 0.000E+0C 1.191E+01 2. 2 53 E- 01 1.214E401 P.u T 9 FACES =-1. 1. 2. 0.0 3. 74 6E-01 1.214E+U1 C.000E +00 1.181E+01 3.749E-01 1.219E+01 0.0 3.74AE-01 1.219L+0! C.0COE+00 1.121C+01 3. 7 4 3E-C 1 1.219E+01 0.J 3.74PE-Ol 1. 21 S E + r. ) 0.000E+00 1.1CIE+01 3.748E-01 1.218E+01
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l 2.0 2. 5 2 7E- C l 1.231E + 01 C.000r+0] 1.205E+C1 2.537E-C1 1.231E+n1
?.4 2.5 7E-11 1.231E+01 0.oCCF+00 1.2C51+01 2. 5 3 7F- C l 1.231E+01
- 2. ' ' 7E- C! 1.??1E+01 0.000E+00 1.205F+01 2.537E-01 1.231E+01 1 2.?
A-M Dev. o l L _ sp _ DGH 2/.?/J3' _ _ _ J
ANALYSIS OF OYSTfF CREEK CONTA! AMENT; 1AT PRESS OF 0.0620 KSI. COC;0 5 Phi S THETA 5 SHEAR 51-52 SI-S3 52-S3 PAhT 9 03EES=-1. !_. 2. 2.0 2. 53 7F- 01 1.231E+01 _ 0.CG0F+00 1 ?05E+01 2.537E-01 1.231E+01 2.0 2. 5 3 7E- 01 1.231E+01 0.000E+00 1.205E+01 2.537E-C1 1.231E+01 2.0 2.537E-01 1.231F+01 0.000E+00 1.205E+01 2. 5 3 7E- 01 1. 2_31 E + 01 4.0 1. 2 R 8E- 01 1. 24 3 E + 01 0.000r+00 1.230E+01 1.288E-01 1.243E+01_ 4.0 1.268E-01 1.243E+01 0.000E+00 1.230E+01 1.2P8E-01 1.243E+01 4.0 1. 2 h d F- 01 1.243E+Cl 0.0c0E+00 1.230r+01 1.2880-01 1.243F+01 4.0 1.208E-01 1.243E+01 0.000E+00 1.230E+01 1. 2 3 3E- 01 1.243E+01
- 4. 0 1.2999-01 1.24 3E+ Cl 0.000E+C0 1.230E+11 1.2E3F-01 1.243F+01 4.0 1. 2 8 9 E- 01 1.243E+01 0.00CE+00 1.230E+01 1.2dSE-01 1.243E+01
- 6. 0 - 2. 8 t 1 E- 0 6 1.256E+C1 0.000'E+00 1.256E+01 -1.907E-06 1.256E+01
(, . 0 - 9. 5 3 7E - 0 7 1.256E+C1 0.000E+00 1.256E+01 0.000E+00 1.2565+01 6.0 -9.53?E-07 1.25(E+C1 0.000E+C0 1.256E+01 -9.537E-07 1.256E+01 PAPT 10 FACES =-1. 1. 2. v.0 2.059E+01 1.025E+01 0.00CE+00 2.3385+00 1. 82 6E + n) 2.059E+01 0.0 1.040E+01 1.519E+01 0.000E+00 4.790E+CC 1.C40F+01 1 51SE+01
- 0. 0 2.20$F-nl 1.214E+01 0.000E+00 1.192F+01 2. 2 03 F- 01 1.214F+01 1.0 1.831F+01 1.764E+Cl C.000E+00 6. 7 CCE- 01 1.764E+01 1.831E+01 1.1 1.040E+01 1.527E+01 0.000E+00 4.663E+00 1. c ' E + a l 1.527E+01 1.C 2.45GE+00 1.209E+G1 0.000E+00 1.040E+01 ..r9^">00 1.289E+01 2.0 1.6?lE+91 1.7 7 3E + C l 0.000E+00 9 223E-01 1.6?lE+C1 1. 72 3E + 01 20 1. C 4 CE + 01 1.546E+C1 0.000E+00 5.059E+JC 1.040F+01 1.546E+01 2.0 4.444E+00 1.369E+01 0.000E+00 9.196E+00 4.494E+00 1.369E+01 3.0 1.459F+Cl 1.701E+01 0.000E+00 2.415E+0C 1.469E+Cl 1.701E+01 3.0 1.040E+01 1.575E+01 C.000E+00 5.347L+0C 1.040E+01 1.575E+C1 3.0 6.214E+00 1.449E+01 0.0uGE+C0 8. 2 80E + 00 6. 214E + 00 1.449E+01
~
4.0 1. 313F + 01 1.602E+01 0.000E+00 3.79PE+00 1.313E+01 1.692E+01 4.0 1.140E+01 1.01CE+01 0.0CCE+00 5.7CIE+00 1.040E+01 1.610E+01 4.3 7.675E+0C _1.529E+01 0.000E+00 7.611E+00 7.675E+00 1.529E+01 5.0 1.191r+01 1.t15F+01 C.000E+00 5.043E+0n 1.141E+01 1.695E+01 5.J 1. 04 0 E + 01 1.657t+01 0.0]OE+00 6. C 9 8 E + 0 C 1.J4JE+Cl 1.65dE+G1 l 5.0 8. 8 9 5 E + 0 ' 1. 6 05 E + 01 0.000Et0C 7.154Ef 0 0 6.395E&OO 1.605E+01 6.* 1.001E+01 1.7C7E+01 0.000E+00 6.16.2 F + 0 0 1.091E+C1 1.707E+01_ l-e A-40 Cev. o J os wer F - - - _ _ - _ - - _ - _ - - _ _ - _ - - _ _ - _ - _ - - - - _ _ _ _ _ - - _ _ _ _ _ _ _
au -- - - - - A.'J A L YS I S GF OYS1ER CR EEK CONTA INPF hT ; INT PEESS OF 0.0523 7.51. 4 COCPD 5 PH! S THETA 5 SHE^k SI-52 S1-53 S2-53 J- P A i< T 10 ___ FACES =-1. 1. 2. __ t.C 1. 04 GF + L I 1.642E+0! 0. 000E +00 6.519E+00 1.040E+01 1.692E+01
/.O 9.R94E+0" 1.(77E+C1 0.00 0E +00 6. 675E + 00 9.094E+00 1.677E+01 7.0 1. 011E + 01 1. 7 2 6E + 01 0.000C+00 7.151E+00 1.011E+01 1.726E+01 7.0 1.040E+01 1.73EE+01 0.C00E+00 6.948E+00 1.040E+01 1.735E+01_
7.0 1.069E+01 1.744E+01 0.000E+00 6.745c+00 1.069E+01 1.744E+01 0.0 0.491F+00 1. 7 5CE 4 C l C.000E+00 6.010E+00 9.491E+00 1.750E+01 L.0 1.04nE+01 1.778E+01 0.000E400 7.272E+CO 1.040E+Cl 1.778E+01~ ' 8.0 1.131 F + C 1 1.805E+01 0.000F+00 6.734E+00 1.131E+C1 1.8C5ET01 90 9.02SE400 1.777E+01 C.000E*C0 U.747F+CO 9.025E+00 1.777E+51 9.0 1.040E+01 1.019F+01 0.000F+00 7.783F+00 1.040E+01 1.819E+01 9.0 1.17 dE + Cl 1.bCOE+Cl 0.000F+00 6.810E+00 1.178E+01 1.860E+01 9.' 9. 07 7E+ CC 1.777E+01 0.CCOE+00 P.747F+00 C.027E+00 1.777E+]l
'.0 1. 0 4 CE + 01 1. 819E + 01 C.000E+00 7.783E+00 1.040E+01 1.819E+01 1.17 aE + C1 1.E60E+01 4 E .c 1.173P+r1 1.660E+0) 0.00CE+00 6.0?CE+00 10.0 3. c.C 5l. + 01 1.8C6F+01 0.000E+00 9.36eF+00 8.696E+00 1.800F+01 10.V 1.D40E+01 1. 8 5 HE + 01 C. 900F + C 0 A.173E+00 1 040E+0! !.858E+01 30.0 5.?11E+01 1.9CoE+01 0.000E+C0 (.077E+CC 1.211E4C1 1. C 9 E_+ 0_1_
!!.0 7. 4 7 ;r + cc 1,g36r+0! 0.000F+GO o.89?F+00 E.479E+00 1.936E+01 11.3 1.04Cl+01 1.804E+01 0.0GOE+00 3. 536E + 00 1. 0 4 0E + C 1 1.094h+01 11.3 1.232F+Cl 1.0G2F+01 0.00CE+00 7.189F+30 1.233E+01 1.452E601 I?.: ?. 59E+00 1. E4 E E + 01 C.000F+00 1. 030E + 01 8. 3 59E + CD 1.666E+01 12.0 1.040F+01 1.977E*01 0.000E+00 C.e690+00 1.040E+C1 1.927C+Cl~
12.0 1.245c+0) 1.9EBE+C) 0.000E+00 7.43aF+C0 1.245E+01 1.939E+01 17.0 C.?!4F+00 1.395E+Cl ~ 0.000E+00 1.0A'E+01 6. 31 RE+ CC 1.895E+01 13.0 1. 04 0E + C1 1.957C+5I 0.0SOE*00 9.170E+00 1.040E*01 1.957E+01 < 13.0 1.24GE+01 2.020F + Cl C.00CE + 00 7.710E+00 1.?40E+01 2.020F +01 14.0 f. ? 4 CE + 0C 1.922E+01 C.000F+00 1.049E+0L C.?40E+0? 1.922E+C1 14.u 1. 04 CE + 01 1.994E+01 0.000E+00 9.439E+00 1.040C+01 1.084F+01 14.o 1. 24 70 + 01 2.046E+01 0.0COE+00 7.994E+0C 1.247E+01 2.046F+01 10.0 E.411E+00 1.943F+J1 0.000F+09 1.107E+01 S.411F+00 1.4489+01 l B l 'i . 0 1r.0 1.340c+01 1.239E+01 2.0CSE+01
?.069E+31 C.?COE+00 0.000E+00
- 9. 6 76 E + "0 8.2 ale +00
- 1. 0 ',0E + 01 1.?31E+01 7.008E+11 2.060E+C1 L 0.000E+03 1.120E+01 S.521E+00 1.u?2E+01
~. / . 0 0.52tE+CC 1. 9 72F + C l 1( .0 1.040E+01 2.0?SE+11 0.000E+00 9. 8 31E + JO 1.040E+01 2.02?E+01 16.0 1 2?sc+C1 2.089E+?! 0.000E+09 S.564E+C0 1.229E+St 7.0Q5f+Cl
{ W A-41 G< v. o ( E _ __ b _ _____ S O__________ l DM afNGC _ _ l
ANALYSIS CF OYSTER CREEK CONTAIN"ENT; INT PRESS OF 0.0620 KSI. CUChD S PHI 5 THETA 5 SHE/R S1-52 SI-S3 52-5 , [ PAPT 10 _ _ FACES =-1. 1. 2. I 7.1 3.657E+00 1.094F+01 0.000E+00 1.128F+01 0.657E+C0 1.994E+01 17.9 1. 04 CE + C1 2.046E+01 0.000E+00 1.006E+01 1.040E+01 2.040E+01 17.0 1.?l5c+01 2.0965+01 0.00CF+C0 8.316E+00 1.215E+01 2. 098 6 +01 10.0 8.EllF+00 2.013E+01 0.0C O E +00 1.132E+01 8.811E+00 2.013E+01 18.0 1.040C+01 2.061E+01 0.000E+00 1.021E+01 1.0406+01 2.061E+01 16.0 1.2CCE+G1 2.109E+0! 0.000E+00 9.093E+00 1.200E+01 2.109E+01 18.0 8. 81 ?E 4 00 2.013E 4 01 0.003E+00 1.132E+01 E.813E+00 ~?.013E+01 10.0 1.040E+01 2.061E+01 0.000E+00 1. 0 21E + 01 1. 04 0E + C 1 2.061F+01 10.0 1.199E+01 2.109E+01 0.000F+00 9.095E+00 1.199E+01 2.109F+01 19.0 9.977E+00 2.031E+01 0.00CE+00 1.133E+01 8. 9 7 7E + 00 2.031E+01 19.0 1.040E+01 2 . 0 7 4 E + 01_ 0.000E+00 1.033Et01 1.040F+01 2. 0 7 4 E + 0.1 19.0 1.1 F ?T + 01 2.116E+01 0.000E+0C 9.334E+00 1.163E401 2.116E+01 20.0 9.145E+00 2.046E+31 0.000E+00 1.132E+01 9.145E+0C 2.046E+01 71.0 1. C4 0E + 01 ?.C34E+01 0.000F+00 1.044E+01 1.0406+01 2.084F+01 20.0 1.16CF+01 2.122E+01 0.000E+C0 9.555E+00 1.1665+01 2.122E401 21.0 9.?l2E+r0 2.059E401 0.000E+0D 1.128E+01 9.312E+00 2.059F+0i 21.0 1.04CE+C1 2. 0 92E+ 01 0 . 0 0_0 E 4 0 0 1.052E+01 1.040F+01 2.092E+01_ 21.0 1.19oE+01 ?.125E+C) 0.000E+C0 9.754E+00 1.149E+C1 2.125E+01 i 22.0 9.473E+C0 2.071E+01 0.000E+00 1.123E&01 9.473E+00 2.071E+01 27.0 1.040C+01 2.099E+01 0.000E+00 1.058E+C1 1.040E+01 2.099E+01 22.0 1.133E+01 2.127E+01 0.000E+00 9.933E+00 1.133E+01 2.127E+01 23.0 9.C25?+0C 2. 0 3 0E + 01 0.100E+C0 1.118E+01 9.625E+00 2.000E+01 23.0 1.060E+01, 2.104E+01 0.000E+00 1.064E+01 1.040E+01 2.104E+01 21.0 1.1185+01 2.127F+01 0.009E+00 1.009E+01 1.ll3E+01 2.12 7 F +01
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2.039E+0i~
~
24.0 0.705E+CC 2.039T+Cl U.000E400 1.112t+C1 9.765E+00 24.0 1.040E+]l 2.10BE+01 0.000E+00 1.067E+31 1.C40E+01 2.108F+01 24.0 1.104E + 01 2.127E+01 0.000E+00 1.023E+01 1.104E+01 2.127E+01 25.0 9.E91E+?? 2.J95E+;l 0.030E+00 1.106E+J1 3. d S 1E + C0 2.095E+01 20.0 1.240F+01 2.111E&01 0.000E+00 1.070E+01 1.040E+01 2.111E+01 25.0 1.092E+0! 2.12 6E + 11 C.0 3 0E + 00 1.034E+01 1.002E+01 2.126E+01 t 26.] 1.J03E+;l 2.101E+01 0.030E+10 1.101E+01 1.300E+0! 2.101E+01 26.0 1.340E+C1 2.113F+01 0.000F+00 1. 0 72 E + 01 1.040E+01 2.113E+01 l ?A.) 1. C d i t: + 01 2.125F&1l 0.001F + 0 3 1.044t+01 1. dele +01 2.125E+01 1 _
? 7. 3 1. C l if + F 1 2.10 5F + 01 0.000P+01 1.096c+01 1.010E+01 2.!39F+01 27.0 1.040E+r1 2.114C+01 C.'00E+00 1.074E+01 1.040E+01 2.114E+01 A-42 Rev- o m Vt/ss __ _
[)RH 2/3/ff
-____ - - ___ _ _ _ _ _ _ _ _ _ _ _________________________________A
ANALYSIS CF OYSTED CREEK CONTAIMENTI It T PRESS OF 0.0620 KSI.
