ML20202B001
| ML20202B001 | |
| Person / Time | |
|---|---|
| Site: | North Anna  |
| Issue date: | 11/24/1997 |
| From: | Ohanlon J VIRGINIA POWER (VIRGINIA ELECTRIC & POWER CO.) |
| To: | Paperiello C NRC OFFICE OF NUCLEAR MATERIAL SAFETY & SAFEGUARDS (NMSS) |
| Shared Package | |
| ML20202B006 | List: |
| References | |
| 97-667, TAC-L22113, NUDOCS 9712030035 | |
| Download: ML20202B001 (100) | |
Text
_ - _ ___ _
.t Waimr Ei.scruic ANI) POWER COMI%NY l
l Ricuuos >, VimaiN A 2326 November 24, 1997 Mr. Carl J. Paperiello, Director Serial No.97-667 Office of Nuclear Material Safety and Safeguards NL&OS/MAE R2 U. S. Nuclear Regu!atory Commission Docket No. 72-16 Washington, D. C. 20555 Gentlemen:
VIRGINIAILEGIBIC AND PQWER COMPANY NORTH ANNA INDEPENDENT SPFNT FUEL STORAGE INSTALLATION (ISES1)
RESPONSE TO REQUEST FOR AUDITIONAL_INFORMATION (TAC h'O. L22113)
Virginia Electric and Power Company (Virginia Power) subm'itted an application for the review and approval of a site-specific license for an independent spent fuel storage installation (ISFSI) at North Ar.na Power Station on May 9,1995 (Serial No.95-195).
The NRC provided a Request for Additional Information to Virginia Power on November 4,1997. Attachect is our response to the Request for Additional Information, with the exception of item 5.
The response to item 5 will be forwarded to you in separate correspondence within thirty (30) days.
Pisase contact us if you have any questions or require additional inforrnation.
Very truly yours, James P. O'Hanlon Senior Vice President - Nuclear Attachments: 1) Response to RAI
- 2) Soil-Structure interaction Calculation & Analyses
- 3) Comparison Cases Performed with CLASSI Program Note: Addressee not to receive Attachments 2 & 3.
Commitments made by this letter:
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Section 7.5 of the SAR will be revised.
9712030035 9711E4
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cc: Mr. J. W. Shea (Att.1, 2, 3)
Office of Nuclear Material Safety and Safeguards U. S. Nuclear Regulatory Commission, Mail Stop 0-6-G 22 Washington, D. C. 20555 United States Nuclear hegulatory Commission (Att.1,2,3)
Attention: Document Control Desk Washington, D. C. 20555 Mr. M. J. Morgan (w/o Att.)
NRC Senior Resident inspector North Anna Power Station
e ATTACHMENT 1 Response To A Request For Additionalinformation NRC Ouestion 1:
Background:
In your September 11,1997, response to RAI Item 4-3, you stated:
A generic cask with a weight and dimensions which enveloped the TN 32 cask was modeled, therefore, comparison to the TN-32 TSAR analysis was not necessary.
Request: Please further explain this statement.
Virginia Power Response:
In response to RAI Item 4-3, the above statement was made conceming re-analysis to demonstrate that the casks will not slide or tip-over as a result of the ISFSI design earthquake. The re-analysis utilized a dynamic, soil-structure interact!on analysis to determine the effect of the design earthquake on the casks and concrete storage pad.
A " generic" cask,16 ft. high x 8 ft, diameter, was used for the analysis. Since cask sliding was the major concem of the re-analysis effort, the generic cask approach is considered acceptably bounding and produces more conservative factors of safety for sliding. A comparison with the generic cask modeled and the TN-32 is shown below:
TN 32 - STABILITY ANALYSIS PROPERTY GENERIC CASK TN-32
. TSAR SECTION 2.2.3.2 Weight 230 kips 230.99 228 kips kips Vertical Distance to Center of Gravity, I, 96" 92.09" 92" Base Radial Distance to Center 48" 43.875" 43.875" of Gravity,I, A finite element model was used to perform the dynamic analysis. The casks were modeled as a rigid beam from the top of the concrete pad to the center of gravity of the generic casks and the translational and rotary weights of the casks were lumped at the top of the 96 inch rigid beams. This is more conservative than using the 92 inch vertical distance of the TN-32 cask and will result in slightly higher accelerations for the casks and a higher moment arm for those accelerations.
Page 1 of 7
The differences in weight between the generic cask and the TN 32 cask is negligible.
The factor of safety against sliding is determined as:
FS = R i H where:
R
= Resistance to sliding = (u) x W x (1 - Az) u
= Coefficient of friction = 0.3 W
= Weight of cask on pad Az
= Vertical acceleration of cask at cask center of gravity H
= Horizontal sliding force = (Sx' + Sy')"
Sx,Sy = Horizontal cask forces at cask center of gravity in x,y directions
= W x Al, i = x,y ; Al = horizontal accelerations
- Thus, FS = 0.3(1 - Az) / (Ax' + Ay')"
As can be seen, higher accelerations will result in a lower factor of safety against sliding and therefore, using the higher center of gravity of the generic casks is conservative and envelops the TN-32 cask, it should also be noted that the weight of the cask is not involvad in ttje final calculation for the factor of safety against sliding.
Using the methodology of TSAR Section 2.2.3.2, the g value necessary to tip the cask is calculated below:
M,, = gW!, + (2/3)gWI, and M,,,, = WI, where:
M,,
= Moment necessary to tip the cask M,,,,
= Stoloilizing moment on cask g
= Acceleration value necessary to tip the cask W
= Weight of cask on pad I,
= Vertical distance to cask CG I,
= Radial distance to cask CG Therefore, the g value necessary to tip the cask is found by equating M,, to M,,,:
-(gWI,)+ (2/3)gWI, = WI, g = (1,) / ( I, + 0 V : 1, )
Solving for the TN-32 cask, g = 0.36.
Page 2 of 7
Solving for the generic cask, g = 0.37 which is virtually the same as for the TN 32 cask.
Using the higher center of gravity of the generic casks will resuh in higher cask accelerations and higher overturning moments which will result in a lower factor of safety against overtuming and is therefore conservative.
We therefore conclude that the generic cask used in the analysis is more conservative than using the TN 32 cask for the critical sliding analysis and is essentially equivalent to the TN-32 cask for overtuming which shows significant margin to the minimum 1.1 safety factor. The lowest factor of safety for overtuming is about 1.6.
NRC Ouestion 2:
Background:
In your September 11,1997, submittal you stated:
For calculating the factor of safety for slicing, a friction coefficient of 0.3 was assumed between the SSCs and the supporting concrete slab.
However, in the TN-32 TSAR sliding analysis, a coefficient of sliding of 0.225 (sic) was used.
Request: P' ease justify using the less conservative value in your September 11,1997, submittal.
Virginia Power Response:
The use of 0.3 as the coefficient of static friction is adequately conservative and consistent with existing industry standards. The TN-32 TSAR value appears to be an overly conservative application of equating static and kinetic values.
The first pt. agraph of the TN-32 TSAR, Section 2.2.1.2.1, states The cask rests in an upright position on a concrete pad. The coefficient of friction between the steel cask and the concrete may be taken as 0.25 for dry concrete. This is based on data in Mark's Handbook which gives a value of 0.29 for steel en sandstone. Steel on concrete would be similar.
The value of 0.25 was used throughout the TSAR for both the coefficient of static friction and for the coefficient of kinetic friction as indicated in TSAR Section 2.2.1.2.2 in which a cask sliding distance of 7.6 inches was determined as a result of tornado missile impact.
The coefficient of static friction is used to calculate the maximum amount of frictional force available to prevent sliding. Once sliding begins, there is lower frictional force available, and the coefficient of kinetic friction should be used. According to the Page 3 of 7
textbook, " Vector Mechanics for Engineers: Statics and Dynamics," by F. P. Beer and E. R. Johnston, Jr., McGraw Hill Book Company,1962, the' coefficient of kinetic friction is approximately 25 per cent smaller than the coefficient of static friction. Thus, using the lower value as done in the TSAR for both the static and kinetic friction values is overly conservative for the condition prior to the initiation of sliding.
In determining the value for the coefficient of static friction for Virginia Power's analysis, several references in addition to Mark's Handbook were evaluated to arrive at an appropriate, conservative value. The following table lists the additional values and references:
Coefficient of Slatic Friction Belprence Metal on Stone: 0.30-0.70 Beer and Johnston, Vector Mechanics for Engineers: Statics and Dynamics, McGraw-Hill Book Co.,1962 Metal on Concrete: 0.30 - 0.40 Walmer, M. E., Manual of Structural Design and Engineering Solutions, Prentic-Hall, Inc.,1972 Concrete to Steel: 0.40 PCI Design Handbook,2nd Edition, Precast Concrete Institute,1978 in addition, Virginia Power's concrete construction specifications require a broom finish for the top surface of the concrete storage pad. This will result in a more coarse texture than a smooth, troweled finish, it is therefore concluded that a coefficient of static friction value of 0.3 is appropriate and conservative for the determination of the factor of safety against cask sliding.
NRC Ouestion 3:
Request:
Please submit the latest soil-structure interaction calculations and analyses which were used for cask sliding and overtuming.
Virginia Power Response:
' contains the soil-structure interaction calculations and analyses transmittal of final results, as well as five (5) separate calculations that were performed.
Copies of the diskettes which are referenced in the calculations are available upon request.
NRC Ouestion 4:
Request: Please submit all comparison cases performed with the CLASSI program for SSI (including acceleration, displacement,_
Page 4 of 7
etc.) by which you verified the personal computer version of the SASSi code.
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t Virginia Power Response: contains the requested information.
The compact disk which is referenced in the calculation is available upon request.
NRC Ouestion 6:
Background:
Table 2.1-2 of the TN-32 TSAR lists design limits for fuel that may be stored in the TN-32 cask. Section 2.1 of the TN-L 32 TSAR states:
Fuel with various combinations of bumup, specific power, enrichment and cooling time can be stored in the TN 32 cask as long as values for decay heat and gamma and neutron sources fal' Phin the design limits specified in Table 2.1-2.
Section 12.3.1, " Functional / Operating Limits..." of the staff SER for the TN 32 states:
"The TN-32 shall be limited to the storage of 32 PWR fuel elements that satisfy the thermal, shielding and radiological design limits on Section 2.1 of the TSAR..."
The proposed TS for the North Anna ISFSI do not list all of the fuel characteristics listed in the above cited sections of the TSAR and the SER. Specifically, specific power, gamma source, and neutron source are not listed in the proposed TS Table 3/4-1.
Request:
Please revise the proposed TS to consider the parameters or justify why they are not necessary to bound the types of fuel that you may choose to load in the TN-32 casks.
Virginia Power Response:
Wei5 the exception of maximum decay heat which cannot be measured, the proposed Technical Specifications for the North Anna ISFSI limit fuel assembly parameters that can be confirmed before cask loading by measurements recoraed in fuel records. The proposed Technical Specifications limit the maximum initial fuel enrichment, maximum fuel bumup, minimum decay time after irradiation, and maximum decay heat per fuel assembly.
The initial U235 enrichment is measured when the fuel assembly is manufactured.
Page 5 of 7
The fuel assembly bumup is determined during irradiation from measured reactor power levels and measured fuel assembly relative power levels based on core flux maps.
The minimem decay time is determined based on the time between the final irradiation date for the fuel assembly and an evaluation date chosen prior to cask loading.
No practical method has been identified to measure either fuel assembly decay heat or fuel temperature during dry storage, which is the cask performance parameter that depends on decay heat. Therefore, under the proposed North Anna ISFSI Technical Specifications, the decay heat for each fuel assembly will be calculated based on its actual irradiation history or with the methodology provided in NRC Regulatory Guide DG-3010.
No practical method has been identified to measure fuel assembly gamma and neutron source terms.
However, average cask external dose rate, which is the cask performance parameter that depends on source term and cask shielding, can and will be measured during cask loading and before transfer to the ISFSI. Proposed Nortn Anna ISFSI Technical Specification 3/4.4 limits the maximum average dose rates (neutron plus gamma) for the TN-32 cask to 129 mrem / hour on the side and 54 mrem / hour on the top of the cask. The external dose rates shown in the TN-32 TSAR were increased by factors of 1.5 on the side and 2.5 on the top in order to provide for uncertainties in source term and shielding analysis and to bound variations in these parameters. These Technical Specification maximum average extemal dose rates were assumed in the analysis of doses to the public from the North Anna ISFSI. It is Virginia Power's position that it is more appropriate to limit measured extemal dose rates in the ISFSI Technical Specifications than to limit calculated source terms which can not be confirmed by measurement.
The gamma and neutron source terma are insensitive to large changes in specific power. For example, Table 2.1.2 of the TN-32 TSAR tists a core average power of 37.5 MW/MTU for the " design" case, versus the current North Anna core average power level of approximately 40 MW/MTU. A sensitivity study increasing the core average specific power from 37.5 to 45 MW/MTU increases the calculated gamma and neutron source terms by 2% and 0.5% respectively. This small increase is well within the uncertainty factors applied to the use of the TN-32 cask at the North Anna ISFSI.
Because of this insensitivity and the fact that cask surface dose rates are already limited by the Technical Specifications, the specific power should not be included in the Technical Specifications.
NRC Ouestion 7:
Background:
Section 7.5 of the SAR does not clearly demonstrate your basis for compliance with 72.104 (a). Section 7.5 of the SAR references Section 5.2.2 of the environmental report (ER). Section Page 6 of 7
5.2.2 of the ER references Section 5.2.1 of the ER which refers back to Section 7.5 of the SAR. None of these sections clearly articu! ate _ the assumptions and calculations used to demonstrate compliance with 72,104.
Request: Provide in a clear and concise fashion the analysis which demonstrates compliance with 72.104 (a).
Clearly list all assumptions.
Virginia Power Response:
Section 7.5 of the SAR will be revised as follows:
The site plan for the North Anna ISFSI and its rcStive location to the North Anna Power Station are provided in Figure 2.1-3. The North Anna site within the boundary is the
. controlled area as defined in 10 CFR 72.
There are 299 permanent residents located within a 2-mile radius of the North Anna site boundary. The nearest permanent resident is located at 2860 feet from the ISFSI.
~
Based on the design basis dose rate versus distance curve for a fully loaded ISFSI (Figure 7.3-5), the maximum annual dose to the nearest resident is 2.57 mrem. Using the conservative assumption that all of the residents within two miles are located at the same distance from the ISFSI as the nearest resident, their maximum annual collective dose from the ISFSI would be:
0.00257 rem / year x 299 persons = 0.77 person-rem / year The maximum annual doss to the nearest permanent resident from the North Anna Power Station has been estimated in Appendix 11C of the North Anna Power Station i
UFSAR as 2.93 mrem due to liquid effluents and 1.93 mrem due to gaseous effluents from both units.
Therefore, the maximum combined radiation contribution to the nearest permanent resident from the operation of the ISFSI (2.57 mrem /yr.) and North Anna Power Station Units 1 and 2 (4.86 mrem /yr.) is 7.43 mrem /yr. This is well below the 25 mrem /yr. limit imposed by 10 CFR 72.104(a).
The North Anna ISFSI has no gaseous or liquid effluents, therefore, these do not contribute to the dose of nearby residents.
Considering the conservatisms in the above calculation and the rapid attenuation of neutron and gamma dose rates with distance, the dose for th's more distant population is negligible.
Page 7 of 7 NRC Ouestion 3 Requested Information e
t Engineering M 4 e h firy e 14..at IN. t hsa t h es At June 13,1997 EQE Project 100031 Correspondence 100031-0-003 Mr. John MacCrimmon VIRGINIA POWER Nuclear Engineering innsbrook Technical Center 5000 Dominion Boulevard Glen Allen, VA 23060 Sub)cct:
Transmittal of Final Resultsfor North Anna Spent Fuel Storage Facility
Dear John:
Attached please find the six Calculation Files documenting the soil structure interaction analysis of the Spent Fuel Storage Facility at North Anna and the verification of the PC version of computer code SASSI. These calculations are:
Calculation 100031-C-01, Development of Soil Profile Calcula.on 100031-C-02, SASSI: Modules POINT and SITE Calculation 100031-C-03 Pad Model and input to Module HOUSE Calculation 100031 C 04, Sliding and Ovenurning Factor of Safety Calculation 100031-C-05, Stress Calculation
. Calculation 100031-C-06, Project Specific Verification of Computer Code l
Super SASSI/PC The analysis was performed for the best estimate soil profile under the pads and for the DDE level defined for soil conditions.
The low strain soil profile is given in Table 2-3 of Calculation C-01 (denominated C-01) und shown in Figures 2-7 and 2-8 of the same Calculation. The strain compatible soil properties are given in Table 4-1 and shown in Figures 4-1,4-2, and 4-3 of C-01.
The North Anna DBE input motion acceleration time histories for soil conditions are shown in Figures 3-1,3 2, and 3-3 of C-01. It is important to note that in those time histories an extreme peak coincides in both horizontal directions at about 3.7 seconds even though the motions are uncorrelated. This will have an impact on the instantaneous 44 9 ntu m m e m s$te3:
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Mr. John MacCrimmon i
Virginia Power Nuclear Engineering May 16.1997 Page 2 of 3 factors of safety calculated at that time. As it will be discussed later, this situation is unrealistic and it is caused by the use of artificial time histories to derme the DBE motion.
