ML18347A504

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Minimum Temperature of Multi-Assembly Sealed Basket (Msb) Shield Lid Plate After 20 Years and 50 Years.
ML18347A504
Person / Time
Site: Palisades Entergy icon.png
Issue date: 08/18/1995
From: Hoang P
Consumers Power Co
To:
Office of Nuclear Reactor Regulation
References
EA-SC-93-083-22
Download: ML18347A504 (69)
v • d • e


Text

MINIMUM TEMPERATURE OF MULTI-ASSEMBLY SEALED BASKET SHIELD LID PLATE AFTER 20 YEARS AND 50 YEARS .

REC'D W/1,TR DTD 9/29/95.*. ~9510060318

- NOTICE~

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THEY HAVE BEEN CHARGED TO YOU FOR A LIMITED TiME PERIOD AND MUST BE RETURNED TO THE RECORDS & ARCHIVES SERVICES SECTION, T5 C3. PLEASE DO NOT SEND DOCUMENTS CHARGED OUT THROUGH THE MAIL. REMOVAL OF ANY PAGE(S) FROM DOCUMENT FOR REPRODUCTION MUST BE REFERRED TO FILE PERSONNEL.

- NOTICE -

  • ATTACHMENT 1 CONSUMERS POWER COMPANY PALISADES PLANT DOCKET 50-255 MINIMUM TEMPERATURE OF MULTI-ASSEMBLY SEALED BASKET (MSB)

SHIELD LID PLATE AFTER 20 YEARS AND 50 YEARS

    • 69 Pages

miiu#S l'Hlllal PALIS ADES NUCLEAR PLANT EA-SC-93-083-22 ENGINEERING ANALYSIS COVER SHEET Total Number of Sheets t:.5 Minimum Tem12erature of MSB Shield Lid Plate After 20 years and 50 years INITIATION AND REVIEW Calculation Status Preliminary Pending Final Superseded D D Oll D Initiated InJt Review Method Technically Reviewed Revr ev Appd App CPCo

  1. Descripdon By Detail Qual d Appd By Date Alt Cale Review Test By Date By

~

P. Hoang 8/l819S e>-2..1-'tt 0 Original Issue

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  • PALIS ADES NUCLEAR PLANT EA-SC-93-083-22 ANALYSIS CONTINUATION SHEET Sheet _2_ Rev # 0 1.0 OBJECTIVE Reference/Comment The objective of this engineering analysis is to calculate the minimum temperature of Multi-Assembly Sealed Basket (MSB) shield lid plate of CMSB-01 through 04 after 20 years and 50 years of service when the ambient temperature is at 0°F. This analysis was performed to reinforce the 10°F movement restriction on CMSB-01 through 04.

1.1 BACKGROUND

Per the requirements of Section 1.2.13 of the Certificate of Compliance Number 1007 under 10CFR72, movement of a loaded MSB when it is inside the Ventilated Concrete Cask (VCC) is only permitted at an ambient temperature of 0°F or above. This limitation is based on the MSB shell material having a minimum Charpy impact energy of 15 ft-lbs at -50°F. The temperature limit for MSB movement, therefore, is established by adding a margin of 50°F to the above test temperature.

The MSB shield lid plate material of CMSB-01 through 04 was not initially considered to be a structural component by the vendor; therefore, a Charpy impact test was not required. Subsequent Charpy testing indicated that the shield lid plate material of the above CMSBs exhibited at least 15 ft-lbs of impact energy at a test temperature of -40°F. The minimum temperature at which the MSBs can be moved is 50°F above the Charpy test temperature of

-40°F. Based on the test data, the future movement of those CMSBs is limited to ambient temperature of 10°F or above to prevent brittle failure.

In this analysis, a calculation similar to those in Chapter 4 of the Safety Analysis Report (SAR) is performed to determine the minimum temperature of the MSB shield lid plate of CMSB-01 through 04 after 20 years and 50 years of operation and with ambient temperature of 0°F. The analysis will first calculate the decay fuel heat generation rate of all four loaded MSBs after 20 years and 50 years of operation.

The lowest heat generation rate case will be used in a thermal hydraulic analysis for MSB shell temperature distribution.

PALISADES NUCLEAR PLANT EA-SC-93-083-22 ANALYSIS CONTINUATION SHEET Sheet _3_ Rev # 0 2.0 ANALYSIS INPUT Reference/Comment 2.1 GOVERNING DESIGN PRINCIPLES AND DOCUMENTS 2.1.1 Safety Analysis Report (SAR) for the Ventilated Storage Cask System, PSN-91-001, Rev. O 2.1.2 Safety Evaluation Report (SER) for the SAR, dated April 28, 1993 2.1.3 NUREG/CR-2397, "Fuel Inventory and afterheat Powers Studies of Uranium-Fueled Pressurized Water Reactor Fuel Assemblies Using the SAS2 and ORIGEN S Modules of Scale with an ENDF/8-V Updated Cross section Library", September 1982.

2.1.4 ANSYS Computer Program and Users Manual Volume I & II, Version 4.4A 2.1.5 Procedure No 4.43, Attachment 6, Revision 3, 3A (Fuel Data) 1.6 E-HAR-94-01, Attachment 9 (Heat Load) 2.2 DESIGN DRAWINGS 2.2:1 MS8 Drawings Dwg. No.: VEN-C-136C:

Sht. 4, Rev. A Sht. 7, Rev. A Sht. 8, Rev. A Sht. 9, Rev. A 2.2.2 VCC Drawings Dwg. No.: VEN-C-1368, Sht. 2, Rev. 3A Sht. 3, Rev. 3A Sht. 4, Rev. 3A Sht. 5, Rev. 2A Sht. 6, Rev. 2A Sht. 7, Rev. 2A Sht. 8, Rev. 2A Sht. 9, Rev. 3A Sht. 11, Rev. 2A Sht. 12, Rev. 2A Sht. 13, Rev. 32A Sht. 14, Rev. OA

PALISADES NUCLEAR PLANT EA-SC-93-083-22 ANALYSIS CONTINUATION SHEET Sheet _4_ Rev # 0 2.3 EXISTING ANALYSIS Reference/Comment 2.3.1 E-SC-93-083-10, "Heat Transfer Analysis of the Ventilated Storage Cask (VSC)", Rev 0 2.4 REFERENCE 2.4.1 ANSYS 4.4 A Verification, E-CRW-91-03 2.4.2 ANSYS Verification Manual Version 4.4A 2.4.3 ANSYS Theoretical Manual Version 4.4.A 2.4.4 Graphics Supplement for ANSYS Revision 4.A on Personal Computers, Swanson Analysis Systems, Inc UpdO DN-G103:44A December 1, 1990 2.5 SOURCE DOCUMENTS

.1 Principles of Heat Transfer by Frank Kreith, Third Edition 2.6 PROCEDURES 2.6.1 FHS-M-32, "Loading and Placing the VSC Into Storage" 2.7 GEOMETRY AND MATERIALS The geometry and the materials used in the analysis were the same VSC model established in the Heat Transfer Analysis of the Ventilated Storage Cask (VSC) (Ref. 2.3.1) which is the same as the model used in SAR (Ref. 2.1.1 ).

2.8 PHYSICAL PROPERTIES All physical properties of the model are from the generic VSC model established for Heat Transfer Analysis of the Ventilated Storage Cask (Ref. 2.3.1 ). For 0°F ambient temperature, the density, thermal conductivity and specific heat of air were modified from the generic VCC model.

PALISADES NUCLEAR PLANT EA-SC-93-083-22 ANALYSIS CONTINUATION SHEET Sheet _5_ Rev # 0 2.9 HEAT GENERATION RATES Reference/Comment For the purpose of the calculation, the heat generation rates of CMSB-01, -02, -03 and -04 were calculated based on the "typical" tabulated data given the Appendix C of NUREG/CR-2397. The "conservative" data from the same reference was used in the SAR (Ref. 2.1.1 ).

2.10 AMBIENT TEMPERATURE Ambient temperature of 0°F is considered in the analysis.

3.0 ASSUMPTIONS 3.1 MAJOR ASSUMPTIONS None 3.2 MINOR ASSUMPTIONS The typical heat generation data given in the NUREG CR-2397 Appendix C is applied in this EA. This typical tabulated data may not be the lower bound of the heat generation. Nonetheless, the impact due to the variation of heat generation should not be of any significance.

3.2.2 The minor assumptions identified in the Heat Transfer Analysis of the VSC (Ref. 2.3.1) are applicable for this calculation.

4.0 ANALYSIS APPROACH 4.1 HEAT LOAD CALCULATION Afterheat power or heat generation rate of uranium-fueled PWR fuel computed by the SAS2/0RIGEN-S method for typical and conservative irradiation histories are provided in Appendix C of NUREG/CR-2397 (Ref. 2.1.3). A simple procedure for afterheat power calculation by linear interpolation of the tabulated data is also provided. (Pg. 71, Ref. 2.1.3). The conservative data in Appendix C of NUREG/CR-2397 was used in the SAR to calculate maximum heat load for the VSC-24 system. The typical data which provides lower heat rate is used for the purpose of calculating the minimum temperature of the MSB shield lid plate.

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~...-. .. PALISADES NUCLEAR PLANT ANALYSIS CONTINUATION SHEET EA-SC-93-083-22 Sheet _6_ Rev # 0 4.2 THERMAL HYDRAULIC CALCULATION Reference/Comment The dry spent fuel assemblies inside the MSB generate heat that is transferred to the MSB outer shell. When the MSB is placed inside a VCC, heat from the MSB shell is convected to the air in the gap between the MSB shell and the VCC inner liner, and radiated to the VCC internal liner. The heat from the VCC internal liner is also convected to the air and a small amount is conducted through the VCC shell to the exterior. The heated air in the gap between the MSB shell and VCC inner liner rises and exits through the top vents and is replaced by the 0°F ambient air entering through the bottom vents (natural convection).

On a sunny day additional heat enters the exterior surfaces of the VCC as solar radiation and is convected and radiated to the environment from the VCC surfaces. However, for the purpose of this EA, the solar energy is conservatively neglected.

5.0 ANALYSIS

.1 HEAT LOAD CALCULATION The detailed heat load calculation is provided in Attachment A*and the following is a summary of the Analysis.

5.1.1 Heat Load Curve for a Lower Bound Burnup Value The burnup value of some fuel cells is lower than the range of burnup value given in the tabulated data of Appendix C of NUREG/CR-2397.

However, a plot of afterheat power as a function of bumup (Figure A.1 , Attachment A of this report) shows that the heat load is nearly linear with respe_ct to the burnup when the burnup level is low.

Therefore, an approximate data for a lower bound burnup value of 1O GWD/MTU could be generated by a linear extrapolation. Plots of afterheat curves of many burnup levels are shown in Figure A.2 of Attachment A of this report 5.1.2 Heat Load Rate lnteroolation Functions for a Given Burnup Value at a Given Time A two dimensional (burnup and time) linear interpolation function for the above afterheat power data is setup using a MATHCAD linear interpolation function. The function KW(t,b)in the attachment A is the afterheat powers of burnup level b (GWD/MTU) at time t (days).

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~~ Im' PALISADES NUCLEAR PLANT EA-SC-93-083-22 ANALYSIS CONTINUATION SHEET Sheet _7_ Rev # 0 5.1.3 Check the Heat Load Rate Interpolation Functions Against the Input Reference/Comment Data A check for the heat load rate function KW(t,b) with the input data was performed in section 4.0 of the Attachment A to verify that the interpolation function reproduces the data given in Appendices C of NUREG/CR-2397. The result indicates that the interpolation function successfully reproduce the input data.

5.1.4 Check the Heat Load Rate Interpolation Functions With the Heat Load of CMBS-04 Provided in Reference 2.1.5 Heat load 'of CMSB-04 calculated in Reference 2.1.6 is 9.34 KW. This value was based on the conservative data in the Appendix C of NUREG/CR-2397. The total heat load of CMSB-04 calculated in Section A.5 of Attachment A using the interpolation function KW(t,b) is 9.023 KW. The total calculated heat load is 3.8% lower than the total heat load reported in Reference 2.1.6. The deviation is the about the same deviation of the "typical" and "conservative" data in NUREG/CR 2397, Table C.2, Case 3 at cooling time=10 years. This result is an additional validation of the interpolation function.

5.1.5 Heat Generation Rate Calculation Fuel data of each fuel cell of each loaded CMSB is available in Reference 2.1.5 and is included in the Attachment B of this EA.

Data used in heat generation rate calculation includes:

Initial weight of Uranium (MTU)

Bum-up (MWD/MTU)

Discharge date MSB loading date The total cooling time t (day) is the sum of time from the fuel bundle discharge date to the date of loading into MSB plus the storage time period of 20 years and 50 years.

The evaluation period of 20 years and 50 years are based on the minimum design life requirements specified in 10CFR72,236(g) and the design life stated in SAR, respectively.

The total cooling time t (day) and the,burn-up b (MWD/MTU) are substituted into the interpolation function KW (t,b) to obtain the afterheat power per unit weight of Uranium. The heat generation rate for each cell is the afterheat power times the initial -Uranium weight

emwn* &ii PALISADES NUCLEAR PLANT ANALYSIS CONTINUATION SHEIT EA-SC-93-083-22 Sheet _8_ Rev # 0 and converted to Kilowatt. The total heat generation is the sum of Reference/Comment heat generation of each of 24 cells of the MSB.

From the fuel data in Attachment B, the total heat load of CMSB-03 is the lowest heat rate of the four CMSBs. The total heat generation rates of CMBS-03 and -04 after 20 years and 50 years in storage are calculated and presented in Tables A.1 through A.4 respectively. The result shows that CMSB-03 has the lowest heat generation rate which is 5.97 KW and 3.883 KW after 20 years and 50 years of storage respectively.

Therefore, the case of CMSB-03 will be analyzed to determine the lowest temperature of the MSB shield lid plate subjected to 0°F ambient temperature.

5.2 THERMAL HYDRAULIC CALCULATION 5.2.1 Analysis Models A detailed description of the heat transfer mechanism inside a MSBNCC assembly (VSC-Ventilated Storage Cask}, applicable heat transfer models and the governing equations are included in the SAR Section 4.4.1 (Ref. 2.1.1 ). The SAR Figure 1.1.1 (Ref. 2.1.1) illustrates the VSC and its components.

The MSB contains dry fuel assemblies that generates heat which is transferred to the MSB shell. The heat from the MSB shell is transferred to the air in the gap between the MSB Shell and the concrete cask liner, and to the concrete cask. The hot air in the gap between the MSB shell and the concrete cask liner rises and exits through the aif outlet at the top and is replaced by the air entering at the bottom air inlet duct. Most of the heat is transferred to the environment by the* above natural convection and a small amount is transferred through the concrete cask.

The heat rate generated by the fuel inside the MSB, any applicable solar radiation, ambient temperature and temperature of the air flowing through the gap between the MSB shell and the concrete cask liner are the main parameters affecting the temperature distribution in the MSB and the VCC. The air temperature in the gap at various elevations is a function of the heat generation rate, the ambient temperature and the convective mass flow rate. The mass flow rate is dependant on the amount of heat removed by natural convection, the flow resistance ill the natural convection flow path

PALISADES NUCLEAR PLANT EA-SC-93-083-22 ANALYSIS CONTINUATION SHEET Sheet _9_ Rev # 0 and the ambient temperature. The relationship among the above Reference/Comment variables is defined the SAR Equation 4.1 (Ref. 2.1.1, Section 4.4.1.1 ).

5.2.2 Convective Air Flow and Temperature Calculations The air flow up the annular gap between the MSB shell and the VCC inner liner is calculated by determining the sum of the flow pressure losses due to all entrances, bends, straight sections, expansions, contractions and exits and equating to the pressure differential caused by heating the air( i.e. stack or furnace effect). The governing equations are defined in the SAR Section 4.4.1.1 (Ref. 2.1.1 ). The equation can be iteratively solved by assuming a VCC air outlet temperature and checking to see whether the left hand side of SAR Equation 4.2 (stack pressure) is equal to the right hand side (flow pressure loss): If the left hand side is lower, then the assumed outlet temperature should be increased and if it is higher then the outlet temperature should be reduced. Once the value of air outlet temperature is determined, the air mass flow rate and the air temperature at various elevations of the annular air gap can be easily calculated. Attachment C of Reference 2.1.2 contains the details of the calculation procedure. The final iteration of the air flow and temperature calculation is included in the VCC Body and MSB Exterior Thermal Model discussed below.

5.2.3 VCC Body and MSB Exterior Thermal Model The heat transfer model of the VSC (including the simplified model of the MSB) is explained in the SAR Section 4.4.1.2 (Ref. 2.1.1 ). The heat transfer analysis of the VSC is performed using the ANSYS computer program and the applicable VSC ANSYS Thermal Model is shown on the SAR Figure 4.4-2 (Ref. 2.1.1 ).

The generic ANSYS input data for the above model and the instructions for using the ANSYS model for performing a thermal analysis of the VSC is included in Attachment D of Reference 2.3.1.