~
COURD S Ph! 5 THETA 5 SH E AP. 51-S2 51-53 52-53 P/J.T 10 __ r FACES =-1. 1. 2. . _ 27.C 1. 0 71E + 01 2.1?4F+01 0.000E+00 1.052F+01 1.071E+01 2.1?4E+01
~
27.0 1.010E+01 2.105E+01 0.000F+00 1.095E+01 1.010E+01 2.105E+01 27.0 1.040E+0! 2.114E+C1 0.000E+00 1.074E+01 1.040E+01 2.114E+01 27.0 1.071E+01 2.124E+01 C.000E+00 1.053E+C1 1. 0 71E + 01 2.124E+01
~
28.0 1. 017E + 01 2.108E+C1 0.000E+00 1 071E+01 1.0170+01 ?.108E+01 2A.0 1.040E+01 2.115F+01 0.000E+00 1.075E+01 1.040E+01 2.115E+01
? 9.0 1.063E+01 2.122E+0! 0.000E+00 1.059E+01 1.064E+01 2.122E+01 29.0 1.023E+01 2.111E+01 0.000E+00 1.088E+01 1.023E+01 2.111E+01 20.0 1.040c+01 2.116E+01 0.000E400 1.076E+C1 1.040E+01 2.116E+01 29.0 1.057E+01 2.121E+01 'C.000E+00 1.064E+01 1.057E+C1 2.121E+01 30.0 1.C?75+01 2.113E+'l 0.000E+00 1. 0 85E + C1 1.027E+C1 2.113E+01 30.0 1.04CE+01 2.116E+01 0.000E+00 1.076E+01 1.040E+01 2.116E+01
'O.0 1. 05 3E + C 1 2.120E + 01 C.C00E+00 1.057F+01 1.053Et01 2.120E+01 31.0 1.030E+01 2.113E+01 0.000E400 1.084E+01 1.030E+01 2.113E+01
?!.0 1.640E*01 2.1 17 E + 0 ! 0.000E+00 1.076E+01 1.040F+01 2.117E401 31.0 1.051E+01 2.120F+01 0.000E+00 1.C69E+01 1.C51E+01 2.120E80!
32.0 1.030E+01 2.114E+01 0.000E+00 1.083E+01 1.030E+01 27514F+C1 17.0 1.040c+01 7.1 17E + 01 0.000F+00 1.076E+01 1.040E+01 2.117F+01 l 32.0 1. 0 51E + S 1 2.12CE+C1 0.000E+00 1.069E+01 1.050E+01 7.120E+01 33.0 1.029E+01 2.113E+01 0.000E+00 1.084F+01 1.027E+01 2.113E+01 31.0 1.040E+01 2.117E+01 C.300E+CO 1.076E+01 1.040E+01 2.117E+01 3340 1 052E+01 2.120E+01 0.000E+00 1.068E+01 1.052F+C1 2.120E+01 34.0 1. 02 SE + 01 2.112E+01 0.000E+00 1.086E+0L 1.025E+01 ?.112E+01 34.0 1.340E+01 2.11(E+01 0.000E+00 1. 0 7 6E + C 1 1.040E+C1 2.116E+01 14.0 1.055E+01 2.121E+31 0.000E+00 1.065E+01 1.055E+C1 2.121E+C1 35.0 1.02CE+01 2.110E+01 0.300E+00 1.089E+01 1.027E+C1 7.110E+01
'6.0 1.040E+31 ?.116E+01 S.100E+00 1.075F+01 1.043E+01 _
2.116E+01 35.0 1.06CE+01 2.122E+01 0.000E+00 1.061E+01 1.060E+01 2.122F+01 30.0 1. 013E + 01 2.107E+01 C.000E+00 1. 0 9 3E + 01 1. 013 E + 01 2.1C7E+01
?!.* 1.343E+01 '
2.115E+31 C.310E+00 1.074E+01 1.040E+01 2.115E+01
~
36.0 1. 06 7E + 01 2.123E+01 0.000E+00 1.056E+01 1.067E+01 2 123E+01 I . m e,a l 7T/A 2 /z,/ss L ORM 2/3/28 c l
AN ALYS 15 or OY ST ER MEEK CONT AIN4EllT1 INT PRES 3 OF 07062.0 KSt. COCP0 S PHI 5 THETA S SHEAR $1-52 51-53 S2-53 , out 11 . FACES =-1. 1. 2. 0.0 1.014E+S1 2.107F+01 0.000E*00 1. C 9 3 E + 01 1.014E+01 2.107E+01 0.0 1.040E+0i 2.115E+01 C.0COE+00 1.075E+01 1.043E*01 2.115E+01 0.0 1.067E+01 2.12 3 E+ C 1 0.000E+00 1.056E601 1.06 T E +01 2.123E+01 1.1 1.004E+01 2.103E+01 0.000E+00 1.0 98E + 01 1. 0 0 4E + C 1 2.103F+01_ 1.1 1.040E+01 2.113E+01 0.C00E+00 1.073E+01 1.040E+n1 2.!13E+01 1.1 1. 0 7 7F + 01 2.124F+01 C.000E+00 1.04BE+01 1.077E+01 2.124E+01 2.2 9.9?SE+00 P.097E+01 0.000E+00 1.104E+01 9.025E+00 2.0975+01 2.2 1. 04 CF + 01 2.111E+01 0.000E+00 1.071E+01 1.040E+01 2.111E+01 2.2 1.0CfE+C1 ?.126E+01 C.000E+00 1. 0 3 7E + 01 1.0895+01 2.126E+01_ 3.3 9.79CF+00 2.090E+01 0.000E+00 1.111E+01 9.790E+00 2.090F+01 3.J 1.04CE+01 2.138E + 01 C.000E+00 1.06SE+01 1.040E+01 2.103E+01 3.3 1.10 2 E + 01 7.127E+01 0.000E+00 1.025E+Cl 1.102E+01 2.127E+01 4.4 0. 6 3 EE + 00 2. 0SI E + 01 0.000E+00 1.117E+01 9.63aE+00 2.091E4nt 4.4 1.040E+01 2.1C4E+01 0.000E*C0 1.064E+01 1.040E+01 2.104E+01 4.4 1.1170+01 2.12 7E + 01 0.700E+C0 1.010E+01 1.117E+01 2.127E+01 5.5 9.471E+03 2.0 71E + 01 C.000E+00 1.123E+01 9.4 71 E + 00 2.071E+01 0,5 1.040E+J1 2.09CE+01 0.000E+00 1.058E+01 1.040E+01 2.098E+01 "5. 1.134E+01 2.126E+01 0.000E+00 9.929E+00 1.134E+01 2.126E+01 1 5.5 9. 4 71 F + b? 2.071E+01 0.000E+00 1.123E+01 9. 4 71E + 00 2.0715+01 5.5 1. 04 0E + 01 2.09EF+C1 0.000E+00 1.058E+01 1.040E+11 2.098E+01 5.6 1.134E+Cl 2.126E+01 0.000E+00 9.929E+00 1.134E+01 2.126E+01 6.6 9. 293E 4 00 /.C5LE+01 0.000E+00 1.129E+01 9.293E+00 2.058E+01 6.6 1.040E+01 2. 091E + 01 0.0COE+00 1.051E+01 1.040E+01 2.091E+01 6.6 1.151t+D1 2.124E+01 0.000E+00 9. 7 31E + 0 0 L.151F + C1 2.124E+01 7.7 9.10'E+00 2.043E+01 0.000F+00 1 132E+01 9.107E+00 2.043E+01 7.7 1.040E+'t 2.082E+C1 0.000E+00 1.C41E+01 1. 0 4 0E + 01 2.062E+01 7.7 1.170E+01 2.120E+01 0.00Cb+00 9.507E+00 1.170E + C1 2.12CE+01 d.F 1.025Evr0 2.'2SE+r1 C.C00E+CO 1.133E+01 C.925E+00 2.02SE+31 0.0 L.041F+01 2.0 70E+ 01 0.000E+00 1.029E+01 1.040E+C1 2. 0 7 0E + 01 R.0 1.18PF+01 2.114E+01 0.000F+00 4.259F+n0 1.igat+01 . 1g4p+;t 9.9 0.74 76 + 00 2.005E+01 0.000E+00 1.131E+01 ?. 74 7E + 0 C 2.CCSE+0! C.9 1.040F+01 2.055F+01 0.000E+00 1.015C+01 1.040E+01 ~ 2.066E+01 l 9.4 1 20C+01 2.105E+01 0.000E+00 n.93dE+00 1.20nF+C1 2.10SF+01 h 11.0 3.58tE+00 1.093E+01 0.0000+10 1.124E+01 3.ce65+00 1.983E+01 11.0 1. 04 0F # 01 2. C 3 7F + 01 0.00CF + 00 9.969E+00 1.040E+01 2.037E+01 A-41 Sv. O l
- 70s 7-/n/ss- ..
OM VJ/8/
- - - . __ O
ANALYSIS CE GYSTER CREEK ECNTAINMENT; INT PRESS OF 0.0620 FSI.
~
C00Ro S PHI S THET4 5 SHEAR 51-52 51-53 S2-53 ofVT l_1 _ FACES =-1. 1. ?. ,__ 0 1.722F+01 2.092E+01 0.000F+00 S.697E+00 1.222E+01 2.092E+01 l 11.0 S.586E+00 1.933E+01 0.000E+00 1.124E+01 8.536E+00 1.983E+01 11.0 1.040E+01 2.037E+01 0.000E+00 9.969E+00 1.040E+01 2.037E+01 11.0 1.22?E+01 2.092E+01 0.000E+00 9.6976+00 1.222E+01 2.092E+01 12.1 8.451E+00 1.9570+0i 0.000E+C0 1.112E+01 8.451E+00 1.957E+01 12.1 1. e4 CE + C 1 2.016E+01 0.000E+00 0.756E+00 1.040E+01 2.01oE+01 12.1 1.235E+01 2.075E+C1 0.000E+C0 8.39CE+C0 1.235E+01 2.075E+01 13.2 E.358E+CO 1.930E+01 0.000E400 1.094E+01 B.358F400 1.930F+01 13.2 1.040E+01 1.991E+01 0.000E+00 9.507E+30 1.040E+01 1.991F+01 13.2 1. 2 '[5 E + 01 2.052E+0! 0.000E+]O 8. 0 75E + 00 1.245E+01 2.052E+01 14.3 P . 3 2 CE + CO 1.900E+0) 0.000E+0] 1.0686+01 8.320E+00 1.000E+01 14.3 1.040E+01 1.962E*01 0.000E+00 9. 2 20E+ 00 1.040E+01 1.962E+01 14.2 1.249E+01 2.025E+01 0.000E+00 7.761E+30 1.249E+01 2.025E+01 15.4 F.356E+CO 1.808E+01 C.000E+00 1.033E+01 8.356E+00 1.B68E401 15.4 1. 0 '+ 0 E + ? ! 1.930E+01 0.000E+00 3.893E+00 1.040E+C1 1.930E+01
] 5. 4 1.246E+C1 1.991E+01 0.000E+00 7.460E+00 1.245E+01 1.491E401 16.5 8.4tLE+00 1.336E+01 0.000E+00 9. 8 70E+ 00 8.486E+C0 1.836E+01 16.5 1.040F+01 1. tt 91 E + c 1 0.000E+00 8.528E+00 1.043E+01 1.893E+01 l 16.5 1. ? 3 2L + 01 1.951E+01 0.000E+00 7.185E+00 1.23?E+01 1.451E+01 r
16.5 S. 4 3f E+ 0C 1. 83 6E + C l 0.000E+07 9.870E+00 8.4350+00 1.216F+01 10.5 1. 0 4 0E+ 01 1.P91E+C1 0. 00 0E + 0.0 8.523E+00 1.040E+01 1.893E401 16.5 1.23?E+^1 1.951E+01 0.000E +00 7.185E+00 1.232E+01 1.951E+01 17.6 8. 7 3 2E+ 00 1.803E+01 0.000E+00 9.296E+00 8.732E+00 1.003E+01 17.o 1.'4CE+01 1.853E+01 0.000E+00 3.126E+00 1.040E+01 1.853E+C1 17.6 1.?O7E+01 1.903E+01 0.000Et00 6.957E+70 1. 2 0 7E + 01 1. 9C 3F + 01 l 1A.7 9.121E+00 1.7 71E + 31 0.000F+00 8.592E+00 9.121E+00 1.771E+01 11.7 t.J40E+01 1.010E+01 0.000E+00 7.694E410 1.040E+Cl 1.810E+01 13.7 1.16 9F + 01 1.84SE+01 0.00)E*00 6.796E+00 1 169E+01 1.84PE+01 17.1 9.678E+00 1.742E+01 C.000E+00 7.745E+00 9. 6 78E + 00 1. 74 2_E + 0 !