For the analysis, a quarter model was used. This model and it< aede and elements numbers are shown in Figures 21 to 2 6 of C-03. The reinforced cuerete slab was modeled by plate elements and the casks by rigid beams with their masses (translational and rotational) lumped at the center of gravity of them.
First, the global responses at the casks (absolute accelerations) were calculated in order to detennine the factor of safety for sliding and overturning and the global forces and moments at the base of the casks. The base shear forces and axial forces and the inverse of the sliding and overturning factors of safety for the seven casks in the quarter model are shown in Figures 3-1 to 3 35 of C-04. These results consider the three components of the input applied simultaneously. For calculating the factor of safety for sliding, a friction coefficient of 0.3 was assumed between the casks arid the supporting concrete slab.
Figures 3-1 to 3 35 of C-04 show, for each of the seven casks (denominated nodes 231 to 237) included in the quarter model, the casks base shear forces in the longitudinal direction (X), the casks base shear forces in the transverse direction (Y), the casks vertical forces (downward), the factor of safety for sliding (the inverse was plotted), and the factor of safety for overturning (the inverse was plotted). From these figures, it can be seen that at about 3.7 seconds the factor of safety for sliding is slightly greater than 1 and for overturning about 1.6. However, as mentioned earlier, the instantaneous value at 3.7 seconds is unrealistic due to the coincidence of two extreme peaks in the horizontal inpta motions. If the values at 3.7 seconds are disregarded, the minimum factor of safety for sliding during the total duration of the earthquake is about 1.25 and about 2.0 for overtuming.
Funhermore, and since the analysis confirmed that the responses due to the 3 components of the input are uncoupled (see Tables 3-1, 3-2, and 3 3 of C-04 for maximum accelerations due to each input direction), a good estimate of the factors of safety could be obtained by calculating them using the maximum responses for each direction and then combining them using the 100%,40%,40% combination rule recommended in the ASCE Standard 4-86, Seismic Analysis of Safety-Related Nuclear Structures and Commentary on Standard for Seismic Analysis of Safety Related Nuclear Structures.
This combination of the maximum values will reduce the impact of the unrealistic and overly conservative situation of extreme peaks occurring at the same instant in the two horizontal directions. Using 100% of the maximum response due to the X input,40% of the maximum response due to the Y input, and 40% of the maximum response due to the Z input, the factor of safety for sliding results to be 1.17. The same value results if 40%
PMikt224Mpa\\Natta3. Doc 4
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Mr. John MacCrimmon V.rginia Power Nuclear Engineering May 16,1997 Page 3 of 3 of X and 100% of Y are used. For the case when 40% of the horizontal cases and 100%
of tiie vertical case are used, then the sliding factor of safety is 2.04.
In a second analysis, the plate moments (per unit length) and stresses and the beam moments and forces were calculated in the plates and beams used to model the slab and the casks, respectively. Figures 2-5 and 2-6 of C-03 indicate the numbers of the beam and plate elements used to model the casks and the concrete slab, it should be noted that the numbers of those two type of elements increase along axis X. Figure 2-1 and 2-2 of C-05 shows the moment and force definition for the plate and beam elements.
Table 3-1 of C-05 gives a list of the seismic maximum moments and forces at the beams representing the casks and the plate elements used to model the concrete slab. The seismic maximum moments and forces at each element and for each input direction are given in this table. Also this table shows the tom en:.ximum values calculated as the SRSS of the values of the three input directions. It sn.ald be noted that the moments and forces at the slab are small and it is expected that they will not control the design of the slab.
I thank you again for the opportunity to participate in this project. Please call me at (415) 989 2000 if you have any questions or comments regarding these results or require more assistance.
Sincerely, mm Alejandro P. Asfura, Ph.D., P.E.
Vice President EQE International P \\ Mkt 224\\Apa\\Natra3. Doc
s Mr. John MacCrimmon Virginia Power Nuclear Engineering May 16,1997 Attachment A:
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JOB NO.100031.01
, JOB North Anna SSI Analysis ofISFSI Pad BY M A-DATE D4)
D DATE N/ k'l7 CALC. NO. 100031C01RQ, SUBJECT Development of Soit Profile CHK'D i
Table 2-3 BEST ESTIMATE SOIL PP.0 FILE FOR ISFSI PAD ANALYSIS LOW STRAIN Soll PROPERTIES S Wave P Wave Unit Layer Elevations Thickness Velocity Velocity Weight Poisson's Number (ft)
(ft)
(fps)
(fps)
(kcf)
Ratio 1
310-305 5.0 887 1761 0.110 0.33 2
305-300 5.0 887 1761 0.110 0.33 3
300 295 5.0 887 1761 0.110 0.33 4
295 290 5.0 887 1761 0.110 0.33 5
200"8 285 5.0 P87 5000")
0.110 0.484"'
6 285 280 5.0 964 5000"'
O.110 0.481"'
7 280 275 5.0 964 5000")
0.110 0.481"'
8 275 270 5.0 964 5000")
0.110 0.481")
9 270-265 5.0 1280 5000")
0.130 )
0.465"'
9 10 265-260 5.0 1595 5000")
0.130 )
0.443")
9 11 260 255 5.0 1595 5000")
0.130 )
0,443"'
9 12 255 Rock Rock Rock Halfspace Notes.
(1) Water Table elevation (2) P Wave Velocity in water (3) Assumed value for harder soil (4) Adjusted value for consistency with VpNs ratio t
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JOB NO.10003101 JOB North Anna SSI Analysis ofISFSI Pad BY MS DATE D DATE M 2 M CALC.NO. 100031C01R0 SUBJECT.,Devetooment of Soil Profile CHK'O l
i TABLE 41 STRAIN COMPATIBLE SOIL r3ROPERTIES S Wave P Wave Unit Laya Elevations Thickness Velocity Velocity Weight Pol: son' Damping Number (ft)
(ft)
(fps)
(fps)
(kcf) s Ratio Ratio 1
310 305 5.0 859.73 1706.77 0.110 0.33 0.020 2
305 300 5.0 824.45 1636.73 0.110 0.33 0.036 3
300 295 5.0 787.21 1562.80 0.110 0.33 0.048 4
295 290 5.0 753.59 1496.06 0.110 0.33 0.058 5
290'" 285 5.0 724.67 5000")
0.110 0.489)
0.069
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6 285 280 5.0 787.21 5000
O.110 0.487)
0.069 7
280-275 5.0 767.82 5000 )
0.110 0.488')
0.075 43 4
8 275-270 5.0 752.03 5000")
0.110 0.488)
0.080 9
270 265 5.0 1116.31 5000
O.130
O.474
O.052 4
10-265 260 5.0 1450.31 -
5000)
0.130)
0.454 'i 0.043 4
11 260-255 5.0 1440.72 5000)
0.130'3' O.455'*
O.045 12 255 Rock Rock Rock Hallspace J
Notes:
(1) Water Table elevation g2) P Wa e Velocity in water (3) Assumed valua for harder soil (4) Adjusted value for consistency with Vp/Vs ratio Le HORKWEPCOCALCSC-01. DOC
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Mk DATE'h W 7-JOB NO 100031.01 JOB North Anna SSI Analysis of ISFSI Pad BY CHK'D M - DATE kh CALC. NO.100031C04RO SUBJECT Slidina and overtumina Factor of Safety Table 3-1 Input X Direction: Maxirnum Absolute Acceleration (g's)
N.P.
X AT TIME Y
AT TIME Z
AT TIME 198 0.2155 6.6400 0.0001 10.0300 0.0022.
9.3800 203 0.2152 6.6400 0.0003 9.7400 0.0044 9.5500 208 0.2145 6.6400 0.0005 5.9100 0.0047 5.8300 213 0.2137 6.6400 0.0006 10.3400 0.0057 5.8200 l
218 0.2121 6.6400 0.0005 6.6600 0.0067 5.9500 223 0.2095 3.7100 0.0010 6.6600 0.0070 6.2700 228 0.2093 3.7100 0.0018 5.7900 0.0243 5.7300 231 0.2276 6.6400 0.0009 10.0300 0.0022 9.3800 0.0044 9.5500 232 0.2285 9.1000 0.0021 9.7400 233 0.2302 9.1000 0.0039 5.9100 0.0047 5.8300 234 0.2283 9.1000 0.0035 5.9000 0.0057 5.8200 235 0.2259 6.6400 0.0034 6.1500 0.0067 5.9500 236 0.2178 9.'1000 0.0091 5.8700 0.0070 6.2700
.237 0.2411 9.1000 0.0142 5.7900 0.0244 5.7300 C \\WORcVEPCO\\CALCSiC 04 DOC
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SHEET No.
JOB NO.10003101 JOB North Anna S31 Analysis of ISFSI Pad B"
Nb DATE UT'7 CALC. NO 100031C04RO SUBJECT Slidina and Overturnina Factor of Safgiy.__CHK'D @
DATEklM Table 3-1(cont.)Maumum Absolute Angular Accelerations (Rads /Sec/Sec/g)
N.P.
XX AT TIME YY AT TIME ZZ
' AT TIME 198 0.0001 10.0300 0.0031 5.7100 0.0000 5.7200 203 0.0002 9.26G0 0.0029 5.7100 0.0000 5.7200 208 0.0004 5.9100 0.0030 5.7100 0.0000 5.7200 213 0.0004 5.9000 0.0031 5.7100 0.0000 5.7200 216 0.0004 6.1500 0.0028 5.7100 0.0000 5.7200 223 0.0010 5.8700 0.0026 5.7100 0.0000 5.7200 228 0.0015 5.7900 0.0056 5.7200 0.0000 5.7200
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231 0.0001 10.0300 0.0035 5.7100 0.0000 5.7200 232 0.0002 9.2600 0.0033 5.7100 0.0000 5.7200 233 0.0004 5.9100 0.0034 5.7100 0.0000 5.7200 234 0.0004 5.9000 0.0035 5.7100 0.0000 5.7200 235 0.0004 6.1500 0.0032 5.7100 0.0000 5.7200 236 0.0010 5.8700 0.0030 5.7100 0.0000 5.7200 237
.0.0016 5.7900 0.0060 5.7200 0.0000 5.7200 J
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NMO JOB NO.100031.01 JOB North Anna SSt Analysis of ISFSI Pad BY A"f 4 DATE I CALC. NO.100031C04R0 SUBJECT Slidina and Overtumino Factor of Safety CHKD N DATEh@
Table 3-2. Input Y Direction. Maximum Absolute Acceleration (g's)
N.P.
X AT TIME Y
AT TIME '
Z AT TIME 198 0.0005 8.0900 0.1960 3.7100 0.0366 14.2600 203
- 0.0014 8.0800 0.1961 3.7100 0.0372 14.2600 208 0.0018 9.2400 0.1960 3.7100 0.0381 14.2600 213 0.0024 9.2400 0.1961 3.7100 0.0388 7.5100 218 0.0029 9.2300 0.1954 3.7100 0.0390 7.5100 223 0.0040 7.9400 0.1879
'il100 0.0373 7.5000 228 0,0047 9.0900 0.1884 3.7100 0.0283 7.5000 1
231 0.0015 8.2500 0.2238 10.2200 0.0367 14.2600 232 0.0032 8.2500 0.2246 4.3500 0.0373 14.2600 233 0.0031 5.2000 0.2278 4.3500 0.0381 14.2600 3
234 0.0038 9.2400 0.2309 4.3500 0.0389 7.5100 235 0.0065 8.0800 0.2328 4.3500 0.0390 7.5100 236 0.0106 8.0700 0.2282 4.3400 0.0374 7.5000-5 t
237 0.0153 8.0400 0.2240 4.3400 0.0284 7.5000 b
a C \\WORKWEPCONCALCS\\C-04 DOC
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SHEET NO. ID 6/4@
JOB NO.1QQ91Lp1 JOB North Anna SSI Analysis of ISFSI Pad BY M 4 DATE N
DATdbl2N1 CALC. t10.100031C04R0 SUBJECT Slidino and Overtumino Factor of Safety CHKD Table 3-2(cont.) Maximum Absolute Angular Acceleratios(Rads /Sec/Sec/g)
N.P.
XX AT TIME YY AT TIME ZZ AT TIME 198
'0.0069 14.2000 0.0001 8.2500 0.0001 4.4400 203 0.0070 14.2000 0.0003 8.2900 0.0002 4.4400 208 0.0072 14.2000 0.0003 4.9800 0.0003 8.0600 213 0.0073 14.2000 0.0003 7.6500 0.0003 9.2400 218 0.0070 14.2000 0.0006 7.6400 0.0004 4.6100 l
223 0.0067 7.4500 0.0010 7.5800 0.0006 5.2700 228 0.0061 7.4400 0.0016 7.5600 0.0007 14.2100 231 0.0074 14.2000 0.0001 8 2500 0.0001 4.4400 3
232 0.0075 14.2000 0.0003 8.2900 0.0002 4.4400 233 0.0076 14.2000 0.0003 4.9800 0.0003 8.0800 234 0.0077 14.2000 0.0004 7.6500 0.0003 9.2400 235 0.0075 14.2000 0.0007 7.6400 0.0004 4.6100 236 0.0071 7.4500 0.0011 8.0700 0.0006 5.2700 237 0.0065 7.4400 0.0017 7.5600 0.0007 14.2100 C \\WORKWEPCO\\CALCSC04 DOC
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o lY f OE WTERNATONAL ll SHEET NO.'
- N N4 DATE JOB NO.100091.01 -
JOB North Anna SSI Analysis of ISFSI Pad BY CALC. NO.100031004R0 SUBJECT SWino and Overturnina Factor of Safety CHK'D' N DATEkillh Table 3-3. Input Z Direction. Maximum Absolute Acceleration (g's)-
N.P.
X AT TIME Y
AT TIME Z
AT TIME 198 0.0006 3.7300 0.0033 7.9900 0.1335 7.2500 203 0.0019 5.7200 0.0032 7.9900 0.1333 7.2500 208 0.0030 5.7200 0.0031 7.9900 0.1315 7.2500 213 0.0036 5.7200 0.0031 5.6800 0.1295 7.2500 218 0.0037 5.7200 0.0032 5.7400 0.1294 7.2500 223 0.0039 5.9400 0.0034 5.7400 0.1304 7.2500 228 0.0058 5.7300 0.0027 1.9800 0.1287 7.2500 231 0.0024 8.4500 0.0263 7.9900
.0.1336 7.2500 232 0.0058 3.7900 0.0255 7.9900 0.1334 7.2500 233 0.0062 3.7800 0.0244 5.6800 0.1316 7.2500
'234-0.0066 5.7600 0.0243-5.6800 0.1295 7.2500 235 0.0064 8.2100 0.0253 5.7400 0.1294 7.2500 236 0,0087 5.8900 0.0268 5.7400 0.1304 7.2500 237 0.0221 5,6800
.0.0205 1.9800 0.1288 7.2500 C uv0RKWEPCO;CALCS\\C-04 DOC
IG1 noe mamica.
i_ E SHEET NO. b.
JOB No.100031.01 JOB North Anna SSI Analvsis of ISFSI Pad BY M-DATE MW7:
C ALC. NO. 100031C04RO SUBJECT.Sidino and Overturnina Factor of Safety CHKD N DATENIND Table 3-3 (cont.) Maximum Absolute Angular Accelerations (Rads /Sec/Sec/g)
N.P.
XX AT TIME YY AT TIME ZZ.
'AT TIME.
198 0.0028 7.9900 0.0002-6.1000 0.0000 8.5100 203 0.0027 7.9900 0.0005 3.7900 0.0000 8.4500 208-0.0026 5.6800 0.0006 3.7800 0.0000 2.1000 213 0.0026 5.6800 0.0005 8.1200 0.0000 8.3400 218 0.0027 5.7400 0.0006 8.1600 0.0000 2.3500 223 0.0029 5.7400 0.0009 8.1300 0.0000 2.0600 l
228 0.0022 5.6800 0.0021 5.6800 0.0000 5.7400 231 0.0029 7.9900 0.0002 6.0400 0.0000 8.5100 232 0.0028 7.9900 0.0005 3.7900 0.0000 8.4500 233 0.0027 5.6800 0.0006 3.7800 0.0000 2.1000
-234 0.0027 5.6800 0.0006 8.1200 0.0000 8.3400 235 0.0028 5.7400 0.0007 8.1600 0.0000 2.3500 236 0.0030 5.7400 0.0009 8.1300 0.0000 2.0600
-237 0.0023 1.9800 0.0022 5.6800 0.0000 5.7400 C \\WORKWEPCO\\CALCSTC-04 DOC
EGI E!E INTERNATIONAL SHEET NO. 7 V/ W JN NO.10003101' JOB North Anna SS! Anaksis ofISFSI Pad BY M
DATE CHK'D D DATENIM CALC. NO. 100031C05RO SUBJECT.S. tress Calculation Table 34. Maximum Forces and Moments in Plates and Beams
. Input X Dir, input Y Dir, Input Z Dir.