The above can be* used to perform a steady state or transient analysis of the VSC. The final iteration of the Convective Air Flow and Temperature Calculations, similar to those in References 2.3.1 is also included in the ANSYS model. Therefore there is no need for a separate spread sheet calculations to document the convective air flow and bulk air temperature calculations.

The ambient temperature, the MSB heat generation rates at the end of 20 years and 50 years of storage, air flow loss coefficient, average specific heat of air (CPAI), average air density(DENA) and the

PALISADES NUCLEAR PLANT EA-SC-93-083-22 ANALYSIS CONTINUATION SHEET Sheet 10 Rev# 0 assumed VCC outlet air temperature (TOAS) are the input to this Reference/Comment ANSYS input deck. The ANSYS output must be reviewed to ensure that the flow pressure loss (DP FLOW) is equal to the pressure change due to air heating (DP STACK) and that the calculated air outlet temperature (TOCA) matches to the assumed value (TOAS).

The formulas for average specific heat (CPAI) and average density (DENA) are modified to the air properties at 0°F. The temperature distribution in the VCC and the MSB shell outside surface are the output from this analysis.

5.2.4 Computer Input Deck The ANSYS thermal hydraulic analysis for a VSC is performed in two parts.

They are:

1. the iterative air flow calculations for determining the air mass flow rate and bulk air temperatures,
2. the computer analysis of MSBNCC using the ANSYS program.

The iterative air flow calculations are explained in Attachment C of EA-SC-93-83-10 (Ref. 2.3.1). The calculations are used to calculate the assumed value of the VCC air outlet temperature for input into the VCC ANSYS Model. The applicable formulas are included in the VCC ANSYS model. However, ANSYS program cannot perform the iterative calculations. The air flow calculations should be manually performed to calculate the value of the VCC air outlet temperature and the value should be input into the VCC ANSYS model. The VCC ANSYS analysis documents the final iteration of the air flow calculation and therefore there is no need to document the air flow calculations ~eparately.

The ANSYS computer model of the VCC includes the final iteration of the air flow calculation is provided in Attachment C of this EA (File MSB3-20 and MSB3-50 dated 08/02/95). These two files are modified from the generic model provided in Attachment C of Reference 2.3.1.

The modification includes:

The heat generation rates

- 5.97 KW for MSB-03 after 20 years of storage

- 3.885 KW for MSB-03 after 50 years of storage

PALISADES NUCLEAR PLANT EA-SC-93-083-22 ANALYSIS CONTINUATION SHEET Sheet 11 Rev # 0 and the following air properties which are applicable for 0°F ambient Reference/Comment condition:

- Air specific heat CPAI = 0.239

- Air density: DENA= 0.081+ 0.005*(32-TAKE)/32 These values are from SAR (Ref. 2.1.1, page 4-5 )

5.3 ANALYSIS PERFORMED The steady state thermal analysis of a loaded VSC was performed for the combinations of following operating conditions:

a. Heat Gen. 5.97 KW, Amb O °F, No Solar Load
b. Heat Gen. 3.885 KW, Amb O °F, No Solar Load 5.3.1 List of Computer Input Files Computer Input Files (No File Extension)
  • Input Name Date Analysis Description MSB3-20 08/02/95 Heat Gen. 5.97 KW, Amb o °F MSB3-50 08/02/95 Heat Gen. 3.885 KW, Amb o °F 5.3.2 List of Computer Output Files Table 5.3.2 Computer Output Files Output Name . Date Analysis Description MSB3-20.0UT 08/02/95 Heat Gen. 5.97 KW, Amb o °F MSB3-50.0UT 08/02/95 Heat Gen. 3.883 KW, Amb o °F 5.3.3 Summary of MSB Shell Temperatures The steady state temperature distribution of the MSB shell outside surface are included in the computer output files listed in Section 5.3.2 (Attachment D of this E). The temperature distribution resulted from the above analyses is presented in Figure 1 and 2.

The lowest temperature of the MSB shield lid is 22°F after 20 years and 16°F after 50 years when the ambient temperature is 0°F.

'I

PALISADES NUCLEAR PLANT EA-SC-93-083-22 ANALYSIS CONTINUATION SHEET Sheet 12 Rev# 0 5.3.4 Warning Massages Reference/Comment The ANSYS/PREP contain warning messages related to the shape of the Element No. 29 which represents the gap between the MSB bottom plate and the fuel assembly. The effect of these warning messages, if there is any, should only pertain to the Element 29.

These warning messages have been reviewed and determined to be inconsequential to the results of this EA. There should be no impact on the predicted temperature of the shield lid.

6.0 RESULTS AND CONCLUSIONS CMSB-03 had the lowest heat generation rates among CMSB-01 through CMSB-04. The heat generation rates were 5.97KW and 3.883KW after 20 years and 50 years in storage with 0°F ambient temperature.

The result of the ANSYS thermal hydraulic analysis indicates that the lowest temperature of the MSB shield lid plate is 22°F for the case of 20 years and 16°F for the case of 50 years of storage.

The typical tabulated data used in this analysis may not be the lower bound of the heat generation. As stated in Subsection 5.1.3, the deviation of the "typical" and "conservative" data in NUREG/CR2397 is about 3.8%. The lower bound of heat generation and the lowest temperature of the MSB shield lid plate can be predicted by using the deviation between the typical and conservative (3.8%). The impact due to the variation of the heat load data presented in NUREG/CR2397 is not significant.

/1~JS/5 VCC THERMAL CHARACTERISTICS FOR S-* 11 KW HEAT LOAD {v.sc.:#- jJ R.~Jut..IS A,'ok: VSC:tl 3;  !>.<t1 kW MTEfl.. 2D fars .

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EA-SC-93-083-22 Attachment A Rev. : 0 Page Al Attachment A

( 13 pages )

HEAT GENERATION RATE CALCULATION

EA-SC-93-083-22 ATTACHMENT A PAGE 1 File Name: NUREG.MCD

.SPENT FUEL HEAT LOAD CURVES

,Spent fuel heat load curves are generated using the interpolation methodology given in NUREG/CR-2397

,- The typical" tabulated data given in the Appendix C of NUREG/CR-2397 was used because it results in a best estimate head load which is appropriate for the purpose of calculating the minimum temperature after 20 years and 50 years of storage.

,1.0 Input data :

6 6 6 6 6 6 2.222* 10 2.165* 10 2.173* 10 2.17* 10 2.149* 10 2.102*10 71832 77597 80557 83617 86349 90862 40350 44554 46852 49271 51423 54968 26867 30426 32266 34269 36151 39312

  • ,pp.=

20814 17019 12243 6338.7 3100.4 24126 20171 15124 8504.7 4418.8 25750 21648 16388 9406.4 5017.8 27546 23301 17831 10470 5748 29293 24953 19333 11630 6542.7 32283 27834 22027 13807 8079.6 980.81 1552.7 1893.9 2323.7 2770.8 3643.7 619.51 987.03 1233.4 1542.1 1849.7 2437.2 481.62 759.66 948.34 1183. l 1409.6 1817 404.01 637.04 792.48 985.62 1168.4 1477.8 345.29 545.53 676.02 838.29 989.94 1232. l 298.65 473.41 584.4 722.78 851.01 1045

,i:=O .. (rows(pp)-1) 261.07 415.52 511.03 630.52 740.68 899.42 j := 0 .. (cols(pp) - 1) 230.62 368.66 451.74 556.l 652.07 784.54

EA-SC-93-083-22 ATIACHMENTA

  • PAGE2 File Name: NUREG.MCD

.Bum-up level data:

.RL T,,;, ( 18 27 33 40 46 55 )

.Time interval data:

,m:= O.. (rows(pp)- 1) .n = 0 .. (cols(pp)"' 1) 2.0 Linear extrapolation to obtain the afterheat power for bum-up level of 10 GWD/MTU

  • 2000

.n := 0 .. 5 .m := 11

/

/

1500 v

/

~

v

~

J/~

soo ..,

0 lS 20 2S 30 3S 40 4S so SS Bumup (GWD/MTIJ)

  • Figure A.1 Plot of Power Level VS. Bumup at time 20 years

EA-SC-93-083-22 ATTACHMENT A PAGE3 r-11e N -*11e: NI '~EG.MCD The power level is linearly proportional to the burnup level in the lower range of burnup.

Therefore, linear extrapolation to obtain the power level for burnup level 10 GWD/MTU is permissible.

~p T) 1

<"> ]

H.I : =linte11' [ RL, , 10 Insert the extrapolation values to the power matrix pp pp : =augment( H, pp)

Update burn-up level data:

RLT=(lO 18 27 33 40 46 55)

EA-SC-93-083-22 ATTACHMENT A PAGE4 File Name: NUREG.MCD 3.0 Plot the afterheat power curves i := 0 .. (rows( pp) - l) j .=O .. (cols(pp)- l)

DRY CASK HEAT LOAD CURVES I\\

\\\I"'-.

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1000

\'~ t:::-===::::::: ~ ~ ,..__ __

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~

~

r-

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...-- ...A 100 5000 u*104 2.s*10 4 3*104 Time (days)

-+- lOGWD/MTU 18GWD/MTU 27 GWD/MTU

-+- 33 GWD/MTU 40GWD/MTU 46GWD/MTU

-e- SSGWD/MTU Figure A.2 Power Level curves 4.0 Set up a two dimensional interpolation function using linear interpolation in time and linear interpolation for logarithmic afterheat power values p ... =In(pp.1,J*)

l,J logarithmic value of afterheat power matrix Linear interpolation in bumup

  • n :=O, l.. 30 Setup burn up interval from 10 to 45 GWD/MTU

EA-SC-93-083-22 ATIACHMENTA PAGES File Name: NUREG.MCD linterp [ RL, ~

- ]

-Kn, i = T) ,B 0 Linear interpolation function for decay time

.The afterheat power curves as a function of time and bumup T)<round(b- 10)> ]]

.Kw(t,b) =exp [ linterp [ RC, ( K ,t

.round(x) =if(x - floor(x)<.5, floor(x), ceil(x))

,t = 0,500 .. 50*365 HEAT LOAD CURVES

  • Kw(t, 10)

~ Kw(t, 18)

~-

~ Kw(t,27) j Kw(t,33) 1*10 4

\\\

\\\.

~\ t.\

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~-+-

i:: Kw(t,40) 1000

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\

~

u

~  : A~

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- - -V"V 100 .4 .4 .4 sooo 1*10 l.5* 10 t

Time in days

-+- lOGWD/MTU

- 18GWD/MTU

- 27GWD/MTU

-+- 33 GWD/MTU

- 40GWD/MTU Figure A.3 Plot of interpolation function KW(t,b)

EA-SC-93-083-22 ATTACHMENT A PAGES File Name: NUREG.MCD 5.0 Check the interpolation NUREG-3697 Appendix C Kw(20*365, 18) =481.62 PPu, 1 = 481.62 OK Kw(20*365,27) = 759.66 pp 11 = 759.66 OK 2

Kw(20*365, 33) = 948.34 PPu, 3 = 948.34 OK 3 3 Kw(10-365,40) = 1.542* 10 pp 10 , 4 =1.542*10 OK 6.0 Comparison of heat load calculation for VCC Number 4 (Loading date: 6/21/94) i =0 .. 23 LoadMonth := 6 Load.Day := 21 LoadYear := 94

  • Cooling time prior to loading numday(month,day,year) :=(LoadMonth- month)*30+Load.Day- day+ (LoadYear-year)*365 time.l :=numday(DDate.l, 0 ,DDate.l, 1 ,DDate.l, 2)

Heat load per cell on loading Kw(time.,BurnUp.)*Initial 1 1 U.1 HeatLoad. * - -

I 1000

  • . i

EA-SC-93-083-22 ATIACHMENTA PAGE7 File Name: NUREG.MCD Discharge Date

,Cell Wt(MTU) ~MWD/MTU) ,Cooling Time ~KW)

.month Day ,Year (Days)

,i + 1 ,Initial_U i .DDatei,O .DDatei, l .DDatei 2 ,timei JieatLoadi 0.415 30.26 8 29 81 4677 0.425 2 0.415 33.027 8 29 81 4677 0.475 3 0.415 33.027 8 29 81 4677 0.475 4 0.387 35.117 8 12 83 3964 0.497 5 0.4 12.99 6 78 6005 0.133 6 0.386 35.333 8 29 81 4677 0.471 7 0.385 35.333 8 29 81 4677 0.47 8 0.387 31.414 8 12 83 3964 0.433 9 0.402 13.366 6 78 6005 0.134 IO 0.402 13.911 6 78 6005 0.147 11 0.401 12.99 6 78 6005 0.134 12 0.416 28.128 8 29 81 4677 0.396 13 0.416 28.824 8 29 81 4677 0.411 14 0.387 35.117 8 12 83 3964 0.497 15 0.402 13.626 6 78 6005 0.147 16 0.401 13.626 6 78 6005 0.147 17 0.387 35.117 8 12 83 3964 0.497 18 0.415 30.26 8 29 81 4677 0.425 19 0.416 28.128 8 29 81 4677 0.396 20 0.386 35.173 8 12 83 3964 0.496 21 0.387 35.173 8 12 83 3964 0.497 22 0.416 33.027 8 29 81 4677 0.477 23 0.416 30.26 8 29 81 4677 0.426 24 0.415 30.353 8 29 81 4677 0.425 23

.Total Heat Load

,TotalHeat := L HeatLoadi i=O

,TotalHeat = 9.034 Kw

.The total heat load for MSB-04 calculated in EA-HAR-94-01, Attachment 9 is 9.38. The deviation of the two calculated value is (9.38-9.034) / 9.034= 3.8%. Note that the conservative data from Appendix C of NUREG/CR-2397 was used in EA-HAR-94-01. The above deviation is in the magnitude of percent difference between conservative and typical data in NUREG/CR,. 2397, Table C.2, case 3, 10 years cooling time. Therefore, the heat load calculation is verified .

EA-SC-93-083-22 ATIACHMENTA PAGES File Name: NUREG.MCD

,7 .0 Heat load *after 20 years in storage for VCC number 3

,timei *= timei + 20* 365 Kw(time.1 ,BumUp.)*Initial 1

U.1 JleatLoad.  := - - -- - -- - - -

I 1000

,Table A. 1 Heat Load of MSB-3 after 20 years in storage Discharge Date

,Cell ,Wt(MTU) ~MWD/MTU) month Day ,Year

.Cooling Time ~KW)

(Days)

.i + l Jnitial_Ui  !>Date.l, 0 DDate.1, 1 DDatei,l ,timei JleatLoadi 0.415 30.26 8 29 81 11977 0.282 2 0.415 33.027 8 29 81 11977 0.314 3 0.415 33.027 8 29 81 11977 0.314 4 0.387 35.117 8 12 83 11264 0.322 5 0.4 12.99 1 6 78 13305 0.093 6 0.386 35.333 8 29 81 11977 0.311 7 0.385 35.333 8 29 81 11977 0.31 8 0.387 31.414 8 12 83 11264 0.281 9 0.402 13.366 6 78 13305 0.093 10 0.402 13.911 6 78 13305 0.102 11 0.401 12.99 1 6 78 13305 0.093 12 0.416 28.128 8 29 81 11977 0.263 13 0.416 28.824 8 29 81 11977 0.273 14 0.387 35.117 8 12 83 11264 0.322 15 0.402 13.626 1 6 78 13305 0.102 16 0.401 13.626 l 6 78 13305 0.102 17 0.387 35.117 8 12 83 11264 0.322 18 0.415: 30.26 8 29 81 11977 0.282 19 0.4'16' 28.128 8 29 81 11977 0.263 20 0.386 35.173 8 12 83 11264 0.321 21 0.387 35.173 8 12 83 11264 0.322 22 0.416 33.027 8 29 81 11977 0.315 23 0.416 30.26 8 29 81 11977 0.283 24 0.415 30.353 8 29 81 11977 0.282

EA-SC-93-083-22 ATTACHMENT A PAGE9

  • Total Heat Load after 20 years Tota!Heat :=

I:

i=

23 Tota!Heat = 5.97 0

HeatLoad.I Kw File Name: NUREG.MCD 8.0 Heat load after 50 years in storage for MSB number 3 time. :=time.+ 30-365 I I Kw(time.,BumUp.)*Initial 1 1 U.1 HeatLoad. := -

I 1000 Table A.2 Heat Load of MSB-3 after 50 years in storage Discharge Date Cell Wt(MTU) (MWDIMTU) Cooling Time (KW) month Day Year (Days) i+1 Initial- U.I BumUp.I DDate.I, 0 DDate. 1 DDate. 2 time.I HeatLoad.I I, I, 0.415 30.26 8 29 81 22927 0.185