- 19. ] 1.040E+01 1.764E+01 0.00]E+]3 7.237F+20 1.04]E&G1 1.764E+01 19.4 1.11 ?c 4 O! 1.786E+Cl 0.000f+00 6.730E+00 1.ll3E+01 1.706F401 l
g 2 ^ .1 1.J?+3E+ol 1.713E+31 0.00]E+00 6.74SE+30 1.0436+C1 1.716E+01 20.9 1.040E+01 1.717E+Cl 0.000E+00 6.768E+70 1.040E+01 1.717E+01 l 20.9 1.'?7E+0! 1.716T+01 C.0CCE*00 6.738E+20 1. 0 3 7E + 01 1.7160+01 B _ A- 4r 12sv. o __ /$_ "" [_______. MH an/88 - _ . - _ . -
~
AfJALYSIS OF OYSTER CREEK CONT A INME'lT ; INT PRESS OF 0.0620 KSI. COORD 5 PHI S TFETo S SHEAP S1-52 S t-5 3 S2-53 PAR 1 L1 FAffS=-1. L. 2. _. 12.0 1.141F+01 1.700E+01 0.000E+00 5.593E+00 1.141E+01 1.700E+01 22.0 1.040E+01 1.670E+C1 0.000E+00 6.2995400 1.040E+C1 1.670F+01 22.0 9.395E+C0 1.64]E+01 0.000F+00 7.005E+00 9.395E+00 1.640E+01 22.0 1.141E+01 1.700E+01 0.000E+00 5.50*>E+00 1.141E+01 1.700E+01
?? 1 1.040E+rl 1. 6 70E + 01 0.000F+00 6.299F+00 1.040E+01 1.670F+01 22.0 9.5cSE+00 1.640F+01 0.000E+00 7.004E+00 9.395E+00 1.640E+01 23.1 1.265E+01 1.693E+01 0.000E+00 '4.279E+00 1.265E+01 1.693E+01 73.1 1. 04 0E + 01 1.625E+01 0.000E+00 5.849F+00 1.040E+01 1.625E+01 23.1 3.lo0E+00 1.55HE+01 0.000E+00 7. 419E + C C 8.160E+00 1.550F+01 26.2 1.4165+01 1.:97E+0! 57000E+00 2 . 810 E + 'J O 1.416E+01 1.697E+01 24.? 1.040E+01 1.585E+C1 C.000E+00 9.44?E+C0 1.040E+01 1.505E+01 24.2 6.643E+00 1.472E+01 0.000E+C0 C.C75E+00 6.643E+00 1.472E+01 25.3 1. 5 0SE + 01 1.719E+C) 0. 0 0 0E + 00 1.197f+00 1.599E+01 1.719E+01 25.3 1.040F+0! 1.551E+01 0.000F+00 5.10 7E + 0 0 1.040E+C1 1.951F+01 2 f. 3 4. 817F + C 0 1.383E+01 0.000E+00 9.017E+JO 4.817E+00 1.383E+01 2 6 . <, 1.M14E+01 1.760E+01 C.000E+00 5.407E-01 1.760E+01 1.814E+01 26.4 1.040E+0! 1.579E+01 0.000E+00 4.878E+00 1.040E+01 1.520E+01 26.4 2.663E+00 1. 2 4 6E + 01 0.000E+00 1.030E+01 2.le3E+00 1.296E+01 l 27.5 2.004E+P1 1.827E+01 0.000E+00 2.372E+00 1.627E+01 2.064E+01 2 7. G 1.040E+Cl 1.520E+01_ 0.000F+00 4.794E+00 1.040E+01 1.520f+0_1_
27.5 1.6602-01 1.213E+01 0.000E+0C 1.196E+Ci 1.66CE-01 1.213E+01 PART 12 _ FACES =-1, 1. 2. __ C.0 3.744E-C1 1.219E+01 0.CCOE+00 1.161E+01 3.749E-01 1.219E+01 i "0. 3. 75 0E- C1 1.219E+01 C.000E+00 1.1 PIE +01 3.750E-01 1.219E+01 0.0 1.750E-01 1.219F+01 0.000E+00 1.182E+01 3. 7 5 0E- 01 1.2190+01 2.0 2 . 5 3 P E_- 01 1.231C+01 C.000f+00 1.?OSE+01 2.5?CE-01 1.231E+01
?.0 2.530E-01 1.231E+01 0.000E+C0 1. 2 0 6E + 01 ?. c ? 9E-C 1 1.231E+01 2.0 2.63dF-CL 1.? TIE +01 0.000E+00 1.206F+01 2.538E-01 1.211E+01 l 2.0 2.538E-C1 1.231E+01 0.000E+00 1.205F+C1 2. 5 3 e E- 01 1.231E+01 1 2.0 2. 5 2 9E- C l 1.'?1F+61 n.000E+00 1.?C6E+01 2.530F-01 1.231E+01~~
?.0 2. 5 3 8E- 01 1.251E+C1 0.0)CE+00 1.206E+01 ?.63SE-01 1.231E+0l l __
A-n 12ev. o ~ TJA %It /so _ vuer ou .J
. s ANALYSIS OF OYSTER ' A E f K CCh T A I N'iS N T ^ INT PP.ESS OF 0.0620 KSI.
COORD S PHI S THETA 5 SHEAR 51-52 51-53 52-S3 PAET 12 . __ , TACTS M . L. _ 1_. 4.0 1.28HF-01 1.?43E+01 0.000E+00 .230f+0L 1.289E-01 1.242E+01 4.C 1.28cE-01 1.244E+01 C.0CCE400 1.231E+C1 1.289E-01 1.244E+01 4.0 1.2PSE-01 1. ? 4 4 E+ 01 , 0.0 00E +00 1.2310001 1. 2 81E- 01 1 244E+01 3 ~ 4.0 1.20aE-01 1.243E+01 0.000E+00 1. 23 0F + 01 1.2835-01' 1.243E+01 4.0 1. 2 9 9 E- C l 1.244E+Cl 0.000F+00 1.231E+C1 1.239E-01 1.244E+01 4.0 '
. 2 E 9E- 01 1.244L+0L 0.000E+00 1.231E+01 1. 2 8 9 E-01 1.244E+01 6.0 -3.E15E-06 1.256E+01 0.0COE+00 1. 2 56F + 01 - 2. 9 61E-0 6 1.255E+01 0.n -1.407E-06 1.2'eF+01 C.000E+00 1.J56F+01 -1.407E-06 1.256F+01_
6.0 -1.007E--br 1.2 5 7E + 01 C.000E+00 1.257E+C1 -5. 5 3 7E-07 1.257E+01 , Pfl T 13 _ F A C I:S =-1. 1. ?. C.0 1. 0,,4T + 01 1. A 2 7F + 01 0.On0E+00 2 ?71E+00 1.?27E+01 2.064E+01 0.0 1. n4 0E 4 n t 1 52CE+C1 0.0001.+00 9.795E+CC 1.040C+01 1.520E+0} J.0 1.6^1E-01 1.71?E+01 0.000E+00 1.196E+01 1. 6 /4 1E-01 1. 213E + 01 1.0 1. 8 3 3r + 01 1.76tE+0! O.00nf+00 0.722E-01 1.766E+01 1.833Et01 1.0 1 140E+Cl 1.520E401 0.000E+00 4. 8 7 5E+ 00 !.040E+C1 1.52RE+01 1.0 2. 4 7 FE + 0 ^ 1.29Cr+o! 0.003E+00 1.042E+01 2.4 76F + CO 1.240C+01
?.0 1.6?lE+0! 1.726E+C1 0.000E+00 9.500E-01 1.631E+01 1.726E+01 2.0 1 040E+01 1.649E+01 0.000E+00 5.084E+00 1.040E+01 1.549E+C1 2.0 4. 4 97F + 00 1.312r+J1 03000E+00 9.219E+00 4.497E400 1.372E+01 3.1 1.4 6 7 F + 01 1.704E+01 0.000F+00 7.470F+00 1. 4 5 7E + C 1 1.704E401
'.1 1. n4 F + 01 1.579f+Cl 0.000E+00 f.389E+00 1.040E+01 1.579E+01 3.1 6.233E+00 1.4 s4 r + C 1 0.000E+00 0.308E+CC o.233E+00 1.*S4E+01 4.1 1 210E + 01 1.607E+01 0.000f+00 3.E72E+00 1.?!0E+01 1.697E+01 4.1 1.04CE+C1 1. 61 Cf + C l C.G00E+00 S.761E+0 1.040C+01 1.615E+01 4.1 7 . 7 0 9.: + o n 1. 4 3 5 E + ^ 1, C.000E+00 7.651E+CO 7.704E+00 1.535E+01 5.1 1.1 E EE + Cl 1.702E+01 C.000E+C0 5.145E+00 1.103E+01 1.702F+01 S.1 1.040E+C1 1.65eE+31 0.000E+00 6.177E+00 1.041E+01 1.63SF+31 d 5.1 S.023E+"O 1.214E+01 0.200E+00 7.210E+ c.928r+00 1.614F'O!~ ~~~
j;f. 0.1 1. 0 8 E E - 01 1.71tl+01 0.000E + 00 6.296E*CO .088E601 1.716E401
% z3 ,;.4{
; _, 6.1 1.040t+01 1.702t+01 0.300E+CS 6.617t+00 1. 0 4 0E + C 1 1.7C2:+01 MMp 6.1 9. 9 21c + r ' l.69BE+01 0.000F+00 6.950ft1C 9.928E+C0 1./88E+01
? Meu ,
, 7.1 Id'?9E+ct 1.737E+31 0.010F+90 7.291E+00 _l.0CRE+0i 1.737E+01 .k[:..[
4%y A-47 Sw. o n-
'lu~h Y1 88 .
DD af3/l78
ANAlf515 CF CYSTER CREEK CON T A int 4E NT ; INT PRESS OF 0.0620 KSt. C00PD 5 PHI 5 THETA S SHEAL S 1- S 2 S1-S3 S2-53 FART 1] __ _ _ FACE 5=-1.__1._ 2. 7.1 1. 0 4 0F + 01 1. 7 4 7F+ C l 0.000E+00 7.065E+00 1.040E+01 1.747E+01 7.1 1.073C+01 1. 7 5 7E + 01 0.000E+C0 6.639E+00 1. 0 / 3 E + 01 1.757E+01
~~
8.1 9. 4 5 9E + 0 0 1.763E+01 0.000E+00 8.169E+00 9.459E+00 1.763E+01 0.1 1.040E+01 1.791E+01 0.000E+00 7.508E+00 1 040E+01 1.791E+01_- C.1 1.135E+01 1.319E+01 0.000E+no 6.347E+00 1.135E+01 1.819E+01 9.2 9.dO2E+00 1.792E+01 0.000E+00 8.924E+00 9.992E+00 1.792E+01 9.2 1.040E+01 1.834E+C1 C.00CE+G3 7.936E+00 1.040E+C1 1.834E+01 9.2 1.181E+01 1.876E+C1 0.000E+00 6.943E+00 1.181E+01 1.876E+01 10.2 8.656E+00 1.022E+G1 0. 000E + 00 9.565E+00 8.656E+00 1.822E+01 10.? 1.04CE+01 1.374E+01 0.000E+00 6.342E+00 1.04GE*C1 1.874E+01 IF.2 1.215E+C1 1.927E+C1 0.000E+00 7.11BF+00 1.2156+01 1.927E+01 11.2 ?.429E+00 1.353E+C1 0.000E+00 1.010E+01 8.429E+00 1.853E+01 11.2 1. 04 CE + 01 1.912E+01 0.000E+00 6.714E+00 1.040E+01 1.912E+01 11.2 1. 2 3 dE + C 1 1. 9 71E + C1 0.000E+00 7.3370&00 1.234E+01 1.971E+01 11.) 9.437E+E0 1.093E+01 0.000E+C0 1.010E+01 8.437E+00 1.053E+01 11.2 1.040E401 1.912E+01 0.0COE+00 C.722E+CC 1.040E+01 1.912E+01 11.2 1.237E+01 1.971E+01 0.000E+00 7.345E+00 1.237E+C1 1.971E+01 12.T S . 3 61 F + 00 1.8P4E+01 0.000E+00 1.054F+01 8.301E+00 1.884E401 1E.2 1.C4CE+01 1. A 7 E +01 C.0CCE+C0 9.068E+00 1.040E+Cl 1.c47E+01 12.7 1.251E+C1 2.0100+01 0.000E+00 7.597E+00 1.251E&C1 2 . 0 1 0 c + 0 1__ 13.2 4.236E+00 1.013E +01 0. 000E + n0 1.090E+01 P.236E+00 1.913E+01 1?.2 1.04CE+01 1.97CE+01 0.000E+00 9.381E+00 1.040E+01 1.978E+01 I?.2 1.257F+nl 2. 04 3 E+ 01 0.nCOE+00 7.864E+00 1.257E+01 2.043E+01 5 14.? 8.225E+PD 1.941E+01 0.000E400 1.118E+01 S.275E+00 1.941E+01 14.2 1. 0 4 0 E + 01 2.006E+01 0.000E+00 9.6591760 1.040E+di 2.006E+01 14.? 1.25EE+0! 2.0'?r>01 0.000E+00 0.134E+00 1.258E401 2.072E+01 l 15.3 C. ? 54 E + 0C 1.966E+01 0.000E+00 1.1410+0! 8.251E+00 1. 9 6 6E + 01 IS.1 1.04Ci+C1 2. 0 30L + U t 0.000f+00 9.901E+00 1.040E+C1 2.030E+01
!5.3 1.25tE+01 2.095E + C1 C.000t+00 8. 397E + C 0 1.255E+01 2.095E+01 16.3 S. 31 CE+ 00 1. 9 38E + C 1 0.000E+nn 1.157E+01 8.310E+CO 1.988E+01 16.3 1.04 0E + 01 2.051:+C1 0.000E+00 1.011E+0! 1.040E+01 2.051E+01 16.3 1.250E+01 2.ll4E+01 0.000E +00 3.044E+00 1. 2 9 2f + C1 ?.114E+01 1
17.1 9. 3 02r + 0C 2.006E+01 0.000F400 1.170E+0] J.332F+00 2.008E+01 17.3 1.24CE+01 ' .069E+01 0.000E +a0 1. 0 2 8 0 + C 1 1.040E+C1 2.069Et01
!?.1 1.742E+01 2.120E401 0.000E400 3.80CE+70 1. 2 4 2E + 01 2.129E+01 l
( A-48 /2et o l -_ WA- 1/2/35 j l ORH 2/3/88 a
ANALYSIS CF OYS7Er Cr.EEK CONTAIN"FNTt INT PCESS OF C.0620 KS!. C00PD S PHI S THETA S 'J f E A R S1-52 SI-S3 S2-S3 P AJ_T_U FALEC=-l u i. 2. _ 1 e.3 8.4 6 C E + 00 7.0?SE+01 0.003E+00 1.179E+01 U.46CF + C0 P. 0 7 5F + 01 10.3 1.04CE+01 2. C 3 3E + 01 0.000F+00 1.043E+01 1.040E+01 2.083E+01 __ l t. 3 1.235r+01 2.141E+01 0.000E+10 9.066E+00 1.235E+01 2.141E+01 19,j 8.937F+00 2.039F+01 0.00GE+00 1.184F+01 9.537E+00 2. 0 3 8E +0 L 19.3 ' . 0 4 CE+ 01 2.094E401 0.000E+00 1.054E+01 1.040E+01 2.094E+01
!O,3 1. ? ? 7 E + 0) ?.150F+01 0.000c+00 9.230E+00 1. 2 2 7E + C1 7.150E+01
. 20.3 St607E+00 P,. 0 4 8 r + 01 0.000E+00 1.187E+0! 0.007E+00 2 048E+01 20.3 1.040E+01 2.102E+01 0.000E+00 1.Cl2E+C1 1.040E+01 2.102E+01 20.2 1,2? 0 E + 01 _ _L.156E+01 0.000E+00 9.360E+30 1.220F+01 P.156E+01
? l . '. 0.666r+00 2.055E+01 0.000F+00 1.19PF+01 0.66LE+00 2.055E+01 21.4 1.040E+01 2.ic7E+01 0.00JE400 1. 0 6 7E + 01 1. 0 4 0 E + C 1 2.1C7E+01 L ?14 L '14E+ C1 2.199E+01 0.000E+00 o,453E+00 1.214E+01 P.159E+01
~ ~ ~
22 4 P .711E +00 ?.059E+01 0.900E+00 1.19 8E + 01 P.711E+00 P.059E+01 f ??.4 1.040E+01 2.110E+31 C.000E400 1.069E+01 1.040E+C1 2.110F+01
- 2.4 1. 2 C 9F + 01 2.160F+01 0.001C+00 9.508E+00 1.209E+01 2.160E+01
~
22.4 C.719E+00 2 . 0 5 9 E + 0'1 0.003E+00 1.187F+01 S.719E+00 2.059E+01
??.4 1. 04 0F + 01 2.110E+01 0.000E+00 1.069E+01 1.040E+01 ?.110E+01 22.4 1.?^9E+01 0.160E+01 0.000E+00 9. 515E + 00 1.209E+01 ?.160E+01 1 23.4 E. 75 CE + CO 2.060E+01 0.000E+00 1.165E+01 8.75GE+00 2.060E+01
'3.4 L.0*0r401 2.1095+31 0.000E+00 1.0(oE+01 1. 04 0E 4 01 P.109E401
?3.4 1.206E+0) 2.154E + 01 0.000E400 9.534F400 1.206E+C1 2.16er + 01 24.4 1. 7 6 5 F + 0 0 2. 0 5 7E + 01 C.0COE+00 1.181E+C1 E.765E+00 2.057E+01 24.4 1.040E+0) 2.107E+01 E .?CDE +00 1. 0 6 6E + 01 1.000E+C1 2.lC7E+01 24.4 1.204E+"1 2.156E+01 J.000E+UO 9.515F+00 1.204E+01 2.156E+C1 25.4 c.706E+03 2.052E+01 0.C00E+00 1.17 5E + Cl 6.766E+00 2.052E+01 25.4 1.040E+01 ?.101F+01 0.000F+07 1.0610+01 1.140E+01 2.1CIE+01_
> 2 5 . .. 1. 2 04E + 01 2.150E+01 C.000F+00 9.460E+00 1.204E+01 2.150E+01 26.4 0.757E+00 2.043E+01 0.0LGE4C0 1.16 81 + 01 2.757E+CC 2. 04 3E + 01 2t.4 1.04dc4e1 ?.093F+C1 C.CCUE+03 1.052F+01 1.040E+01 ?.093E+01 20.+ 1. 2 0G E 4 01 2.142E+01 C.uCOE +00 9. 3 71E + 00 1.205E+C1 2.142E+01 I 17.5 o. 74?E+ 33 2.03?E+C. 0.000E+00 1.198F+01 E.74?E+CC 2.032E+01 l ?7.G 1. 04 CF + 01 7.082E+01 C.000E+00 1.0(IF+01 1.040E+01 ?.002F+01 J7 5 1.20ct+21 2.132E+01 C.u.mE+00 9.251E+00 1.2CLE+01 ?.13?E+01 22.5 C.726C+0D ? . 018F + 01 0.001E+00 1.145L+01 S.726E+00 ?.01dE+01 2M.5 1.^4 M+C1 7. 00 SE + 31 C .00nF + 00 1.C2PC+01 1.c40E+C1 ?.068EiO1_
th - 44 /2cv. o
.- '7 M' Ytf03 0/?B 2/3/M
ANAL.YS15 or OYSTER CP.EEK CONTAINf*ENT; !NT PRESS OF 0.0620 KS t. COnRD S PHI S THETA 5 SHEAR 51-52 51-53 32-53 _2ff T 13 FAr_fS=-L. 1. 2.