SRSS Plate NO= 1 0
0 0
0 S XX= (ksf) 2.29E 02 1.48E-01 4.65E-01 0.48849278 S Wa (ksf) 8.67E-03 1.05E-01
-3.55E-01 0.37060943 S XY= (kst) 6.12E-02 1.81E-01 6.16E-03 0.19155745 M XX= (kip-ft/ft) 2.30E+00 3.91E-01 5.73E-01 2.39843448 M W= (kip-ft/ft) 3.75E-01 2.57E+00 1.32E+00 2.91736046 M XY= (kip ft/ft) 5.65E-01 5.99E-01 3.06E-02 0.82370582 Plate NO= 2 0
0 0
0 S XX=
8.10E-02 1.49E-01 4.53E-01 0.48335907 S YY=
4.67E-02
-2.32E 01
-4.96E-01 0.54929523 S XY=
1.62E-01
-4.29E 01 5.54E-02 0.46173191 M XX=
2.31E+00 1.62E+00 1.10E+00 3.02782893 M W=
3.92E-01 4.68E+00 1.80E+00 5.0250971 M XY=
-5.63E-01 2.56E+00
-4.44E-01 2.6565486 Plate NO= 3 0
0 0
0 S XX= -
4.97E-01 1.52E-01 4.45E-01 0.68410221 S W=
-3.52E-02
-2.29E-01
-4.93E-01 0.54462269 S K/=
-1.55E-01 3.37E-01
-5.32E-02 0.37475116 M XX=
2.27E+00
-1.63 E+ 00 1.08E+00 2.99357395 M W=
4.07E-01
-4.68E+00 1.80E+00 5.02792794 M XY=
5.73E-01
-2.56E+00 4.48E-01 2.66512193 Plate NO= 4 0
0 0
0 S XX=
4.61E-01
-1.47E-01 4.45E-01 0.65762024 SW=
2.94E-02 1.05E-01
-3.47E 01 0.36392982 S XY=
5.94E-02 '
2.04E-01 7.28E-03 0.2121084 M XX=
2.29E+00 3.88E 01
-5.61 E-01 2.38953069 M W=
4.05E-01
-2.58E+00 1.32E+00 2.92223904 M XY=
5.60E-01 6.03E-01
-4.15E 02 0.82418516 Plate NO= 5 0
0 0
0 S XX=
4.81E-01 1.50E-01 4.36E-01 0.66610471 S W=
2.62E-02 1.00E-01
-3.44 E-01 0.35886821 S XY=
6.39E-02
-4.25E-01
-5.04E-03 0.42990533 M XX=
2.33E+00 3.95E-01 5.65E-01 2.42597775' M W=
3.96E-01
-2.59E+00 1.30E+00 2.92531482 M XY=
5.59E 5.96E-01 3.63E-02 0.81807121 Plate NO= 6-0-
0 0
0 S XX=
4.71E-01
-1.64E-01 4.23E-01 0.65360175 S W=
8.47E-02
-2.34E 01.
4.78E 01 0.53911535 S XY=
1.70E-01
-6.27E-01 5.62E-02 0.65209351 M XX=
2.36E+00
-1.63E+00 1.09E+00 3.06289063-M W=
-4.27E-01
-4.69E+00 1.77E+00 5.02657865.
M XY=
-5.56E-01 2.56E+00
-4.35E-01 2.65748551 C.WYORKWEPCOCALCSC-OkDOC
bOE ECE WTECNAT:DNAL gn.
SHEET NO. b.
OW JOB NO.10003101 JOB North Anna SSI Analysis of ISFSI Pad BY M A-DATE N DATE5 N 7 CALC. NO.100031005R0 SUBJECT Stress Calculation CHKD Plate NO. 7
. S XX=
9.60E 01 1.55E-01 3.98E 01 1.05100286 S YY=
5.43E 02 2.25E-01 4.72E 01, 0.52538499 S XY=
1.52E 01 3.52E 01 5.07E 02 0.38663467 M XX=
2.24E+00 1.63E+00 1.02E+00 2.95355328 M YY=
4.53E 01 4.69E+00 1.78E+Lc 5.03167063 M XY=
5.84E-01 2.56E+00 4.50E 01
. 2.6679265d Plate NO= 8 0
0 0
0 S XX=
9.27E 01 1.61 E-01 3.89E-01 1.01782048 S YY=
4.11E 02 9.77E-02 3.26E 01 0.34318866 S XY=
5.82E 02 3.46E 01 8.23f.-03 0.35047103 M XX=
2.28E+00 3.88E-01 6.iuE;01 2.38803225 M YY=
4.34E-01 2.58E+00 1.31 E+00 2.92715962 M XY=
5.75E 01 6.09E 01
-4.37E 02 0.83912388 Plate N O = 9 0
0 0
0 S XX=
9.50E 01 1.66E 01 3.7c5-01 1.03470282 S YY.
3.42E 02 8.96E 02 3.23E-01 0.3372217 S XY=
6.76E 02 5.89E-01 5.46E-03 0.59329249 M XX=
2.33E+00 4.01 E-01 5.77E-01 2.42967884 M YY=
-4.00E 01 2.60E+00 1.29E+00 2.92548203 M XY=
5.75E 01 5.94E 01 4.11E 02 0.82773771 Plate NO= 10 0
0 0
0 S XX=
9.40E 01 1.81E 01 3.56E 01 1.02122353 S YY=
1.12E 01 2.38E 01 4.59E-01 0.52876563 S XY=
1.78E 01 7.59E 01 5.52E-02 0.7816273 M XX=
2.37E+00
-1.63E+00 1.06E+00 3.06463848 M YY=
-4.22E 01 4.73E+00 1.74E+00 5.05600963 M XY=
5.63E 01 2.58E+00 4.31 E-01 2.67954316 Plate NO= 11 0
0 0
0 S XX=
1.44E+00 1.75E 01 3.47E 01 1.48667113 S YY=
6.41E 02 2.22E 01 4.56E 01 0.51155799 S XY=
1.48E 01
-3.56E 01 5.03E 02 0.38884794 M XX= -
L28E+00 1.65E+00 9.96E 01 2.98556201 M YY=
4.66E 01 4.73E+00 1.75E+00 5.06673067 M XY=
5.90E 01 2.58E+00 4.46E 01 2.6868347 Plate N O n 12 0
0 0
0 0XX=
1.39E+00 1.79E 01 3.39E-01 1.44283452 S YY=
4.36E-02 8.67E 02 3.11E 01 -
0.32608527 S XY=
5.65E-02 3.78E 01 8.32E-03 0.3825908 M XX=
2.38E+00 3.92E 01
-6.49E 01 2.49974211 M YY=
4.49E 01 2.62E+00 1.30E+00 2.95545128 M XY=
5.77E-01 6.20E 01 3.81E 02 0.84789959 0
0 0
0 C \\WORKWEPCOiCALCSiC-os DOC L
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M Eof WTERNATONAL f.4..p SHEET NO.
9
^~
OM DATE M
JOB NO 100031.01 JOB North Anna SSI Analysis of ISFSI Pad BY CALC. NO.100031C05R0 SUBJECT Stress Calculation CHK'D N DATEbf/2/T7 Plate NO= 13 S XX=
1.40E+00 1.81E 01 3.32E 01 1.45410817 S YY=
2.89E 02 7.85E 02 3.10E 01 0.32098161 S XY=
7.11 E-02 5.96E-01
. 5.78E-03 0.60064977 M XX=
2.27E+00 4.04E 01 5.98E 01 2.37707509 M YY=
3.73E 01 2.66E+00 1.29E+00 2.97663735 M XY=
5.77E-01 6.01E 01
-3.75E 02 0.83356865 Plate NO 14 0
0 0
0 S XX=
1.41 E+00
-2,25E-01 3.26E-01 1.46069395 S YY=
1.38E-01 2.43E 01 4.59E 01 0.53730794 S XY=
1.82E 01 7.52E-01 5.31E 02 0.77521249 M XX=
2.3; % 00 1.67E+00 1.04E+00 3.05038063 M YY=
3.83E 01 4.84E+00 1.75E+00 5.15963573 M XY=
5.63E 01 2.64E+00 4.38E-01 2.73090592 Plate NO= 15 0
0 0
0 S XX=
1.93E+00 1.94E-01 3.10E 01 1.96034208 S YY=
7.89E 02 2.28E 01 4.62E 01 0.52133392 S XY=
1.43E 01 2.85E 01 5.31E 02 0.32334539 M XX=
2,31 E+00 1.68E+00 1.06E+00 3.04823441 M YY=
4.83E-01 4.85E+00 1.75E+00 5.17774234 M XY=
5.83E 01 2.65E+00 4.40E-01 2.74870952 0
0 Plato NO= 16 0
0
+
S XX=
1.89E+00 2.08E 01 3.01E 01 1.92019051 S YY.
-4.30E 02 7.17E 02 3.19E 01 0.32976052 S XY=
5.48E 02 0.57E 01 7.20E 03 0.26326732 M XX=
2.40E+00 4.04E 01 6.21 E-01 2.51168462 M YY=
-4.62E 01
-2.68E+00 1.30E+00 3.0156342 M XY=
5.62E-01 6.23E 01 3.22E 02 0.83938714 l
Plate NO= 17 0
0 0
0 S XX=
1.90E+00 -
2.26E 01 2.89E 31 1.93612607 S YY=
2..;E 02 6.25E 02 3.26E 01 0.33315691 S XY=
7.35E 02
-4.55E 01 5.75E 03 0.46094058 M XX=
2.21 E+00 4.03E 01 5.72E-01 2.32194832 M YY=
3.79E-01
-2.71 E+00 1.31 E+00 3.03605709 M XY=
5.64E-01 6.25E-01
-4.39E 02 0.84294041 Plate NO= 18 0
0 0
0 S XX=
1.89E+00 2.76Ce 01 2.77E-01 1.93201429 S YY=
1.61E 01
-2.50E-01 4.82E 01 0.56658947-S XY=
1.86E 01 5.90E-01 5.38E 02 0.62089338 M XX=
2.25E+00 1.72E+00 1.11 E+00 3.04256619 M YY=
4.05E 01
-4.94 E+00 1.79E+00 5.26886259 M XY=
5.48E-01 2.68E+00
-4.46E 01 2.77531444 0
0 0
0 C \\WORKWEPCO\\CALCS'C-05 00C 4
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EQE INTEQNATsONAL -
SHEET NO. M JOB NO.10003101 JOB North Anna SSI Analysis of ISFSI Prd
'BY MM DATE ON!
CHKD - DJD DATE $287 O ALC. NO.100031C05RO SUBJECT Stress Calculation Plate NO= 10 S XX=
2.41 E+00 2.46E 01 2.61E 01 2.43754062 S W=
-1.16E 01 -
2.46E 01 4.90E 01 0.5600295 S XY=
1.34E 01 3.84E 01 5.45E 02 0.41047884 1.69 +00 -
1.19E+00 3.05135281 E
^
M XX=
2.24E+00 M YY=
.69E 01 4.94E+00 1.79E+00 5.27540683 M XY=
5.73E 01 2.71 E+00 4.41 E+1 2.80003356 Plate NO= 20 0
0 0
0 S XX=
2.37E+00 2.58E 01 2.73E 01 2.39767299 S YY=
5.48E 02 4.82E 02 3.50E 01 0.35772019 j
S XY=
5.36E 02 3.31E 01 7.73E 03 0.3352557 M XX=
1.31E+00 4.2BE-01 534E 01 2.41010622 M YY=
-4.92E 01 2.72E+00 1.31 E+00 3.05745378 M XY=
5.59E 01
-6.03E-01
-4.06E-02 0.82310217 Plate NO= 21 0
0 0
0 S XX=
2.38E+00 2,61E 01 2.71E 01 2.40601535 S YY=
4.74E 02 4.42E 02 3.53E 01 0.35900003 S XY=
7.64E 02 2.94E 01
-5.49 0E3 0.30380664 M XX=
2.30E+00 4.02E 01 5.57E 01 2.40234622 i
M YY=
5.20E 01 2.71 E+00 1.29E+00 3.04425361 M XY=
5.63E 01 6.68E 01 4.27E-02 0.87414249 Plate NO= 22 0
0 0
0 S XX=
2.37E+00 2.56E 01 2.53E-01 2.39424004 S YY=
2.29E 01 2.60E 01 5.05E 01 0.6121365 S XY=
1.92E 01 3.20E 01 5.84E 02 0.37765367 M XX=
2.50E+00 1.72E+00 1.29E+00 3.29494492 M YY=
6.20E 01
-4.91 E+00 1.76E+00 5.25091926 M XY=
5.64E-C1 2.70E+00 4.50E 01 2.79371387 Plate NO= 23 0
0 0
0-S XX=
2.84E+00
-2.95E 01
-2.49E 01 2.87004099 S YY=
1.75E 01 2.76E-01 5.03E-01 0.59351455
' S XY=
1.28E 01 6.17E 01
-5.22E-02 0.63253218 M XX=
2.12E+00 1.67E+00 1.29E+00 2.99191928
. M YY=
5.55E 01
-4.89E+00 1.76E+00 5.22594174 M XY=
5.35E-01 2.67E+00 4.21E 01 -
2.75722011 Plate NO= 24 0
0 0
0 S XX=
2.80E+00 2.39E-01
-2.62E 01 2.8243605.
S YY=
1.01E 01 2.34E 02 3.43E 01 0.35816087 S XY=
5.55E 02
-6.17E-01 1.07E-02 0.61958656 M XX=
1.86E+00 4.70E 01 3.87E 01 1.9580422 M YY=
3.82E 01
-2.64 E+00 1.17E+00 2.91166634 M XY=
-6.64E 5.51 E-01 1.31 E-01 0.87237568 0
0 0
0 C \\WORKWEPCO\\CALCSfeOS DOC y
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(N E0E MEMNATIONAL
+
! SE SHEET NO. //
MM DATE N
JOB NO.100C31.01 JOB North Anna SSI Analysis of ISFSI Pad
-BY C.4C. NO.1DOO31C05R0 SUBJECT Stress calculation
_CHK'D N DATE Y !
Plate NO= 25 S XX=
2.85E+00 2.14E-01 2.42E 01 2.86327376 S YY=
9.56E 02 -
2.86E-02 3.29E 01 0.34331331 S XY=
- 3.52E 02.
-5 48E-01 L 7.39E 03 0.55423928 M XX=.
3.15E+00 5.18E 01 2.94E-01 3.204841-M YY=
7.00E 01 2.56E+00 9.94E 2.83589494.
M XY=
6.40E 01 8.25E-01 7.76E 02 1.04701226 Plate NO= 26
'O O
O
-0 S XX=
2.89E+00 1.29E 01 1.96E-01 2.90247083 EYY=
2.15E 01 2.73E 01 -
4.27E 01
.0.55003071 S XY=
2.08E 01 5.03E-01 6.02E-02 0.54783263 M XX=
2.74E+00 1.59E+00 1.45E+00 3.4789303 M YY=
8.97E 01 -
-4.64E+00 1.34E+00 4.915498S8 M XY=
7.97E 01 2.95E+00
-3.18E 01 '
3.07594888 Plate NC= 27 0
0 0
.0
- S XX=
3.49E+00 2.72E 01 1.38E 01 3.50730303 S YY=
1.79E-01 3.04E-01 3.81E 01
-0.51904718 S XY=
1.53E 01 1.26E+00 3.31E 02 1.26470041 M XX=
2.74E+00 1.65E+00 1.13E+00 3.39381261 M YY=
-5.50E 01 4.54E+00 1.35E+00 d.7722809 M XY=
6.60E 01
-2.28E+00 3.71G 01 2.40508789 Plate NO= 28 0
0 0
0 S XX=
3.51 E+00 '
1.34E 01 1.35E 01 3.51i12819
- S YY=
-1.75E 01 -
2.97E 02 2.16E 01 0.27937632 S XY=
5.23E 02 1.29E+00
-4.01 E-03 1.29306393 M XX= -
3.47E+00 3.12E 01
-4.67E-01 3.51510658 M YY=
-8.59E 01 2.02E+00 8.65E 01 2.35595684-M XY=
2.19E 01 5.75E-01 1.25E 01 0.62821888 Plate NO= 29 0
0 0
0 S XX=
3.56E+00 1.29E 01 1.332 01 3.56084237 S YY=
1.88E 01 7.03E 02
- 1.61E 01 0.25687636 S XY=
4.18E 02 1.15E+00 5.63E 03 1.15476904 M XX=
8.86E 01 1.13E 01 5.50E 01 1.04880769 M YY=
-4.96E 01
-5.62E 01 5.18E 01 0.9i133924
- M XY= :
3.55E 01
-2.15E-01 1.17E 01 0.43112213-Plate NO= 30 0
0 0
0 t S XX=
3.37E+00
-7.09E. 02
-1.34E-01 3.37738393 i
. S YY= -
1.24E 01 9.72E 02 1.27E 01
-0.20244526 S XY=
4.79E-02 9.2SE-01 3.99E 03 0.92594993 1
M XX=
3.41 E-01, 2.77E-02
-4.50E-01 0.56534207
' M YY=
1.66E 01
' 1.49E 01 3.45E 01 -
0.41068794 M XY=
-1.44E 01 2.85E 01 6;48E-02 0.32613188 0 0
0 C \\WORKWEPCOiCALCS\\C-05 DOC.
a p
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c fGI soc mawrow.--
NI z :
h SHEET NO.