  • 2 3

4 5

6 7

0.415 0.415 0.387 0.4 0.386 0.385 33.027 33.027 35.117 12.99 35.333 35.333 8

8 8

8 8

29 29 12 6

29 29 81 81 83 78 81 81 22927 22927 22214 24255 22927 22927 0.205 0.205 0.208 0.06 0.202 0.202 8 0.387 31.414 8 12 83 22214 0.183 9 0.402 13.366 6 78 24255 0.06 10 0.402 13.911 6 78 24255 0.066 11 0.401 12.99 6 78 24255 0.06 12 0.416 28.128 8 29 81 22927 0.173 13 0.416 28.824 8 29 81 22927 0.179 14 0.387 35.117 8 12 83 22214 0.208 15 0.402 13.626 . 1 6 78 24255 0.066 16 0.401 13.626 6 78 24255 0.066 17 0.387' 35;117 8 12 83 22214 0.208 18 0.415 30.26 8 29 81 22927 0.185 19 0.416 28.128 8 29 81 22927 0.173 20 0.386 35.173 8 12 83 22214 0.207 21 0.387 35.173 8 12 83 22214 0.208 22 0.416 33.027 8 29 81 22927 0.205 23 0.416 30.26 8 29 81 22927 0.185 24 0.415 30.353 8 29 81 22927 0.185

r * - -:-93-083-22

." ' ' '\CHMENT A PAGE10

  • Total Heat Load after 50 years Totillleat - L 23 i=0 HeatLoad.l File Name.: NUREG.MCD Total.Heat = 3.885 Kw 9.0 Heat load after 20 years in storage for MSB number 4 dd : =READPRN( rnsbn4)

.. dd<o> dd<l>

Initial U :=- - BUi:nUp :=- -

- 106 1000

<o> <2>

DDate  :=dd DDate<2> :=dd<4>

time.l :=num.day(DDate.l, 0 ,DDate.l, 1,DDate.1, 2) + 20*365

  • Heat load per cell an loading HeatLoad. :=

l Kw(time.,BumUp.)*Initial 1

1000 1

U.1

EA-SC-93-083-22 A TTAC HM ENT A PAGE 11 File Name: NUREG.MCD Table A.3 Heat Load of MSB-4 after 20 years in storage Discharge Date Cell Wt(MTU) (MWD/MTU) Cooling Time (KW) month Day Year (Days) i+ 1 Initial- U.I BurnUp. DDate.I, 0 DDate.I, 1 DDate. time. HeatLoad.l I l, 2 I 0.415 30.343 8 29 81 11977 0.282 2 0.415 30.26 8 29 81 11977 0.282 3 0.416 30.585 8 29 81 11977 0.293 4 0.387 35.117 8 12 83 11264 0.322 5 0.402 13.626 1 6 78 13305 0.102 6 0.416 30.585 8 29 81 11977 0.293 7 0.415 30.343 8 29 81 11977 0.282 8 0.387 35.117 8 12 83 11264 0.322 9 0.401 13.626 6 78 13305 0.102 10 0.404 13.366 6 78 13305 0.094 11 0.401 13.11 6 78 13305 0.093 12 0.415 30.353 8 29 81 11977 0.282 13 14 0.414 0.388 33.629 33.517 8

8 29 12 81 83 -11977 11264 0.324 0.313 15 0.401 13.366 6 78 13305 0.093 16 0.387 35.333 8 29 81 11977 0.312 17 0.387 34.93 8 12 83 11264 0.322 18 0.415 33.629 8 29 81 11977 0.324 19 0.415 31.787 8 29 81 11977 0.303 20 0.387 33.517 8 12 83 11264 0.312 21 0.387 35.173 8 12 83 11264 0.322 22 0.415 30.26 8 29 81 11977 0.282 23 0.416 30.26 8 29 81 11977 0.283 24 0.401 12.99 6 78 13305 0.093 23 Total Heat Load after 20 years TotalHeat :=

L i= 0 HeatLoad.I TotalHeat =6.035 Kw

EA-SC-93-a83-22 ATIACHMENTA PAGE12 File Name: NUREG.MCD 1a.a Heat load after 50 years in storage for MSB number 4 time.l :=nwnday(DDate.1, 0 ,DDate.l, 1 ,DDate.l, 2 ) + 50*365 Heat load per cell on loading Kw(time.,1 BurnUp.)*

1 Initial U.1 HeatLoad. := -

I 1000 Table A.4 Heat Load of MSB-4 after sa years in storage Discharge Date Cell Wt(MTU) (MWD/MTU) Cooling Time (KW) month Day Year (Days) i+ l Initial- U.I BurnUp.I DDate.1, 0 DDate.I, 1 DDate.1, 2 time.I HeatLoad.I 0.415 30.343 8 29 81 22927 0.185 2 0.415 30.26 8 29 81 22927 0.185 3 0.416 30.585 8 29 81 22927 0.192 4 0.387 35.117 8 12 83 22214 0.208 5 0.402 13.626 1 6 78 24255 0.066 6 0.416 30.585 8 29 81 22927 0.192 7 0.415 30.343 8 29 81 22927 0.185 8 0.387 35.117 8 12 83 22214 0.208 9 0.401 13.626 l 6 78 24255 0.066 10 0.404 13.366 1 6 78 24255 0.061 11 0.401 13.11 1 6 78 24255 0.06 12 0.415 30.353 8 29 81 22927 0.185 13 0.414 33.629 8 29 81 22927 0.211 14 0.388 33.517 8 12 83 22214 0.202 15 0.401 13.366 6 78 24255 0.06 16 0.387 35.333 8 29 81 22927 0.203.

17 0.387 34.93 8 12 83 22214 0.208 18 0.415 33.629 8 29 81 22927 0.211 19 0:415. 31.787 8 29 81 22927 0.198 20 0.387 33.517 8 12 83 22214 0.202 21 0.387 35.173 8 12 83 22214 0.208 22 0.415 30.26 8 29 81 22927 0.185 23 0.416 30.26 8* 29 81 22927 0.185 24 0.401 12.99 6 78 24255 0.06

EA-SC-93-083-22 ATTACHMENT A PAGE13 File Name: NUREG.MCD 23 Total Heat Load after 50 years Tota!Heat :=

2:

i 0

=

HeatLoad.

I Tota!Heat = 3.925 Kw 11.0 Result Summary Table A.5 : Heat Generation Rate of MSB-03 and MSB-04 20 years 50 years MSB-03 5.97-KW 3.885-KW MSB-04 6.035-KW 3.925-KW

EA-SC-93-083-22 Attachment B Rev.: 0 Page Bl Attachment B (4 pages)

FUEL DATA

EA- SC - q 3 _ 08'~ _ 2 2-

/+TT ACH AA ENT I; VSC-24 STORAGE SHEET PA-<iE r;2

  • VCC Number:

Date MSB Loaded:

1 oS"-07-93@003'-f Isl asse"'"f Storage Pad Position: .1.

MSB Number:

Placement Date:

1 M0.1 I 2 1 l'1Cf3 Comments:

FUEL ASSEMBLY LISTING

~

Fuel Assembly Parameters ID No Initial u Initial U Burnup Discharge Visual Enr (w/o) Wt (g) (MWD/MTU) Date Exam Date 1 G-01 3.00 386,946 33,997.0 08-12-83 09-25-92 2 G-02 3.00 387,078 33,997.0 II 09-25-92 3 G-03 3.00 386,901 33,997.0 n 09-25-92 4 G-04 3.00 387,469 31,413.8 II 09-25-92 5 G-05 3.00 387,077 33,997.0 II 09.:.25-92

  • 6 7

8 9

G-06 G-07 G-08 G-09 3.00 3.00 3.00 3.00 387,248 387,815 387,372 388,101 33,997.0 33,997.0 33,997.0 33,516.6 n

II II II 09-25-92 09-25-92 10-05-92 10-05-92 10 G-10 3.00 387,117 33,997.0 II 10-05-92 11 G-11 3.00 388,019 33,516.6 II 10-05-92 12 G-12 3.00 387,677 31,413.8 II 10-05-92 13 G-13 3.00 387,921 30,972.2 II 10-05-92 14 G-14 3.00 387,670 32,722.6 II 10-05-92 15 G-15 3.00 388,214 32,722.6 II 09-24-92 16 G-16 3.00 387,915 30,972.2 II 10-08-92 17 G-17 3.00 386,138 32,410.2 II 10-08-92 18 G-18 3.00 387,127 34,929.8 II 10-08-92 19 G-20 3.00 387,491 32,410.2 II 10-08-92 n 10-09-92 20 G-21 3.00 385,931 30,972.2

  • 21 22 23 G-22 G-23 G-24 3.00 3.00
3. 00.

3.00

_-387,641 387,841 387,677 387,993 32,410.2 32,410.2

  • 3 0, 9 72. 2 32,722.6 II II II II 10-09-92 10-09-92 10-09-92 10-09-92 24 G-25

C:A,SC- q~- 08 ~ - 2. 2 A-TTlrCH MEN7 .g VSC-24 STORAGE SHEET PA-G-E e,~

  • VCC Number:

Date MSB Loaded:

z..

5- JlJ-Cf 3 Storage Pad Position: 2 MSB Number:

Placement Date:

Z 5--16-93 Comments:

PUEL ASSEMBLY LISTING

~

Fuel Assembly Parameters ID No Initial U Initial U Burnup Discharge Visual Enr (w/o) Wt (g) (MWD/MTU) Date Exam Date 1 G-27 3.00 386,612 32, 722. 6 08-12-83 10-09-92 2 G-28 3.00 386,663 31,413.8 n 10-09-92 3 G-29 3.00 386,449 34,929.8 n 09-24-92 4 G-31 3. 00 . 387,923 31,413.8 II 10.-09-92 5 G-32 3.00 387,452 33,516.6 II 10.:.09-92

  • 6 7

8 G-33 G-34 G-37 G-38 3.00 3.00 3.00 3.00 388,150 387,834 387,458 386,736 33,516.6 33,516.6

.31,413.8 34,929.8

  • n n

n II 10-09-92 10-09-92 09-25-92 10-09-92 9

10 G-39 3.00 387,441 31,413.8 II 09-25-92 11 G-40 3.00 387,700 32,722.6 II 10-09-92 12 G-41 3.00 387,494 32,722.6 II 09-25-92 1.3 G-43 3.00 388,586 32,410.2 II 10-09-92 14 G-44 3.00 386,959 32,410.2 II 10-09-92 15 G.-45 3.00 388,062 30,972.2 II 10-09-92 16 G-46 3.00 387,235 34,929.8 II 10-09-92 17 G-48 3.00 387,739 32,410.2 II 10-14-92 18 G-50 3.00 387,813 32,410.2 II 09-25-92 19 G-53 3.00 386,913 34,929.8 II 10-14-92 n 10-14-92 20 G-54 3.00 386,371 34,929.8 21 G-57 3.00 . 387, 399 30,972.2 II 10-14-92 22 G-59 3.00 387,242 34,929.8 II 10-14-92 23 G-60 3.00 386,196 32,722.6 II 10-14-92 I

24 G-63 3.00 386,985 30,972.2 II 10-14-92

EA-sc_q3_ Of?-2.2-A-TT AC..tf A.I E: N 7 (~

  • VCC Number:

VSC-24 STORAGE SHEET 3 MSB Number:

PMiE &If 3

Date MSB Loaded: 6/20-6/21 /94 Storage Pad Position: 3 Placement Date: 6/30/94 Comments:

FUEL ASSEMBLY LISTING MSB Fuel Assembly Parameters Cell Initial U Initial U Burn up Discharge Visual No. ID No Enr (w/o) Wt <al lMWD/MTlJ) Date Exam Date 1 EFOOOO 2.74 415,213 30,260 08/29/81 04/07/94 2 EF0001 2.74 415,470 33,027 08/29/81 04/11/94 .

3 EF0002 2.74 415,208 33,027 08/29/81 04/11/94 "

4 G026 3.00 386,826 35,117 08/12/83 01/24/94 .

1.51 5 XF02 400,106 12,990 01/06/78 04/07/94  :

6 D102 3.05 385,792 35,333 08/29/81 01/19/94 7 E014 3.05 385,292 35,333 08/29/81 04/06/94 8 G068 3.00 387,137 31,414 08/12/83 03/18/93 9 XF08 1.5 401,697 13,366 01/06/78 01/19/94 10 XF09 1.5 401,583 13,911 01/06/78. 04/06/94 11 XF10 1.5 400,690 12,990 01/06/78 04/08/94 12 EF0011 2.74 415,913 28,128 08/29/81 03/21/94 13 EF0013 2.74 416,121 28,824 08/29/81 03/21/94 14 G047 3.00 387,028 35, 117 *08/12/83 04/07/94 15 XF15 1.5 401,962 13,626 01/06/78 04/05/94 16 XF16 1.51 401,039 13,626 01/06/78 04/08/94 I

I 17 G051 3.00 386,875 35,117 08/12/83 03/30/94 18 EF0014 2.74 415,481 30,260 08/29/81 03/21/94 19 EF0016 2.74 415,795 28,128 08/29/81 03/25/94 I 20 GOSS 3.00 386,489 35,173 08/12/83 03/31/94.

21 G056 3.00 386,901 35,173 08/12/83 04/04/94 22 EF0018 2.74 415,751 33,027 08/29/81 01/13/94 23 EF0019 2.74 415,660 30,260 08/29/81 04/05/94 24 EFOOOH 2.74 415432 30353 08/29/81 04/11/94

.eA- - s c - .q? - 0 .v.; - 2 z.,

~Tl.+uf A.I ENT ~

VSC-24 STORAGE SHEET p~ &5 VCC Number: 4 MSB Number:

Date MSB Loaded: -

Storage Pad Position: Placement Date:

Comments:

FUEL ASSEMBLY LISTING MSB Fuel Assembly Parameters Heat Cell Initial U Initial U Burn up Discharge Visual Load No. ID No Enr (w/o) wt (a) (MWD/MTU) Date Exam Date (KW) 1 EFOOOC 2.74 415,192 30,343 08/29/81 03/30/94 0.4152 2 EFOOOX 2.74 415,199 30,260 08/29/81 03/31/94 0.4152 3 EFOOOY 2.75 415,810 30,585 08/29/81 01/10/94 0.4158 4 G061 3.00 387,249 35, 117 08/12/83 04/08/94 0.5034 5 XF20 1.50 401,817 13,626 01/06/78 01/18/94 0.2009

  • 6 7

8 9

10 EFOOOZ EF001G G062 XF22 XF30 2.73 2.74 3.00 1.51 1.50 415,647 415,453 387,358 401,013 404,306 30,585 30,343 35,117 13,626 13,366 08/29/81 08/29/81 08/12/83 01/06/78 01/06/78 04/04/94 04/11/94 01/20/94 03/31/94 04/07/94 0.4156 0.4155 0.5036 0.2005 0.2022 11 XF46 1.50 401,473 13, 110 01/06/78 01/14/94 0.2007 12 EF001H 2.74 415,333 30,353 08/29/81 04/11/94 0.4153 13 EF001J 2.73 414,477 33,629 08/29/81 04/11/94 0.4559 14 G065 3.00 387,876 33,517 08/12/83 03/28/94 0.5042 15 XF51 1.50 401,056 13,366 01/06/78 04/06/94 0.2005 16 E065 3.05 386,524 35,333 08/29/81 04/05/94 0.4638 17 G066 3.00 386,896 34,930 08/12/83 01/21/94 0.5030 18 EF001K 2.73 415,010 33,629 08/29/81 04/11/94 0.4565 19 EF001R 2.74 414,830 31,787 08/29/81 04/05/94 0.4563 20 G067 3.00 387,422 33,517 08/12/83 03/30/94 0.5036 21 G030 3.00 386,654 35,173 08/12/83 04/08/94 0.5027 22 EF0006 2.74 415,135 30,260 08/29/81 04/11/94 0.4151 23 EF0010 2.74 415,726 30,260 08/29/81 04/11/94 0.4157 24 XF53 1.51 400975 12 990 01/06/78 01/18/94 0.2005 EAvg 29585 Total Ht I 9.381 XFAvg 17071

. GAvg 34562

EA-SC-93-083-22 Attachment C Rev.: 0 Page Cl Attachment C (2.~pages )

ANSYS INPUT DECK

EA-SC-93-083-22 ATTACHMENT C Page C2

  • /PREP7

/TITLE VCC-MSB-3 AMB= 0.0 F 5.97 KW AFTER 20 YEARS IN STORAGE

/SHOW,BNCHVCC2,GEO,,

/SHRINK, .3 KAN,-1

- GGGG=5.97

  • Total Heat Generation of MSB assenilly KW/MSB y AAAA=0.00
  • Anbient Air Tet11Jerature F SOTO=O.O
  • Solar Load on Top BTU/hr/ft**2 SOSI=O.O
  • Solar Load on Side BTU/hr/ft**2 SOCO=O.O
  • Solar Load on Cover Plate BTU/hr/ft**2 SUMK=.61936569
  • ClElll. friction Loss K For Air Flow

~ TOAS=29.846

  • Assuned Value; Must match TOCA; Outlet Air t~ F DRHI=13.69167
  • Draft Height TOOO=AAAA
  • Air T~ at Bott of MSB TAVE=((AAAA+TOAS)/2)

C*** ******************************************************

C*** CALCLATIONS ARE VALID FOR 0 < TAVE <32 F C*** ******************************************************

HEAT=CGGGG*3412.0)

  • Total heat generation BTU/Hr v- CPAl=0.2390
  • CONSTRAINT 0 < TAVE < 32 MFLO=CHEAT/(3600.0*CPAl*CTOAS-AAAA)))
  • Air Mass Flowrate through VCC lb/Sec v* DENA=(0.081+0.005*(32-TAVE)/32.)
  • CONSTRAINT 0 < TAVE < 32 C*** ******************************************************

C*** DP Stack DPST 111.1st be equal to DP Flow DPFL C*** ******************************************************

DPST=CDENA*32.2*DRHl*CTOAS-AAAA)/(32.2*CTAVE+460)))

  • DP Stack DPFL=CMFLO*MFLO*SUMK/C2*32.2*DENA))
  • DP Flow DELT=CMFLO*MFLO*SUMK*CTAVE+460)/(2*32.2*DENA*DENA*DRHI))

C*** ********************************************************************

C*** Calculated Air outlet t~ TOCA lllJSt be equal to assl.Jlled value TOAS C*** ********************************************************************

TOCA=CAAAA+DELT)

  • MUST BE EQUAL TO 11 TOAS" Air outlet T~ F Q016=CGGGG*3412.0*0.69*16.0/144.0)
  • Heat Gen El. 0 -16 In BTU/hr Q032=CGGGG*3412.0*1.08*16.0/144.0) *Heat Gen El. 16 -32 In BTU/Hr Q048=(GGGG*3412.0*1.20*16.0/144.0)
  • Heat Gen El. 32 -48 In BTU/Hr Q064=(GGGG*3412.0*1.19*16.0/144.0) *Heat Gen El. 48 -64 In B'l'U/Hr Q080=(GGGG*3412.0*1.17*16.0/144.0) *Heat Gen El. 64 -80 In BTU/Hr Q096=(GGGG*3412.0*1.12*16.0/144.0) *Heat Gen El. 80 -96 In BTU/Hr Q112=CGGGG*3412.0*1.05*16.0/144.0) *Heat Gen El. 96 -112 In BTU/Hr Q128=CGGGG*3412.0*0.90*16.0/144.0)
  • Heat Gen El. 112 -128 In BTU/Hr C144=(GGGG*3412.0*0.60*16.0/144.0)
  • Heat Gen El. 128 -144 In BTU/Hr T016=CTOOO+Q016/(3600.0*CPAl*MFLO)) *Air T~ at 16 In.