?h.5 1.703E+rl 2.119F401 0.000E+00 9.105E+00 1.?03E+01 7.119E+01
?9.5 8. 7] f t: +00 2.001E+01 0.000E+00 1.130E + 01 P.716E400 7.001E+01 .
29.5 1.040E+01 2.092E+01 0.000E+00 1.012E+01 1.040E+01 2.052E+01 29.5 1.209F+01 2.103E+0! 0.000E*00 0.935E+00 1.?O9E+01 2.103E+01 20.5 9.723E+00 1. 9 8 3E + 01 C.000E+00 1.110E+01 E.723E+00 1.983E+01 30.5 1. 04 0E + 01 2.033E+01 0.0COE+00 9.926E+00 1.040E+01 2.0 3 3 E +01 - l 30.5 L. 2 0f:F + 01 2.083E+C1 C.0COE+00 9.750E*00 1.20SE+01 2.083E+0) 21.5 0.754c+CO 1.952E+01 C.000E+0C 1.036E+01 9.7 54E + 00 1. 4 6 2_E_ + 01 31.5 1.040E+01 2.011E + 01 0.0CCE+00 9.7C9E+C0 1.040E+01 2.G11E+01 T1.5 1.205F+01 ?.061E+01 0.000E+C0 8.55cE+00 1.205E+01 2.061F+01 32.3 d. 32 3E+ 00 1.939E+01 0.000E+00 1.057F+01 8.623F+00 1.939E+01 32.5 1.04rE+01 1.937E+01 C.000E+00 9.466b+00 1.040E+01 1.987E+01 12.5 1.198E+Al 2.034E+01 0.000E+00 S.360E+00 1.198E+01 2._0_3 4E + 01 31.6 a.04?E+CD 1. 916E + 11 C.aCOE+00 1.022E+01 8.942E+00 1.916F+01 33.6 1.34dE+J1 1.'m0E+31 0.000E+UO 9.197F+C0 1.043E+01 1.960E+01
, 13.6 1.1 B 6E + 01 2.n04E+01 0.000E+00 8.174E+00 1.186E+01 2.004E+01 33.6 0.)GOE+no 1.917E+01 0.000E+00 1.0??E+01 8. 9 5 0E + 00 1.917E+01 33.6 1. %CF+01 1.760E+01 0.00CE+00 9.194Ev00 1.040E+01 1.960E+01 l 33.6 1.1J6E+J1 2.014E+01 0.0C0E+00 d.182E+00 1.18 6E + 01 2.004E+01 34.6 9.13 3E + 00 1.893E+C1 0.000F+00 9.796E+00 9.133E+00 1.393E+01 34.6 1.2402+01 1. 9 31E + C 1 0.000E+00 8.907c+0C 1.040E+0' 1.931E+01 34.6 1.167E+01 1.969E+01 0.000E+0'O 8.019E+00 1.15 7F + 0i 1.969F+3i at.o 9.396E+00 1.S70t+C1 0.000F+00 G.300E.+00 9.34oE+00 1.070E*01 35.o 1.040E+01 1.900E+01 0.000E +03 3.cSSE+00 1.040E+C1 1.1C0t+01 .
35.5 1.141E+31 1.930F+01 0.000f+00 7.690E+00 1.141E+01 1 930E+01
~
l 36.c 9.7$5E+0' 1,848E+01 0.CCOE+2.7 R. 721E + 00 9.755E+00 1.848E+01-3 6 . e. 1.0402+11 1.367F+01 0.000E+00 3.267E+00 1.040E+01 1.367E+01
- 8. 6 . 5 1.10 51: + 01 1.dH6E+01 0.0C01+00 f.el*E+00 1.10SE+01 1.886E+01 37.9 1.023E+01 1.8280+01 0.v?0F+00 3. 0 51E+ 00 1.?23E+C1 1.828E+01 3'.9 1.040c+'l 1.P\?F+01 0.000E+00 7.G?9E+00 1.043E+01 1.833E+01 I 3i.o 1. 0 5 PE + 01 1.030E+Cl 0.000E+00 7.P06E+00 1.05dE+01 1.838F+01 l
33.5 1.083t+01 1.012E+t'~~0.UJ0E+00 7.? bee +00 1.033E+01 1.812E+01 30.6 1. 0 4 0E + C 1 1. 7 9 9E + C 1 0.000E+00 7.588E+00 1.040F+01 1.799E+01 19 . t 4.974E+0) 1.7960+C1 0.000E+0C 7.30BE+00 4.074E+00' 1.736E+01 { ___ l - A-so %o a w_ _ l __ m .v v es
,1
]
ANALYSIS OF DY ST ER CREEK CGNTAINM2NT ; INT PRESS OF 0.0620 KSt. r.00R0 3 PHI S TEETA S SHEAR S I- S 2 S1-53 S2-S3 PART 13 RACES -1. 1. 2. _ 39.7 1.137E+01 i.901E+0) 0.000c+00 6.426E+00 1.157E+C1 1. S 01 E +01 39.7 1.040E+01 1.766E+01 0.000E+00 7. 2 54E + 00 1.040E+01 1.766E+01 39.7 9.220E+00 1.730f+01 0.000E403 3.032E+00 9.22CF+00 1.730E+01 40.7 1.251E+01 1.797E+01 0.000E+00 5.4670+00 1. 2 51E + C 1 1.797E+01 40.7 1.04CE+01 1.734E+01 0.000E'00 6.939F+00 1.040E+01 1.734E+01 40.7 8. 30 0E + 00 1.671F+Cl 0.000E+00 8.412E+00 6.300E+00 1.671E+01 41.7 1.361E+01 1.902E+01 0.000E+00 4.413E+00 3.361E+01 1.002E+01 41.7 1.040E+C1 1.706E+01 C.000E+00 6.659E+00 1.040E+01 1.706F+01 41.7 7.19AE+00 1. 610E + 01 0.000E+00 8. 9 0 5E+ 0C 7.195E700 1.610E+01 42.7 1.402E+01 1.819E+01 0.000F+00 3.272E+00 1.492E+01 1.819E+01 42.7 1.E4CE+01 1.683E+C1 0.000E +00 6.430F+00 1.040E+01 1.663E+01 42.7 5.871E+00 1.54SE+01 0.000E+00 9.589F+CO 5.091E+00 1.54SE+01 43.7_ 1. 6 4 3c+ 01 1.d49E+01 0.000E+00 2.056E+00 1.643E+01 1.849E20_1_ 41.7 1.040E+01 1. 6 f,80 + 01 C.000E+00 6.275E + 00 1. 04 0E + 01 1.556E+21 43.7 ,4 . ' 7 7 9 + 0 0 1.4P7E+01 0.000E+00 1.049E+31 4. 3 7 7E +00 1.487E+01 44.7 1.?l6E+01 1.995E+C1 C.000E+00 7.349F-01 1.016E+01 1.995E+01 44.7 1.34JE+0) 1.662E+01 0.CCOE+00 6. 217E + 00 1. 0 4 0E + 01 1.66?E+01 44,7 2.641E+20 1.429E+01 3.003E+00 1.165E+01 2.643E+03 1. ',2 9 E + 01_ PAFT 14
~ ~
FACES =-1. 1. 2. 0.0 4.192E-91 1 363E+01 0.000E+00 1.321F+01 '4 .17 2 E- 01 1.363E+nt n.0 4.1920-01 1.3630401 0.0 00F +00 1.321E+01 4.172E-01 1.363E+01 0.c 4.192E-01 1.363E+0! 0.000E+00 1.321E+01 4.19 2 E - 01 1.303E+01 ( 2.0 ?.437L-31 1.376E+C1 0.000 E +00 1 34SE+01 2.837E-01 1.376E+01 2.0 2. ? 3 7E- 01 1.37'3+C1 0.000E+00 1.34SE+01 2.d17F-01 1.376E+01 l 1.148E&O1 2.S17E-01 1.376t+01 p ?.0 2.337E '1 1.376E+01 0.003E+00 l =- 2.0 2.1379- 01 1.376E+01 C . 001E + 00 1.348E+01 2. 3 3 7 E-01 1.376E+01
?.0 2.337E-01 1.3 7 6E + 01 0.00]C+00 1.34SE+01 2. 9 ? 7E- 01 1.376E+01 2.0 2. 3 3 TE- 01 1. 3 7 6E + 01 0.000E+00 1.348E+01 2. d 3 7 c-01 1.376r+ct 4.n 1. '. 41 E- 01 1.393E+01 C.000E+00 1. 3 76E + 11 1. 4 41E - 01 1.390E+01 l 4.1 1. 4 41 E- 01 1.390f+01 ?.LOOE+0a 1.376E+01 1 4 41E- 01 1. MOE+01 4.7 1. 4 41 L- C 1 1. ' 7 0c + 01 0.000E+01 1.376E+01 1.491E-01 1.390E+0!
g-s, n e w. o __7UA t/3/M D/?H 2/J/ $8 - l ud
A'l AL Y S IS rd OY ST ER CF.EL K C ONT A I NVE NT ; INT PRESS OF 0.0620 KSI. COORD S PHI $ THETA S SHEAR S1-S2 51- 53 S2-S3 DfET_ls_ t _ F ACES =-1. 1 2 .. 4.0 1. 4 41 E- 01 1.390F+01 0. OP V + 00 1.37AC+01 !.441E-01 1.390E+01 4.0 1.441E-01 1.390E+01 0.000E+00 1.s 3 76E + 01 1. 4 41E- 01 1.390E+01 4.0 1.441E-01 1.390F+01 0.CC0F+00 1.376F+01 1. 4 4 t C-01 1.390F+01_ t; . a 3.915E-06 1.405E+01 C 000E+00 1. 4 0 5E + 01 4. 7 6 3F-06 1.405F+01 6.0 5.712E-06 1.405E+01 0.000E+00 1.405E+01 6.6765-06 1. 4C SE + 01 e.0 E . 7 ? ? r_- OL , 1. 4 0 5 F + 01 0.000F+00 1.405E+01 6.676E-06 1.40SE+01 PAPT 15 FACES =-1. 1. 2.
~
- 0. 0 1.L17E+01 1.89;E+01 0.000E+00 7.315E-01 1.P17E+01 1.895E+01 0a L. 04 0E + 01 1.662E+0j 0.000J+00 6 11_9f+00 1.0iH +01 1.o62r+gt 0.3 2.6.TSE+0C 1.424E+01 0.000E+00 1.156E+01 2. 6 3 5E + 0 0 1.429E+01 1.0 1. 6 4 0E + 01 1.a50f+01 0.000E40'i 2.036E+00 1.646E+01 1.350E+01
,1 . n 1.q41r+01 1.(60E+01 0. 0 0 0F + 00 6.277E+00 1.040E+01 1.6636+01, 1.0 4.346E+00 1.486E+01 0.000F+00 1.052E+01 4.346E+CC 1.496F+C1
'~~ ~~
2 . 11 1.4G7E+01 1. E 2 0E + 01 C. 000F + 00 3.237E+00 1.497E+C1 '"1.B20E+01 2.0 1.040E+01 1.613E+01 0.000E+00 6.431E+00 1.040E+C1 1.683F+01 2.0 5.64CE+ua 1.547E+01 0.000E+00 9.626E+00 5.840F+00 1.547E+01 3.0 1.366E+01 1.60SE+01 .C.CCOE+00 4.36*E+00 1.363E+01 1.005E+01 1.0 1.040E+01 1.706E+01 0.000E+00 6.6590+00 1.040E+01 1.7C6F+01 3.0 7.12 SE + 00 1.e083+01 0.000F+00 8.953E+00 7.125E+00 1.608E+01
~
4.0 1.259E+01 1.800E+01 0.000E+00 5.406E+00 1.259E+C1 1.8C6E+01
- 4. ) 1.040E+D1 1. 7 3 4 E + 01 0.007E+00 6.939F+00 1.043F+01 1.734E+01
*.J 0.213E+CO 1.663F+01 0.000f+C0 0.472E+00 8.213E+00 1.653E+01 5.1 1.169E+01 1.004E+01 0.000E+GO 6.356E+00 1.169E+01 1.SO4E+01 5.1 1. 04 0E + 01 1. 7 6 6 F + 01 0.000F+00 7.254E+00 1.040E+01 1.766E+01_
i C.1 9.1?OE+?' l.727E'C1 0.030E+C0 C.152E+0C 9.120dFOO 1.727E+01 1 6.1 1.095FtC1 1.01cE+0i V.000E+00 7.210E+00 1.099E+01 1.816E+01 6.1 1.04rF+F1 1.79CE+01 0.000E+00 7.59CE+00 1.04ad+01 1.799E+01~ 6.1 9.851E+00 1.763E+01 0.000E+00 7.c70F+00 S.061E+CC 1.793E+01 l 7.1 1. 0 3 5E + 01 1.832E+C1 0.000E+00 7.970E+00 1.035E+01 1.8?2E+01 B 7.1 1.04^E+01 1.AT4E+01 0.000E + 00 7.495F+00 1,04]E+01 1.P34E+01 7.1 1. 0 4 t b + 01 1.S2SE+Cl 0.000E+00 7.900E+00 1.045E+C1 1.835E+01 l 1 7 .1 1.035E+11 1. 9 3 ?E +01 0.000E+00 7.971E+00 1. 0 3 5E + C 1 1.832F+01 A-AG %.o u
- - - NA $_ 3 OAM U3/CC
AN AL YS I S l'F OYSTE S EE K C ON T A I N'C NT I I t'7 PPESS CF 0.0620 KSI. COMD S PHI S THETA S SHEAP S t- 5 2 S1-S3 52-S3 I 9AE! 15 FACES =-1. 1. 2.