JOB NO 100031101 JOB North Anna SSI Anatvsis of ISFSI Pad BY MA DATE M7 N DATE N MT7
' OALC. NO.1Qp031005RO SUBJECT Stress ca.jgylation CHK'D
- Plate NO= 31 S XX=
3.10E+00 3.99E 02 1.27E 3.10486377 S YY=
1.03E 01 8.63E 02 9.90E 02 --
0.16657148
- S XY=
8.06E 02 7.14E 01 3.51E 03 0.71864731 M XX=
5.76E 01 4.57E 02 3.26E 01 0.66328417 M YY= -
1.49E 01 5.10E-02 2.68E 01 0.31042283 M XY=
2.52E 02 2.34E 3.64E 02 0.23854073 Plate NO 32 0
0 0
0 S XX=
2.80E+00 3.89E 02 1.17E 01 2.80671729 S YYa 8.93E 02 7.44E 02 8.36E 02
-0.14314689 S XY=
9.46E 02 5.31 E-01 ~
3.13E 03 0.53065829
. M XX=
4.95E 01
-3.45E 02 1.99E-01 0.53485944 M YY=
1.28E 01 2.71E 02 2.24E-01 0.2592348 M XY=
1.20E 02 1.71 E-01 2.18E-02 0.17320273 Plate NO= 33 0
0 0
0 S XX=
2 49E+00 4.75E 02 1.05E 01 2.49466699 SYY=
8.14E-02 G.34F 02 7.36E-02 0.12670961 S XY=
1.05E 01 3.80E 01 2.96E 03 '
O39413815 M XX=
3.74E-01 2.27E-02 1.10E-01 0.30081624 M YY=
1.10E 01 2.01E 02 1.99E 01 0.22801142 M XY=
1.44E 02 1.25E 01 1.5CE 02 0.1270091
. Plate NO= 34 0
0 0
0 S XX=
2.16E+00 5.05E 02 9.16E-02 2.16452943 S YY=
7.20E 02 5.36E 02
-6.70E-02 0.11204957 S XY=
1.15E-01 2.70E-01 3.13E-03 0.29385537 M XX=
-3.06E-01 1.59E-02 6.45E 02 0.31351213 M YY=
9.47E 02 1.70E 02 1.84E 01 0.20721014 M XYa -
1.09E-02 9.36E 02 1.14E 02 0.08496024 Plate NO= 35 0
0 0
0 S XX=
1.81 E+00 4.80E-02 7.69E 02 1.81426492 S YY=
9.79E-02 4.51E 02 6.24E 02 0.124598 S XY=
1.18E 01
-1.81E 01
-3.20E 03 0.21612429 M XX=
2.85E 01 1.26E 02 7.34E 02 0.29417147 M YY=
8.08E 02 1.46E 02 1.71 E-01 0.18997883 M XY=
7.08E-05 7.36E-02
-9.58E 03 0.07458715 Plate NO= 36 0
0 0
0 S XX=.
1.46E+00 4.00E-02
-6.10E-02 1,46082293 S YY=
2.51E 01
- 3.69E 02,
-5.91 E-(
0.26040583 3.15E-03 0.17727432 S XY=
1.01E 01 1.46E 01 M XX= -
-2.78E 01 1.06E-02 1.03E 01 0.296701 M YYa 7.21 E-02 1.26E 02 1.59E 01 0.17505339 M XY=
4.99E 03 G.03E 02 8.83E-03 0.06117657 0
0 0
0
' g.
C W/ORKWEPCO\\CALCSNC-05 DOC
tot minunoun SHEET NO.
O
- '~'
NW JOB NO.100031.01 JOB North Anna SSI Analysis of ISFSI Pad.
BY MA DATF Tf D DATEk.&M C ALC. NO. 100031C05RO SUBJECT Stress Calculation CHK'D Plate NO. 37 S XX.
1.13E+00 3.03E 02 4.43E-02 1.1322716 8 YY=
0.29E-0.
2.75E 02 5.65E 02 0.63223038 S XY=
5.83E 02 1.18E 01 2.61E 03 0.1317409 M XX.
2.28E 01 7.75E 03 1.16E 01 0.25570483 M YY=
6.45E 02 1.04E 02 1.43E 01 0.15692701 M X Y.=
3.96E 03 4.88E 02 0.66E 03 0.04969036 Plato NO= 38 0
0 0
0 S XX.
8.34E 01 2.06E 02 2.74E 02 0.83470479 S YY.
1.24 E+00 2.74E 02 5.96E 02 1.24373061 S XY=
1.19E 02 8.15E 02 1.71E 03 0.08240171 M XX=
9.23E 02 2.97E 03 5.57E 02 0.10788113 M YY.
6.07E 02 9.25E 03 1.15E 01 0.12991948 M XY-3.70E 03 3.93E 02 9.26E 03 0.04055375 Plaw N = 39 0
0 0
0 S Nr,=
3.15E 01 5.42E 01 5.23E 01 0.81615581 S YY.
9.60E 03 2.36E 01 3.09E 01 0.38925556 S XY=
1.13E 01 2.50E 01 3.82E 02 0.27660236 M XX=
4.16E+00 3.72E 01 4.09E 01 4.19360394 M YY=
1.45E+00 2.35E+00 1.20E+00 3.01259257 M XY=
2.28E+00 0.55E 01 1.79E 01 2.43690221 Plate l' O= 40 0
0 0
0 S XX.
8.93E 02 3.32E 01 3.88E 01 0.5181957 S YYa 5.35E 0?
2.78E-01 2.15E-01 0.35542141 S XY=
1.55E 01 3.54E 01 8.04E-02 0.39486289 M XX=
4.04E+00 1.49E+00 7.76E 01 4.37065682 M YY=
1.47 E+00 4.35E+00 1.45E+00 4.8172927 M XY=
2.33E+00 2.59E+00 1.03E+00 3.62918241 Plate NO= 41 0
0 0
0 S XX=
3.11 E-01 3.41E 01 3.84E 01 0.59978261 S YY=
4.94E 02 3.04E 01 2.14E 01 0.374B173 S XY=
1.76E-01 3.21E 01 7.54E 02 0.37384534 M XX=
4.06E+00
- 1.50E+ 00 7.32E 01 4.3914798 M YY=
1.46E+00 4.36E+00 1.43E +00 4.81127561 M XY=
2.31 E+00 2.59E+00 1.01E+00 3.61067002 Plato NO= 42 0
0 0
0 S XX=
8.46E 01 5.13E 01 5.02E 01 1.10887392 S YY=
2.36E 02 2.55E 01 3.03E 01 0.39658345
- W=
1.34E Oi 2.69E 01 3.34E-02 0.30242115 9 XX=
4.14E+00 3.45E 01 3.34E 01 4.16378267 M YYa 1.48E+00 2.36E+00 1.18E+00 3.02285378 M XY=
2.27E+00 8.60E 01 2.20E 01 2.43260789 0
0 0
0 C WVOROVEPCOCALCSiC-05 DOC
o
'HM EQE MEMAhoNAl, SHEET NO-N
'~
Mb DATENM7 JOB NO.100031.01 JOB.tlorth Anna SSI Analysis of ISFSI Pad BY DJ1DATE k/2/3-)
CALC. NO.100031C05R0 SUBJECT Stress Calculation CHK'D Plate NO. 43 S XX=
2.95E 01 5.15E 01 5.00E 01 0.77596086 S YY=
2.63E 02 2.10E 01 2.99E 01 0.36634126 SXY=
9.49E 02 4.40E 01 4.07E 02 0.45176329 M XX=
. 4.20E+00 3.76E 01 4.31E 01 4.23581119 M YY=
1.51 E+00 2.36E+00 1.20E+00 3.04982049 M XY=
2.29E+00 0.69E 01 1.77E-01 2.45936486 Plate NO= 44 0
0 0
0 S XX=
4.85E 01 3.19E 01 3.63E 01 0.68409064 S YY=
6.73E 02 2.52E 01 2.06E 01 0.33202388 SXY=
1.41E 01 4.97E 01 7.98E 02 0.52309426 M XX=
4.15E+00 1.49E+00 8.00E 01 4.48347869 M YY=
1.61 E+00 4.36E+00 1.44 E+00 4.83685611 M XY=
2.35E+00 2.60E+00 1.03E+ 00 3.65264685 Plate NO= 45 0
0 0
0 S XX=
6.98E 01 3.19E 01 3.47E 01 0.84162641 S YY=
5.29E 02 3.14E 01 2.02E 01 0.37713212 S XY=
1.98E 01 3.191 31 6.86E 02 0.38212337 M XX=
4.01 E+00 1.51 E+00 7.31E 01 4.35193497 M YY.
1.45E+00 4.38E+00 1.39E+00 4.82131318 M XY.
2.29E+00 2.59E+00 9.74E 01 3.59596591 Plate NO= 46 0
0 0
0 S XX=
1.39E+00 5.53E 01 4.35E 01 1.55507243 S YY=
3.57E-02 2.61E 01 2.88E 01 0.39003498 S XY=
1.60E 01 3.23E 01 2.6BE 02 0.36132217 M XX=
4.11 E+00 3.71E 01 4.31E 01 4.14716096 M YY=
1.47E+00 2.39E+00 1.13E+00 3.02901304 M XY=
2.33E+00 8.44E 01 2.49E 01 2.4897005 Plate NO= 47 0
0 0
0 S XX=
8.39E 01 5.75E 01 4.33E 01 1.10538785 S YY=
3.36E 02 1.86E-01 t!.86E 01 0.34226161 S XY=
7.87E 02 6.10E 01 3.86E 02 0.61626139 M XX=
4.21 E+00 3.77E 01 3.85E 01 4.24042991 M YY=
1.52E+ 00 2.41 E+00 1.16E+00 3.07228856 M XY=
2.31 E+00 9.01E 01 1.67E 01 2.48141884 Plate NO. 48 0
0 0
0 S XX=
8.75E 01 3.58E 01 3.06E 01 0.99351544 S YY=
7.07E 02 2.37E 01 1.88E 01 0.31062701
- .72E 02 0.61461346 S XY=
1.2SE 01 5.972 01 M D.=
4.18E+00 1.50E+00 8.06E 01 4.51135505 M YY=
1.52E+ 00 4.40E+00 1.41 E+00 4.8585185 M XY=
2.35E+00 2.64E+00 1.01 E+00 3.67066138 0
0 0
0 C \\WORKWE PCOC ALCSiC-05 00C 4
4
EGE tcE MEFt4 ate 0NAL SHEET NO. h N' W Mb DATE JOB NO.10003101 JOB North Anna SSI Analysis of ISFSI Pad BY C ALC. NO.100031C05R0 SUBJECT Stress Calculation CHKD D DATEh/12/D P'ste NO= 49 XX=
1.09E+00 3.63E 01 2.92E 01 1.18889108 S YY=
4.45E 02 3.08E 01 1.84E 01 0.36142807 S XY=
2.19E 01 2.95E 01 6.60E 02 0.37344833 M XX=
4.16E400 1.54E+00 7.75E 01 4.49920751 M YY=
1.47E+00 4.42E+00 1.37E+00 4.85747146 M XY=
2.33E+00 2.62E, JO 9.53E 01 3.63253532 Plate NO. 50 0
0 0
0 RXX=
1.94 E+ 00 6.19E 01 3.93E 01 2.07103218 S YY=
3.66E u2 2.44E 01 2.76E 01 0.36985595 S XY=
1.84E 01 2.84E 01 2.54E 02 0.33898185 M XX=
4.27E+00 3.76E 01
-4.66E 01 4.3097262 M YY=
1.52 E+00 2,43E+00 1.11 E+00 3.07672634 M XY=
2.35E + 00 8.43E 01 2.49E 01 2.50428158 Plate NO= 51 0
0 0
0 S XX=
1.38E+00 6.36E 01 3.87E-01 1.57142905 S YY=
2.95E 02 1.65E 01 2.75E 01 0.32212108 S XY=
7.92E-02 6.67E 01
- sE 02 0.6725717 M XX=
4.13E+00 4.02E-01 4.35E.41 4.1702974 M YY=
1.47E+00 2.46E+00 1.14E+00 3.0862542 M XY=
2.29 E+00 9.16E 01 1.99E 01 2.47803611 Plate NO= 52 0
0 0
0 S XX=
1.27E+00 4.03E 01 2.75E 01 1.35942902 S YY=
7.24E 02 2.19E 01 1.74E 01 0.28911519 S XY=
1.11E 01 6.09E-01 7.21E 02 0.62316035 M XX=
4.12 E+00 1.55E+00 7.61E 01 4.46548385 M YY=
1.49E+00 4.50E+00 1.40E+00 4.94330881 M XY=
2.29E+00 2.71 E+00 1.00E+00 3.68564051 Plate NO 53 0
0 0
0 S XX=
1.51 E+00 4.00E 01 2.61E 01 1.57997375 S YY=
3.61E 02 2.83E 01 1.76E 01 0.33486802 S XY=
2.43E 01 2.79E-01 7.09E 02 0.3769083 M XX=
4.13E+00 1.54E+00 7.97E 01 4.48287046 M YY=
1.49E+00 4.52E+ 00 1.40E+00 4.96323 M XY=
2.38E+00 2.68E+00 9.89E 01 3.71482768 Plate NO= 54 0
0 0
0 S XX=
2.51 E+00 7.33E 01 3.50E 01 2.M196866 S YY=
3.51 E-02 2.03E 01 2.78E 01 0.34619317 S XY=
2,12E 01 2.91E 01 2.91E 02 0.36139271 M XX=
4.27E+00 4.03E 01 4.35E 01 4.31197742 M YY=
1.54E+ 00 2.45E+00 1.17E+00 3.1186348 M XY=
2.31 E+00 8.76E 01 2.01E 01 2.48060006 0
0 0
0 C %YORKWEPCOCALCScos DOC 4
m__
._______m_-.__
0 e
I fU E0E WTERNATIONAL I 1E SHEET NO. h JOB NO.1QDQ31.01 JOB North Anna SSI Analysis of ISFSI Pad OY M 4 DATE N4"l I
' cal.C. NO.1QQO31005R0 SUBJECT Stress calculation CHK'D N DATEl# 12/T~7 1
Plate NO= 55 S XX=
1.94 E+ 00 8.05E 01 3.42E 01 2.12613326 S YY=
2.85E 02 1.38E 01 2.85E 01 0.31833655 SXY=
7.54E 02 5.71E 01 3.04E 02 0.57695332 M XX=
4.01 E+00 4.13E 01 4.01E 01 4.05503675 M YY=
1.41 E+00 2.48E+00 1.19E+ 00 3.09328078 M XY=
2.25E+00 9.04E 01 2.47E 01 2.43289403 Plate NO= 56 0
0 0
0 S XX=
1.68E+00 5.42E 01 2.31E 01 1.78314722 S YY=
6.96E 02 1.99E 01 1.88E 01 0.2823868 SXY=
9.58E 02 5.17E 01 7.32E 02 0.53067556 M XX=
4.02E+00 1.57E+00 7.90E 01 4.38290511 M YY=
1.43E+00 4.60E+00 1.45E+ 00 5.03082001 M XY=
2.24 E+00 2.77E+00 1.05E+00 3.71435391 Plate NO= 57 0
0 0
0 S XX=
1.92E+00 5.34E 01 2.18E 01 2.00380175 S YY.
3.81E 02 2.30E 01 1.93E 01 0.30240891 S XY=
2.73E 01 3.55E 01 7.81E 02 0.45447594 M XX=
3.98E+00 1.51 E+00 8.75E 01 4.34730146 M YY=
1.46E+00 4.57E+00 1.46E+00 5.01752299 M XY=
2.31 E+ 00 2.73E+00 1.08E+00 3.7302965 Plate NO= 58 0
0 0
0 S XX=
3.07E+00 9.26E 01 3.04E 01 3.2237846 S YY=
4.29E 02 1.34E 01
-3.02E 01 0.33308556 S XY=
2.47E 01 4.13E 01 3.40E 02 0.48256193 M XX=
4.13E+00 4.47E 01 4.55E 01 4.18188521 M YY=
1.C2E+00 2.45E+00 1.26E+00 3.13956207 M XY=
2.22E+00 9.62E-01 1.76E 01 2.42122504 l
Plate NO= 59 0
0 0
0 S XX=
2.31 E+M 9.40E 01 3.00E 01 2.69688937 S YY=
5.37E 02 1.21E 01 3.08E-01 0.33491933 S XY= '
9.08E 02 3.48E 01 3.90E 02 0.36157353 M XX=
4.07E+00 4.18E 01 4.68E-01 4.12000251 M YY=
1.48E+00 2.48E+00 1.30E+00 3.1645728 M XY=
2.27E+00 8.36E-01 2.94E 01 2.43696192 Plate NO. 60 0
0 0
0 S XX=
2.07E400 5.63E 01 2.08E 01 2.15617496 S YY=
8.88E 02 1.86E 01 2.03E 01 0.28935424 S XY=
9.16E-02 3.24E 01 8.43E 02 0.34397887 M XX=
4.09E+00 1.60E+00 9.45E 01 4.49418269 M YY=
1.55E+00 4.59E+00 1.53E+00 5.0768768 M XY=
2.31 E+00 2.71 E+00 1.13E+00 3.73913867 0
0 0
0 C \\WORIOVEPCO\\CALCSTC-os DOC
EQE tot m m te tioe n f7
/
SHEET NO.