T032=CT016+Q032/(3600.0*CPAl*MFLO))

  • Air T~ at 32 In.

T048=CT032+Q048/(3600.0*CPAl*MFLO))

  • Air T~ at 48 In.

T064=CT048+Q064/(3600.0*CPAl*MFL0))

  • Air T~ at 64 In.

T080=(T064+Q080/(3600.0*CPAl*MFL0))

  • Air T~ at 80 In.

T096=(T080+Q096/(3600.0*CPAl*MFL0))

  • Air T~ at 96 In.

T112=CT096+Q112/(3600.0*CPAI*MFL0)) *Air T~ at 112 In.

T128=CT112+Q128/(3600.0*CPAl*MFL0)) *Air T~ at 128 In.

T144=CT128+Q144/(3600.0*CPAl*MFL0))

  • Air T~ at 144 In.

C*** ELEMENT TYPE MODULE C*** DEFINES THE ELEMENT TYPES ET,1,70

  • STIF 70 3-D ISOPAR. THERMAL SOLID ELEMENTS ET,2,31
  • STIF 31 RADIATION LINK ELEMENTS C*** OPTIONS MODULE C*** DEFINESANALYSIS OPTIONS KYPOST,O TOFFST,460 *Used for Rad. T Abs= T F + 460 F C*** END OF OPTIONS MODULE C*** MATERIAL MODULE C*** DEFINES MATERIAL PROPERTIES BTU/hr-ft-F C*** Conduction Elements Kxx=Kyy MP,KXX,1,26.2
  • MP,KXX,2,0.719
  • MPTEMP,1,-50,0,32,100,200,300 MPTEMP,7,500,700 .

MPDATA,KXX,3,1,0.0114,0.0130,0.0140,0.0154,0.0174,0.0193 MPDATA,KXX,3,7,0.0231,0.0268 MP,KXX,4,2.38

  • MP,KXX,5,0.10
  • MP,KXX,9,10.0
  • EA-SC-93-083-22 ATTACHMENT C Page C3 MP,KXX,10,0.3.0
  • C*** Conduction Elements Density Lb/FT**3-F MP,DENS,1,490
  • MP,DENS,2,141.30
  • MPDATA,DENS,3,1,0.094,0.086,0.081,0.071,0.060,0.052 MPDATA,DENS,3,7,0.0412,0.0373 MP,DENS,4,176.80
  • MP,DENS,5,0.0065
  • MP,DENS,9,488
  • MP,DENS,10,106
  • C*** Conduction Elements Spec. Heat BTU/Lb-F MP,C,1,0.11
  • MP,C,2,0.21
  • MPDATA,C,3, 1,0.2385,0.239,0.240,0.240,0.241,0.243 MPDATA,C,3,7,0.247,0.253 MP,C,4,0.0715
  • MP,C,5,1.24
  • MP,C,9,0.11
  • MP,C,10,.22
  • EMIS CARDS MP,EMIS,1,.8 MP,EMIS,2,.9 MP ,EMIS,3, .85 MP,EMIS,6,.85 MP,EMIS,7,.85 MP,EMIS,8,.85 C*** END OF MATERIAL MOOULE C*** REAL CONSTANT MOOULE R,1 *FOR STIF55 Elements C*** Real Const.For Radiation Area,From Geo.Fact.,Emiss, SBC R,97,0.4400,0.140,0.9,0.17140E*08 R,98,0.4800,0.140,0.9,0.17140E*08 R,99,0.0500,0.140,0.9,0.17140E*08 R,100,0.0250,0.140,0.9,0.17140E-08 R,101,0.0950,0.140,0.9,0.17140E-08 R,102,0.7188,0.140,0.9,0.17140E-08 R, 103,0.9600,0.140,0.9,0.17140E*08 R,104,0.9600,0.140,0.9,0.17140E-08 R,105,1.2793,0.140,0.9,0.17140E*08*

R,106,1.2810,0.140,0.9,0.17140E-08 R,107,1.0500,0.140,0.9,0.17140E-08 R,108,0.6590,0.140,0.9,0.17140E-08 R,109,0.3794,0.140,0.9,0.17140E*08 R,110,0.1290,0.140,0.9,0.17140E-08 R,111,0.04895,1.0,0.8,0.17140E*08 R,127,0.0165,1.0,0.8,0.17140E-08 R,128,0.0446,1.0,0.8,0.17140E*08

  • R,129,0.3380,1.0,0.8,0.17140E-08 R,130,0.4510,1.0,0.8,0.17140E*08 R,131,0.4510,1.0,0.8,0.17140E-08 R,132,0.6000,1.0,0.8,0.17140E*08 R,133,0.6020,1.0,0.8,0.17140E-08 R,134,0.4930,1.0,0.8,0.17140E-08 R, 135,0.4270,1.0,0.8,0.17140E*08 R,145,0.0606,1.0,0.8,0.17140E*08 R, 146,0.2470, 1.0,0.8,0.17140E*08 R,148,0.0606,1.0,0.8,0.17140E-08 R,149,0.1740,1.0,0.8,0.17140E-08 R,151,0.6650,1.0,0.9,0.17140E*08 R,166,0.1620,1.0,0.8,0.17140E*08 R,168,0.2400,1.0,0.9,0.17140E*08 C*** END OF REAL CONSTANT MOOULE C*** NOOE MOOULE C*** DEFINES NOOES BY DIRECT INPUT N,1,0.0000,0.00000,0.0000 N,2,1.2500,0.00000,0.0000 N,3,2.5208,0.00000,0.0000 N,4,2.5830,0.00000,0.0000 N,5,2.9170,0.00000,0.0000 N,6,3.0833,0.00000,0.0000 N,7,4.2708,0.00000,0.0000

EA-SC-93-083-22 ATTACHMENT C Page C4

  • N,8,5.5000,0.00000,0.0000 N,9,1.2310,0.21706,0.0000 N,10,2.4825,0.43773,0.0000 N,11,2.5438,0.44853,0.0000 N,12,2.8727,0.50653,0.0000 N,13,3.0365,0.53541,0.0000 N,14,4.2059,0.74162,0.0000 N,15,5.4164,0.95S06,0.0000 N,17,0.0000,0.00000,1.8333 N,18,1.2500,0.00000,1.8333 N,19,2.5208,0.00000,1.8333 N,20,2.5830,0.00000,1.8333 N,21,2.9170,0.00000,1.8333 N,22,3.0833,0.00000,1.8333 N,23,4.2708,0.00000,1.8333 N,24,5.5000,0.00000,1.8333 N,25, 1.2310,0.21706, 1.8333 N,26,2.4825,0.43773,1.8333 N,27,2.5438,0.44853,1.8333 N,28,2.8727,0.50653,1.8333 N,29,3.0365,0.53541,1.8333 N,30,4.2059,0.74162,1.8333 N,31,5.4164,0.95506,1.8333 N,33,0.0000,0.00000,2.0000 N,34,1.2500,0.00000,2.0000 N,35,2.5208,0.00000,2.0000 N,36,2.5830,0.00000,2.0000 N,37,2.9170,0.00000,2.0000 N,38,3.0833,0.00000,2.0000 N,39,4.2708,0.00000,2.0000 N,40,5.5000,0.00000,2.0000 N,41,1.2310,0.21706,2.0000 N,42,2.4825,0.43773,2.0000 N,43,2.5438,0.44853,2.0000 N,44,2.8727,0.50653,2.0000 N,45,3.0365,0.53541,2.0000 N,46,4.2059,0.74162,2.0000 N,47,5.4164,0.95506,2.0000 N,49,0.0000,0.00000,2.0417 N,50,1.2500,0.00000,2.0417 N,51,2.5208,0.00000,2.0417 N,52,2.5830,0.00000,2.0417 N,53,2.9170,0.00000,2.0417 N,54,3.0833,0.00000,2.0417 N,55,4.2708,0.00000,2.0417 N,56,5.5000,0.00000,2.0417 N,57,1.2310,0.21706,2.0417

. N,58, 2 .4825 ,0.43773,2.0417 N,59,2.5438,0.44853,2.0417 N,60,2.8727,0.50653,2.0417 N,61,3.0365,0.53541,2.0417 N,62,4.2059,0.74162,2.0417 N,63,5.4164,0.95506,2.0417 N,65,0.0000,0.00000,2.1040 N,66,1.2500,0.00000,2.1040 N,67,2.5208~0.00000,2.1040 N,68,2.5830;0.00000,2.1040 N,69,2.9170,0.00000,2.1040 N,70,3.0833,0.00000,2.1040 N,71,4.2708,0.00000,2.1040 N,72,5.5000,0.00000,2.1040 N,73,1.2310,0.21706,2.1040 N,74,2.4825,0.43773,2.1040 N,75,2.5438,0.44853,2.1040 N,76,2.8727,0.50653,2.1040 N,77,3.0365,0.53541,2.1040 N,78,4.2059,0.74162,2.1040 N,79,5.4164,0.95506,2.1040 N,81,0.0000,0.00000,2.4375 N,83,2.5208,0.00000,2.4375 N,84,2.5830,0.00000,2.4375

EA-SC-93-083-22 ATTACHMENT C Page cs N,85,2.9170,0.00000,2.4375 N,86,3.0833,0.00000,2.4375 N,87,4.2708,0.00000,2.4375 N,88,5.S000,0.00000,2.4375 N,90,2.4825,0.43773,2.4375 N,91,2.5438,0.44853,2.4375 N,92,2.8727,0.50653,2.4375 N,93,3.0365,0.53541,2.4375 N,94,4.2059,0.74162,2.4375 N,95,5.4164,0.95506,2.4375 N,97,0.0000,0.00000,5:1042 N,99,2.5208,0.00000,5.1042 N,100,2.5830,0.00000,5.1042 N,101;2.9170,0.00000,5.1042 N,102,3.0833,0.00000,5.1042 N,103,4.2708,0.00000,5.1042 N,104,5.50Q0,0.00000,5.1042 N,106,2.4825,0.43773,5.1042 N,107,2.5438,0.44853,5.1042 N,108,2.8727,0.50653,5.1042 N,109,3.0365,0.53541,5.1042 N,110,4.2059,0.74162,5.1042 N,111,5.4164,0.95506,5.1042 N,113,0.0000,0.00000,6.4376 N,115,2.5208,0.00000,6.4376 N,116,2.5830,0.00000,6.4376 N,117,2.9170,0.00000,6.4376 N,118,3.0833,0.00000,6.4376 N,119,4.2708,0.00000,6.4376 N,120,5.5000,0.00000,6.4376 N,122,2.4825,0.43773,6.4376 N,123,2.5438,0.44853,6.4376 N,124,2.8727,0.50653,6.4376 N,125,3.0365,0.53541,6.4376 N,126,4.2059,0.74162,6.4376 N,127,5.4164,0.95506,6.4376 N,129,0.0000,0.00000,9.1043 N,131,2.5208,0.00000,9.1043 N,132,2.5830,0.00000,9.1043 N,133,2.9170,0.00000,9.1043 N,134,3.0833,0.00000,9.1043 N,135,4.2708,0.00000,9.1043 N,136,5.5000,0.00000,9.1043 N,138,2.4825,0.43773,9.1043 I. N,139,2.5438,0.44853,9.1043 N,140,2.8727,0.50653,9.1043 N,141,3.0365,0.53541,9.1043

  • N, 142,4.2059,0. 74162,9.1043 N,143,5.4164,0.95506,9.1043 N,144,7.9696,0.69725,9.1043 N,145,0.0000,0.00000,11.771 N,147,2.5208,0.00000,11.771 N,148,2.5830,0.00000,11.771 N,149,2.9170,0.00000,11.771 N,150,3.083310.00000,11.771 N,151,4.2708,0.00000,11.771 N,152,5.5000,0.00000,11.771 N,154,2.4825,0.43773,11.771 N,155,2.5438,0.44853,11.771 N,156,2.8727,0.50653,11.771 N,157,3.0365,0.53541,11.771 N,158,4.2059,0.74162,11.771 N,159,5.4164,0.95506,11.771 N,161,0.0000,0.00000,14.438 N,163,2.5208,0.00000,14.438 N,164,2.5830,0.00000,14.438 N,'165,2.9170,0.00000, 14.438 N,166,3.0833,0.00000,14.438 N,167,4.2708,0.00000,14.438 N,168,5.5000,0.00000,14.438 N,170,2.4825,0.43773,14.438

EA-SC-93-083-22 ATTACHMENT C Page C6 N,171,2.5438,0.44853,14.438 N,172,2.8727,0.50653,14.438 N,173,3.0365,0.53541,14.438 N,174,4.2059,0.74162,14.438 N,175,5.4164,0.95506,14.438 N,177,0.0000,0.00000,16.143 N,178,1.2500,0.00000,16.143 N,179,2.5208,0.00000,16.143 N,180,2.5830,0.00000,16.143 N,181,2.9170,0.00000,16.143 N,182,3.0833,0.00000,16.143 N,183,4.2708,0.00000,16.143 N,184,5.5000,0.00000,16.143 N,185,1.2310,0.21706,16.143 N,186,2.4825,0.43773,16.143 N,187,2.5438,0.44853,16.143 N,188,2.8727,0.50653,16.143 N,189,3.0365,0.53541,16.143 N,190,4.2059,0.74162,16.143 N, 191,5.4164,0~95506, 16.143 N,193,0.0000,0.00000,17.186 N,194,1.2500,0.00000,17.186 N,195,2.5208,0.00000,17.186 N,196,2.5830,0.00000,17.186 N,197,2.9170,0.00000,17.186 N,198,3.0833,0.00000,17.186 N,199,4.2708,0.00000,17.186 N,200,5.5000,0.00000,17.186 N,201,1.2310,0.21706,17.186 N,202,2.4825,0.43773,17.186 N,203,2.5438,0.44853,17.186 N,204,2.8727,0.50653,17.186 N,205,3.0365,0.53541,17.186 N,206,4.2059,0.74162,17.186 N,207,5.4164,0.95506,17.186 N,209,0.0000;0.00000,17.724 N,210,1.2500,0.00000,17.724 N,211,2.5208,0.00000,17.724 N,212,2.5830,0.00000,17.724 N,213,2.9170,0.00000,17~724 N,214,3.0833,0.00000,17.724 N,215,4.2708,0.00000,17.724 N,216,5.5000,0.00000,17.724 N,217,1.2310,0.21706,17.724 N,218,2.4825,0.43773,17.724 N,219,2.5438,0.44853,17.724.