.1 1.040r+Cl 1.634E+0) 0.000E+00 7.935E+00 1.040E+01 1.834E+01 7.1 1.045E+01 1.0 35 E +01 0.000E + 00 7.899E+00 1.045E+01 1.835E+01 8.1 9.Pb,:'00 1.853E+01 0.000E+C0 6.639E+00 9.889E+00 1.S53E+01~
8.1 1.n40E+0i 1.863E+01 0.000E+00 9.274E+00 1.040E+01 1.86SE+01 8.1 1.092E+01 1.524E+01 0.000E+00 7.919E+00 1.092E+01 1.084E+01 9.1 9 . 5 3 0 2. + 0 m 1. F 7 tE + 01 0.000E+00 9.221E+00 9.533E+00 1.676E+01 1 0.1 1.040E+01 1.9n2E+01 0.000E+00 8.615E+00 1.040E+01 1.9C2F+01 9.1 1.12 7E + 01 1.928r+C1 0.000E+00 B.009E+00 1.127E+01 1.928E+01 10.1 9.23?E+0C 1.900E+01 0.000E+00 9.724E+JO 9.23]EsCO 1.90CE+01 10.1 1.040E+C1 1.934E+01 1.001E+00 9.938E+00 1.040E+01 1.934E+01 10.1 1.15 3E + C 1 1.9ubE+01 0.000E+00 9.152E+00 1.153E+01 1. 96 8 P+01 11.1 9.100E+00 1.425E+01 0.000E+00 1.015E+C1 G.10]E+00 1.925E+01 11.1 1 . ~. 4 ^ E + C 1 1 965F+01 0.000F+00 9.242E+00 1.040f+01 1.965F+01_ 11.1 1.171C+01 2.004C+01 0.0COE + 00 S.330E+00 1.171 E + C1 2.004E+01 12.1 8.961E+00 1. 9 5 9 E + 31 0.003E+02 1 0 5 2 E + ',' 1 C.VC1EtCC 1.95Cr+0! I?.1 1.040E+C1 1. q u 3E + 01 0.000F+00 9. 526E+ 00 1.043E+C1 1.903E+01 12.1 8.19?E+01 2.036E+01 0.000E+00 R. 531E + 00 1.18 3E + 01 2.036E+01 13.2 o. 90 8E + 00 1. 9 7 4 E + 01 0'.000E+r0 1.083E+01 C.908E+00 1.974E+01 l'.2 1. 64 E + d i 2.0190+ll 0.000c400 9.738E+00 1.040E+01 2.019E+01 19.2 1.190F+01 2.0c4E+0! 0.000F+00 8.741E+0C 1.190E+01 2.064F+01 i 14.2 c.6cdC+00 1.497E+01 0.000E+00 1.110E+01 2.36TE+0'0 1.907E+01 14.2 1.040E+01 2.043E+01 0.000E+00 1.003E+01 1.04".E+01 2.043E+01_ 14.2 1.194E+C1 2.069E+0) 0.000E+00 8.951E+00 1.10'E+01
. 2.089E+01 14.2 8.J6Sb+D0 1.097E401 0.000E+00 1.110E+01 9.8(8E+C0 1.997E+01 14.2 1 04CE+01 2.043E+Cl 3.000E+00 1.003E+01 1.040E+01 2.043F+01 14.? 1.19 4 t' + " I 2. 069E + U I 0.000E+30 S. 950E + 0 0 1.194E+01 2.089E+01 i
15.2 ?.348P+0u 2. 017F + 0 i 0.000F+00 1.133E+01 E.848E+00 2.017F+01_ 15./ 1.04CC+0i 2.0c4E+01 0.0000+C3 1.024E+01 1. U* 0E + C1 2.004E+01 15.? 1.116E+0! 2.111E+ni C.000E+00 9.149E+00 1.19 5E + 01 2.111E+01 l 1(.? 9.??fE+00 2. 0 ' 6! + 01 0.000F+00 1 152E+01 8.d36E+00 2.036E+01 It.' l.340E+01 2.083E+C1 0.'00F+00 1. 04 3E + 01 1.040E+01 2.093E+01 l '. 2 1.197f+01 ?.110f+01 0.000F+00 9.330E+00 1.107E+01 2.13CE+01 l 17.2 E.924F+^( 2.052E+01 0.000E+00 1.170E+01 6.e?4c+00 2.052E+01 g 17.2 !.040E+01 2. U';9 L + 01 G.00]E+00 1.059E+01 1.040E+01 2.099E+01 l ,17.? 1.190F+C1 2.14TE+Al 0.900E+00 3.494E+00_ 1.198E+01 2 .14 7 E + 0_1_ A - 59 Q < v. o maps _ i?RH 2/3/88 _ I
ANALYSIS CF CYSTER CREEK CCATAIM4ENTI INT PRESS OF 0.0(23 KSI.
~
'COORD S PH; 5 THETA 5 SHEAR S1-S2 S1-53 52-53 PUT l_5 _
FAEES=-1. 1. 7 18.2 6.831F+ne 2.C6SE401 0.0CJE 600 1.185E+01 8.801E+00 2.065F+01 1E.2 1.040E401 ?.113E+01 0.000E+)0 1 073E+01 1.0400t01 2.1135+01 1E.7 1.2]OC+01 2.161E+01 0.0COE +00 9.60AE+00 1.200C+01 2.161E+01 19.? E.762E+C0 2.075F+0! 0.000F100 1.199E601 0.7L2E+00 2.073E+01 19.e 1.040E+01 2.124E+01 C.000E+00 1.004EtC1 1.040E+01 2.1245+01 lo.' 1.204E+31 2.174E+01 0.000F+00 9.69tE+00 1.204E+01 2.174F+01 20.2 E. 7 0 0C + 00 2.082E+C1 0.000E+00 1.212f+01 8.700r+00 2.082E+01 20.2 1.040E+ol 2.133E+01 0.00CE +0C 1.C93E+Ci i.040E+C1 2.133E+01
?O.2 1.211F+01 ? 184E+01 0.000E+00 0.734E+00 1.211E+01 2.134E+01 21.? R.611E+1? F.0CSE+01 0.000E+00 ~
1.224E+01 8.611E+00 ?.0PSE+01 21.2 1.040E+01 2.139E+01 0.000E+00 1.099E+01 1.040F+01 2.139E+01 21.2 1.2?OE+01 2.193E+01 0.000F+00 9.731F+00 1.270E+01 2.193E+01_. 21.2 0.011E+00 2.095E+0) 0. 0 0'J E i n n 1.224E+'l 9. 611E + 00 2.d55fiCI 71.7 1.340re01 ?.139E+01 0.00CE+00 1.099F+01 1.040E+01 2.139E+01 21.2 1.220E+01 2.193E+0! C.00]E+00 9. 7 31E + 00 1 2206+01 2.193E+01
~
22.? E.4 91E 4 00 2. 0 65E + 01 0.000F+00 1.235E+01 8.491F+00 2'. 0 P 51T01 22.3 1.040E+01 2.14 2E + 01 C.000E+00 1.102E+01 1.040E+Cl 2.142E+01 22.3 1.237C+01 2.109E+01 0.000E+00 9.677E+00 1.202E+01 2.199F+01
> 20.3 G. 33 9E+ 00 2.0 80E + C1 0.000E+00 1.246E+C1 d.339E+00 2.030E+01 23.3 1.040f+31 2.142E+01 0.000E400 1.102F + C 1 1.040E+01 P.142E+01 23.3 1.247E+'l 2.204E+01 0.000E+30 9.571E+00 1.24?E+01 2.204E401
?4.3 0.155F400 2.0 71E + 01 0.0COE+00 1. 2 56E + 01 0.lbSE+UC ?.071E+01 24.? !.041E+01 2.119E+01 0.000F+03 1.090F+01 1.04)F+01 2.139E+01
?4.3 1.265E+C1 2.200E+01 0.000E+uo 9.407E+00 1.205E&01 2.20$t+01 25.3 7 . 5 4 1 E + .' O 2.0GPE+01 0.000E+00 1.264E+01 7.041E+00 2.05CE+01 25.3 1.04N+r1 2.132E+01 0.000E+90 1.091E+01 1.040E+01 2 ._13 2 E + 01 l Of.0 1. 2 4 7C + C 1 2.200E+C1 0.00CE+00 0.1935+0C 1.2!7E+01 2.200E+01
/6.3 7./30E+<; 2.040E+01 0.CUJE+0D 1.270E+01 7.70]E+00 2 040E+01 26.3 1.040E+01 2.121F + 01 0.0000+00 1.CROEt01 1.040E+01 2.121E+01 2t.3 1.3tlE+71 2.202E+01 0.000E+C0 S. 913E + 0 0 1. 311E + 01 ?.202E+c1
~
27.3 1. 4 3 EE + i G 2.01?E+01 0.CCOE tCO 1.273E+01 7.438F+00 2.017E+01 C.000E+00 1. 0 6 5 F + c l 1.040E+01 p.10cE+01
?7.3 1.040C 401 2.1000+01 2'.) 1.337E+)1 2.195F+01 0.900E+00 6.578E+00 1. 3 3 7E + 01 2.195f+01 l
1.272E+01 7.163E+00 7.16 3E + 00 1.089Es01 0.000E+00 1.989F+01. _ _ . _ _ . . 28.3 29.3 1.C40E+01 ?.calE+C1 0.00]E+C0 1.045E+01 1.040E+01 2.096E+C1 A-54 A- v. o WJL t/c /93_ _ DRM 2/3/88 _ __
ANALYSIS OF OYSTEP CR EEK CONTA lf#E NT ; INT PRESS C5 0.0620 KSt. C00R0 S PHI 5 TFETA 5 SPEAP SI-52 SI-S3 52-S3 o P ', F T 13 _ IACES=-L,_ L, 2. __
?f.1 1.364r+01 7 t h 3r + 01 0.001F+00 P. . l A 7 r + n o t.'64E+01 2.1P3F+01 20.2 7.163E+00 1.989E+01' O.000F+00 1 272E+01 7.lfI32+00 '.989E+01 23.1 1;C4CF+01 2.096E+01 0.000E+00 L,045E+01 t,040E+01 2.aC6 E +0 L 2L.3 1.364E+n1 ?.183E+01 0.000F+00 3.186F+00 1.364E+01 2.103F+01 24.3 6. 9 06E + C 2 1.955E+01 0.000E+00 1 267F+01 6.866E+00 1.955c+01 29.3 L,0 4 0E + 0L_P . 0 61E 6 01 0 100E + 0 0 L. 0 20E + 01 1.040E+0) ? . 06 LE +0J_
20.3 1.392E+01 2.166E+01 0.000E+C0 7.742F+00 1.392F+C1 2.166F+01 3C.4 0.515E+00 1. 917E + 01 C.000E+00 1.255E+01 6.619E+00 1.917E+01
'o.4 1.040F+01 ?.030E+01 0.000F+00 9.897F+00 1. 04 0!: & C 1 2.030F+01 30.4 1.419E+01 2.144E+01 0.000E+00 7.249E+00 1.419F+01 2.144E+01 31.4 t.32CE+00 1.S73E+01 Co000E+CO 1. 2 3 5E + 01 6. 3 8 0E+ 00 1. 8 7 3IE + 01 3 1.
- 1.140F+01 1.793F+0) 0.000E+00 9.530E+00 1.040E+01 1. 9 9 3F + 01 31.4 1. 44 3r + 01 2.114F+01 0.000E+00 6.714E+00 1.443E+01 2.114E+01 3 P . <. 6.1SSE+00 1.024E+01 0.i00E+00 1 205E+01 6.l E6r.+ C0 1.824E+C1
, 11. A__1 04 CE + C l 1.450F+0? 0. tone +00 4.009F+00 1.040E+01 1.950F+01 32.4 1.462E+01 2.0 7 7E + 01 0.;COE+UO 6.148E+00 1.462E+01 2.077E+01 33.4 5.062E+00 1.770E+11 0.GUOF+0S 1.164E+0i 6.062E+C0 1 770E+01 33.4 1. 04 ci+ C l 1.910F+01 0.000E+00 8.40lF+00 1.040E+01 1.900E+01 , 33.4 1.4 /4t + 01 2.031E+01 0.0COE+00 5.562F+0D 1.474L+01 2.031E+01 34.4 ' 03 3E + 00 1. 713r + 11 0.uOOE+00 1.100E+01 6.033F+00 1.713E+01' 16.4 1.040E+01 1 444E+01 0. 00 0E + 00 3.033E+00 1.040E+01 1.F.44E+01_
34.4 1.477E+01 1.975E+01 0.000E+00 4. 9 74E + 00 1.477E+C1 1.975F+01 35.4 6.12 6E + 00 1.652F+01 U.000E+00 1.039E+01 6.123E+00 1.652F+01 19 . ., 1.040E4il 1.730E+01 0.000E+00 7. 3 96E + CO 1. 0 4 0E + C 1 1.78CE+01 35.4 1. 4 6 C E + 01 1.903E+]1 0.000E+00 4.404E+00 1.46SE+01 1.908E+01 35.4 6.124E+90 1.'52E+01 0.000E+00 1.039E+01 6.12 9F + CO 1.652F+01 15.4 1. C 4 0' + C 1 1./ ROE +C1 0.003E+00 7.396F+00 1.040E+01 1.73CE+01
, 35.4 1.46dE+01 1.900E+Cl 0.000E*00 4.404L&CO 1,.468E+01 1.40SE+01 36.4 5.3E2E+0C 1.c49E+01 0.000E+00 0.506E+00 6.3F2E+00 1.589E+01~
P:.4 1. 04 05 + 01 1.709E+01 0.3C0E+00 6.6c1E+00 1.040E+01 1.700E+01 3( .4 1.442E+c1 1.630E+01 0.C'1E+60 3.877E+00 1. 4 4 2E + 01 1.830E+01 37.4 /.E32E+CO 1. 5 2 5F + C l 0.000F+00 9.423E+00 6.832E+00 1.525E+01_ 37.4 1.}40E+^1 1.6?3E+C1 C.^00E+00 5.9'3E+07 1.C40E+01 1.633E+01 l 31.4 1.397E+01 1.740E+01 0.000F+00 3.422E+00 1.397E+01 1.74CE+01 l , A-D' Ga o rJn 2b.fas DA'N 1/J/78 l l _ _ _ _ _ _ _ _ _ _ _ _ . _ _ _ . ]
.. --. . ~ n. : .