Nb D ATE,,f, 6
O JOB NO.10003101 JOB North Anna SSI Analysis of ISFS! Pad BY C ALC. NO. 100031C05RO SUBJECT Stress Calculation CHKD N DATM., 2 f ^
- .'"2 Plate NO. 61 S XX=
2.30E+00 5.90E 01 2.02E 01 2.37816944 S YY=
3.30E 02 1.27E 01 1.96E 01 0.23589231 S XY=
2.92E 01 5.31E 01 8.03E 02 0.6109797 M XX.
3.81 E+00 1.50E+00 8.83E 01 4.'.d498789 M YY=
1.51 E+00 4.48E+00 149E+00 4.95837685 M XY=
2.23E+00 2.75E+00 1.15E+ 00 3.71987164 Plate NO= E2 0
0 0
0 S XX.
3.54 E+ 00 8.80E 01 2.96E 01 3.66155108 S YY.
5.05E Ok 3.38E 02 2.95E 01 0.30100181 S XY=
2.70E 01 6.83E 01 3.54E 02 0.73476436 M XX=
3 65E+00 5.95E 01 3/BE 01 3.71739449 M YY=
1.47E+00 2.33E+00 1.32E+00 3.05436884 M XY=
2.44E+00 1.09E+00 3.20E 01 2.69350998 Plate NO= 63 0
0 0
0 S XX=
3.00E400 7.83E 01 3.01E 01 3.11697955 S YY.
8.17E 02 1.24E 01 2.89E 01 0.32525142 S XY=
1.06E 01 3.57E 01 4.89E-02 0.37552418 M XX.
5.24 E+00 7.21E 01 6.97E 01 5.33119538 M YY=
1.90E+00 2.19E+00 1.47E+ 00 3.25025876 M XY=
2.76E+00 7.32E 01 4.01 E-01 2.88343737 Plate NO= 64 0
0 0
0 S XX=
2.55E+00 3.65E 01 1.59E-01 2.57791247 S YY=
1.27E 01 2.01E 01 1.69E 01 0.29172907 S XY=
8.45E 02 2.47E 01 8.96E 02 0.27619741 M XX=
4.75E+00 1.35E+00 1.34E+00 5.11761136 M YY=
1.71 E+00 4.20E+00 1.47E+00 4.770285 M XY=
2.50E+00 2.17E+ 00 1.18E+00 3.51809309 Plate NO= 65 0
0 0
0 S XX=
2.8J+00 4.54E-01 1.27E 01 2.86806531 S YY=
8.26E 02 3.93E 02 1.48E 01 0.17388954 S XY=
3,65E-01 9.48E 01 5.34 E-02 1.01748536 M XX=
4.44 E+00 1.50E+00 9.71E 01 4.78383774 M YY=
2.07E+ 00 4.20E+00 1.09E+00 4.80647594 M XY=
2.74 E+00 3.10E+00 1.02E+00 4.25960937 Plate NO= 66 0
0 0
0 S XX=
4.38E+00 4.91E 01 1.65E 01 4.40558647 SYY=
1.36E 01 1.04E 01 2.04E 01 0.26620779 S XY=
3.44E 01 1.30E+00 2.99E 02 1.34121154 M XX=
5.26E+ 00 6.32E 01 6.86E 01 5.34104808 M YY=
2.95E+ 00 1.85E+00 7.88E 01 3.57042321 M XY=
1.86E+ 00 1.75E+00 5.58E 01 2.61743591 0
0 0
0 C \\ WORT (WEPCO\\C ALCSNC-05 DOC
7_ _. _ _ _ _ _ _ _. _ _ _ _
tot emmuow..
b i
i SHEET NO.
i JOB NO.100031.01 JOB North Anna SSI Analysis of ISFSI Pad BY M4 DATE @ M 'i CALC. NO 100031C05R0 SUBJECT Stress Calcultt. ion CHK'D @ DATE M 7 l
Plate NO= 67 S XX=
3.84 E+00 3.17E 01 1.50E 01 3.85497254 S YYa 1.08E 01 2.79E 01 1.43E 01 0.33205911 S XY=
6.98E 02 1.01 E+00 1.46E 02 1.01451152 M XX-7.21E 01 8.86E 02 4.59E 01 0.R594348 M YY=
1,39E+00 5.63E 01 4.86E 01 1.57726819' M XY=
4.53E 01 9.22E 01 2.85E 01 1.06593315 Plate NO= 68 0
0 0
-0 i
S XX=
3.45E+00 1.82E 01 1.40E 01 3.45864753 S YY=
9.66E 02 2.63E 01 1.16E 01 0.30300703 S XY=
2.01E 01 8.16E 01 1.27E 02 0.84048663 M XX=
4.84E 01 2.05E 01 4.33E 01 0.68157196 M YY=
5.09E 01 2.06E 01 3.21E 01 0.63608988 M XY=
1.10E 01 4.81E 01 1.65E 01 0.52041784 i
Plate NO= 69 0
0 0
0 S XX=
3.13E+00 1.22E 01 1.30E 01 3.13607573 S YY=
8.94E 02 2.44E 01 9.16E 02 0 27564214 S XY=
2.47E 01 6.34E 01 1.01E 02 0.6798433 M XX=
0.25E 01 1.71E 01 3.13E 01 0.71938261 M YY=
2.20E 01 9.62E 02 2.52E 01 0.34812676 M XY.
4.83E 02 2.72E 01 9.66E 02 0.29228749 Plate NO= 70 0
0 0
0 S XX=
2.84E+00 1.28E 01 1.19E 01 2.84239594 S YY=
8.29E 02 2.11E 01 7.62E 02 0.23907406 S XY=
2.72E M 4.76E 01 8.75E 03 0.54789413 M XX=
4.96E 01 1.10E 01 1.88E 01 0.54111113 M YY=
1.29E 01 6.58E 02 2.18E 01 0.261834 M XY=
6.24E 02 1.73E 01 6.23E 02 0.19408299 Plate NO. 71 0
0 0
0 S XX=
2.55E+00 1.56E-01 1.07E 01 2.55199792
(
S YY=
7.34E 02 1.80E 01 6.80E 02 0.2058505 S XY=
2.98E 01 3.41E 01 8.30E 03 0.45279809 M XX=
3.63E 01 0.79E 02 1.03E 01 0.38304938 M YY=
1.03E 01 5.19E 02 1.97E 01 0.22871286 M XY=
. 5.09E 02 1.22E 01 4.32E 02 0.13871546 Plate NO. 72 0
0 0
0 S XX=
2.24E+00 1.63E 01 9.29E 02 2.24881683 S YY=
7.19E 02 1.52E 01 6.32E 02 0.17978933 S XY=
3.27E 01 2.51E 01 8.80E 03 0.41177726 M XX=
2.94E 01
-4.69E 02 6.03E 02 0.30364814 M YY=
8.65E 02 4.40E-02 1.83E 01 0.20714901
- M XY=
3.40E 02 9.08E 02 3.31E 02 0.10243424 0
0 0
0 C WiOACVEPCONCALCSiC-05 DOC
o fG1 tot msuncem SHEET NO. N i
EN"l JOB NO.100031.01 JOB North Anna SSI Analvsis of ISFSI Pad BY M 4 DATE CALC. NO.100031C05R0 SUBJECT.DRgss Calculation CHKD _ DM DATE N2M j i
e Plate NO. 73 S XX=
1.91 E+00 1.55E 01 7.81E 02 1.91982895 S YY=
8.76E 02 1.28E 01 5.87E 02 0.16596081 1.76E 01 9.51E 03 0.38532394 S XY=
3 43E 01
+
3.70E 02 7.24E 02 0.28609022 M XX=
2.74E 01 M YY.
7.43E 02 3.85E 02 1.72E 01 0.19163236 M XY=
2.05E 02 7.04E 02 2.78E 02 0.07844555 Plate NO. 74 0
0 0
0 S XX=
1.56E+00 1.31E 01 6.23E 02 1.5617087 S YY=
1.93E 01 1.06E 01 L.56E 02 0.22603068 1.37E 01 9.65E 03 0.33992405 S XY= -
3.11E 01 3.12E 02 1.03E 01 0.29090194 M XX=
2.70E 01 M YY=
6.67E 02 3.32E 02 1.61E 01 0.17748714 M XY.
1.41E 02 5.72E 02 2.56E 02 0.06421027 Plate NO= 75 0
0 0
0 9.83E 02 4,52E 02 1.18893215 S XX=
1.18E* 00 8.07E 02 5.34E 02 0.5302018 S YY=
5.21E 01 1.16E 01 8.17E 03 0.22337752 S XY=
1.91E 01 2.30E 02 1.15E 01 0.25227315 M XX=
2.23E 01 M YY.
6.10E-02 2.73E 02 1.47E 01 0.16167485 M XY=
1.09E-02 4.56E 02 2.47E 02 0.05299997 Plate NO= 76 0
0 0
0 6.56E 02 2.80E 02 0.86125386 S XX=
8.58E-01 7.78E 02 5.57E 02 1.16294755 S YY=
1.16E+00 8.41E 02 5.28E 03 0.09128735 S XY=
3.52E 02 8.91 03 5.56E 02 0.10698386 E
M XX=
9.10E 02 M YY=
5.96E-02 2.37E 02 1.23E 01 0.13889085 M XY=
9.89E 03 3.75E 02 2.58E 02 0.04659042 Plate NO. 77 0
0 0
0 S XX=
3.34E 01 8.42E 01 5.18E 01 1.04345651 S YY=
6.57E 02 8.98E-01 1.93E 01 0.92078691 S XY=
7.42E 01 3.02E 01 3.20E 02 0.80218903 M XX=
4.16E+00 8.43E 01 4.06E 01 4.26789973 M YY=
1.50E +00 2.25E+00 9.42E 01 2.86619267 M XY=
2.32E+00 7.18E 01 1.93E 01 2.43138514 Plate NO= 78 0
0 0
0 S XX=
6.13E 02 6.51E 01 3.86E 01 0.75939449 S YY=
2.36E 02 6.57E 01 -
1.58E 01 0.67614484 S XY=
6.03E 01 4.64E 01 4.96E-02 0.762L5332 M XX=
4.11 E+00 1.90E+00 6.48E 01 4.57347984 M YY=
1.49E+00 3.87E+00 1.18E+00 4.30981601 2.70F+00 8.34E 01 3.B4182516 M XY=
2.30E+00 0
0 0
0 l
C \\WOACVEPCOC/.CSC05 DOC 4
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SHEET NO. M Mb DATED 4 7 JOB NO.10003101 JOB North Anna SSI Analysis of ISFSI Pad BY CALC. NO.100031C05R0 SUBJECT Stress calculation CHK'O N DATE kl2/9~?
Plate NO= 79 S XX=
3.94E 01 6.24E 01 3.82E 01 0.83051331 S YY.
3.26E 02 6.41E 01 1.57E 01 0.66064583 S XY.
6.30E 01 3.94E 01 4'99E 02 0.74444609 M XX=
, 4.07E+00 1.86E+00 6.95E 01 4.52830975 M YY=
1.48E+00 3.84E+00 1.20E+00 4.2907384 M XY=
2.30E+00 2.69E+00 8.78E 01 3.64490744 Plate NO= 80 0
0 0
0 S XX=
8.66E 01 7.82E 01 4.9eE 01 1.26849744 SYY=
6.9BE 02 8.90E 01 1.90E 01 0.91261921 S XY=
7.64E 01 2.68E 01 3.32E 02 0.80996766 M XX.
4.14E+ 00 8.61E 01 3.39E 01 4.24322373 M YY=
1.50E+00 2.21 E+00 9.71E 01 2.84450461 M XY=
2.25E+00 7.43E 01 1.78E 01 2.37903003 Plate NO= 81 0
0 0
0 S XX=
2.88E 01 7.60E 01 4.96E-01 0.95189757 S YY=
7.18E 02 9.14E 01 1.89E 01 0.93585956 S XY.
7.22E 01
-4.27E 01 3.17E 02 0.83873044 M XX=
4.21 E+ 00 8.36E 01 4.25E 01 4.31210835 M YY=
1.51 E+00 2.22E+00 9.39E 01 2.83979994 M XY=
2.32E+00 7.26E 01 2.01E 01 2.44011214 Plate NO= 82 0
0 0
0 S XX.
4.10E 01 5.73E 01 3.59E 01 0.79072982 S YY=
2.53E 02 6.68E 01 1.50E 01 0.68461475 6.iY=
5.83E 01 5.41E 01 4.96E 02 0.7966854 M XX=
4.13E+00 1.89E400 6.31E 01 4.58815026 M YY.
1.48E+00 3.86E+00 1.17E+00 4.29665242 M XY=
2.31 E+00 2.70E+00 8.06E 01 3.64333607 Plate NO= 83 0
0 0
0 S XX.
7.80E 01 5.99E 01 3.46E 01 1.04201567 S YY=
4.42E 02 6.28E 01 1.48E 01 0.64717042 S XY=
6.51E 01 3.68E 01 4.81E 02 0.74917564 M XX=
4.31 E+00 1.86E+00 7.62E 01 4.7512571 M YY=
1.52 E+00 3.85E+00 1.24 E+00 4.32045472 M XY=
2.32E+00 2.67E+00 9.38E 01 3.65520506 Plate NO= 84 0
0 0
0 S XX=
1.41 E+00 7.71E 01 4.32E 01 1.66318166 S YY=
-0.89E 02 8.91E 01 1.82E 01 0.91198748 S XY=
7.87E 01 2.67E-01 3.77E 02 0.8316292 M XX= -
4.10E+00 8.77E 01 3.46E 01 4.20610016 l
M YY=
1.52E+00 2.20E+00 1n3E+00 2.86375051 M XY=
2.30E+00 7.31E 01 47E 01 2.41538383 l
0 0
0 0
e swomvtococAtese.os Doc v
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SHEET NO. M N
DM DATE JOB NO.100031.01 JOB North Anna SSI Analysis of ISFSI Pad BY CALC NO.100031C05RO SUBJECT Stress calculation CHKD N DATE NG M Plate NO= 85 S XX=
8.22E 01 7.99E 01 4.28E 01 1.22362944 i
S YY=
7.56E 02 9.34E 01 1.81E 01 0.95386471 S XY=
6.97E 01 5.12E 01 3.23E 02 0.86576443 M XX=
4.22 E+00 8.48E 01 4.18E 01 4.32845184 M YY=
1.50E+ 00 2.21 E+00 9.70E 01 2.8396817 M XY=
2.32E400 7.49E 01 2.02E-01 2.44718714 Plate NO 86 0
0 0
0 S XX=
7.94E 01 6.58E 01 3.04E 01 1.07536697 SYY=
2.03E 02 6.67E 01 1.37E 01 0.68144094 SXY.
5.61E 01 5.82E 01 5.02E 02 0.80962868 M XX.
4.14 E+ 00 1.90E+00 6.40E 01 4.60480805 M YY=
1.46E+ 00 3 86E+00 1.18E+00 4.2892342 M XY=
2.31 E400 2.70E+00 8.07E 01 3.64673324 Plate N O = 87 0
0 0
0 S XX=
1.17E+00 6.82E 01 2.92E 01 1.3880586 SYY=
4.80E-02 6.13E 01 1.35E 01 0.62964874 S XY=
6.58E 01 3.28E 01 4.73E 02 0.73682837 M XX=
4.18E+00 1.89E+00 8.13E 01 4.66133907 M YY=
1.58E+00 3.86E+00 1.26E+00 4.36119548 M XY=
2.43E+00 2.69E+00 9.75E 01 3.75246546 Plate NO= 88 0
0 0
0 S XX=
1.96E+00 8.79E 01 3.94 E-01 2.18287282 S YY=
6.40E 02 8.90E 01 1.740 01 0.9088731 S XY=
8.02E 01 2.51E 01 3.7dE 02 0.84133448 M XX=
4.27E+00
' 8.97E 01 3.61E 01 4.3762232 M YY=
1.60E+00 2.22E+ 00 1,09E+00 2.94291165 M XY=
2.32E+00 7.12E 01 1.72E 01 2.43395537 Plate NO= 89 0
0 0
0 S XX.
1.37E+00 9.07E 01 3.88E 01 1.68839083 S YY.
7.71E 02 9.42E 01 1.74E 01 0.96062281 S XY=
6.66E 01 5.21E 01 2.94E 02 0.84633158 M XX.