N,220,2.8727,0.50653,17.724

. N,221,3.0365,0.53541,17.724 N,222,*4. 2059 ,0. 74162, 17. 724 N,223,5.4164,0.95506,17.724 N,225,0.0000,0.00000,17.786 N,226,1.2500,0.00000,17.786 N,227,2.5208,0.00000,17.786 N,228,2.5830,0.00000,17.786 N,229,2.9170,0.00000,17.786 N,230,3.0~;0.00000,17.786 N,233,1.2310,0.21706,17.786 N,234,2.4825,0.43773,17.786 N,235,2.5438,0.44853,17.786 N,236,2.8727,0.50653,17.786 N,237,3.0365,0.53541,17.786 N,241,1.7999,0.015708,19.500 N,242,5.4800,0.00000,0.0000 N,243,5.3967,0.95159,0.0000 N,258,5.4800,0.00000,1.8330 N,259,5.3967,0.95159,1.8330 N,274,5.4800,0.00000,2.0000 N,275,5.3967,0.95159,2.0000 N,290,5.4800,0.00000,2.0tt17 N,291,5.3967,0.95159,2.0417 N,306,5.4800,0.00000,2.1040

EA-SC-93-083-22 ATTACHMENT C Page C7

  • N,307,5.3967,0.95159,2.1040 N,322,5.4800,0.00000,2.4375 N,323,5.3967,0.95159,2.4375 N,338,5.4800,0.00000,5.1042 N,339,5.3967,0.95159,5.1042 N,354,5.4800,0.00000,6.4375 N,355,5.3967,0.95159,6.4375 N,370,5.4800,o~ooooo,9.1042 N,371,5.3967,0.95159,9.1042 N,386,5.4800,0.00000,11.771 N,387,5.3967,0.95159,11.771 N,402,5.4800,0.00000,14.437 N,403,5.3967,0.95159,14.437 N,418,5.4800,0.00000,16.143 N,419,5.3967,0.95159,16.143 N,434,5.4800,0.00000,17.185 N,435,5.3967,0.95159,17.185 N,450,5.4800,0.00000,17.724
  • N,451,5.3967,0.95159,17.724 N,468,3.0833,0.00000,17.703 N,469,4.2708,0.00000,17.703 N,470,5.4800,0.00000,17.703 N,471,5.5000,0.00000,17.703 N,472,3.0365,0.53541,17.703 N,473,4.2059,0.74162,17.703 N,474,5.3967,0.95159,17.703 N,475,5.4164,0.95506,17.703 N,476,0.0000,0.00000,16.643 N,477,1.2500,0.00000,16.643 N,478,2.5208,0.00000,16.643 N,479,2.5830,0.00000,16.643 N,480,0.0000,0.00000,16.809 N,481,1.2500,0.00000,16.809 N,482,2.5208,0.00000,16.809 N,483,2.5830,0.00000,16.809 N,484,1.2310,0.21706,16.643 N,485,2.4825,0.43773,16.463 N,486,2.5438,0.44853,16.463 N,487,1.2310,0.21706,16.809 N,488,2.4825,0.43773,16.809 N,489,2.5438,0.44853,16.809 NP LOT C*** End of Node Module C*** Element Module TYPE,1 REAL,1 MAT,2

. EN I 1 I 1 I 2 I 9 I 9 I 17 I 18 I 25 I 25 EN,2,2,3,10,9,18,19,26,25 EN,3,3,4,11,10,19,20,27,26 EN,4,4,5,12,11,20,21,28,27

. EN,5,5,6, 13, 12,21,22,29,28 EN,6,6,7,14,13,22,23,30,29 EN,7,7,242,243,14,23,258,259,30 MAT,1 EN,8,17,18;25,25,33,34,41,41 EN,9,18,19;26,25,34,35,42,41 EN,10,19,20,27,26,35,36,43,42 EN,11,20,21,28,27,36,37,44,43 EN,12,21,22,29,28,37,38,45,44 MAT,2 EN,13,22,23,30,29,38,39,46,45 EN,14,23,258,259,30,39,274,275,46 EN,15,33,34,41,41 .. 49,50,57,57 EN,16,34,35,42,41,50,51,58,57 MAT,1 EN,17,35,36,43,42,51,S2,59,58 EN,19,37,38,45,44,53,54,61,60 MAT,2 EN,20,38,39,46,45,54,55,62,61 EN,21,39,274,275,46,55,290,291,62 t

EA-SC-93-083-22 ATTACHMENT C Page C8

  • MAT,1 EN,22,49,50,57,57,65,66,73,73 EN,23,50,51,58,57,66,67,74,73 EN,24,51,52,59,58,67,68,75,74 EN,26,53,54,61,60,69,70,77,76 EPLOT MAT,2 EN,27,54,55,62,61,70,71,78,77 EN,28,55,290,291,62,71,306,307,78 MAT,5 EN,29,65,66,73,73,81,83,90,90 EN,30,73,74,90,90,66,67,83,83 MAT,1 EN,31,67,68,75,74,83,84,91,90 EN,33,69,70,77,76,85,86,93,92 MAT,2 EN,34,70,71,78,77,86,87,94,93 EN,35,71,306,307,78,87,322,323,94 MAT,4 EN,37,81,83,90,90,97,99,106,106 MAT,1 EN,38,83,84,91,90,99,100,107,106 EN,40,85,86,93,92,101,102,109,108 MAT,2 EN,41,86,87,94,93,102,103,110,109 EN,42,87,322,323,94,103,338,339,110 MAT,4 EN,44,97,99,106,106,113,115,122,122 MAT,1 EN,45,99,100,107,106,115,116,123,122 EN,47,101,102,109,108,117,118,125,124 MAT,2 EN,48,102,103,110,109,118,119,126,125 EN,49,103,338,339,110,119,354,355,126 EPLOT MAT,4 EN,51,113,115,122,122,129,131,138,138 MAT,1 EN,52,115,116,123,122,131,132,139,138 EN,54,117,118,125,124,133,134,141,140 MAT,2 EN,55,118,119,126,125,134,135,142,141 EN,56,119,354,355,126,135,370,371,142 MAT,4 EN,58,129,131,138,138,145,147,154,154 MAT I 1 EN,59,131,132,139,138,147,148,155,154
  • EN,61,133,134,141,140,149,150,157,156 MAT,2 EN,62,134,135,142,141,150,151,158,157 EN,63,135;370,371,142,151,386,387,158 MAT,4 EN,65,145,147,154,154,161,163,170,170 EN,66,147,148,155,154,163,164,171,170 MAT I 1 . *'

EN,68, 149, 1~0, 157, 156, 165, 166, 173, 172 MAT ,2 .

EN,69,150,151,158,157,166,167,174,173 EN,70,151,386,387,158,167,402,403,174 EPLOT MAT,5 EN,71,161,163,170,170,177,178,185,185 EN,72,185,170,186,186,178,163,179,179 MAT I 1 EN,73,163,164,171,170,179,180,187,186

  • EN,75,165,166,173,172,181,182,189,188 MAT,2 EN,76,166,167,174,173,182,183,190,189 EN,77,167,402,403,174,183,418,419,190 MAT,1 EN,78,177,178,185,185,476,477,484,484

EA-SC-93-083-22 ATTACHMENT C Page C9 EN,79,178,179,186,185,477,478,485,484 /

EN,80,179,180,187,186,478,479,486,485 EN,82,181,182,189,188,197,198,205,204 MAT,2 EN,83,182,183,190,189,198,199,206,205 EN,84,183,418,419,190,199,434,435,206 MAT,3 EN,85,193,194,201,201,209,210,217,217 EN,86,194,195,202,201,210,211,218,217 MAT,1 EN,87,195,196,203,202,211,212,219,218 EN,88,196,197,204,203,212,213,220,219 EN,89,197,198,205,204,213,468,472,220 MAT,2 EN,90,198,199,206,205,468,469,473,472 EN,91,199,434,435,206,469,470,474,473 MAT,1 EN,92,209,210,217,217,225,226,233,233 EN,93,210,211,218,217,226,227,234,233 EN,94,211,212,219,218,227,228,235,234 EN,95,212,213,220,219,228,229,236,235 EN,96,213,214,221,220,229,230,237,236 EPLOT TYPE,2 MAT,3 REAL,97 EN,97,8,144 REAL,98 EN,98,24, 144 REAL,99 EN,99,40, 144 REAL,100 EN, 100,56, 144 REAL, 101 EN, 101, 72, 144 REAL,102 EN, 102,88, 144 REAL,103 EN, 103, 104, 144 REAL,104 EN, 104, 120, 144 REAL,105 EN, 105, 136, 144 REAL,106 EN, 106, 152, 144 REAL,107 EN,107,168,144 REAL,108 EN, 108, 184, 144 REAL,109 EN, 109,200, 144 REAL 110 I

EN, 110,216, 144 REAL,111 EN, 111,230,241:

REAL,97 EN,112,15,144 REAL,98 EN,113,31,144 REAL,99 EN,114,47,144 REAL,100 EN, 115,63, 144 REAL,101 EN,116,79,144 REAL,102 EN, 117,95, 144 REAL, 103 .

EN,118,111,144 REAL, 104 EN, 119, 127, 144

- .t

EA-SC-93-083-22 ATTACHMENT C Page C10 REAL,105 EN, 120, 143, 144 REAL,106 EN, 121, 159, 144 REAL,107 EN, 122, 175, 144 REAL, 108 EN, 123, 191, 144 REAL,109 EN, 124,207, 144 REAL, 110 EN, 125,223, 144 REAL,111 EN,126,237,241 REAL,127 EN,127,52,53 REAL,128 EN,128,68,69 REAL,129 EN,129,84,85 REAL,130 EN, 130, 100, 101 REAL,131 EN, 131, 116, 117 REAL, 132 EN, 132, 132, 133 REAL, 133 EN, 133, 148, 149 REAL,134 EN, 134, 164, 165 REAL, 135 EN, 135, 180, 181 REAL,127 EN,136,59,60 REAL,128 EN, 137 I 75 , 76 REAL,129 EN,138,91,92 REAL,130 EN,139,107,108 REAL,131 EN, 140, 123, 124 REAL, 132 EN, 141, 139, 140 REAL,133 EN, 142, 155, 156 REAL,134

. EN, 143, 171, 172 REAL, 135 EN, 144, 187, 188 REAL,145 EN, 145, 193,209 REAL, 146 EN, 146, 194,210 REAL, 146 EN, 147,201,217 REAL, 148 '

EN, 148,225,241 REAL, 149 EN,149,227,241 REAL,149 EN,150,234,241 REAL,151 EN,151,215,241 REAL,151 EN,152,222,241 EPLOT TYPE,1 REAL,1 MAT,2 EN,153,242,8,15,243,258,24,31,259

EA-SC-93-083-22 ATTACHMENT C Page C11 EN,154,258,24,31,259,274,40,47,275 EN,155,274,40,47,275,290,56,63,291 EN,156,290,56,63,291,306,72,79,307 EN,157,306,72,79,307,322,88,95,323 EN,158,322,88,95,323,338,104,111,339 EN,159,338,104,111,339,354,120,127,355 EN,160,354,120,127,355,370,136,143,371 EN,161,370,136,t43,371,386,152,159,387 EN,162,386,152,159,387,402,168,175,403 EN,163,402,168,175,403,418,184,191,419 EN,164,418,184,191,419,434,200,207,435 EN,165,434,200,207,435,450,216,223,451 EPLOT TYPE,2 MAT,3 REAL,166 EN,166,226,241 REAL, 166 EN,167,233,241 REAL, 168

  • EN,168,214,241 REAL, 168 EN, 169,221,241 EPLOT TYPE,1 REAL,1 MAT,1 EN,170,221,472,220,220,214,468,213,213 MAT,2 EN,171,468,469,473,472,214,215,222,221 EN,172,469,470,474,473,215,450,451,222 EN,173,470,471,475,474,450,216,223,451 MAT, 10 EN,174,476,477,484,484,480,481,487,487 EN,175,477,478,485,484,481,482,488,487 MAT,1 EN,176,478,479,486,485,482,483,489,488 EN,177,480,481,487,487,193,194,201,201 EN,178,481,482,488,487,194,195,202,201 EN,179,482,483,489,488,195,196,203,202 EPLOT C*** END of Element Module C*** LOAD MODULE C*** DEFINE INITIAL TEMPERATURES AND HEAT TRANSFER COEFFICIENTS TIME,0.0 ITER, 12,3,3 POSTR,,1,3,2,3
  • LPRINT,0 KTEMP, -1 C*** CONVECTIVE HEAT TRANSFER

'r' C*** h=2 BTU/ft*Ft-F-Hr EC,17,3,2.000,AAAA EC,24,3,2.000,AAAA EC,31,3,2.000,AAAA EC,38,3,2.000,(0.5*T016+0.5*T032)

EC,45,3,2.000,T048 EC' 52 ,3 I 2.000*, (0.5*T064+0. 5*T080)

EC,59,3,2.000,(0.5*T096+0.5*T112)

EC,66,3,2.000,(0.S*T128+0.S*T144)

EC,73,3,2.000,T144 EC,80,3,2.000,T144 EC,19,5,2.000,AAAA EC,26,5,2.000,AAAA EC,33,5,2.000,AAAA EC,40,5,2.000,(0.S*T016+0.S*T032)

EC,47,5,2.000,T048 EC,54,S,2.000,(0.5*T064+0.S*T080)

EC,61,5,2.000,(0.5*T096+0.S*T112)

EC,68,5,2.000,(0.S*T128+0.5*T144)

EC,75,5,2.000,T144 EC,82,5,2.000,T144

EA-SC-93-083-22 ATTACHMENT C Page C12 EC,171,6,2.000,AAAA EC,172,6,2.000,AAAA EC,164,3,2.000,AAAA EC;96,6,2.000,AAAA EC,95,6,2.000,AAAA EC,94,6,2.000,AAAA EC,93,6,2.000,AAAA EC,92,6,2.000,Al\AA EC,153,3,2.000,AAAA EC,154,3,2.000,AAAA EC,155,3,2.000,AAAA EC,156,3,2.000,AAAA EC,157,3,2.000,AAAA EC,158,3,2.000,AAAA EC,159,3,2.000,AAAA EC,160,3,2.000,AAAA EC,161,3,2.000,AAAA EC,162,3,2.000,AAAA EC,163,3,2.000,AAAA EC,165,3,2.000,AAAA EC,173,3,2.000,AAAA EC,173,6,2.000,AAAA EC,179,3;2.000,T144 EC,176,3,2.000,T144 NT,144,TEMP,AAAA NT,241,TEMP,AAAA C*** ELEMENT TEMPERATURE MODULE C*** INPUT HEAT GENERATION LOADS BTU/hr*ft*ft*ft QE,37,C336.2*0.97*GGGG/24.00)

QE,44,C336.2*1.20*GGGG/24.00)

QE,51,C336.2*1.17*GGGG/24.00)

QE,58,(336.2*1.10*GGGG/24.00)

QE,65,C336.2*0.77*GGGG/24.00)

QE,92,SOCO QE,93,SOCO QE,94,SOCO QE,95,SOCO QE,96,SOCO QE, 153,SOSI QE,154,SOSI QE,155,SOSI QE,156,SOSl QE, 157,SOSI QE,158,SOSI QE,159,SOSl QE,160,SOSI QE,161,SOSI

. QE, 162,SOSI QE, 163,SOSI QE, 164,SOSI QE,165,SOSI QE, 171,SOTO QE, 172,SOTO QE,173,SOTO ETLIST,ALL MPLIST ,ALL RLIST,ALL NLIST,ALL ELIST,ALL ECLIST ,ALL NTLIST ,ALL QELIST,ALL LWRITE TIME,0.0 ITER,-20,20,20 LWRITE TIME,0.0 ITER,-40,20,20 LWRITE AFWRITE FINISH L

EA-SC-93-083-22 ATTACHMENT C Page C13

/INPUT ,27 FINISH

EA-SC-93-083-22 ATTACHMENT C Page C14

  • /PREP7

/TITLE VCC-MSB-3 AMB= a.a F 3.885 KW AFTER so YEARS IN STORAGE

/SHOW,BNCHVCC2,GEO,,

/SHRINK,.3 KAN,-1 1 GGGG=3.885 AAAA=0.00 SOTO=O.O

  • Total Heat Generation of MSB assembly K'J/MSB
  • Ant>ient Air Tell1)erature F
  • Solar Load on Top BTU/hr/ft**2

, SOSI=O.O

  • Solar Load on Side BTU/hr/ft**2 SOCO=O.O
  • Solar Load on Cover Plate BTU/hr/ft**2 SUMK=.61936569
  • Curm. friction Loss K For Air Flow TOAS=22.254
  • Assuned Value: Must match TOCA: Outlet Air t~ F DRHl=13.69167
  • Draft Height TOOO=AAAA
  • Air T~ at Bott of MSB TAVE=( CAAAA+TOAS)/2) .