n: : :a n . , ... :.._. f; ' . ,
- u. -
ANALYSIS OF OYST E0 CP EEK CONTAIN4EN1; INT PRESS OF 0 ~ C004D 5 PHI S TFETA S SHfAP 01-S? SI-S3 r<- . _-- S2-53
,, PAPT IS FACFS=-1. 1. (, _ _ _
36.5 7. 517E + 0 0 _- -- _. 1.463E+01 3 C. 5 1.040E+01 0.000E+00 7.117E + 0 0 3P.5 1.550E+01 0.000C+00 7. 517E + CO 1.463E+01
- 1. 3 29E + 01 1. 6 3 7E + 01 5.097E+0C 1.040E+01 0.000E+00 3.077E+00 1.550F+01
_iL9.5 1.320E+01 1.637t+n! 0.43?f+00 1.40}j+01 19.5 1. 04 CC + 01 0.000E+00 5.571E+00 19.5 1.453E+C1 0.000E+00 6.4P2E+00 1.40SE+01 1.232F+91 1. 5 21F + 0 ! 4 226C+00 1.040E601 0.000E+00 2.031E+00 1.463E+01 40.5 1.?!?E+01 1.521E+01 9.772r+Co 1.354E+01 40.S 1.040E+01 0.0"3F+00 3.766E+00 40.5 1.373E+01 0.000E+00 9.77?F+00 1.354F+01 1.103F+01 1.392E+01 3.324E+CO 1.040E+Cl 0.000E+C0 2.8E2E+CO 1.373E+01 41.5 1.1 C 3E + 01 1.392E+C1 1.143E+01 1 313f + 01 41.S 1.C40L+01 0 000E+00 1.692f+00 41.5 1.292E+01 C.000E+00 1.143E+01 1.313E+01 9.272E+00 1.251E+01 2.413E+iiO 1.04dh+01 0.000E+00 3.135E+0C 1.2826+01 42.5 9. 3 7?F +00
- 1. 3 5 2E + C1 1. 2 51 F + C 1.
42.5 1.2A6E+01 0.000E+00 1.041E+01 1.192E+Cl 6.599E-01 1.2869+C1 43.5 7.29CE+00 0.000E+00 1.519E+00 1.352E+01 1.099E+01 0.000E+00 1.040E+01 1.19? E + 01 3.693E+00 7.2 9 0E + C0
\
-- 1.099r+01 PWT 16 FA C c S = -1. 1. 2.
C.] 1.300E+01 2.0 1.292E+01 0.000E+C0
- 4. 91 CE + 00 1. 0 2 70 + 01 5. 6 5 7 E-01 1. 2 9 2 E + 01 l U." -3.iclE+00 0.000F+00 5.364E+00 1.33CA+01~
- 7. 7 3 3E + 00 C.300E+00 4.910E400 1.027E+01 1.129E + 01 -3. 5 61 E+ 00
?.0 1. 4 4 0E + 01 7.733E+0A 2.0 1.152E401 0.003F+00 4.410E+00 9.6 7 5E + 00 2.880E+00 1.15?E&C1 2.0 ', . 5 3 2 t + 3 ) 0.000E+00 3.764E+00 1.440E+01 5.6 2 7c +00 0.000E +00 4.c10r+00 8.675E+00
- 1. 041E + Q 1 -4. 5 62E + 00 40 1.553C+C1 E. 82 7E + 00~
4.0 1. 054E + 01 0.000E400 4.910E+0a 7.354E+r0 4.992E+00 1.054C+01 1 4.0 - 5.713E+'l 0.000E+10 2. 4 4 4 E + 10 1.553E+01 4.16 7E + 3 0 0.'00E+00 4. 910E + C O 7.354F+00
^
C.0 9.880E + 00 - 5. 713E + 00 4 16 7E + 0 C
- 1. 6 9 0 E + 4 's . 9 4 4 f+ 0 0 6.0 4.910E+1) C.LCOE + 00 e. 990E+ 00
- 6. 0 - 7, 0 79E + 0c 6.347E+00 0.000E+00 9.944E+CC 1.690E+01' 7.7sCr+9c 1. 4 3 7E + 00 4.910E+00 c,390g,JO C. 34 7F+ 00 9.829E+00 -7.U79F+00 2.750C+00 s-l-
A ~A6_lcK 6 I 7330 * /c (SA on unr2
ANA1.Y315 Of UYSTED CREEK CONTAINME NT; ifN DRESS Of 0.0620 KSI. C00n] S PHI S THETA 5 S HE A P. 51-52 S I-S 3 52-53 PAdT 17 I: A C E S =- 1. 1. t. _
- 0. 0 - 8. 514E- 0 2 4.115F+00 0.0000+00 4.200E+00 -3.519E-02 4.ll5E+00 3.3 -2.262E-Ol 4.049F+GO 0.003E+00 4. S 7 5E + 00 - 2. 26 2E- 01 4.649E+00
- 0. 0 -3. 6 71 E- 01 5.183E+00 0.000E+00 5.5SOE+00 -2.671E-C1 5.183E+0C 3.0 - 1. 09 3 E- 0 2 4.041E+00 0.000E+00 4. 0 52E + 00 -1. 09 6E-02 4.041E+00 3.6 -1. 4 0 0E- 01 4.563E+00 0.000E+00 4.703E+00 -1.4C0E-01 4.563E+00 3.6 - 2. 6 91 F- 01 S.ORSF+0C 0.000F+00 5.354E+00 -?.691E-01 5.065F400 7.2 -1.594E-01 4.600F+03 0.000E+00 4. 7 58E + 0 0 - 1. 5 8 4E- 01 4.600E+00 7.2 -1.65fE-01 4.79(F+00 0.000E400 4.962E+00 -1.055E-01 4.796E+00 7 . 2 - 1. 7 2 6 E- 01 4.993E + 00 0.000E+00 _S .16 5E + 0 0 - 1. 7 2 6 E-01 4.993E+00
- 7. 2 - 1. 5 0 3E- 01 4.600E+00 0.000F+00 4.758E+00 -1.583E-01 4.o00E+00
- 7. 2 - 1. 6 51 F- 01 4.796E+0c 0.000E+00 4.962E+00 -1.651E-01 4.796E+30 7.2 -1.718E-01 4.993E+00 0.003E+00 5.16 5 E + 00 - 1. 718E- 01 4.993E+00 10.F -7.711E-02 4. 519E+ 00 C.000E + 00 4.596E+00 -7.711E-02 4.519f403 10.A -i.0406-F2 4.712E+00 0.or0E+00 4. 792E+ 00 -8. 04 0E-02 4.712E+0C 10.0 -o.370E-C2 4.905E+00 0.00]E+JO 4.930E+00 -8.370E-C2 4. 90 3H + 0 f 14.4 7.6 29E ^6 4.442E+00 0.0C0E+00 4.442E+00 0.583E-06 4.942E+33 14.4 2.861E-06 4.631E+00 0.000E+00 4.631E+00 2.8610-06 4.631E+C0 14.4 - 1. 9 07E- 06 4.021E+00 0.000F+00 4.821E+00 -1.907E-06 4.821F+00
? ART IS _ _
FACrs -l. 1. 2. 0.0 1.711F+0! 1.001E+01 0.000F+00 7.109F+00 1. 0 01E + 01 1.711E+01 0.0 4. 910E + C0 6.347L+00 0.000L+00- 1.437E+0C 4.910E+00 o.347E+00
" .3 -7.293E+07 2.606E+00 0.0CCE+C0 9.979E+00 -7.293E+00 2.696E+00_
1.' l.?65F+Al 7.753E+00 3.300E+00 4.a94E+00 7.763E+00 1.265E+01 i ).] 4.01rE+cq 5.442E+0C 0.000E+01 5.217E-01 9.910E+00 5.442E+30 l 3.0 -2.826E+C0 3.121E+30 3.103F+00 5.947E+]J -2.P26E+C0 1.121E+00 s .J 9.12 7E + 0C 6.319E + 00 0.000E+00 2.903E+00 t.?19E+30 7.12 7 F +30 i C.) 4.910E+00 5.054E+00 0.300E+00 1.;40E-01 4.910E+00 5.054E+0C l 6.F 6. C ) 7 F- 11 3.7aoE+0n 1.700E+00 3.096E+00 A.937E-01 3.789E+00_ 9.1 6.642:+3r S . 4 71E + 10 0.000F+nS 1.171E + 00 5. 4 71 E + 00 6.642E+00 l 4.J 4.01CE+GJ 4. 81L+00 0.3CJE+03 4.1059-02 4.911L+17 4.951F+10 9.0 3.17 9E + C 3 4.4?2E+00 0.000E+00 1.253F+00 3.179E+00 4.432E+00 p_ __ _ _ . _ . . A -er7 Eev. o 7:/A 0/_t/S9___ _ DAW :./ 3/??
A'l A L Y S I S GF CY ST ER CREE K CCNTA IF! MENT; INT PRESS OF G.0620 KSI. COURD 5 PHI 5 THETA S SHEAR SI-52 51-S3 52-53 Pf R T 11 FACES -1. _L. ?. 9.0 6. C 4 20 + 00 G.471E+00 ,q.000c+00 1.171E+00 5.471E+00 6.642E+00 9.0 4.u10E+00 9.45]E+00 C.000E+00 4.10 5E- 0 2 4. 910E + 00 4.951F+00 C.0 ?.179F+01 4.432E+00 0.000E+'O 1.253E+00 3.179E+00 4.432E+00 12.3 5.217E+00 6. 061E + 06 1 000E+00 1.559E-01 5.061E+00 ? 52 _11FdC_0_ 12.0 4.910E+09 4.969E+10 0.000E+00 5.857E-02 4.910E+00 4.969E+00 12.n 4.6r4r+00 4.877E+00 0.100F+00 2.730r-01 4.604F+00 4.877F+00 15,0 4,15_0c+C_0 4.994E+00 0.000E+00 1.445E-01 4. 810FJ_00 4 ._9 9.4 Ft+A0_ 15.0 4. 91 CE + 00 5.012E+00 0.000E+00 1.022E-01 4.710E+00 5.012E+00 15.0 4, 7 71E + 00 5.031E+00 0.000E+00 5.989E-02 4.971E+00 S.031F+Q0_ 18.J S.53?F+00 E.244E+00 0.000E+00 ?.977E-O L 5.?44E+00 5.532F+00 10.0 4.910F6(0 6.058E+00 0.000E+00 1.476E-01 4.910Et00 S.05SE+00 14._0 4.2tfE+03 4. S 71E + 0C 0.00CE+00 5.030E-Ot 4. 2 8 3E + 00 *.871E+00 PART 19 FACE 5=-1. 1. 2. O.0 2. 2 91E- C 1 ?.653f+00 0.000E*00 3.425E+00 2.261E-01 3.653E+05-0.0 2.?87E-Cl 3.663E+]O 0.000E+00 3.434E+0C 2. 2 8 7E- 01 3.663E+00 0.0 2.29?E-Cl T.672E+00 0.000E+00 3.443F+00 2.293F-01 3.672E+00 2.0 1. l i C E- 01 3.689f400 0.000E*00 3.495E+00 1.939E-01 3.60SE+05'
?.0 1.035E-01 3.6980+00 0.000F+00 3.504E+00 1.935E-01 3.698E+0C 2.' l.440F-r! 3.707E+00 0.000F+00 3.513F+00 1.440E-01 3.707E+00 2.1 1.930F-01 3.68SE+0C 0.000E+00 3.495E+00' 1.9 30E- 01 3.693E+00 2.0 1. G 3 5F - C l 3. C G 8F + 0C C.0LOF+00 3.504E+00 1.935E-01 3.698E+00
, ?.1 1.440E-C! 3 . 7 0. i E 4 0 C 0.000C+co 3.513E+10 1.940E-01 3.7C7E+00 l l 4.0 1.*'PE-01 3.725F+CC 0.000E+00 ?.568F+00 1.568E-01 3.725F+00_ l 4.0 1. 5 7 2C- C 1 3.734E+00 0.061E600 3.577F+00 1. 5 7 2 f- 01 3.734r+0c 4.0 1. 6 7 /.F - 01 3.744F+uO 0.003E+00 3.586E+CO 1.476E-C1 3.744E+0C I 4.3 1. 5 t S F- C l 3.725E+0C C.100E*00 3.566E+00 1. 5 6 C E'- 01 3.72SE+00 4.3 1 572E-01 1.734E+00 0.000r+00 3.577E+00 1.572E-Cl 3. 7 3 4 F + 0_0_ 4.3 1. 6 7 6E- C 1 ?.744E+00 0.000E+00 3.516F+n0 1.576E-01 3.744E+00 i 6.C 1.194E-01 3.762E+JO 0.000E +G0 3.643E&O7 1.17 4 E- 01 3.762F+00 1 (.1 1.197F-0? 3.772F+0C 0.010E+00 3.652E+10 1.19 /F-01 3.772E+00 5.0 1. 2 0 0 c- C l 2.701E+00 0.00CE+00 3.661E+00 1.201E-01 3.761E+00 , A-D Rev.o b b l _ DJ?N 2/3/8d' l
AN AL YS I S OF OY ST EF. CR E E K C CN T A l tlitE N T ; INT PRESS OF 0.0620 KSt. COORD i PHI 5 THETA S SHEAR 51-52 51-53 52-53 [ PAPT Jj _ FACES =-1. 1. 2. _ _ 6.0 1. l o 4 E- 01 3.762E +00 0.000E+30 3.643E+00 1.lc4E-11 3. 762 6 +0 0 6.0 1.197E-01 3.7720+00 0.000EiOO 3 652E+00 1.19 7E- 01 3. 7 72E+ JC 6.0 1. 2 0 0E- 01 3.781E+00 0.000E+00 T.661F+00 1.200E-01 3.781E400 0.0 8.035E-02 3.800E+0C C.000E+00 3.720E+00 8.085E-C2 3.800E+00_ 8.0 3.106E-02 3.81CE+00 0.000E+00 3.729E+00 0.106E-02 ?.610E+0C 8.0 8.12 7F- 0 2 3.820F+00 0.000E+00 3.739E+00 8.127E-02 3.820E+00 0.0 0. 0 8 6E- 02 1.SCOE+00 0.000E+00 3.720E+00 8.086E-C2 3.800E+00 8.0 8.19 6E- 02 3.810E+00 0.000E+00 3.729E+00 C .1 0 65- 02 1.810E+00 8.0 8.1270-02 3.820E+00 0.000E+00 3.739E+CO 2.12 7E- C 2 3.820F+00 10.0 4.10 7E- 02 3.640E+0L 0.000E+00 3.799E+00 4.107E-02 3.040E+00 10.0 4.11RE-9' 3.850E+00 0.000E+00 3.809E+00 4.11SE-02 3.850i+0C 10.0 4.128E 02 3.860E+00 0.000E+00 3.319E+00 4.12 0 E- 0 2 3.060E+0C 10.3 4.108E-02 3.P40E+00 0.030F+00 3.799E+00 4.1 C 3E- 02 3.C40E+0C IL.0 4.118E-02 3.860E+00 0.000E+00 3.309E+00 4.113E-C2 3.350E+0C 10.0 4.12 aF- 0 2 3.660E+00 0.000E+03 3.a19E+00 4.128E-02 3.860"+00 I?.9 3.21SE-Of ' .?81E+00 0.000E+00 3.881E+00 3.815E-06 3.CBIE+00 12.P 2. 0 61E- 0 6 3.891E+00 0.000E+00 ?.391E+00 2.861E-06 3.891E+00 1 J . '. , a.000E+0) 3.901F+00 0.000E+00 3.901E+00 0.000E+00 3.901F+00 PARI 20 FACES =-1. 1. 2. 0.0 '5.972F+CC S. 316E+ 00 0.000E + 00 5.954E-01 5.376E+00 5.972E+00 0.0 4.910F+30 5.356E+0C 0.000E+C0 1.476E-01 4.910E+00 5.058E+0C 0.] 3.249r+00 4.739E+00 0.00J E +03 3.906E-01 3.849E+00 4.739 +C0 3.b 4.79dF+70 5.162E+00 0.000E+00 1. 9 2 3 E- 01 4.040E+00 5.192E+00 1 3." 4.910E+00 5.198E+00 0.000E+00 2. 4 81 E- C ) 4.910E+C0 0.158E+00 3 ."I 4.631f+(c 5.134E+CC 0.000E+00 3.031F-01 4.031F+00 5.134r+oc l DATT 21 FACES =-1. 1. 7. l C.0 2. 3 3 5 F- 01 3.755F+0C 0.000E+00 3.622E+JO 2. 3 3 5E-01 3.755E+00 C.000E+00 2.731E+00 1.364E+00 4.095E+00 l 0.0
, 0.3
- 1. 3 t 4F + 0 0
?.494E+?1 4 . 0 7 51 + 0 C 4.434E+10 0.3 00F + ^ 3 1.039F+00 ?.494F+no 4.434E+0C A-39 Oc v. o CA Sh/ee PAW :U3/88 _
~
/W /iL YS I S O F Ov 5T FR CP E E K C CNT A I NV.EN T i INT PRESS OF 0 0620 KSt.