4.15E+00 8.92E 01 3.88E 01 4.26236849 M YY=
1.46E+00 2.22E+00 1.04E+00 2.85463921 M XY=
2.30E+00 7.64E 01 1.97E 01 2.42964117 Plate NO= 90 0
0 0
0 S XX=
1.19E+00 7.38E 01 2.74E 01 1.42371394 S YY=
1.79E 02 6.60E-01 1.26E 01 0.67221486 S XY=
5.33E 01 5.53E-01
-4.78E 02 0.76961052 M XX=
4.10E+00 1.96E+00 7.17E 01 4.60147153 M YY=
1.44E+00 3.94 E+00 1.21 E+00 4.36011296 M XY=
2.27E+00 -
2.77E+00 8.65E 01 3.68520597 0
0 0
0 C \\WORKWEPCO;CALCSic.05 00C m.
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Nb DATE W
JOB NO.10003101 JOB North Anna SSI Analysis of ISFS! Pad BY CALC. NO.1MQ31C05R0 SUBJECT Stress Calculation CHK'O N DATE D b Plate NO 91 S XX.
1.58E+00 8.06E 01 2.67E 01 1.79369033 S YY=
5.45E 02 5.90E 01 1.26E 01 0.6053573 S XY=
0.67E 01 2.83E-01 4.57E 02 0.72611457 M XX.
4.17E+00 1.95E+00 7.98E 01 4.66642739 M YY.
1.59E+ 00 3.92E+00 1.23E400 4.40480351 M XY=
2.42E+ 00 2.70E+00 9.33E 01 3.74247151 PW.e NO= 92 0
0 0
0 S XX=
2.54E+ 00 1.08E+00 3.54E 01.
2.77803017 S YY.
6.13E 02 8.76E 01 1.74E 01 0.89517398 SXY=-
B.09E 01 2.26E 01 3.13E 02 0.c4003841 M XX=
4.27E+00 8.84E 01 3.99E 01 4.37578906 M YY.
1.63E+00 2.22 E+00 1.10E400 2.9662537 M XY=
2.32E400 7.56E 01 1.90E 01 2.45018317 Plate NO= 93 0
0 0
0 S XX=
1.93E+00 1.16E+00 3.47E 01 2.27511302 S YY=
8.47E 02 9.16E 01 1.77E 01 0.9372489 S XY=
6.25E 01 4.22E 01 3.09E 02 0.75448374 M XX=
4.03E+ 00 9.02E 01 3.39E 01 4.13978106 M YY=
1.44 E+00 2.27E+00 1.10E+ 00 2.90335978 M XY=
2.28E+00 7.88E 01 2.08E 01 2,41944887 Plate NO= 94 0
0 0
0 S XX=
1.60E+00 9.84E 01 2.29E 01 1.88903618 S YY=
2.0BE 02 6.28E 01 1.29E 01 0.64158617 SXY=
4.98E 01 4.62E 01 5.30E 02 0.68144403 M XX=
4.04E+ 00 1.98E+00 8.10E 01 4.57009389 M YY=
1.45E+00 4.01 E+00 1.25E+00 4.44729288 M XY=
2.26E+00 2.80E+00 9.69E 01 3.72161688 Plate NO= 95 0
0 0
0 S XX=
1.99E+00 1.07E+ 00 2.19E 01 2.26820409 S YY=
5.36E 02 5.54E 01 1.31E 01 0.57148556 S XY=
6.70E 01 3.20E 01 4.2SE 02 0.7438035 M XX=
4.01 E+00 2.02E+00 6.62E 01 4.53510857 -
M YY=
1,53E+00 4.04E+00 1.15E+00 4.47428274 M XY=
2.30E+00 2.84E+00 8.06E 01 3.74100465 Plaie NO= 96 0
0 0
0 S XX=
3.10E+00 1.37E+00 2.92E 01 3.39852113 S YY=.
4.97E 02 8.37E 01 1.86E 01 0.85866252 S XY=
8.08E 01 3.13E 01 2.87E 02 0.86718257 M XX=
4.14 E+00 8.11E 01 4.70E 01 4.24291642 M YY=
1.56E+00 2.31 E+00 1.02E+ 00 2.97346835 M XY=
2.30E+ 00 7.81E 01 2.29E 01 2.4360614 0
0 0
0 C \\WOACVEPCOiCALCS\\C-05 DOC
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(, N Ib SHEET NO.
JOB NO.10003101 JOB North Anna SSI Analvsis of ISFSI Pad BY Nb DATE %@ 7 CALC. NO.100031C05R0 SUBJECT Stress Calculation CHKD D3 DATENI N Plate NO= 97 i
S XX.
2.49E400 1.40E+00 2.87E 01 2.87447991 S YY=
9.06E 02 8.31E 01 1.90E 01 0.85759938 S XY=
5.79E 01 2.56E 01 3.83E 02 O_63381158 M XX.
4.07 E+ 00 8.93E 01 4.31E 01 4.18510651 M YY=
1.50E+ 00 2.28E+00 1.10E+ 00 2.9451073 M XY=
2.28E+00
+7.52E 01 2.49E 01 2.41751159 Plate NO= 98 0
0 0
0 S XX.
1.98E400 1.15E+00 2.08E 01 2.30041603 8 YY=
2.65E 02 5.06E 01 1.36E 01 0.52497045 S XY=
4.64E 01 3.01E 01 5.73E 02 0.5560229 M XX=
4.03E+00 1.96E+00 8.52E 01 4.56460976 M YY=
1.51 E+00 4.02E+00 1.23E+00 4.46661046 M XY=
2.34E+ 00 2.73E+ 00 1.00E+00 3.72985214 Plate NO 99 0
0 0
0 S XX=
2.36E400 1.09E+00 2.04E 01 2.60549503 S YY.
7.47E 02 5.05E 01 1.33E 01 0.52774188 S XY=
6.86E 01 4.64E 01 5.19E 02 0.82939604 M XX=
3.8$ E+00 2.16E+00 6.78E 01 4.42791886 M YY.
1.46E+00 4.10E+00 1.12E+ 00 4.49320431 M XY=
2.29E4 00 3.00E+00 8.12E 01 3.86393162 Plate NO= 100 0
0 0
0 S XX=
3.57E400 1.31 E+00 2.79E 01 3.81207625 S YY=
0.47E 02 7.68E 01 1.86E 01 0.79254927 SXY=
8.39E 01 5.2SE 01 4.65E 02 0.99067284 M XX=
3.70E+00 6.89E 01 4.13E 01 3.78620459 M YY=
1.39E+00 2.43E+00 9.73E 01 2.96357154 M XY=
2.15E+ 00 9.64E 01 2.98E 01 2.3729968 Plate NO= 101 0
0 0
0 S XX=
2.99E+00 1.23E+00 2.86E 01 3.24903306 S YY=
8.43E 02 6.56E 01 1.85E 01 0.68709525 S XY.
5.85E 01 2,48E 01 3.91E 02 0.63659678 M XX=
5.25E+00 5.38E 01 8.44E 01 5.34754609 M YY=
1.93E+00 2.36E+00 1.03E+00 3.21888987 M XY=
2.39E+ 00 5.94E 01 3.10E 01 2.47918523 Plate NO= 102 0
0 0
0 S XX=
2.46E+ 00 9.56E 01 1.57E 01 2.64757003 S YY=
6,50E 02 3.65E 01 1.10E 01 0.38689733 S XY=
- 4.62E 01 1.38E 01 5.52E 02 0.48508236 M XX=
4.74E+00 2.16E+ 00 9.00E 01 5.28572426 M YY=
1.62E+00 3.77E+00 1.03E+00 4.22783503 M XY.
2.86E+ 00 2.43E+00 9.92E 01 3.88064985 0
0 0
0 C \\WONVEPCOCALCSNC 05 DOC 1
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SHEET NO.
M4 DATE UU JOB NO.100031.01 JOB North Anna SSI Anatvsis of ISFSI Pad BY CALC. NO.100031C05R0 SUBJECT Stress calculation CHK'D D D DATE ki b Plate NO 103 S XX=
2.89E4 00 6.25E 01 1.30E 01 2.96072291 S YY=
1.10E 01 4.65E 01 9.8BE 02 0.48747178 S XY.
7.27E 01 7.71E 01 6.41E 02 1.06157774 M XX=
4.33E4 00 2.13E+00 1.08E+00 4.94751574 M YY.
2.12E+00 3.50E+00 1.11 E+00 4.24013066' M XY=
2.96E+00 3.03E+00 9.34E 01 4.33896375 Plate No.104 0
0 0
0 S XX=
4.40E400 6.22E 01 1.73E 01 4.44210992 S YY.
1.07E 01 6.79E 01 1.29E 01 0.69929316 SXY=
8.55E 01 1.03E+00 6.86E 02 1.34345979 M XX=
5.18E+00 4.01 E-01 6.32E 01 5.23965477 M YY.
3.16E+00 1.60E+00 0.11E 01 3.65330188 M XY=
1.84 E+00 1.69E+ 00
-4.85E 01 2.54156748 Plate NO= 105 0
0 0
0 S XX=
3.84E+00 4.09E 01 1.58E 01 3.86593214 S YY.
1.32E 01 3.87E 01 1.16E 01 0.42511555 S XY=
4.94E 01 7.79E 01 3.41E 02 0,92326009 M XX=
6.65E 01 7.05E 01 3.86E 01 1.0432122 M YY=
1.60E+00 4.62E 01 4.99E 01 1.73773288 M XY.
5.78E 01 9.78E 01 3.35E 01 1.184491 Plate NO.106 0
0 0
0 S XX=
3.45E+00 2.39E 01 1.46E 01 3.46230551 S YY=
9.13E 02 3.87E 01 9.31E 02 0.408292 S XY=
4.06E 01 6.18E 01 2.14E 02 0.73979584 M XX=
5.11E 01 5.38E 01 3.93E 01 0.83956401 M YY.
0.33E 01 1.45E 01 2.85E 01 0.70954053 M XY=
3.51E 01 4.75E 01 2.22E 01 0.63125201 Plate NO= 107 0
0 0
0 S XX=
3.15E+00 2,12E 01 1,35E 01 3.15698993 S YY=
B.32E 02 3.50E 01 7.43E 02 0.36687321 S XY=
3.91E 01 4.79E 01 1.48E 02 0.61816947 M XX=
6.04E 01 3.29E 01 2.80E 01 0.74243454 M YY.
2.59E 01 8.39E 02 2.22 E-01 0.35176574 M XY=
2.30E 01 2.52E 01 1.43E 01 0.36973496 Plate NO 108 0
0 0
0 S XX=
2.88E+00 2.61E 01 1.23E 01 2.89634935 S YY=
7.53E 02 3.04E 01 6.42E 02 0.3200684 S XY=
4.02E 01 3.64E 01 1.24E 02 0.54239248 M XX=
4.56E 01 1.86E 01 1.65E 01 0.51936582 M YY=
1.27E 01 6.89E 02 1.91E 01 0.2395438 M XY=
1.54E 01 1.56E 01 9.44E 02 0.23879486 0
0 0
0 C \\WORKWEPCONCALCSC 05 DOC t
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SHEET NO.
DO JOB NO.10003101 JOB North Anna SSI Analysis of ISFSI Pad BY th k DATE N DATEbb2lil CALC. NO.100031C05RO SUBJECT Stress Calcutation
_CHKD 2
Plate NO= 109 S XX=
2.63E+ 00 2.96E 01 1.09E 01 2.65083933 S YYa 7.24E 02 2.61E 01 5.95E 02 0.27691797 f
S XY=
4.31E 01 2.73E 01 1.24E 02 0.51033691 M XX=.
-3.27E-01 1.09E 01 9.32E 02 0.35704631 M YY=
8.02E 02 5.81E 02 1.74E 01 0.19984985 "
M XYa 9.76E 02 1.12E 01 6.64E 02 0.16249607 Plate NO.110 0
0 0
0 S XX=
2.38E+00 3.07E 01 9.57E 02 2.40555337 S YY=
7.16E 02 2.21E 01 5.52E 02 0.2389691 4
S XYe 4.73E 01 2.11E 01 1.33E 02 0.51743901 M XX=
2.65E 01 7.43E 02 5.59E 02 0.28094749 M YY=
6.55E 02 5.04E 02 1.62E 01 0.18175829 M XY=
5.74E 02 8.61E 02 5.09E 02 0.11533165 Plate NO.111 0
0 0
0 S XX=
2.12E+00 2.91E 01 8.11E 02 2.14239256 S YY=
7.90E 02 1.87E 01 5.10E 02 0.20903146 S XY=
5.12E 01 1.63E 01 1.47E 02 0.53771616 M XX=
2.53E 01 5.88E 02 6.94E 02 0.2685739 M YY=
5.64E 02 4.40E 02 1.53E 01 0.1687t294 M XY.
3.15E 02 6.88E 02 4.33E 02 0.08724719 Plate NO 112 0
0 0
0 S XXe 1.82E+00 2.52E 01 6.57E 02 1.835L8922 S YY=
1.20E 01 1.56E 01 4.79E 02 0.20260596 SXY=
5.16E 31 1.18E 01 1.56E 02 0.52926507 M XX=
2.55E 01 5.02E-02 9.93E 02 0.27859041 M YY=
5.11E 02 3.77E 02 1.45E 01 0.15865497 M XY=
2.11E 02 5.38E 02 3.98E 02 0.070168 Plate NO 113 0
0 0
0 S XX=
1.41 E+00 1.98E 01
-4.90E-02 1.42374315 S YY=
3.00E 01 1.27E 01 4.63E 02 0.32860065 S XYa 3.94E 01 1.07E 01 1.47E 02 0.40892879 M XX=
2.16E 01 3.79E 02 1.13E 01 0.2462119 M YY=
4.81E 02 3.04E 02 1.37E 01 0.14807475 M XY=
1.53E 02 4.08E 02 3.70E 02 0.05712859 Plate NO.114 0
0 0
0 S XX=
9.19E 01 1.20E 01 3.00E 02 0.92703538 S YY=
9.66E 01 1.23E 01 5.00E 02 0.97528224 S XY=
7.21E 02 8.76E 02 9.43E 03 0.11388222 M XX=
8.89E 02 1.51E 02 5.52E 02 0.10569928 M YY=
5.52E 02 2.49E 02 1.23E 01 0.13673108 M XY=
1.30E 02 3.33E 02 3.53E 02 0.05021298 0
0 0
0 c uvoROVEPCO'CALCSC05, DOC 4'
HM soc memucu 5I t
b SHEET NO.
M DATE MMM *7 JOB NO.10003101 JOB North Anna SSI Analvsis of ISFSI Pad BY CHKD D7D DATE bl2 k) l C ALC. NO. 100031 COSR0 SUBJECT.Stross Calculation Plate NO= 115 S XX=
2.60E 02 1.05E+00 4.40E 01 1.13956615 S W.
1.51E 02 9.10E 01 1.26E 01 0.91835209 S XY=
6.32E 01 1.25E 01 1.37E 02 0.64429203 M XX=
2.17E+00 1.96E+00 5.97E 01 2.98365879 M W.
6.99E 02 1.89E+00 5.30E 01 1.96703569 M XY=
7.70E 01 1.19E 02 4.05E 02 0.77155605 Plate NO= 116 0
0 0
0 S XX=
1.07E 01 1.09E+00 4.50E 01 1.18129142 S YY=
2.41E 02 1.21 E+00 1.43E 01 1.22160169 S XY=
6.73E 01 3.82E 01 4.82E 02 0.77467649 M XX=
2.16E+ 00 2.93E+00 7.68E 01 3.72021731 M W=
7.80E 02 3.71 E+ 00 9.95E 01 3.84479822 M XY=
7.53E 01 1.50E+00 4.36E 01 1.73329745 Plate NO= 117 0
0 0
0 S XX=
5.31E 01 1.06E+00 4.43E 01 1.26342333 S YY=
1.86E 02 1.21 E+00 1.43E 01 1.21949727 S XY=
6.63E 01 3.79E 01 4.80E 02 0.76533625 M XX=
2.13E+00 2.92E+00 7.95E 01 3.69619953 M W.
7.39E 02 3.71 E+00 9.95E 01 3.84276011 M XY=
7.60E 01 1.50E+00 4.08E 01 1.73116598 Plate NO 118 0
0 0
0 S XX=
4.45E 01 9,81E 01 4.26E 01 1.15886732 S YY=
1.78E 02 9.09E 01 1.25E 01 0.91793891 S XY=
6.25E 01 1.31E 01 1.27E 02 0.63876911 M XX=
2.16E+00 1.98E+00 5.69E 01 2.97855556 M YY.
6.90E 02 1.88E+00 5.31E 01 1.95861529 M XY=
7.69E 01 3.22E 02 4.40E 02 0.77073439 Plate NO= 119 0
0 0
0 S XX=
4.89E 01 9.32E 01 4.18E 01 1,13272264 S YY=
2.36E 02 9.13E 01 1.24E 01 0.92205392 S XY=
6.37E 01 1.90E 01 1.39E 02 0.66506879 M XX=
2.21 E+00 1.96E+00 6.11E 01 3.01411869 M YY=
7.92E 02 1.88E+ 00 5.34E 01 1.95776026 M XY.