C*** ******************************************************

C*** CALCLATIONS ARE VALID FOR 0 < TAVE <32 F C*** ******************************************************

HEAT=CGGGG*3412.0)

  • Total heat generation BTU/Hr

..- CPAl=0.239

  • CONSTRAINT 0 < TAVE < 32 MFLO=CHEAT/(3600.0*CPAl*CTOAS-AAAA)))
  • Air Mass Flowrate through VCC lb/Sec v DENA=C0.081+0.005*(32-TAVE)/32.)
  • CONSTRAINT 0 < TAVE < 32 C*** ******************************************************

C*** DP Stack DPST lllJSt be equal to DP Flow DPFL C*** ******************************************************

DPST=CDENA*32.2*DRHI*CTOAS-AAAA)/(32.2*CTAVE+460)))

  • DP Stack DPFL=CMFLO*MFLO*SUMK/C2*32.2*DENA))
  • DP Flow DELT=CMFLO*MFLO*SUMK*CTAVE+460)/(2*32.2*DENA*DENA*DRHI))

C*** ********************************************************************

C*** Calculated Air outlet t~ TOCA 111Jst be equal to assl.Jlled value TOAS C*** ********************************************************************

TOCA=CAAAA+DELT)

  • MUST BE EQUAL TO 11 TOAS 11 Air outlet T~ F QQ16=CGGGG*3412.0*0.69*16.0/144.0)
  • Heat Gen El. 0 -16 In BTU/hr Q032=CGGGG*3412.0*1.08*16.0/144.0) *Heat Gen El. 16 -32 In BTU/Hr Q048=CGGGG*3412.0*1.20*16.0/144.0) *Heat Gen El. 32 -48 In BTU/Hr QQ64=CGGGG*3412.0*1.19*16.0/144.0)
  • Heat Gen El. 48 -64 In BTU/Hr QQ80=CGGGG*3412.0*1.17*16.0/144.0) *Heat Gen El. 64 -80 In BTU/Hr QQ96=CGGGG*3412.0*1.12*16.0/144.0) *Heat Gen El. 80 -96 In BTU/Hr Q112=CGGGG*3412.0*1.05*16.0/144.0)
  • Heat Gen El. 96 -112 In BTU/Hr Q128=CGGGG*3412.0*0.90*16.0/144.0)
  • Heat Gen El. 112 -128 In BTU/Hr Q144=CGGGG*3412.0*0.60*16.0/144.0) *Heat Gen El. 128 -144 In BTU/Hr T016=CTOOO+Q016/C3600.0*CPAI*MFLO))
  • Air T~ at 16 In.

T032=CT016+Q032/C3600.0*CPAl*MFLO)) *Air T~ at 32 In.

T048=CT032+Q048/(3600.0*CPAI*MFLO))

  • Air T~ at 48 In.

T064=CT048+QQ64/C3600.0*CPAl*MFLO))

  • Air T~ at 64 In.

T080=(T064+Q080/(3600.0*CPAl*MFLO))

  • Air T~ at 80 In.

T096=CT080+Q096/(3600.0*CPAI*MFLO))

  • Air T~ at 96 In.
  • T112=CT096+Q112/C3600.0*CPAl*MFLO)) *Air T~ at 112 In.

T128=CT112+Q128/(3600.0*CPAI*MFLO)) *Air T~ at 128 In.

T144=CT128+Q144/(3600.0*CPAI*MFL0))

  • Air T~ at 144 In.

C*** ELEMENT TYPE MODULE .

C*** DEFINES THE ELEMENT TYPES ET,1,70

  • STIF 70 3-D ISOPAR. THERMAL SOLID ELEMENTS ET,2,31
  • STIF 31 RADIATION LINK ELEMENTS C*** OPTIONS.MODULE C*** DEFINES.ANALYSIS OPTIONS KYPOST,0 TOFFST,460 *Used for Rad. T Abs= T F + 460 F C*** END OF OPTIONS MODULE C*** MATERIAL MODULE C*** DEFINES MATERIAL PROPERTIES BTU/hr-ft-F C*** Conduction Elements Kxx=Kyy MP,ICXX, 1,26.2 **

MP,ICXX,2,0.719

  • MPTEMP,1,-50,0,32,100,200,300 MPTEMP,7,500,700 MPDATA,ICXX,3,1,0.0114,0.0130,0.0140,0.0154,0.0174,0.0193 MPDATA,ICXX,3,7,0.0231,0.0268 MP,ICXX,4,2.38
  • MP,KXX,5,0.10
  • MP,KXX,9,10.0 *

. 1

EA-SC-93-083-22 ATTACHMENT C Page C15 MP,KXX,10,0.3.0

  • C*** Conduction Elements Density Lb/FT**3-F MP,DENS,1,490
  • MP,DENS,2,141.30
  • MPDATA,DENS,3,1,0.094,0.086,0.081,0.071,0.060,0.052 MPDATA,DENS,3,7,0.0412,0.0373 MP,DENS,4,176.80
  • MP,DENS,5,0.0065 *
  • MP,DENS,9,488
  • MP,DENS,10,106
  • C*** Conduction Elements Spec. Heat BTU/Lb-F MP,C,1,0.11
  • MP,C,2,0.21
  • MPDATA,C,3,1,0.2385,0.239,0.240,0.240,0.241,0.243 MPDATA,C,3,7,0.247,0.253 MP,C,4,0.0715
  • MP,C,5,1.24
  • MP,C,9,0.11
  • MP,C,10,.22
  • EMIS CARDS MP ,EMIS, 1, .8 MP,EMIS,2,.9 MP,EMIS,3,.85 MP,EMIS,6,.85 MP,EMIS,7,.85 MP,EMIS,8,.85 C*** END OF MATERIAL MODULE C*** REAL CONSTANT MODULE R,1 *FOR STIF55 Elements C*** Real Const.For Radiation Area,From Geo.Fact.,Emiss, SBC R,97,0.4400,0.140,0.9,0.17140E-08 R,98,0.4800,0.140,0.9,0.17140E-08 R,99,0.0500,0.140,0.9,0.17140E*08 R,100,0.0250,0.140,0.9,0.17140E-08 R, 101,0.0950,0.140,0.9,0.17140E-08 R,102,0.7188,0.140,0.9,0.17140E-08 R,103,0.9600,0.140,0.9,0.17140E-08 R,104,0.9600,0.140,0.9,0.17140E*08 R,105,1.2793,0.140,0.9,0.17140E-08 R,106,1.2810,0.140,0.9,0.17140E*08 R,107,1.0500,0.140,0.9,0.17140E-08 R,108,0.6590,0.140,0.9,0.17140E*08 R,109,0.3794,0.140,0.9,0.17140E-08 R, 110,0.1290,0.140,0.9,0.17140E-08 R, 111,0.04895,1.0,0.8,0.17140E-08 R,127,0.0165,1.0,0.8,0.17140E-08 R, 128,0.0446,1.0,0.8,0.17140E-08
  • R,129,0.3380,1.0,0.8,0.17140E-08 R,130,0.4510,1.0,0.8,0.17140E-08 R,131,0.4510,1.0,0.8,0.17140E-08 R,132,0.6000,1.0,0.8,0.17140E-08 R, 133,0.6020,1.0,0.8,0.17140E-08 R,134,0.4930,1.0,0.8,0.17140E*08 R,135,0.4270,1.0,0.8,0.17140E*08 R,145,0.0606,1.0,0.8,0.17140E-08 R,146,0.2470,1.0,0.8,0.17140E*08 R,148,0.0606~1.0,0.8,0.17140E-08 R,149,0.1740,1.0,0.8,0.17140E-08 R,151,0.6650,1.0,0.9,0.17140E-08 R,166,0.1620,1.0,0.8,0.17140E*08 R, 168,0.2400, 1.0,0.9,0.17140E-08 C*** ENO OF REAL CONSTANT MODULE C*** NOOE MODULE C*** DEFINES NODES BY DIRECT INPUT N,1,0.0000,0.00000,0.0000 N,2,1.2500,0.00000,0.0000 N,3,2.5208,0.00000,0.0000 N,4,2.5830,0.00000,0.0000 N,5,2.9170,0.00000,0.0000 N,6,3.0833,0.00000,0.0000 N,7,4.2708,0.00000,0.0000

EA*SC*93*083*22 ATTACHMENT C Page C16

  • N,8,5.5000,0.00000,0.0000 N,9,1.2310,0.21706,0.0000 N, 10,2.4825,0.43773,0.0000 N, 11,2.5438,0.44853,0.0000 N,12,2.8727,0.50653,0.0000 N,13,3.0365,0.53541,0.0000 N,14,4.2059,0.74162,0.0000 N,15,5.4164,0.95506,0.0000 N,17,0.0000,0.00000,1.8333 N,18,1.2500,0.00000,1.8333 N,19,2.5208,0.00000,1.8333 N,20,2.5830,0.00000,1.8333 N,21,2.9170,0.00000,1.8333 N,22,3.0833,0.00000,1.8333 N,23,4.2708,0.00000,1.8333 N,24,5.5000,0.00000,1.8333 N,25,1.2310,0.21706,1.8333 N,26,2.4825,0.43773,1.8333 N,27,2.5438,0.44853,1.8333 N,28,2.8727,0.50653,1.8333 N,29,3.0365,0.53541,1.8333 N,30,4.2059,0.74162,1.8333 N,31,5.4164,0.95506,1.8333 N,33,0.0000,0.00000,2.0000 N,34,1.2500,0.00000,2.0000 N,35,2.5208,0.00000,2.0000 N,36,2.5830,0.00000,2.0000 N,37,2.9170,0.00000,2.0000 N,38,3.0833,0.00000,2.0000 N,39,4.2708,0.00000,2.0000 N,40,5.5000,0.00000,2.0000 N,41,1.2310,0.21706,2.00QO N,42,2.4825,0.43773,2.0000 N,43,2.5438,0.44853,2.0000 N,44,2.8727,0.50653,2.0000 N,45,3.0365,0.53541,2.0000 N,46,4.2059,0.74162,2.0000 N,47,5.4164,0.95506,2.0000 N,49,0.0000,0.00000,2.0417 N,50,1.2500,0.00000,2.0417 N,51,2.5208,0.00000,2.0417 N,52,2.5830,0.00000,2.0417 N,53,2.9170,0.00000,2.0417 N,54,3.0833,0.00000,2.0417 N,55,4.2708,0.00000,2.0417 N,56,5.5000,0.00000,2.0417 N,57,1.2310,0.21706,2.0417 N,58,2.4825,0.43773,2.0417 N,59,2.5438,0.44853,2.0417 N,60,2.8727,0.50653,2.0417 N,61,3.0365,0.53541,2.0417 N,62,4.2059,0.74162,2.0417 N,63,5.4164,0.95506,2.0417 N,65,0.0000,0.00000,2.1040 N,66,1.2500,0.00000,2~1040 N,67,2.5208",0~00000~2.1040 N,68,2.5830,*0.00000,2.1040 N,69,2.9170,0.00000,2.1040 N,70,3.0833,0.00000,2.1040 N,71,4.2708,0.00000,2.1040 N,72,5.5000,0.00000,2.1040 N,73,1.2310,0.21706,2.1040 N,74,2.4825,0.43773,2.1040

. N, 75,2.5438,0.44853,2.1040 N,76,2.8727,0.50653,2.1040 N,77,3.0365,0.53541,2.1040 N,78,4.2059,0.74162,2.1040 N,79,5.4164,0.95506,2.10~0 N,81,0.0000,0.00000,2.4375 N,83,2.5208,0.00000,2.4375 N,84,2.5830,0.00000,2.4375

EA-SC-93-083-22

- ATTACHMENT C Page C17 N,85,2.9170,0.00000,2.4375 N,86,3.0833,0.00000,2.4375 N,87,4.2708,0.00000,2.4375 N,88,5.5000,0.00000,2.4375 N,90,2.4825,0.43773,2.4375 N,91,2.5438,0.44853,2.4375 N,92,2.8727,0.50653,2.4375 N,93,3.0365,0.53541,2.4375 N,94,4.2059,0.74162,2.4375 N,95,5.4164,0;95506,2.4375 N,97,0.0000,0.00000,5.1042 N,99,2.5208,0.00000,5.1042 N,100,2.5830,0.00000,5.1042 N,101,2.9170,0.00000,5.1042 N,102,3.0833,0.00000,5.1042 N,103,4.2708,0.00000,5.1042 N,104,5.5000,0.00000,5.1042 N,106,2.4825,0.43773,5.1042 N,107,2.5438,0.44853,5.1042 N,108,2.8727,0.50653,5.1042 N,109,3.0365,0.53541,5.1042 N,110,4.2059,0.74162,5.1042 N,111,5.4164,0.95506,5.1042 N,113,0.0000,0.00000,6.4376 N,115,2.5208,0.00000,6.4376 N,116,2.5830,0.00000,6.4376 N,117,2.9170,0.00000,6.4376 N,118,3.0833,0.00000,6.4376 N,119,4.2708,0.00000,6.4376 N,120,5.5000,0.00000,6.4376 N,122,2.4825,0.43773,6.4376 N,123,2.5438,0.44853,6.4376 N,124,2.8727,0.50653,6.4376 N,125,3.0365,0.53541,6.4376 N,126,4.2059,0.74162,6.4376 N,127,5.4164,0.95506,6.4376 N,129,0.0000,0.00000,9.1043 N,131,2.5208,0.00000,9.1043 N,132,2.5830,0.00000,9.1043 N,133,2.9170,0.00000,9.1043 N,134,3.0833,0.00000,9.1043 N,135,4.2708,0.00000,9.1043

_N, 136,5.5000,0.00000,9.1043 N,138,2.4825,0.43773,9.1043 N,139,2.5438,0.44853,9.1043 N,140,2.8727,0.50653,9.1043 N,141,3.0365,0.53541,9.1043

- N, 142,4.2059,0.74162,9.1043 N,143,5.4164,0.95506,9.1043 N,144,7.9696,0.69725,9.1043 N,145,0.0000,0.00000,11.771 N,147,2.5208,0.00000,11.771 N,148,2.5830,0.00000,11.771 N,149,2.9170,0.00000,11.771 N,150,3.0833,0.00000,11.771 N,151,4.2708~0.00000,11.771 N,152,5.5000,0.00000,11.771 N,154,2.4825,0.43773,11.771 N,155,2:5438,0.44853,11.771 N,156,2.8727,0.50653,11.771 N,157,3.0365,0.53541,11.771 N,158,4.2059,0.74162,11.771 N,159,5.4164,0.95506,11.771

- N, 161,0.0000,0.00000, 14.438 N,163,2.5208,0.00000,14.438 N,164,2.5830,0.00000,14.438 N,165,2.9170,0.00000,14.438 N,166,3.0833,0.00000,14.438 N,167,4.2708,0.00000,14.438 N,168,5.5000,0.00000,14.438 N,170,2.4825,0.43773,14.438 L

EA-SC-93-083-22 ATTACHMENT C Page C18

  • N,171,2.5438,0.44853,14.438 N,172,2.8727,0.50653,14.438 N,173,3.0365,0.53541,14.438 N,174,4.2059,0.74162,14.438 N,175,5.4164,0.95506,14.438 N,177,0.0000,0.00000,16.143 N,178,1.2500,0.00000,16.143 N,179,2.5208,0.00000,16.143 N,180,2.5830,0.00000,16.143 N, 181,2.9170,0.00000, 16.143 N,182,3.0833,0.00000,16.143 N,183,4.2708,0.00000,16.143 N,184,5.5000,0.00000,16.143 N,185,1.2310,0.21706,16.143 N,186,2.4825,0.43773,16.143 N,187,2.5438,0.44853,16.143 N,188,2.8727,0.50653,16.143 N,189,3.0365,0.53541,16.143 N,190,4.2059,0.74162,16.143 N,191,5.4164,0.95506,16.143 N,193,0.0000,0.00000,17.186 N,194,1.2500,0.00000,17.186 N,195,2.5208,0.00000,17.186 N,196,2.5830,0.00000,17.186 N,197,2.9170,0.00000,17.186 N,198,3.0833,0.00000,17.186 N,199,4.2708,0.00000,17.186 N,200,5.5000,0.00000,17.186 N,201,1.2310,0.21706,17.186 N,202,2.4825,0.43773,17.186 N,203,2.5438,0.44853,17.186 N,204,2.8727,0.50653,17.186 N,205,3.0365,0.53541,17.186 N,206,4.2059,0.74162,17.186 N,207,5.4164,0.95506,17.186 N,209,0.0000,0.00000,17.724 N,210,1.2500,0.00000,17.724 N,211,2.5208,0.00000,17.724 N,212,2.5830,0.00000,17.724 N,213,2.9170,0.00000,17.724 N,214,3.0833,0.00000,17.724 N,215,4.2708,0.00000,17.724 N,216,5.5000,0.00000,17.724 N,217,1.2310,0.21706,17.724 N,218,2.4825,0.43773,17.724 N,219,2.5438,0.44853,17.724 N,220,2.8727,0.50653,17.724
  • N,221,3.0365,0.53541, 17.724 N,222,4.2059,0:74162,17.724 N,223,5.4164,0.95506,17.724 N,225,0.0000,0.00000,17.786 N,226,1.2500,0.00000,17.786 N,227,2.5208,0.00000,17.786 N,228,2.5830,0.00000,17.786 N,229,2.9170;0.00000,17.786 N,230,3.o~,o.ooooo,11.186 N,233,1.2310,0.21706,17.786 N,234,2.4825,0.43773,17.786 N,235,2.5438,0.44853,17.786 N,236,2.8727,0.50653,17.786 N,237,3.0365,0.53541,17.786 N,241,1.7999,0.015708,19.500 N,242,5.4800,0.00000,0.0000 N,243,5.3967,0.95159,0.0000 N,258,5.4800,0.00000,1.8330 N,259,5.3967,0.95159,1.8330 N,274,5.4800,0.00000,2.0000 N,275,5.3967,0.95159,2.0000 N,290,5.4800,0.00000,2.0417 N,291,5.3967,0.95159,2.0417 N,306,5.4800,0.00000,2.1040