CPCRD 5 PHI S THETA 5 SHEAR S1-52 S1-53 52-53 PALT 21 FACE 5=-1. 1. 2. . - -- 2.3 2.014F-01 3 . 9 0 9 E,+ 0 C 0.000f+00 3.607E+CO 2. 01_4 E- 01 3.909E+00 2 . .. 1.3(4t+CC 4.1576+00 0.003E + 30 2.793E+00 1.3t4E+0D 4.157E+00 2.3 2.52(E+CO 4.5C6F+00 0.000E+00 1.930E+00 2.526E+00 4 . 5 0 6 F + 0_0_ 2.3 2.014E-01 3.909E+00 0.0C]E+00 3.607E+00 2.014E-C1 3.6C90+0C 2.' 1.?64E+CO 4.157F+00 0.000E+00 2.793E+00 1.364F+0,0 4.157E+00 2.3 Z.526E+00 4.506E+00 3.000E+00 1.980E+00 2.526E+00 4.506E+00 4.5 1. 2 0 7 E- 01 3.035E400 0.000E+00 3.715E+00 1.2C7E-01 3.835E+0C 4.9 1.364E+00 4.208E+C0 0.000E+00 2. 34 4 E + 00 1.364E+00 4.208E+30 4.5 2.607E+00 4.591E&OO 0.000E+00 1.974E+00 2. 6 C 7E + CO 4.581E+00 PAET 22 __ _ FACES =-1. 1. 2. __ O.0 5.17 PE + CO 5.353E+00 0.0C0F+00 1.742E-01 9.178E4 00 S.353r+0S D . ') 4.09PE40] 5.027E+00 0.000E+00 9. 3 4 7E- 01 4.052E+00 5.C27E+CC , 0.' 3.C05F+00 4.701F+00 0.000F+00 1.695E400 3.OE5E+00 4.70]E+00 5.: 3.33CE+CC 5.092E+00 C.0000+00 1.254E+CO 1.038E+00 5.092E+00 5.1 4.092E+00 5.lf.9E+0C 0.000E+00 1.077E+00 4.092E+C0 5.169E+0C r.1 4.'4tE+CO 6. 2 4'F + 0 0 0.000F+00 8.939F-o; 4.346E+00 6.245F+00 5.1 s. 6 3 bE + 0C 5.072E+00 C.000E+00 1.254E+00 3.030E+C0 5.092F+00 5.1 4.042E+00 5.169E+00 0.000E+00 1.077E+00 4.092E+03 5.169E+no 5.1 4.346E+00 5.245E+30 0.000E +00 3. 9 0 9E - 01 4.346E+00 5.245E+0C IJ.3 4. o w 1E + 00 f . 2 93E + 00 0.00ub*00 1.194E+00 4.u'/9E+00 5.293n+]c 10.3 4.072E+r0 5.291E+CC 0.000F +00 1.199E+00 4.002E+00 5.291F+00 10.? 4.005E+0c 6.201E+00 0.000E+00 1.2C4E+00 *.0SSE+00 5.289E+00 a 11.3 4.04cF+co '; . 2 71 E + 0 r C 100E+00 1.194E+00 4.099E+00 c.29?E+0C 10.3 4.072E+JC 5.291E+00 0.003E+30 1.199'+30 c 4.072E+C0 5.?91F+00 10.3 '4 . 0 n 5 F + C O 5.2RCE+00 0.000F+00 1.20*E+00 %.085E+00 5.239F 1 15.4 5.195E+ED 5.976F+00 0.030E+03 3.167E-02 9.395E+00 0.976F+CS 15.4 4 . 0 9 2 F + r' 0 s.435E+00 0.000E+00 1.344E+00 4.092F+00 5.435E+00 15.4 ' . ? . 9 E + r n 4.095F+0c 0.000F+00 2.6CSE*00 2.2 PCE+ CO 4.8'5E+03 15.4 5.045F+CO 5.9 76E + 00 0.000E+00 3.167E-07 3.n45E+00 '. 076E+00 l'.4 4.04?E+0n 5. 4 *. 5E + 3 C C.3TJE+93 1.344E+0h 4.0920+0C f.435E+CC A-co llev. o
.- ._. "Cin_ 2-/JfS8 _-.
06 2/2/98 __-
A?!ALY$k S OF OY ST ER GR EEK CG ATA IN'4dNT ; I fli PRESS OF 0.0620 KSI. C')O <D S PHI $ THETA S SHEAR 51-52 S1-53 52-53 OA" T 22 F A C d s - 1 ,__ ,_l , ?. _ _ _ , , . 15.4 2.2897+00 4.995E400 0. 0 0 0 F + 0_ ) 2.605F+00 ?.299C+00 4.!'orr+00 23.5 9.1 L5E + 0 0 7.402E+00 0.000E+00 1.733E+00 7.40?[+00 4.135E+0C 20.5 4.092Et00 5.BG9E+00 0.000E+03 1 797E+00 4.092F+00 6.8CvE+00 20.6 - 9. 516 E- 01 4.3 74E+ 00 0.000c+00 5.328E+00 -9.J165-q1 _4 . ;L7Eg100_
~
PART 23 FACES =-1. 1. 2. 0.0 -1.317E-01 4. CC9E + 00 0.000E+00 4.940E+00 -1.317E-01 4.809E+00 0.0 -1.?7?E 01 4.64Lr+00 0.000E+00 4.769E+00 -1.?7)E-01 4.642F+00 C.0 -1 226E-01 4.476E+00 0.000E+00 4. 5 9 9 E + 0 0 - 1. 2 2 6E- 01 4. 4 76E + 0C
? . A -6. 4 5 0E- C 2 4.741E+00 0.000E+00 4. 006 E + 00 -6.4 5 0 E-02 4.741E+00 18 -6.E 7E-c' 4 . c 7 7_E + C 0 0.0 00E + 0 0,_4. 64 0E + 0 0 - 6. 2 RE- 0 2 4 5778+00 2.9 -0.004F r2 4.413E+00 0.000E+00 4.473E+00 -6.0C4E-02 4.411F+00 2_. 3 -6,450E-0? 4.741F+00 L OOOF.400 4. 8 0 6 E + 0 0 - 6. 4 ', K _0 2,__ 4. 7 41 E + 0_0_
2.C -6.2'7E-02 4.577E+0C 0.000E+00 4.640E+00 -6.227E-02 4.577E+00 P.0 - e, , 0 ') 4 E- 0 2 4. 4.lj edC_0 0.000E+00 4.472(+00 -6.nO4E-07 4.413E+00 c.6 1. c S 7 F- no 4.A77F+00 n 000E400 4.677F+00 1.007f-06 4.677F+0C 5.5 1. 3 0 7E- OL 4.515E+00 0.000E+C0 4.515E+00 1.90?E-06 4.515f+00 5,5 9,337E-07 4.353E+00 1 100E+00 4.353F+09 9. 5 3 7E- C 7 4.357E+0C PART 24 FArFL=-1. 1. 2. l 0.0 9.241E+0C 7.434f+00 0. 000E + 0 9 1.P07E+00 7.4 34 E + 00 0.241E+96 0.J 4.092E+00 6.030E+70 C.000E+00 1. 7 0 7E + 00 4.092E+C0 5.989r+00 C. 0 - 1. 0 5 7 E + 0 0 4.745F+00 0.0n0E+00 9.402E+00 -1.057E+00 4.34SE+00 1 D.3 0.24/E500 7.473L+C0 0.000E+00 1.769E+00 7. 4 7 :i. + 0 0 9.242E+0C O.3 4.392F+00 5.42CF+SO 0.0D"E+00 1.835f+00 4.092E+C0 5.928F+0C l 0. 3 - 1. 0 5 SF + 00 4.3336 00 0.0005+00 5. 4 41 E + 0 0 - 1. 0 6 ti E + 0 0 4. 2 93F +00 1 A- 4.1 Qw.. o- .- l rn sh(_se 0$U 2/Z/6V l l
w AN AL YS IS OF OY ST ER CR EEK CONTAl.4:4E f111 INT PRESS OF 0.0620 KSI. CCORD S PHI 3 THETA S SliEAP S1-52 51-53, 52-S3 It ?_ PAk7 25 5- -- FACCSs-1. 1. 2. 0.0 1.?79F-01 4.542F+00 0. '100E + 00 4.414f+00 1.279E-01 4.542F+00 0.0 1 329E-n1 4.720E+00 0.000E+00 4. 5 8 7E + 00 1.329E-01 4.720E+0C 0.0 1.3BCE-01 4.h98F+00 0.000E+00 4.7600+00 1.380F-01 _4.898F+00 2.8 6.532E-02 4.605E+00 0.000E400 4. 54 0E + 00 6.53?E-02 4.605E+00 . 2.8 6.787F-02 4.7C5F+00 0.000E+00 4.717E+00 6. 7 0 7E- 0 2 4.785E+0C 2.8 7. 04 3F-02 4.966F+00 0.000E+00 4.695E+00 7.044E-0? 4.966r+00 2.8 6.'37E-C2 4.605E+00 0.000E+00 4.540F+00 6.5??E-02 '.605E+0C _ 2.0 6. 7 S 7 E- 0 2 4.735F+00 0.000E+00 4.717E+00 6.788E-02 4.735d+00 2.8 7.043E-02 4.966E+00 0.000E+00 4.8 95E + 00 7. 0 4 3 r- C 2 4.966E+00 ! 5.5 c. S T 7E- 07 4.6 70E+ 00 0.000E+00 4.670E+00 9.537E-07 4.670E+00 5.5 9.537E-07 4.C53E+00 0.930E+00 4.853F+CO 5. 5 3 7E-07 4.PS3E+00 5.5 0.000E+0C 5.036E+00 0.000E+00 5.036E+00 C.000E+00 5.036E+0C PALT 26 L ra c t S=- 1. 1. 2. 0.0 9.253E+CO 7.4 76E + 00 0.000E +00 1. 7 77E + 00 7. 4 76E + 00 9.253E+0C
- 0. 0 4.710E+00 6.173E+00 0.000E+00 1.263E+00 4.910E+C0 6.173E+00 0.0 5. 6 7 5E- 01 4. 870E + 00 0.000F+00 4.303E+00 5.675E-01 4.870F+00 l 0.0 2.015E+vc 7.1570+0C O.000E+00 4.842E+C0 2.315E+00 7.1575+00 9.5 4.910E+00 7.9360+00 C.00nE+00 3.025E+00 4.910E+00 7.936E+00 E. . G 7.600E+00 8.714E+09 0.00CE+00 1.209E+10 7.5C6E+C0 9.714E+00 S.5 t. 31 SE + CC 7.157E+00 0.000E*0.0 4.04eE+00 2.315E+00 7.157E+00 8.5 4.91CE+00 7.93tE*0C 0.000E+00 3.C25E+00 4.910E+00 7.936E+00 C.5 7. 5 06 E + 00 0.714E+66-~0.000E+00 1.200E+00 7.506E +00 S.714E+0C l
j 11.0 -1.129E+CO 6.(57E+00 0.000E4G3 7.78t.E+00 -1.129E+00 (.667E+0) l'.0 4 . 91 0 E + 0 0 8.460E+00 0.000F+00 3.559F+C0 4.910F+00 E.469E+00
'I7.0 1. 0 9' E + 01 ' t . 02 dE + ill n.000E+00 6.689E-01 1 023E+01 1 095E*01' s 17.0 -l.129E+00 ( .6 9 7 E +'J O 0.000F+00 7. 7 86 E + 00 - 1.129t + 00 6. 6 57E + 0 0 17.0 -4 . 91 CE + 00 E.469E+00 0.000E+00 3.559E+00 9.910E+00 S.469E+00 17.0 1.015E+01 1.0?df+01 0.001E+00 6. 6 89E- 01 1.021E+01 1.095E+01 24.5 - 1. 7 4 3 E + C U 3.911E+00 0.000E+00 9.654E+00 -1.743E+CO ?.911E+CC 75.5 4.91CE+00 5.907E+00 0.000E+00 9.963E-11 4.910F+00 5.9070+S0
~ 25.5 1.lSOF+01__?.903E+00 0.000E+00 3. f. 61 F + 0 0 7. 9 0 3E + 00 1 196E + 01 l A-Le %o ' TJ4 %l35 DRP an/88 +- J
l ANALYSIS EF OYSTEP CREEK COATAINVENTi INT PR ES S O F 0.00 20 X Si.~ COGre S PHI S THET/. S SilEAR S1-52 51-53 S2-53 u
, DART 20 ,, _
FACES 2-1. 1. 2. __ 25.5 -1.743E+70 3.011E+00 0.J00E+00 5. 6 54F + 00 - 1. 74 3E + 00 3.911E+00 25.5 4. 91 CF + CC 5.9C7F+0u O.GodE+00 9.953F-01 4.910E+00 5.907F+00
?S,e 5 1.15 6E + 0,1 7.903F+00 0.000E+10 3.661E+JO 7.903E+00 1.156E+01
'ti. 4. 9 9 7E + 0C 1.478E-01 0.000E+GO 4.849Eo00 1.478E-01 4.997E+0C_