7.63E 01 3.33E-02 5.96E 02 0.76574978 Plate NO= 120 0
0 0
0 S XX=
4.41E 01 9.95E 01 4.21E 01 1.16667831 S YY=
3.53E 02 1.22E+00 1.41E 01 1.23059006 S XY=
6.81E 01 4,43E 01 4.77E 02 0.81317474 M XX=
2.16E+00 2.93E+00 7.58E 01 3.71545214 M W=
9.72E 02 3.71 E+00 1.00E+00 3,.84293195 M XY=
7.78E 01 1.49E+00
-4.63E 01 1.74591012 0
0 0
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N# 7 JOB NO.10003101 JOB North Anna SSI Analysis of ISFSI Pad BY k9 4 DATE CALC. NO,100031C05RO SUBJECT Stress Calculation CHKD D TD DATE bl2N~l Plate NO= 121 S XX=
9.97E 01 1.03E+00 3.99E 01 1.48585983 S W=
1.88E 02 1.22E+ 00 1.40E 01 1.22610687 S XY=
6.51E 01 3.75E 01 4.82E 02 0.75288527 M XX=
2.13E+00 2.90E+00 8.41E 01 3.70000241 M YY=
8.94E 02 3.71 E+00 9.99E 01 3.84407462 M XY=
7.48E 01 1.51 E+00 3.90E 01 1.73157714 Plate NO= 122 0
0 0
(
S XX=
9.05E 01 8.79E 01 3.75E 01 1.31588243 S W=
1.89E 02 9.14E 01 1.22E 01 0.92188951 S XY=
6.14E 01 1.50E 01 1.25E-02 0.63232515 M XX=
2.13E+00 1.98E+00 5.23E 01 2.94925441 M W=
7.34E 02 1.89E+00 5.35E 01 1.96285866 M XY=
7.60E 01 4.06E 02 5.50E 02 0.76316172 Plate NO= 123 0
0 0
0 S XX=
9 55E 01 8.96E 01 3.61E 01 1.35067934 S YY=
2.69E 02 9.20E 01 1.20E-01 0.92825567 S XY=
6.41E 01 2.41E 01 1.42E 02 0.68530571 M XX=
2.22E+00 1.98E+00 5.83E 01 3.02871231 M YY=
9.25E 02 1.90E+00 5.36E 01 1.97242289 M XY=
7.65E 01 3.83E 02 5.94E 02 0.76835591 Plate NO= 124 0
0 0
0 S XX=
9.11E 01 1.14 E+00 3.54E 01 1.50177997 SYY=
4.39E 02 1.24E+00 1.35E 01 1.24613553 S XY=
6.86E 01 4.83E 01 4.67E 02 0.84036591 M XX=
2.16E+00 2.93E+00 7.65E 01 3.71389823 M W=
1.27E 01 3.71 E+00 9.99E 01 3.84816534 M XY=
8.01E 01 1.51 E+00 4.70E 01 1.76863591 Plate NO= 125 0
0 0
0 S XX.
1.47E+00 1.18E+00 3.46E 01 1.91620102 S YY.
2.52E 02 1.23E+00 1.33E 01 1.23443386 S XY.
6.35E 01 3.61E 01 4.66E 02 0.73204162 M XX=
2.23E+00 2.94E+00 8.75E 01 3.79324481 M YY.
1.09E 01 3.71 E+00 9.99E 01 3.843t,1017 M XY=
7.79E 01 1.51 E+00 3.65E 01 1.74024603 Plate NO= 126 0
0 0
0 S XX=
1.37E+00 1.02 E+00 3.39E 01 1.74047398 S YY=
2.06E 02 9.13E 01 1.14E 01
-0.91993583 S XY=
6.00E 01 1.48E 01 1.42E 02 0.61785373 M XX=
2.23E+00 2.01 E+00 4.52E 01 3.04095542 M YY=
7.95E 02 1.88E+00 5.36E 01 1.9602658 l
M XY=
7.45E 01 4.20E 02 5.39E 02 0.74802459 l
0 0
0 0
l P
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e fM EO( WitRNATKWAL SHEET NO. N A'[4 DATE NV'7 7 JOB NO.100031.01 JOB North Anna SSI Analysis of ISFSI Pad BY CALC, NO.100031C05R0 SUBJECT 3.kess Calculation CHKD D DATE 6ffik*I Plate NO 127 S XX=
1.41 E+00 1.05E400 3.33E 01 1.79006581 S YY.
3.00E 02 9.18E 01 1.12E 01 0.9248708 S XY.
6 41E 01 2.52E 01 1.48E 02 0.68906465 M XX=
2.17E+ 00 1.98E+00 5.26E 01' 2.98230481 M YY=
9.88E 02 1.90E+00 5.33 01 1.9787264 E
M XY=
7.48E 01 4.58E 02 5.31E 02 0.75128298 Plate NO= 128 0
0 0
0 S XX=
1.39E+00 1.27E+00 3 27E 01 1.90955882 S YY=
6,00E 02 1.24 E+ 00 1.29E 01 1.2500803 S XY=
6.88E 01 4.84E 01 4.74E 02 0.84215354 M XX.
2.13E400 3.02E+00 7.99E 01 3.77990271 M YY.
1.31E 01 3.78E+00 9.85E 01 3.90742931 M XY=
7.87E 01 1.51 E+00 4.33E 01 1.76049354 Plate NO= 1,19 0
0 0
0 S XX=
1.96E+00 1.37E+00 3.17E 01 2.41300502 S YY.
3.88E 02 1.22E+00 1.27E 01 1.23121383 S XY=
6.13E 01 3.57E 01 4.27E 02 0.71086815 2.22 +00 2.96E+00 8.39E 01 3.79644613 E
M XX=
M YY=
1.07E 01 3.79E+00 9.84E 01 3.91231001 M XY=
7.65E 01 1.55E+00 4.03E 01 1.77726707 Plate NO.130 0
0 0
0 S XX=
1.86E+00 1.27E+00 3.06E 01 2.27048617 S YY=
2.50E 02 8.94E 01 1.09E 01 0.90105328 8 XY=
5.80E 01 1.51E 01 1.68E 02 0.5995902 M XX=
2.22E+00 2.04E+00 5.05E 01 3.05906019 M YY=
7.62E 02 1.93E+00 5.30E 01 2.00284621 M XY=
7.49E 01 7.41E 02 5.45E 02 0,75492409 Plate NO.131 0
0 0
0 S XX=
1.90E+00 1.41 E+00 2.89E 01 2.38564805 S YY=
3.44E 02 8.93E 01 1.09E 01 0.89992564 S XY=
6.35E 01 2.08E 01 1.63E 02 0.66823988 M XX=
2.10E+ 00 2.03 E+00 4.41E 01 2.94971504 M YY=
1.01E 01 1.96E+00 5.27E 01 2.03301129 M XY=
7.75E 01 8.27E 02 6.26E 02 0.78180573 Plate NO= 132 0
0 0
0-S XX.
1.87E+ 00 1.75E+00 2.74E 01 2.57166898 S YY=
7.27E 02 1.21 E+00 1.29E 01 1.22302894 S XY.
6.83E 01 4.33E 01 5.2SE 02 0.80995252 M XX=
2.15E+00 3.09E+00 8.61E 01 3.8622836 M YY=
1.31E 01 3.88E+00 9.75E 01 4.00558954 M XY=
7.46E 01 1.58E+00 3.48E 01 1.78532973 0
0 0
0 C \\WORKWEPCocALCsc-os Doc
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o tot etwcam SHEET NO. b JOB NO.10003101 JOB North Anna SSI Analysis of ISFSI Pad BY Ob DATE NM7 CALC. NO.100031CMBQ. SUBJECT Stress Calculation CHK'O N DATE k 7 h Plate NO.133 S XX=
2.45E+ 00 1.86E+00 2.53E 01 3.08998532 i
S YY=
4.82E 02 1.19E+ 00 1.30E 01 1.20107101 0 XY=
5.86E Ot 3.96E 01 4.27E 02 0.70890197 4
i M XX=
2,12E+00 3.13E+00 7.55E 01 3.85033197 M YY=
1.16E 01 3.89E+00 9.73E 01 4.00756172 M XY=
7.80E 01 1.55E+00 4.73E 01 1.80092036 Plate NO= 134 0
0 0
0 S XX=
2.34E400 1.69E+00 2.36E 01 2.89093162 S YY=
2.23E 02 8.45E 01 1.15E 01 0.85267084 S XY.
5.57E 01 2.00E 01 2.18E 02 0.59205219 M XX.
2.18E+ 00 1.99E+00 5.96E 01 3.00977291 M YY=
8.44E 02 1.98E+00 5.20E 01 2.04588406 M XY=
7.71E 01 1.23E 01 6.47E 02 0.7831952
' Plate NO 135 0
0 0
0 S XX=
2.37E+00 1.72E+00 2.39E 01 2.93710357 S YY=
3.04E 02 8.29E 01 1.17E 01 0.83773801 S XY=
6.21E 01 1.20E 01 1.922 02 0.63349575 M XX=
2.14 E+00 2.04E+00 5 23E 01 2.99982481 M YY=
1.21E 01 1.99E+00 5.16E 01 2.05536588 M XY=
7.89E 01 1.32E 01 7.52E 02 0.80220038 Plate NO= 136 0
0 0
0 S XX=
2.34 E+ 00 2.01 E+00 2.50E 01 3.0952084 S YY.
7.93E 02 1.13E+00 1.35E 01 1.14083904 SXY.
6.70E 01 3.29E 01 5.5GE 02 0.74892971 M XX=
2.20E+00 3.14E+00 8.76E 01 3.92927141 M YY=
1.85E 01 3.91 E+00 9.62E 01 4.03372467 M XY=
7.76E 01 1.67E+00 3.73E 01 1.87623949 Plate NO= 137 0
0 0
0 l
S XX=
2.88E+ 00 1.9BE+00 2.46E 01 3.50386484 S YY=
5.26E 02 1.11 E+00 1.36E 01 1.11658732 S XY=
5.66E 01.
4.95E 01 4.74E 02 0.75326177 M XX=
2.01 E+00 3.29E400 7.73E 01 3.93346875 M YY.
1.64E 01 3.91 E+00 9.57E 01 4.02971062 M XY=
8.31E 01 1.45E+00 4.96E 01 1.74419287 Plate NO.138 0
0 0
0 SXX=
2.78E+ 00 1.67E+00 2.25E 01 3.24742837 S YY=
2.36E 02 7.45E 01 1.19E 01 0.75463457 S XY=
5.40E 01 3.02E 01 3.42E 02 0.6193941 M XX.
1.85E+00 1,68E+00 5.41E 01 2.55805414 i
M YY=
6.97E 02 1.96E+00 4.91E 01 -
2.02178889 M XY=
6.97E 01 1.75E 01 1.22E 01 0.72863352 0
0 0
0 C \\ WOR *GvEPCONCALCSiC 05 DOC s
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b SHEET NO.
job hb.100031.01 JOB North Anna SS1 Analysis of ISFSI Pad
_BY U+
DATE MW7 C ALC. ND. 100031C05R0 SUBJECT Stress Calculation CHK'D N DATEb IIIO t
Plate NO.139 1.55E+00 2.06E 01 3.25085599 l
S XX.
2.85E+00 S YY=
4.72E 02 7.03E 01 1.16E 01 0.71390146 8 XY.
6.29E 01 1.45E 01 1.92E 02 0.64587064 1.57E+00 5.94E 01 3.40197409 M XX=
2.96E+00 M YY.
1.87E 01 1.84 E+00 4.45E 01 1.9022333 -
M XY.
5.74E 01 1.74E 01 1.73E 01 0.62438109 Plate NO.140 0
0 0
0 1,64E+00 1.89E 01 3.32540515 S XX=
2.89E+ 00 S YY.
6.96E 02 9.37E 01 1.20E 01 0.94723505 SXY.
0.86E 01 1.43E 01 3.90E 02 0.70219831 M XX=
2.55E+00 3.16E+00 7.38E 01 4.12146437 M YY.
4.22E 01 3.49E+00 7.94E 01 3.60679138 1.43E+ 00 1.52E+00 4.38E 01 2.13167124 M XY=
Plate NO 141 0
0 0
0 S XX=
3.55E+00 1.35E+00 1.44E 01 3.79700747 S YY=
6.38E 02 9.11E 01 1.10E 01 0.92020734 S XY=
5.48E 01 6.39E 01 5.21E 02 0.84292221 1.02 +00 4.29185566 E
2.36E400 3.44 E+00 M XX=
M YY=
3.80E 01 3.40E+00 7.72E 01 3.50335752 1.38E+00 1.18E+00 5.27E 01 1.88949993 M XY=
:.. h""5 1d".
0 0
0 0
S XX=
3.48E+00 8.56E 01 1.39E 01 3.58744871 S YY=
7.39E 02 5.47E 01 8.44E 02 0.55877457 S XY=
4.91E 01 5.44E 01 3.70E 02 0.73344888 M XX=
3.03E+00 7.59E 01 2.86E-01 3.13195293 M YY=
2.08E 01 1.38E+00 3.58E 01 1.44166085 M XY=
1.14E 01 3.72E 01 4.16E 01 0.56975203 Plate NO= 143 0
0 0
0 S XX=
3.51 E+00 4.42E 01 1.53E 01 3.53896065 S YY=
8.30E 02 4.84E 01 7.70E 02 0.49717242 S XY=
5.22E 01 4.24E 01 2.91E 02 0.67336346 M XX=
6.50E 01 1.22E+00 3.45E 01 1.42209214 M YY=
2.11E 01 3.92E 01 1.73E 01 0.47728788 M XY=
6.98E 01 3.88E 01 3.55E 01 0.87380419 Plate NO.144 0
0 0
0 S XX=
3.35E+00 3.18E 01 1.52E 01 3.37250134 S YY=
6.66E 02 4.15E 01 6.12E 02 0.42484181 S XY=
4.55E 01 3.17E 01 1.91E 02 0.55505687 M XX=
3.83E 01 8.17E 01 3.59E 01 0.97126547 M YY=
1.94E 01 1.05E 01 1.19E 01 0.25012553 M XY=
5.84E 01 2.65E 01 2.60E 01 0.69167271 0
0 0
0 i
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tot WitPWsATONAL I. N SHEET NO. M JOB NO.10003101 JOB North Anna Ssl Analysis of ISFSI Pad BY M DATENW4"7 CALC. NO.100031COSRO SUBJECT Strass CCeulation CHK'D W DATEI2 i
Plate NO= 145 S XX.
3.14E+ 00 3.82 E-01 1.44E 01 3.16444371 S YY=
0.50E 62 3.68E 01 5.32E 02 0.37765061 8 XY=
4.24E 01 2.51E 01 1.50E 02 0.4929002 4
M XX.
4.82E 01 4.54E 01' 2.47E 01 0.70631974 M YY=
1.03E 01 4.02E 02 9.47E 02 0.14565392 M XY=
3.76E 01 1.75E 01 1.73E 01 0.44912728 Plate NO= 146 0
0 0
0 SXX=
2.92E+00 4.67E 01 1.33E 01 2.95816313 S YYu 6.65E 02 3.21E 01 4.97E 02 0.33155598 8 XY=
4.24E 01 2.02E 01 1.42E 02 0.46955976 M XX.
3.63E 01 2.41E 01 1.41E 01 0.45841707 M YY=
5.43E 02 3.07E 02 8.31E 02 0.10391482 M XY.
2.31E 01 1.26E 01 1.14E 01 0.28705827 Plate NO.147 0
0 0
0 S XX.
2.723+ 00 4.98E 01 1.18E 01 2.76482612 S YY=
6.49E 02 2.77E 01 4.60E 02 0.28839671 S XY.
4.41E 01 1,70E 01 1.47E 02 0.47271533 M XX=
2.64E 01 1.40E 01 8.71E 02 0.31102151 M YY.
3.31E 02 2.03E 02 7.59E 02 0.08683004 M XY=
1.36E 01 9.92E 02 8.13E 02 0.18670095 Plate NOu 148 0
0 0
0 S XX=
2.55E+00 4.98E 01 1.03E 01 2.59631393 S YY=
6,95E 02 2.40E 01 4.22E 02 0.25302242 S XY=
4.70E 01 1.44E 01 1.55E 02 0.49199263 M XX=
2.20E 01 9.50E 02 5.66E 02 0.2467473 M YY.
2.55E 02 2.31E 02 7.09E 02 0.07881094 M XY=
7.43E 02 8.18E 02 6.31E 02 0.12723352 Plate NO= 149 0
0 0
0 S XX=
2.40E+00 4.68E 01 B.77E 02 2.44966086 S YY.
7.63E 02 2.04E 01 3.84E 02 0.22154225 S XY=
5.09E 01 1.24E 01 1.65E 02 0.52422084 M XX.
2.22E 01 7.65E 02 6.14E 02 0.24252123 M YY=
2.18E 02 2.01E 02 6.75E 02 0.07370107 M XY= -
3.75E 02 6.72E 02 5.42E 02 0.09412161 Plate NO= 150 0
0 0
0 S XX=
2.28E+00 4.17E 01 7.39E 32 2.31599292 S YY=
8.77E 02 1.72E 01 3.54E 02 0.19665244 S XY=
5.53E 01 1.14E 01 1.74E 02 0.56471867 M XX=
2.37E 01 6.65E 02 8.62E 02 0.26118821 M YY=
1.99E 02 1.71E 02 6.52E 02 0.07024899 l
M XY=
2.49E 02 5.35E 02 5.00E 02 0.07733726 l
0 0
0 0
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101 f or witmtoat
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SHEdT NO.