EA*SC*93*083*22 ATTACHMENT C Page C19

  • N,307,5.3967,0.95159,2.1040 N,322,5.4800,0.00000,2.4375 N,323,5.3967,0.95159,2.4375 N,338,5.4800,0.00000,5.1042 N,339,5.3967,0.95159,5.1042 N,354,5.4800,0.00000,6.4375 N,355,5.3967,0.95159,6.4375 N,370,5.4800,0.00000,9.1042 N,371,5.3967,0.95159,9.1042 N,386,5.4800,0.00000,11.771 N,387,5.3967,0.95159,11.771 N,402,5.4800,0.00000,14.437 N,403,5.396710.95159,14.437 N,418,5.4800,0.00000,16.143 N,419,5.3967,0.95159,16.143 N,434,5.4800,0.00000,17.185 N,435,5.3967,0.95159,17.185 N,450,5.4800,0.00000,17.724 N,451,5.3967,0.95159,17.724 N,468,3.0833,0.00000,17.703 N,469,4.2708,0.00000,17.703 N,470,5.4800,0.00000,17.703 N,471,5.5000,0.00000,17.703 N,472,3.0365,0.53541,17.703 N,473,4.2059,0.74162,17.703 N,474,5.3967,0.95159,17.703 N,475,5.4164,0.95506,17.703 N,476,0.0000,0.00000,16.643 N,477,1.2500,0.00000,16.643 N,478,2.5208,0.00000,16.643 N,479,2.5830,0.00000,16.643 N,480,0.0000,0.00000,16.809 N,481,1.2500,0.00000,16.809 N,482,2.5208,0.00000,16.809 N,483,2.5830,0.00000,16.809 N,484,1.2310,0.Z1706,16.643 N,485,2.4825,0.43773,16.463 N,486,2.5438,0.44853,16.463 N,487,1.2310,0.21706,16.809 N,488,2.4825,0.43773,16.809 N,489,2.5438,0.44853,16.809 NP LOT C*** End of Node Module C*** Element Module TYPE, 1 REAL,1 MAT,2 EN,1,1,2,9,9,17,18,25,25 EN,2,2,3,10,9,18,19,26,25 EN,3,3,4,11,10,19,20,27,26 EN,4,4,5,12,11,20,21,28,27 EN,5,5,6,13,12,21,22,29,28 EN,6,6,7,14,13,22,23,30,29 EN,7,7,242,243,14,23,258,259,30 MAT, 1 EN,8, 17, 18,25,_25,33,34,41,41 EN,9,18,19,26,25,34,35,42,41 EN,10,19,20,27,26,35,36,43,42 EN,11,20,21,28,27,36,37,44,43 EN,12,21,22,29,28,37,38,45,44 MAT,2 EN,13,22,23,30,29,38,39,46,45 EN,14,23,258,259,30,39,274,275,46 EN,15,33,34,41,41,49,50,57,57 EN,16,34,35,42,41,50,51,58,57 MAT,1 EN,17,35,36,43,42,51,52,59,58 EN,19,37,38,45,44,53,54,61,60 MAT,2 EN,20,38,39,46,45,54,55,62,61 EN,21,39,274,275,46,55,290,291,62

EA-SC-93-083-22 ATTACHMENT C Page C20

  • MAT,1 EN,22,49,50,57,57,65,66,73,73 EN,23,50,51,58,57,66,67,74,73 EN,24,51,52,59,58,67,68,75,74 EN,26,53,54,61,60,69,70,77,76 EPLOT MAT,2 EN,27,54,55,62,61,70,71,78,77 EN,28,55,290,291,62,71,306,307,78 MAT,5 EN,29,65,66,73,73,81,83,90,90 EN,30,73,74,90,90,66,67;83,83 MAT,1 EN,31,67,68,75,74,83,84,91,90 EN,33,69,70,77,76,85,86,93,92 MAT,2 EN,34,70,71,78,77,86,87,94,93 EN,35,71,306,307,78,87,322,323,94 MAT,4 EN,37,81,83,90,90,97,99,106,106 MAT,1 EN,38,83,84,91,90,99,100,107,106 EN,40,85,86,93,92,101,102,109,108 MAT,2 .

EN,41,86,87,94,93,102,103,110,109 EN,42,87,322,323,94,103,338,339,110 MAT,4 EN,44,97,99,106,106,113,115,122,122 MAT,1 EN,45,99,100,107,106,115,116,123,122 EN,47,101,102,109,108,117,118,125,124 MAT,2 EN,48,102,103,110,109,118,119,126,125 EN,49,103,338,339,110,119,354,355,126 EPLOT MAT,4 EN,51,113,115,122,122,129,131,138,138 MAT,1 EN,52,115,116,123,122,131,132,139,138 EN,54,117,118,125,124,133,134,141,140 MAT,2 EN,55,118,119,126,125,134,135,142,141 EN;56,119,354,355,126,135;370,371,142 MAT,4 EN,58,129,131,138,138,145,147,154,154 MAT,1 EN,59,131,132,139,138,147,148,155,154 EN,61,133,134,141,140,149,150,157,156 MAT,2 EN,62,134,135,142,141,150,151,158,157 EN,63,135,370,371,142,151,386,387,158 MAT,4 EN,65,145,147,154,154,161,163,170,170 EN,66,147,148,155,154,163,164,171,170 MAT, 1 .

EN,68, 149, 150, 15.7, 156, 165, 166, 173, 172 MAT,2 EN,69,150,151,158,157,166,167,174,173 EN, 70, 151,386,387, 158, 167,402,403, 174 EPLOT MAT,5 EN,71,161,163,170,170,177,178,185,185 EN,72,185,170,186,186,178,163,179,179 MAT,1 EN,73,163,164,171,170,179,180,187,186 EN,75,165,166,173,172,181,182,189,188 MAT,2

.EN,76,166,167,174,173,182,183,190,189 EN,77,167,402,403,174,183,418,419,190 MAT 1 I

EN,78,177,178,185,185,476,477,484,484

EA-SC-93-083-22 ATTACHMENT C Page C21 EN,79,178,179,186,185,477,478,485,484 EN,80,179,180,187,186,478,479,486,485 EN,82,181,182,189,188,197,198,205,204 MAT,2 EN,83,182,183,190,189,198,199,206,205 EN,84,183,418,419,190,199,434,435,206 MAT,3 EN,85,193,194,201,201,209,210,217,217 EN,86,194,195,202,201,210,211,218,217 MAT, 1 EN,87,195,196,203,202,211,212,219,218 EN,88, 196, 197,204,203,212,213,220,219 EN,89,197,198,205,204,213,468,472,220 MAT,2 EN,90,198,199,206,205,468,469,473,472 EN,91,199,434,435,206,469,470,474,473 MAT,1 EN,92,209,210,217,217,225,226,233,233 EN,93,210,211,218,217,226,227,234,233 EN,94,211,212,219,218,227,228,235,234 EN,95,212,213,220,219,228,229,236,235 EN,96,213,214,221,220,229,230,237,236 EPLOT TYPE,2 MAT,3 REAL,97 EN,97,8,144 REAL,98 EN,98,24,144 REAL,99 EN,99,40,144 REAL, 100 EN,100,56,144 REAL,101 EN, 101, n, 144 REAL,102 EN,102,88,144 REAL, 103 EN, 103, 104, 144 REAL,104 EN, 104, 120, 144 REAL,105 EN, 105, 136, 144 REAL, 106 EN, 106, 152, 144 REAL,107 EN, 107, 168, 144

  • . REAL, 108 EN, 108, 184, 144 REAL,109 EN,109,200,144 REAL,110 EN,110,216,144 REAL,.111 EN, 111,230~_241 REAL,97 . _,.

EN, 112, 15, 144 REAL,98 EN, 113,31,144 REAL,99 EN,114,47,144 REAL, 100 EN,115,63,144 REAL,101 EN,116,79,144 REAL,102 EN, 117,95, 144 REAL, 103 EN, 118, 111, 144 REAL,104 EN,119,127,144

EA-SC-93-083-22 ATTACHMENT C Page C22

  • REAL,105 EN, 120, 143, 144 REAL,106 EN, 121, 159, 144 REAL,107 EN, 122, 175, 144 REAL,108 EN, 123, 191, 144 REAL,109 EN, 124,207, 144 REAL,110 EN, 125,223, 144 REAL,111 EN, 126,237,241 REAL,127 EN, 127,52,53 REAL, 128 EN,128,68,69 REAL, 129 EN,129,84,85 REAL, 130 EN, 130, 100, 101 REAL,131 EN, 131, 116, 117 REAL, 132 EN, 132, 132, 133 REAL,133 EN, 133, 148, 149 REAL,134 EN, 134, 164, 165 REAL,135 EN, 135, 180, 181 REAL,127 EN,136,59,60 REAL, 128 EN, 137,75,76 REAL,129 EN,138,91,92 REAL,130 EN,139,107,108 REAL, 131 EN, 140, 123, 124 REAL, 132 EN, 141, 139, 140 REAL, 133 EN, 142, 155, 156 REAL,134 EN, 143, 171, 172 REAL, 135 EN, 144, 187, 188 REAL, 145 EN, 145, 193,209 REAL,146 EN,146,194,210 REAL, 146 EN, 147,201,217 REAL,148 EN,148,225,241 REAL,149 EN,149,227,241 REAL, 149 EN,150,234,241 REAL,151 EN,151,215,241 REAL,151 EN, 152,222,241 EPLOT TYPE, 1 REAL, 1 MAT,2 EN,153,242,8,15,243,258,24,31,259

EA*SC-93-083-22 ATTACHMENT C Page C23 EN,154,258,24,31,259,274,40,47,275 EN,155,274,40,47,275,290,56,63,291 EN,156,290,56,63,291,306,72,79,307 EN, 157,306, 72, 79*,307,322,88, 95 ,323 EN,158,322,88,95,323,338,104,111,339 EN,159,338,104,111,339,354,120,127,355 EN,160,354,120,127,355,370,136,143,371 EN,161,370,136,143,371,386,152,159,387 EN,162,386,152,159,387,402,168,175,403 EN,163,402,168,175,403,418,184,191,419 EN,164,418,184,191,419,434,200,207,435 EN,165,434,200,207,435,450,216,223,451 EPLOT TYPE,2 MAT,3 REAL, 166 EN,166,226,241 REAL, 166 EN,167,233,241 REAL,168 EN,168,214,241 REAL, 168 EN,169,221,241 EPLOT TYPE,1 REAL,1 MAT,1 EN,170,221,472,220,220,214,468,213,213 MAT,2 EN,171,468,469,473,472,214,215,222,221 EN,172,469,470,474,473,215,450,451,222 EN,173,470,471,475,474,450,216,223,451 MAT,10 EN,174,476,477,484,484,480,481,487,487 EN,175,477,478,485,484,481,482,488,487 MAT,1 .

EN,176,478,479,486,485,482,483,489,488 EN,177,480,481,487,487,193,194,201,201 EN,178,481,482,488,487,194,195,202,201 EN,179,482,483,489,488,195,196,203,202 EPLOT C*** END of Element Module

  • c*** LOAD MODULE C*** DEFINE INITIAL TEMPERATURES AND HEAT TRANSFER COEFFICIENTS TIME,0.0 ITER, 12,3,3 POSTR,, 1,3,2,3 LPRINT,0 KTEMP,-1 C*** CONVECTIVE HEAT TRANSFER C*** h=2 BTU/ft*Ft*F*Hr EC,17,3,2.000,AAAA EC,24,3,2.000,AAAA EC,31,3,2.000,AAAA EC,38,3,2.000,(0.5*T016+0.5*T032)

EC,45,3,2.000,T048 EC,52,3,2;000,(0.5*T064+0.5*T080)

EC,59,3,2.000,(0.5*T096+0.5*T112)

EC,66,3,2.000,(0.5*T128+0.5*T144)

EC,73,3,2.000,T144 EC,80,3,2.000,T144 EC,19,5,2.000,AAAA EC,26,5,2.000,AAAA EC,33,5,2.000,AAAA EC,40,5,2.000,(0.5*T016+0.5*T032)

EC,47,5,2.000,T048 EC,54,5,2.000,(0.5~T064+0.5*T080)

EC,61,5,2.000,(0.5*T096+0.5*T112)

EC,68,5,2.000,(0.5*T"128+0.5*T144)

EC,75,5,2.000,T144 EC,82,5,2.000,T144

EA-SC-93-083-22 ATTACHMENT C Page C24 EC,171,6,2.000,AAAA EC,172,6,2.000,AAAA EC,164,3,2.000,AAAA EC,96,6,2.000,AAAA EC,95,6,2.000,AAAA EC,94,6,2.000,AAAA EC,93,6,2.000,AAAA EC,92,6,2.000,AAAA EC,153,3,2.000,AAAA EC,154,3,2.000,AAAA EC,155,3,2.000,AAAA EC,156,3,2.000,AAAA EC,157,3,2.000,AAAA EC,158,3,2.000,AAAA EC,159,3,2.000,AAAA EC,160,3,2.000,AAAA EC,161,3,2.000,AAAA EC,162,3,2.000,AAAA EC,163,3,2.000,AAAA EC,165,3,2.000,AAAA EC,173,3,2.000,AAAA EC, 173,6,2.000,AAAA*

EC,179,3,2.000,T144 EC,176,3,2.000,T144 NT,144,TEMP,AAAA NT,241,TEMP,AAAA C*** ELEMENT TEMPERATURE Ma>ULE C*** INPUT HEAT GENERATION LOADS BTU/hr-ft*ft*ft QE,37,(336.2*0.97*GGGG/24.00)

QE,44,(336~2*1.20*GGGG/24.00)

QE,51,(336.2*1.17*GGGG/24.00)

QE,58,(336.2*1.10*GGGG/24.00)

QE,65,(336.2*0.77*GGGG/24.00)

QE,92,SOCO QE,93,SOCO QE,94,SOCO QE,95,SOCO QE,96,SOCO QE,153,SOSI QE,154,SOSI QE,155,SOSI QE,156,SOSI QE, 157,SOSI QE,158,SOSI QE, 159 I SOSI QE, 160,SOSI QE,161,SOSI

. QE, 162,SOSI QE, 163,SOSI QE,164,SOSI QE,165,SOSI QE,171,SOTO QE,172,SOTO QE, 173,SOTO ETLIST ,ALL MPLIST ,ALL RLIST ,ALL NLIST ,ALL ELI ST ,ALL ECLIST ,ALL NTLIST,ALL QELIST,ALL LWRITE TIME,0.0 ITER I -20, 20 I 20 LWRITE TIME,0.0 ITER, -40,20,20 LWRITE AFWRITE FINISH

EA*SC-93-083-22 ATTACHMENT c Page C25

/INPUT ,27 FINISH

  • . ~

EA-SC-93-083-22 ATTACHMENT D Page Dl ATTACHMENT D

( q pages)

ANSYS OUPUT

ATTlrc.tf Uf.AJT D PAGE 02.

ANSYS - ENGINEERING ANALYSIS SYSTEM REVISION 4.4 A 16 CONSUMERS POWER MAY 1, 1990 ANSYS(R) COPYRIGHT(C) 1971, 1978, 1982, 1983, 1985, 1987, 1989, 1990 SWANSON ANALYSIS SYSTEMS, INC. AS UNPUBLISHED WORK.

PROPRIETARY DATA - UNAUTHORIZED USE, DISTRIBUTION OR DUPLICATION IS PROHIBITED. ALL RIGHTS RESERVED.

FOR SUPPORT CALL LEROY N. REISS PHONE (517) 788-2344 TWX TITLE 9.2863 AUG 2, 1995 CP= 10. 770

          • ANSYS ANALYSIS DEFINITION CPREP7) *****

NEW TITLE= VCC-MSB-3 AMB= 0.0 F 5.97 KW AFTER 20 YEARS IN STORAGE PARA IUETC.ll. s OtJTPUT MSB 3_ 2a. ovT

/SHOW SWITCH PLOTS TO FILE BNCHVCC2.GEO - RASTER MODE.

SHRINK SET TO 0.3000 ANALYSIS TYPE= -1 (THERMAL ANALYSIS)

PARAMETER= GGGG 5.970 PARAMETER= AAAA O.OOOOE+OO PARAMETER= SOTO O.OOOOE+OO PARAMETER= SCSI O.OOOOE+OO PARAMETER= SOCO O.OOOOE+OO PARAMETER= SUMK 0.6194

  1. . !\~
  • r TOCA~*.,'\.

PARAMETER= TOAS 29.85 .,,..._

PARAMETER= DRHI 13.69 PARAMETER= TOOO O.OOOOE+OO PARAMETER= TAVE 14.92 C*** ******************************************************

C*** CALCLATIONS ARE VALID FOR 0 < TAVE <32 F

. C*** ******************************************************

PARAMETER= HEAT 0.2037E+05 PARAMETER= CPAI 0.2390 PARAMETER=.MFLO 0.7932 PARAMETER= *DENA* 0.8367E-01 C*** ******************************************************

C*** DP Stack DPST llLISt be equal to.DP Flow DPFL C*** ******************************************************

  • PARAMETER= DPST PARAMETER= DPFL o.7199e-01 0.7233E-01

. j

  • e.A - S C _ qS _ O8 ~ - L L Jr.IT Jr<.,t-1 Ai f NT D PAU'! D ?J
  • PARAMETER= DELT 29.98 C*** ********************************************************************

C*** Calculated Air outlet teq:> TOCA llPJSt be equal to assi.med value TOAS C*** ********************************************************************

pJi./LA Lt e.T ER.~ o tJf PuT PARAMETER= TOCA 29.98 PARAMETER= Q016 1562. ~~~?-20. OUT PARAMETER= Q032 2444.