34.0 4. 910F + 00 1.218F-01 0.000E+00 4.788E+00 1.219E-01 4.910E+00 34.C 4.024E+00 9. 5 9 3 E- 0 2 0.000E+00 4. 7 2 3,E + 0 0 9. ?P S-C2 4.824F+00 FACES =-1. 1. 2. 90.0 4.4 S 3E + CO - 1. 524E-0? 0.?00Et00 4. 4 59E + 00 - 1. 524 E-02 4.453E+70 90.0 5.167F+00 1.997E-01 0.000F+00 4. 968E + 00 1. 9 0 7E- 01 5.1'IC+00 40.0 5. E L CE+ 00 4.126E-91 0.090E+00 5.467E+00 4.126E-01 5.380E+00 97.3 1.lq7E+01 -2.045C+0C 0.00CE+00 1. 3 7 2E + 01 - 2. 6 4 5F + 0 0 1.1C7E+01 07.3 5.?09c+00 -4.451E+00 0.000F+00 9.660 F + 09 -4. 4 51F + C0 5.209F+00 9 7 ~ 3 - 0. 54 0E-01 -6. 2 5 7E + 0 0 C.000F+00 5.603F+00 -0.257E+00 -6.540E-01 97.3 1.10 7E + 01 -2.645E+00 0.000E400 1.372F+01 -2.645E+00 1.107F+01 07.3 5. 2 09E + 00 -4. 4 51E +0C 0.000E+00 9.660E+00 -4.451E+00 5.209E+00 97.3 -6.540E-01 -6.257E+00 0.000E+00 5. 60 3F + 00 -6. 2 5 7F + CD -6. 540E-01 1G4.6 1.17CE + 01 -5.554F+00 0.000E+00 1.725E+01 -5.554E&O0 1.170E+01 104.6 5. ?i>E + C0 - 7. 521E + 00 0.000E+00 1. 2 81E + 01 -7. 521 E + 00 5.285E+00 1,f. 4 . 6 -1.127E+0C -9.400E+00 0.000E+00 8. 3 62 F + 3 0 - 9. 4 8 a E + 0 0 - 1.12 7E + 0 0_ 104.f 1.170E+cl -5.554E+00 0.0006+C0 1. 7 2 5E + C 1 - 5. 5 54L + CC 1.170c+01 104.6 5. 2 t: 5f + CO -7. 521 F + C 0 0.000E*00 1.2SIE+01 -7.521E+00 5.285E+00 10 4. 6 - 1.12 7F + 00 -9.5Ecr+00 0.000E+00 8.362E+00 -9.489E+00 -1.127E+00 111.9 9.3E9E+C0 -?.260F+00 0.000E+00 1. 712 E + 01 - 7. 2 6 0E + 00 9.959E+0C 111.9 5.432F+ J -S.536F+00 0.000E+00 1.402E+01 -R.566E+00 5.432F+00 111." 1. 0 0$ t + 0 0 - 9.912E + 10 C.C00E+00 1.092E+01 -s.912E+00 1.005E+00 111.9 9.000F+JD 7.200E+00 0.000E+00 1.712E+01 -7.200E+00 9.a5?E+00 111.9 5.4 32E + 0 ' -d.566E+CO 0.000E+07 1.432F+01 -% 566t + 09 5.432E+00 111.1 1.'?5E*00 -0.C12E+00 0.000F+01 1.092F+01 -9.912E+00 1.005E+00 117.1 7. 7 5 EE + C C - 1. 3 9 Cf + 0 0 0.030F+09 1.515E+01 - 7. 34 3E+ 00 7.756E+00 119.1 5. '.71 L + 0 2 -7.754F+00 0.000E+00 1 362F+01 -7.9F'.F+C0 % 671 E + 00 111 1 1. Mn F + C O -0.41aE+JO 0.001E+C9 1.210F+31 A.518E+30 3.583F400 , A - 4 *4 Qw. o _3~)A t . l8k - MM 1/3 tJ'6' _ _
VNVlASIS CJ C A 513 d' D!133 M 3 9NIV inh 3 NI t INI dULSS 03 O*0920 MSI* 303dU S Ml} 3 1H31V S Slp VU SI-92 SI-SE 52-SL
~' aV31 ZL g y 3g y. y+ gm- - - - --
116*1 L* L a Jd+ CJ -L*t6)d+CO 0*0003+00 1*5193+01 -l'E533+00 L*L583+00 116*1 s '9 L 1]+ 30 -L ' 5 593 4 00 0*0003+00 T
- E 42 3 + 01 -L
- 6 59 3 + 00 5*9213+00 I T U'[ E
- 5 J' E 3 + 0 0 -e*3189+00 C*0003+0C 1
- 2103 + 01 -d' 5183+ 00 C*58E3+00
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I()*t 9*99OJ+00 -9'19E3+00 0'0003+00 I*2993+01 -9*19E3+00 ?'9303+00 129'v o*0C83+00 -9*1653+cO 0'0003+00 1*2201+CI -9*I553+0C 9* 0003 +00 t29*9 5*sibd+00 -9*2dLd+00 O*OJOJ+00 ~ 1*l19d+01 -V*22Ld+JO 5*SE5d+00
,_,12 0*9 o '9 5 I3+ 00 -?'I9E3+00 0'0003 +00 l*2993+01 -9*19E3+0C 9' V 613 + 0C ,
129*9 9*003d+vO -9*I633+03 0'0003+03 1*2203+01 -9*1653+G0 9*00834C0 129*9 5
- 5 E S3+ 03 -9
- 22 23 + 00 0'0001+00 1*T19d+01 -0*22L3^00 S'9E53+00 lCL*L 9*2E5j+00 -V*0953+CU 0*0007+00 1*0EC3+CI -9*0953+00 4*2E63+CO lts't o ' 9 9T3 + c O - T e o L 2. + 0 0 0'000d+00 l ' CET3 + 01 -E'9?ls+00 l i' M 5 JF0~
IEE'L 9 * ) 5 3 3'+ 0 0 -E'99o3+00 C
- 0003 +00 I*0E23+CI - E' 99b3 + 00 9*9603+CC i t i' L 9 ' uh 0jt oG -9
- 09 53 + 00 0'0003+00 1*0E03+UI -**095d+00 9*dt03+OU LEE'l 9*9953+00 -E'89Ld+CJ O*C003+00 1*0E13+CI -E*09L3+00 9'9953+03 lE6*1 9* 99 63 + L C -L
- 996 3 +0 0'COC3+00 I*Gt23+Ol -E'996J+00 4*9963+03
~f91*0 9'v613+Ce -l'5Lc3+00 O*0003+00 8*2913+00 -l'5L03+00 9*9613*00 191*D 9*5093+0L -I*CE21+00 O'c003+00 S*E163+00 -I*EE2d+00 9*6893+00 L11'L L ' c 3 dJ
- ua -l
- 069J + 00 C*0063+00 8*649d+00 -l*0693+00 /*482d+00 T91*C )*7653+CO -I*9953+0C 0'0003+00 5*2993+00 -I'5903+0C 9*9653+00 ivI'0 9 ' EJ'9a + u O - I
- E t 2 3 + 0 0 0'0003+00 8*E18d&00 -l*EE23+00 9*6893+00 191*0 L*.7483+00 -l*0653+O3 0'0007+00 0* ELE 1+ 00 -I* 0053+ 00 L*2L83+CG 155*E L* 9 LG3 + 03 T ' OLC3 + 00 0*00C3+0C 9*EE53+00 1*0L03+00 L*9053+00
~ ~ ~~15d*( L
- 99 2G 0 0 l'TD13TCO 0'0C03+00 ?*E913+0C f*E013+00 l*9923*LC IV d *i L*OLS3+00 1*SE13+CO 0'0003+00 9*EVL3+00 1*5E13+0C L*9L83+00 it?'t c 'vv,3+00 I 'JL0J + JC Q*OCU3+GG J*FE9?+00 1*JLC3+OG L*9043+CO 193*E L'9923+00 1*ECI3+09 0*0003+00 "9*t913+CO 1*E013+00 L*9923+UJ lyP'c L
- aL0J+ OL I*sE13+00 0'0003+00 9*E99d+00 1*5E13+00 L'8LE3+00-
] IGS'9 C*E903+)V C*0983+00 0'0003+C0 5*VL23+CC E*88b3+00 6*E903+00 l 162 *9 C* 9C? 3 + OC 9*OG93+00 G*C003+0C 4'i223+00 y*0893+00 S'9093&CC~ l 195*o H*9523+d3 9*2603+00 O*0003+00 9'sLCJ+00
' 4*2sCd+LO '
G'952d+CG lai*, F
- E L :3 + 06 t
- GLE3 + CG 0*0903+00 9*9L13+00 E'06E3+00 8*EL03+00 t s i * , 3'9093+sO ?*obL3+00 O'6003+GO t*E163+.C 9* 06 L3+ OC F'9C93+CC~
ft ~ 3 # )[ M ' 0 = ) 16 V 1lL @~ CNH Y/[/22 l I
ANALYSIS Or OYSTER CPEFK CCNT AINMEN18 ! .N T PRESS OF 0.0620 KSI. C0040 5 Phi S THETA S SHEAR S1- 52 51-53 S2-S3 PART 27 ff _ _ FACES =-1. 1. P. __ 155.r. 8.442E+00 4.280E+00 0.000E+00 4.161F+00 4.280E+00 9.442F+00 162.9 8.192E+00 7.?09E+00 0 . 0 0.0 E + 0 0 9.824E-01 7.209E+00 8.192E+00 162.9 9.1120+00 7.725F+C0 0.000E+00 1.387E+00 7.725E+CC S.112E+00 16?.7 1. 0 0 3E + 01 P.2410'00 0.000E+00 . 1.791E+00 8.241F+00 1.003E+Cl_ PART 78
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FACES =-1. 1. 2. 162.9 S. 216E + 00 7.227E+00 0.000F+00 9.S95E-01 7.227E+00 E.216E+00 16?.9 4.112F+00 7.739E+00 0.000F+0* 1.373F+00 7.739I+00 9.11?E+00 1(2.9 1.00lf'01 8.251E+00 0.000E+00 1. 7 5 7E + 0C 8.251E+Cd 1. C C 1 E + 01 165.3 ' . 6 4 'J E + 0 0 8. 3 50E+ 00 0.000E+00 7.024E-01 7.648C+00 9.350E+06-165.5 9.?21E+30 0.007F+0C 0.000F+00 3.148E-01 8.0076+CC t.221F+00 165.3 1.CSUE401 9.463E+00 0.000E+00 1.33?F+00 9.463E+00 1.CSOE+0T' 165.3 7.645E+CO C.350E+0C 0.000E+00 7.046E-01 _7.645E+00 6. ? 5 00 + 0_0_
. 165.3 1.221F+00 9.507E+00 0.000E+00 3.145F-01 0.907E+C0 9.221E+C0 165.1 1. 0 4 0E + 01 9.4o4F+00 0.000E+00 1.334E+00 9.464E+00 1. 0 0 0 d + 01_
167.7 0.3 00F + 90 0.F'lF+00 0.000E+07 2. 511 E- C 1 8.300F +00 8.551E+00 167.7 9. ? S OF + 60 0.706F+00 0.000E+03 5 7350-01 8.706E+00 9.260t+00 167.7 1.026F+01 8.862E+CD 0.000Ft00 1.398E+0C P.662E+00 1.02tE+01
~
167.7 8.206f+00 n.55GE+00 0.000E+00 2.530F-01 d.29%E+00 6.550E+00~ 167.7 9.274E+00 r.706E+00 0.000E+00 5.729E-01 8.7C6E+00 9.279E+0C 167.7 1.0?cE+01 6.462E+tIU 0.0000+00 1.400E+00 6.662E+00 1.02eE+01 170.1 1.121E+01 E.111E+00 0.000E+00 3.098E+00 8.1 11 E + 0 0 1.121E+01 170.t 9.G65E+00 7.431E+00 0.000E+00 2.133E+00 7.4 31 E + n0 9.565E+00 170.1 7. i21E + "3 f.752E+00 0.000E+03 1.169F+00 o.762E+00 7.921E+00 170.1 1.121E+01 0.110E+00 0.0000+00 3.095E+00 9.110C+00 1.121E + 11 170.1 S.5640+00 7.432E+00 0.000E+C0 2.133E+00 7.432E+00 9.564C+00 179.1 7.07 3E + 0c 6.753E+0C E.000E*00 1.17 0E + CO 6.7ETE+CO 7.923E+00 172.6 ?.120f+a1 ;. 64 CF+ CC 0.000r400 1.156E+01 9.640E+00 2.120E+01 17?.6~ 1.03 E+n1 7.7e4E+00 C.0CCE+00 2.551F+00 1.7e4E+00 1.033t+11 17?.6 -5.3?oF-01 S.729E+00 0.000E+00 6. 4 6 2 E + 3 0 - 5. 3 2 9E- 01 5.129E+00_
^
A-CC Rev. o 7Zq th/BA__ _ DRM 2-/3/23
l A'1/, L Y S I S C F CY S T E r: CREEK CCNT A INMENT ; INT PRESS OF 0.0620 KSI.
~
CC CP.3 S PHI S THETA 5 SHE/.R S1-52 S1-53 52-53
.N 'y PAPT 2 P, FACES =-1. 1. 2. _
172.6 2.120E+01 9.640E+00 0.000E+00 1.156E+01 9.640E+00 2.120E+0! 1/2.6 1.033Et01 7. / d5E+ 0C 0.000E+00 2.549E+]O T./SSE+00 1.033E+01 172.6 - 5.293F-01 5.930E+00 0.000E+00 U.460E+00 -0.243E-01 5.930E+00_ 175.0 3. 6 81E + 01 1. 9 01E + 01 0.000E+09 1.780F+01 1.9 01 E + 01 3.681E+01 175.0 9.203E400 ?.197f+01 0. 0 20E + 00 1.277E+01 3.203E+00 2.1975+01 179.3 - 1.841E+01 2.4930+01 0.030E+00 4. 3 3 3 E+ 01 - 1. 34 tE + 01 ?.413E+01
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