JOB NO.100,03101 JOB North Anna SSI Anabis ofISFSI Pad BY M
DATE
.CHK'O N DATE N 2 D cal.C. NO. 100031COSR0 SUBJECT.gtress Calculation Plate NO= 151 3.58E 01
-6.06E 02 2.12614845 SXX=
2.10E*00 S YY=
1.17E 01 1.45E-01 3.34E 02 0.18908136 1.05E 01 1.81E 02 0.5843059 5.75E-01 3 XY=
5.30E-02 1.0$E 01 0.24127226 M XX=
2.11E 01 M YY=
1.90E 02 1.36E 02 6.30E-02 0.06718498 11XYa 1.84E 02 4.01E-02 4.51 E-02 0.06308629 Plate NO= *52 0
0 0
0 2.74 E-01 4.54E-02 1.67814112 S XX=
1.66E+ 00 1.59E 01 4.01E-02 0.57101267 S YYs 5.47E-01 1.14E 01 1.66E-02 0.37878553 S XYa.
3.91E 01 2.20E 02 5.30E 02 0.10569325 M4Xe
-8.88E 02 Mm 2.58E-02 1.04E 02 5.86E 02 0.06485186 MkW 1.45E-02 2 65E 02 3.20E-02 0.04402118 Beam 04 NODE 198 0
0 0
0 8.44E+ 00 3.00E+01 31.9480679 P 1(MAX)= (kip) 5.07E 01 P 2(MAX)= (kip) 5.26E+01 3.46E-01 5.49E 01 52.6040023 5.10E+01
-0.06E+00 51.3594201 P 3(MAX)= (kip) 2.05E-01 1.52E 01 2.19E 03 0.17292715 M 1(MAX)= (kip ft) 8.17E-02 M 2(MAX)= (kip ft) 2.23E+00 4 47E+02 6.55E+01 451.583947 M 3(MAX)= (kip ft) 4.29E+02 3.53E 70 5.87E+00 428.554724 NPDE231 0
0 0
0 P 1(M;V()=
5.07E-01 8.44E+00 3.06E+01 31.9480679 3 46E 01 5.49E 01 52.6040023 P 2(MAX)=
5.26E+01 P 3(MAX)=
2.05E 01 5.10E+01 dO6E+00 51.3594201 M 1(MAX)=
8.17E-02 1.52E 01 2.19E 03 0.17292715 M 2(MAX)=
5.78E 01 4.31E+01 1.70E+01 46.3647479 7.58E-01 1.35E+ 00 20.3985306 M 3(MAA)=
2.03E+01 Beam 65 NODE 203 0
0 0
0 8.57E+ 00 3.07E+01 31.8702039 P 1(MAX)=
9.93E 01 P 2(MAX)=
5.26E+01 7.22E 01
-1.35E+00 52.6223259 5.10E+01 5.87E+00 51.2997596 P 3(MAX)=
5.02E 01 M 1(MAX)=
8.14E 02 3.86E-01
-4.14E 03 0.3948068 M 2(MAX)=
5.47E+00 4 46E+02 6.35E+01 450.330168 M 3(MAX)=
4.35E+02 7.25E+ 00 1.40E+ 01 435.486039 NODE 232 0
0 0
0 P 1(MAX)=
9.93E 01 8.57E+00 3.07E+01 31.8702039 P 2(MAX)=
5.26E+01 7.22E-01 1.35E+00 52.6223259 P 3(MAX)=
5.02E 01 5.iOE+01 5.87E+00 51.2997596 M 1(MAX)=
8.14E 02 3.86E 01 4.14E 03 0.3948068 M 2(MAX)=
1,40E+00 4.36E+01 1.65E+01 46.6C66446 M 3(MAX)*
1.95E+01 1.61E+03 3.14 E+00 19.8568598 0
0 0
0 CAWORKWEPCOCALC5CMDOC s
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sos memnow SHEETNO, h k JOB NO.100031.01 JOB North Anna SSI Analysis of ISFSI Pad BY Mb DATE MW7' CALC. NO.100031C05R0 SUBJECT Stress Calculation CHKD N DATE klM i
Beam 66 NODE 208 P 1(MAX).
1.07E+00 8.78E+00 3.03E+01 31.535514 P 2(MAX)=
5.28E+01 7.05E 01 1.47E+ 00 52.8650838 P 3(MAX).
8.89E 01 5.14E+01 5.62E+00 51.7034809 I
M 1(MAX)=
748E 02 5.04E 01 4.11E 03 0.50980517 M 2(MAX).
9.52E+ 00 4.48E+02 6.07E401 451.79466 M 3(MAX).
4.58E+02 7.05E+00 1.73E+ 01 438.296662 NODE 233 0
0 0
0 I
l P 1(MAX)=
1.07E+00 8.78E+ 00 3.03E+01 31.535514 i'
P 2(MAX).
5.28E+01 7.05E 01 1.47E+00 52.8650838 P 3(MAX)=
8.89E 01 5.14E+01 5.62E+00 51.7034809 M 1(MAX)=
7.98E 02 5.04E 01 4.11E 03 0.50989517 M 2(MAX)=
2.51 E+00 4.44 E+01 1.58E+ 01 47.2218337 i
M 3(MAX)=
1.99E+01 1.57E+00 3.55E400 20.2359036 Beam 67 NODE 213 0
0 0
0 8.91 +00 2.98E+01 31.1599257 E
P 1(MAX).
1.31 E+00 1.49 +00 52.4584397 E
P 2(MAX)=
5.24E+01 8.68E 01 P 3(MAX)=
8.15E 01 5.27E+01 5.60E+00 53.0024317 M 1(MAX).
7.65E 02 5.36E 01 3.90E 03 0.54174267 M 2(MAX).
8.77E+00 4.59E+02 6.03E+01 462.530088 M 3(MAX).
4.34E+ 02 8.65E+00 1.50E+01 434.546198 NODE 234 0
0 0
0 P 1(MAX).
1.31 E+ 00 8.91 E+00 2.98E+ 01 31.1599257 P 2(MAX)=
5.24E+0t 8.68E 01 1.40E+00 52.4584397 i
P 3(MAX)=
8.15E 01 5.27E+01 S.60E+00 53.0024317 M 1(MAX).
7.65E 02 5.36E 01 3.90E 03 0.54174267 M 2(MAX)=
2.25E+00 4.49E+01 1.57E+ 01 47.6252056 M 3(MAX).
2.04 E+01 2.14E+ 00 3.26E+00 20.7204897 i
Beam 68 NODE 218 0
0 0
0 P 1(MAX).
1.54E+00 8.97E+00 2.97E+01 31.090197 P 2(MAX)=
5.20E+01 1.42E+00 1.49E+00 52.0004989 P 3(MAX).
7.85E 01 5.36E+01 5.82E+00 53.9606267 M 1(MAX).
7.37E 02 6.94E 01 5.21E 03 0.69811751 i
M 2(MAX).
8.52E+00 4.68E+02 6.29E+01 472.185798 M 3(MAX)=
4.29E+02 1.50E+01 1.56E+01 426.647802 NODE 235 0
0 0
0 P 1(MAX)=
1.54E+00 8.97E+00 2.97E+ 01 31.090197 P 2(MAX)=
5.20E+01 1.42E+00 1.49E+00 52.0004989 P 3(MAX).
7.85E 01 5.36E+01 5.82E+00 53.9606267 M 1(MAX)=
7.37E 02 6.94E 01 5.21E 03 0.69811751 I.
M 2(MAX)=
2.25E+00 4.38E+01 1.63E+ 01 46.8403374
. M 3(MAX)=
1.87E+01 3.89E+00 3.87E+ 00 19.4488556 0
0 0
0 i
i l
l C \\WORKWEPCO\\ CAL CSCOS D00 t
,.,. + -
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O fOf tor mswmm (B
SHEETNO. b JOB NO.100031.01 JOB North Anna SSI Analvsis of ISFSI Pad BY h1P 4 DATE D'Y 7 l
@ _DATE kl2N7 cal.C. NO.100031C05R0 SUBJECT Siress Calculation CHKD L
i Beam 69 NODE 223 P 1(MAX).
1.60E+ 00 8.55E+00 3.00E+01 31.2555757 l
P 2(MAX)=
5.00E401 2.44E+00 2.02E400 50.090001 P 3(MAX)=
2.09E+00 5.32E+ 01 0.10E+00 53.5892754 M 1(MAX)=
6.47E 02 1.02E+00 7.58E 03 1.02407524 M 2(MAX)=
2.28E+01 4.65E+02 6.59E+ 01 469.806818 M 3(MAX)=
4.09E402 2.58E+01 2.04E+01 410.719969 NODE 236 0
0 0
0 P 1(MAX).
1.60E+00 8.55E+00 3.00E+ 01 31.2555757 P 2(MAX).
5.00E+ 01 2.44 E+00 2.02E+00 50.090001 P 3(MAX)=
2.09E+00 5.325>01 6.10E+00 53.5892754 M 1(MAX).
6.47E 02 1.02E+00 7.58E 03 1.02407524 M 2(MAX)=
6.05E+00 4.13E+01 1.71 E+01 45.1551394 M 3(MAX).
1.83E+01 6.24E+00 5.31E+00 20.0117664 Beam 70 NODE 228 0
0 0
0 P 1(MAX)-
5.61E+00 6.54E+00 2.97E+01 30.9534286 P 2(MAX)=
5.52E+01 3.51 E+00 5.05E+00 55.5417291 P 3(MAX)=
3.26E400 5.09E+01 4.75E+00
$1.2252149 M 1(MAX)=
5.99E 0.
1.37E+00 1.37E 02 1.36738207 i
M 2(MAX)=
3.53E+01 4.38E+02 5.13E+01 442.407588 M 3(MAX).
4.67E+02 3.76E+01 5.34 E+01 471.143603 NODE 237 0
0 0
0 P 1(MAX)=
5.61 E+ 00 6.54E400 2.97E+ 01 30.9534286 P 2(MAX)=
5.52E+01 3.01 E+00 5.05E+00 55.5417291 P 3(MAX)=
3.26E+ 00 5.09E+01 4.75E+ 00 51.2252149 M 1(MAX)=
5.99E 02 1,37E400 1.37E 02 1.36738207 M 2(MAX)=
9.19E+ 00 3.81 E+01 1.33E +01 41.4159317 M 3(MAX).
3.53E+01 1.01 E+01 1.28E+01 38.844069 s
c %YOACVEPCOC ALCSic.05 DOC m
r_..,,
Mr. John MacCrimmon Virgin'a Power Nuclear Engineering May 16,1997 Attachment B:
Figures P StLt22tApa\\Nana3 Doc
+
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Rgure 2-7. Low Strain Sheer Wave Velocity 310
%s-300-t 295 - -------- --------.-------- --------.---
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.1 C 285 -
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o G. rt10 Figure 2-8. Low Strain P-Wave Velocity 4
310 sos.
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t,..arti Figure 4-1. High Strain P-Wave Velocity Profile 310 305- ------*---- -.- - - - - - -.-
300 _
295 -- - - - - - -. * - - - - -
=~----- - - - - - -
290 -
c 2&
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> 280 - - - - - - -.- - - - - - - - - - - - ------**----*-.******************-****-
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O u..et2 Figure 4-2. High Strain Sheer Wave Velocity Profile 310 305 -
3o0 _
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290---------
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c C 285 -
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o 280 -- - - - - - - - -. - - - - - - - -. - - - - - - - -. - - - - - - - -
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Figure 3-12. Node 233 - Shear Y Direction ~ 40-W ,e 6 M g 1% i 7l j a so V)I I i Nk pj e e ,e ze wi Page1
t W q :s 3 I c . qa e%hh O'y e $J 52 02 dao L la ix 5 A 1 3 + 3 1 2 e e e g e s a n d P o e u m N p T i 3 1-3 e 0 1 rug iF l. l, 0 0 5 5 0 5 9 7 4 0 8 2 2 k 2 2 2 1 6 ~
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~' cl. (4) Figure 3-17. Node 234 - Shear Y Direction 60 40 I-0- l h t 20 - ) l " ~ ~ l Ef 60 Q 0 5 10 15 20 25
m. f ) 7 ~ ~ NH"4 s2 o2 dao L la i x s A i 4 ) 1 5 3 c e ( 2 e g e s a d P o e l C m N iT 8 1 -3 o e i rug iF s o 5 o 5 8 9 7 1 2 2
il 1 j g j y y te fa l S f fo ro tca l F gn id 1 i e 1 g l g S l a P c 432 e d o N 9 1 -3 e ru O g iF ~ if a 7 e ~ l l 1
~ ch (2) Figure 3-20. Node 234-Overturning Factor of Safety 1 0.9 0.8 - 0.7 - 0.6 $~ l o 5 to 15 20 25 y Page 1
lO003\\- C-Oh I' > *) (py, l}-f& 6//l/9 ~7 ( c yr: Dw silth1 N O W C .9tie .h 7% Iii O z a w h-tb E ~ ~ g a 6 W-E A ~ ' o ~ ~ l Ei E - m _-am4ll=::== o 8 ? 8 Py 9 d >t Joeys i
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==# e .9 U W 8 o. -j o Z I Nh t . o e 3.9 u. u ~_ 8 ? 8 8 y g dog. Joeys ^
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~ Ct. (5) ~ Figure 3-23. Node 235-Axial Load ( 290 i 275 260 245
- pe je f f[
215 1- = D l g V 9: 200-D 0 hh 185 3 yN J 4 1 170 [ o 5 to 15 20 25 l Tim. - sec Page 1 + i
t. Figure 3-24. Node 235 - Sliding Factor of Safety 1.1 l 09-I 0.8 - i l a, I \\ g ~ l as i nG_; h$ 8: i T'k[5 0.3 x 02 j g. a f ~ a1 55 0 5 Time - sec l N Page1 g( I
..a-... a. _.... _ .a u____._-_.,-u.n _na- ___a-.s_,-_. a. us-_. - _, ~. -.__..s. ID 0031-C - 0 4 py. y A 6Jnn 1 eHg'. @ blnIV a 4 h ~ e OU F e --.amena l7 t h h e O
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~ Cl (3) Figure 3-26. Node 236 - Shear X Direction 60 40 i [ hfy' ej 47 at: lo ls o s 2o 2s Time - sec l Page 1
i) cts a l Figure 3-27. Node 236 - Shear Y Direction 60 40 [l Q pg j L g %g l-2o ?{' e io is 20 2s o s Time - see Page1
, q u - 1000 bl-O O Q y 1 T3ys r194 G//H 9 9 Cils t b7L, lo Itl93 4 0 { e .g L - w N ~ ~ W f R 0 ~ d z n + .&s o ~ g C h \\ _ m o b k k d y. lejry l ..g
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.l ct. (2) Figure 3-30. Node 236 - Overturning Factor of Safety l \\ 1 l l f 0.9 O.8 l i O.7 0.6 1 $ 0.5 l 0 10 16 ~ Time - sec Page 1 l I
Ci (3) Figure 3-31. Node 237 - Shear X Direction 60 i 40 20 -[ a
- h
-40 { 'j 3 e" l j 30 0 5 10 15 20 25 I Time - se: l Page 1 ( W'
.-. an -A s. a <m-.4 a >e u,..s .a-4__r.- A m m.w,be., nr c.,a~a D h.;a .e 1-=.r b L. .l ... m - se. x ~,_ 1 pa;s ajl o o s so is 2o 2s ? 'L
Cs (5) Figure 3-33. Node LT-Axial Load 290 27s j l 260-I rp 3% io is u e o s Time - sec Page1
Figure 3-34. Node 237 - Sliding Factor of Safety 0.9 i 0.8 0.7 -- l- -~ i } o s to is 20 2s Time - see Page 1 1-
Ct. (2) i Figure 3-35. Node 237 - Overturning Factor of Safety 1 l l OSo h i 0.6 t 0.7 - l 0.6 $5 r 0.4 3 '- Ol 8 l o.: jl 2 0.1 49( ma 9 I a d q , v. O 5 to 15 20 25 J G f '4 Tim. - see y Page1 i
4 EOE NfEMatsoMAL SHEET NO. 4 D DATEIAI/97 f JOB NO.10003i.01 JOB North Anna SSI Analysis of ISFSI Pad BY CHK'D N DATE b UM CALC. NO.100031005RO. SUBJECT Stress calculation Figure 21 Membrane Stresses and Bending Moments in Plate Elements i f / 'A%m L r \\ J / / t r s.s s, K \\N NruTEsd nEuper )- Y i o er S S,y Sy Mff Syf g.,, i ~~, i ~~. Srr Mye y N *
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,y ' uff N*w r / siv S,y s,y ,f gy r r scf - s,y e M,y..uy,. r BDiDN3 8TktsSES MEMMANE STRESSES Figure 2 2 Local Coordinate System for Forces and Moments, for Beam Elements f' (3) / ,/ (-x ) - 2 x s / / / / / .! / !/ 3(-Y) / / t C \\WOAeGVEPCOCALCSC oS DOC 4}}