PARAMETER= Q048 2716.

PARAMETER= Q064 2693.

PARAMETER= Q080 2648.

PARAMETER= Q096 2535.

PARAMETER= Q112 2376.

PARAMETER= Q128 2037.

PARAMETER= Q144 1358.

PARAMETER= T016 2.288

  • PARAMETER= T032 PARAMETER= T048 PARAMETER= T064 PARAMETER= TOSO 5.870 9.849 13.80 17.68 PARAMETER= T096 21.39 PARAMETER= T112 24.87 PARAMETER= T128 27.86 PARAMETER= T144 29.85 C*** ELEMENT TYPE MODULE C*** DEFINES THE ELEMENT TYPES ELEMENT TYPE 1 USES STIF 70 KEYOPTC1*9)= 0 0 0 0 0 0 0 0 0 INOPR= 0 NUMBER OF NODES= 8 ISOPAR. SOLID THERMAL CURRENT NODAL DOF SET IS TEMP THREE-DIMENSIONAL STRUCTURE ELEMENT TYPE 2 USES STI F 31 KEYOPT( 1*9)= 0 0 0 0 0 0 0 0 0 INOPR= 0 NUMBER OF NODES= 2 RADIATION LINK

t:-M-- _, __

' -'- - Q -

AIS'8 3 _2.Q. OUT J;rT A-c.ff M 6 NT D 7~ PE/l.A-IVA,E. tJu7 Pu T

- PA-<i"E D 4-ANSYS - ENGINEERING ANALYSIS SYSTEM REVISION 4.4 A 16 CONSUMERS POWER MAY 1, 1990 ANSYS(R) COPYRIGHT(C) 1971, 1978, 1982, 1983, 1985, 1987, 1989, 1990 SWANSON ANALYSIS SYSTEMS, INC. AS UNPUBLISHED WORK.

PROPRIETARY DATA - UNAUTHORIZED USE, DISTRIBUTION OR DUPLICATION IS PROHIBITED. ALL RIGHTS RESERVED.

FOR SUPPORT CALL LEROY N. REISS PHONE (517) 788-2344 TWX VCC-MSB-3 AMB= 0.0 F 5.97 KW AFTER 20 YEARS IN STORAGE 9.3898 AUG 2,1995 CP= 383.490

          • TEMPERATURE SOLUTION ***** TIME = O.OOOOOE+OO LOAD STEP= 3 ITERATION= 40 CUM.

ITER.= 72 NOOE TEMP NOOE TEMP NOOE TEMP NOOE TEMP NOOE TEMP

19. 728 2 18.176 3 13.743 4 13.589 5 12.537 6 11.662 7 6.9164 8 1.4032 9 ' 18. 176 10 13.743 11 13.589 12 12.537 13 11.662 14 6.9165 15 1.4033 17 24.559 18 23.143 19 20.334 20 19.847 21 17.319 22 16.597 23 7.1158 24 1.4351 25
23. 143 26 20.334 27 19.847 28 17.319 29 16.597 30 7.1159 31 1.4352 33 24.717 34 23.112 35 20.578 36 20.343 37 16.861 38 16.341 39 7.1548 40 1.4622 41 23.112 42 20.578 43 20.343 44 16.860 45 16.341 46 7 .1549 47 1.4623 49 26.087 50 23.668 51 21.613 52 21.023 53 16.397 54 16.223 55 7.1685 56 1.4676 57 23.668 58 21.615 59 21.023 60 16.397 61 16.223 62 7.1686 63 1.4677 65 26.227 66 23.626 67 21.807 68 22.036 69 15.892 70 15.930 71 7.2114 n 1.4675 73 23.626 74 21.810 75 22.029 76 15.892 77 15.930 78 7.2115 79 1.4676 81 110.63 83 32.369 84 32.175 85 14.278 86 14.322 87 7.3909 88 1.5057 90 32.134 91 31.966 92 14.276 93 14.321 94 7.3912 95 1.5057 97 136.98 99 48.924 100 48.634 101 15.660 102 15.632 103 8. 1923 104 1.6623 106 48.630 107 48.371 108 15.657 109 15.630 110

. 8. 1928 111 1.6623 113 149.27 115 56.886 116 56.579 117 19.699 118 19.639 119 9.5820 120 1.9897 122 56.554 123 56.283 124 19.696 125 19.636 126 9.5826 127 1.9898 129 154.81 131 61.959 132 61.743 133 25.179 134 25 .118 135 12.283 136 2.4113 138 61.657 139 61.470 140 25 .176 141 25 .116 142 12.283 143 2.4114 144 O.OOOOOE+OO 145 134.36

E.A-- .)C- q ~- 0 2 '- J_,Z.,

IS~ PE fl~IV/lf 01.iiPur ~ S8 3 - 2. D . OUT A,.iTlrCH AA ENI D l>A<dE. 0 s-147 61.315 148 60.802 149 28.695 150 28.608 151 13.763 152 2.6608 154 60.998 155 60.525 156 28.691 157 28.606 158 13.764 159 2.6609 161 115.08 163 46.407 164 45.895 165 26.931 166 26.855 167 12.750 168 2.4754 170 46.193 171 45.714 172 26.930 173 26.854 174 12.750 175 2.4755 177 22.979 178 22.920 179 24.198 180 24.475 181 21.928 182 21.812 183 9.7170 184 1.8560 185 22.928 186 24.179 187 24.450 188 21.928 189 21.812 190 9.7171 191 1.8561 193 17.504 194 17.944 195 17.433 196 17.037 197 16.357 198 16.415 199 5.7373 200 1.0331 201 17.945 202 17.429 203 17.051 . 204 16.357 205 16.415 206 5.7374 207 1.0332 209 5.6380 210 7.4616 211 13.730 212 14.089 213 14.339 214 13.725 215 1.7698 216 0.76870 217 7.4613 218 13.732 219 14.084 220 14.340 221 13.725 222 1.7698 223 0.76872 225 5.5853 226 7.4559 227 13.618 228 13.977 229 14.226 230 13.733 13.619 235 233 7.4558 234 13.974 236 14.226 237 13.734 241 O.OOOOOE+OO 242 1.4827 243 1.4828 258 1.5196 259 1.5198 274 1.5468 275 1.5469 290 1.5531 291 1.5532 306 1.5534 307 1.5535 322 1.5877 323 1.5878 338 1. 7610 339 1. 7611 354 2.0985 355

. 2.0986 370 2.5537 371 2.5538 386 2.8198 387 2.8199 402 2.6211 403 2.6212 418 1.9633 419 1.9635 434 1.0805 435 1.0806 450 0.81278 451 0.81280 468 13.914 469 1.9460 470 0.83491 471 0. 77589 472 13.914 473 1.9460 474 0.83495 475 0.77591 476 22.556 477 23.232 478 22.747 479 22.463 480 18.042 481 17.633 482 18.728 483 19.126 484 23.165 485 23.355 486 23.213 487 17.635 488 18.711 489 19.003 MAXIMUM TEMPERATURE= 154.81 AT NODE 129 MINIMUM TEMPERATURE= O.OOOOOE+OO AT NODE 241

_ _,. _____ IJ- _.-,---

ANSYS - ENGINEERING ANALYSIS SYSTEM REVISION 4.4 A 16 CONSUMERS POWER MAY 1, 1990 ANSYSCR) COPYRIGHT(C) 1971, 1978, 1982, 1983, 1985, 1987, 1989, 1990 SWANSON ANALYSIS SYSTEMS, INC. AS-UNPUBLISHED WORK.

PROPRIETARY DATA - UNAUTHORIZED USE, DISTRIBUTION OR DUPLICATION IS PROHIBITED. ALL RIGHTS RESERVED.

FOR SUPPORT CALL LEROY N. REISS PHONE (517) 788-2344 TWX TITLE 9.3978 AUG 2, 1995 CP= 10.660

          • ANSYS ANALYSIS DEFINITION CPREP7) *****

NEW TITLE= VCC-MSB-3 AMB= 0.0 F 3.885 KW AFTER 50 YEARS IN STORAGE M~B; _ ~- ovr

/SHOW SWITCH PLOTS TO FILE BNCHVCC2.GEO - RASTER MOOE.

SHRINK SET TO 0.3000 ANALYSIS TYPE= -1 (THERMAL ANALYSIS)

PARAMETER= GGGG 3.885 PARAMETER= AAAA O.OOOOE+OO PARAMETER= SOTO O.OOOOE+OO PARAMETER= SOS! O.OOOOE+OO PARAMETER= SOCO O.OOOOE+OO PARAMETER= SUMK 0.6194 PARAMETER= TOAS 22.25 ~ ToCP.. =L.:..?,~

PARAMETER= DRHI 13.69 PARAMETER= TOOO O.OOOOE+OO PARAMETER= TAVE 11.13 C*** ******************************************************

C*** CALCLATIONS ARE VALID FOR 0 < TAVE <32 F C*** ******************************************************

PARAMETER= HEAT 0.1326E+05 PARAMETER= CPAI 0.2390 PARAMETER= MFLO 0.6923 PARAMETER= OED 0.8426E-01 C*** ******************************************************

C*** DP Stack DPST rrust be equal to DP Flow DPFL C*** ******************************************************

  • PARAMETER= DPST PARAMETER= DPFL 0.5449E-01 0.5470E-01

EA- SC- q)_,_ oK~ _i,,z_,

JrTilt<-HM £NT 0 D7 P.+t;.t PARAMETER= DELT 22.34 C*** ********************************************************************

C*** Calculated.Air outlet t~ TOCA rrust be equal to assuned value TOAS C*** ********************************************************************

PA-11-1+ A.4 E.TER.. <; O()/ Pi.Ji PARAMETER= TOCA 22.34 PARAMETER= Q016 1016. N ~;g  ::; - ~-o . Dur PARAMETER= Q032 1591.

PARAMETER= Q048 1767.

PARAMETER= Q064 1753.

PARAMETER= Q080 1723.

PARAMETER= Q096 1650.

PARAMETER= Q112 1546.

PARAMETER= Q128 1326.

PARAMETER= Q144 883.7 PARAMETER= T016 1.706

  • PARAMETER= T032 PARAMETER= T048 PARAMETER= T064 PARAMETER= TOSO 4.377 7.344 10.29 13.18 PARAMETER= T096 15.95 PARAMETER= T112 18.55 PARAMETER= T128 20.77 PARAMETER= T144 22.25 C*** ELEMENT TYPE MODULE C*** DEFINES THE ELEMENT TYPES ELEMENT TYPE 1 USES STI F 70 KEYOPT( 1*9)= 0 0 0 0 0 0 0 0 0 INOPR= 0 NUMBER OF NODES= 8 ISOPAR. SOLID THERMAL CURRENT NODAL DOF SET IS TEMP THREE-DIMENSIONAL STRUCTURE ELEMENT TYPE 2 USES STIF 31 K.EYOPT(1 *9)= 0 0 0 0 0 0 0 0 0 INOPR= 0 NUMBER OF NODES= 2 RADIATION LINK

r;A.._sc_q.,_ 013_i,z..,

hrfTA-C.H A.I ENT D

  • OIJT Pur MS8~_!,7J,our ?AVE D~

ANSYS - ENGINEERING ANALYSIS SYSTEM REVISION 4.4 A 16 CONSUMERS POWER MAY 1,1990 ANSYS(R) COPYRIGHT(C) 1971, 1978, 1982, 1983, 1985, 1987, 1989, 1990 SWANSON ANALYSIS SYSTEMS, INC. AS UNPUBLISHED WORK.

PROPRIETARY DATA - UNAUTHORIZED USE, DISTRIBUTION OR DUPLICATION IS PROHIBITED. ALL RIGHTS RESERVED.

FOR SUPPORT CALL LEROY N. REISS PHONE (517) 788-2344 TWX VCC-MSB-3 AMB= 0.0 F 3.885 KW AFTER 50 YEARS IN STORAGE 9.5000 AUG 2,1995 CP= 378.330

          • TEMPERATURE SOLUTION ***** TIME = O.OOOOOE+OO LOAD STEP= 3 ITERATION= 40 CUM.

ITER.= 72 NOOE TEMP NOOE TEMP NOOE TEMP NOOE TEMP NOOE TEMP

13. 165 2 12.134 3 9.1846 4 9.0812 5 8.3765 6 7. 7927 7 4.6270 8 0.94004 9 12.134 10 9.1846 11 9.0811 12 8.3765 13 7.7926 14 4.6270 15 0.94010 17 16.349 18 15 .424 19 13.582 20 13.26D 21 11.589 22 11.110 23 4.m9 24 0.96308 25 15.424 26 13.582 27 13.260 28 11.589 29 11.110 30 4.m9 31 0.96313 33 16.454 34 15.403 35
13. 743 36 13.588 37 11.286 38 10.944 39 4.8027 40 0.98226 41 15.403 42 13.743 43 13.588 44 11.286 45 10.944 46 4.8028 47 0.98232 49 17.352 50 15.767 51 14.429 52 14.038 53 10.980 54 10.867 55 4.8125 56 0.98621 57 15.767 58 14.431 59 14.038 60 10.980 61 10.866 62 4.8125 63 0.98627 65 17.444 66 15. 738 67 14.558 68 14.709 69 10.647 70 10.674 71 4.8419 72 0.98659 73 15. 738 74 14.560 75 14.705 76 10.647 n 10.674 78 4.8419 79 0.98665 81 72.745 83 21.564 84 21.437 85 9.5939 86 9.6217 87 4.9654 88 1.0166 90 21.411 91 21.301 92 9.5928 93 9.6211 94 4.9655 95 1.0166 97 90.290 99 32.859 100 32.670 101 . 10.653 102 10.635 103 5.5953 104 1.1344 106 32.668 107 32.498 108 10.651 109 10.634 110 5.5955 111 1.1344 113 98.578 115 38.550 116 38.351 117 13.597 118 13 .554 119 6.6140 120 1.3n9 122 38.334 123 38.158 124 13.595 125 13.553 126 6.6143 127 1.3780 129 102.86 131 42.475 132 42.334 133 17.659 134 17 .617 135 8.6229 136 1.6946 138 42.279 139 42. 157 140 17.657 141 17.616 142 8.6231 143 1.6947 144 O.OOOOOE+OO 145 89.937

A,.7T)rUf!J EIV1 D

" ~ PE-ILA-TUU OvT1'VI ~ s~ ~ _ sz:J. oul 1A<iE. DC(

147 42.532 148 42.200 149 20.456 150 20.395 C) 42.019 151 9.8200 152 1.8997 154 42.326 155 156 20.454 157 20.393 158 9.8203 159 1.8998 161 77.515 163 32.874 164 32.539 165 19.597 166 19.541 167 9.2646 168 1. 7932 170 32.735 171 32.422 172 19.596 173 19.540 174 9.2648 175

1. 7933 177 16.882 178 16.839 /

179 17. 791 180 17.979 181 16. 161 182 16.073 183 7.1284 184 1.3572 185 16.846 186 17.774 187 17.958 188 16.161 189 16.073 190 7.1285 191 1.3573 193 12.921 194 13.246 195 12.870 196 12.580 197 12.083 198 12. 125 199 4.2242 200

o. 75808 201 13.246 202 .12.867 203 12.590 204 12.083 205 12.125 206 4.2242 207 0.75813 209 4.1317 210 5.4813 211 10.144 212 10.408 213 10.593 214 10.141 215 1.3045 216 0.56534 217 5.4811 218 10.145 219 10.404 220 10.593 221 10.141 222 1.3045 223 0.56535 225 4.0928 226 5.4776 227 10.061 228 10.325 229 10.509 230
10. 147 233 5.4775 234 10.061 235 10.323 236 10.509 237 10.147 241 O.OOOOOE+OO 242 0.99322 243 0.99329 258 1.0199 259 1.0200 274 1.0391 275 1.0392 290 1.0436 291 1.0437 306 1.0444 307 1.0445 322 1.0716 323 1.0716 338 1.2020 339 1.2020 354 1.4529 355 1.4530 370
1. 7946 371 1. 7947 386 2.0132 387 2.0133 402 1.8991 403 1.8993 418 1.4358 419 1.4359 434 0.79287 435 0.79293 450 0.59780 451 0.59781 468 10.280 469 1.4344 470 0.61395 471 0.57063 472 10.280 473 1.4344 474 0.61398 475 0.57064 476 16.574 477 17.069 478 16.739 479 16.539 480 13.315 481 13.016 482 13.819 483 14. 111 484 17.020
  • - 485 17.180 486 17.082 487 13.018 488 13.807 489 14.021 MAXIMUM TEMPERATURE= 102.86 AT NODE 129 MINIMUM TEMPERATURE= O.OOOOOE+OO AT NODE 241
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