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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
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

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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- 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of MSB Shield Lid Plate After 20 years and 50 years INITIATION AND REVIEW Calculation Status Preliminary Pending Final Superseded D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 Descripdon By Detail Qual d

Appd By Date Alt Cale Review Test By Date By P. Hoang 8/l819S (J1t*

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PALIS ADES NUCLEAR PLANT ANALYSIS CONTINUATION SHEET EA-SC-93-083-22 1.0 OBJECTIVE 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 1 OCFR72, 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.

Sheet _2_ Rev #

0 Reference/Comment

2.0 ANALYSIS INPUT PALISADES NUCLEAR PLANT ANALYSIS CONTINUATION SHEET 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 EA-SC-93-083-22 Sheet _3_ Rev # 0 Reference/Comment

PALISADES NUCLEAR PLANT ANALYSIS CONTINUATION SHEET EA-SC-93-083-22 2.3 EXISTING ANALYSIS 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.

Sheet _4_ Rev #

0 Reference/Comment

PALISADES NUCLEAR PLANT ANALYSIS CONTINUATION SHEET EA-SC-93-083-22 2.9 HEAT GENERATION RATES 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.

Sheet _5 _ Rev #

0 Reference/Comment

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PALISADES NUCLEAR PLANT ANALYSIS CONTINUATION SHEET EA-SC-93-083-22 4.2 THERMAL HYDRAULIC CALCULATION 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 1 O 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).

Sheet _6_ Rev # 0 Reference/Comment

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PALISADES NUCLEAR PLANT ANALYSIS CONTINUATION SHEET EA-SC-93-083-22 Im' 5.1.3 Check the Heat Load Rate Interpolation Functions Against the Input 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 1 OCFR72,236(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 Sheet _7_ Rev # 0 Reference/Comment

emwn*

&ii PALISADES NUCLEAR PLANT ANALYSIS CONTINUATION SHEIT EA-SC-93-083-22 and converted to Kilowatt. The total heat generation is the sum of 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 Sheet _8 _ Rev # 0 Reference/Comment

PALISADES NUCLEAR PLANT ANALYSIS CONTINUATION SHEET EA-SC-93-083-22 and the ambient temperature. The relationship among the above 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 Sheet _9_ Rev # 0 Reference/Comment

PALISADES NUCLEAR PLANT ANALYSIS CONTINUATION SHEET EA-SC-93-083-22 assumed VCC outlet air temperature (TOAS) are the input to this 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 Sheet 10 Rev# 0 Reference/Comment

PALISADES NUCLEAR PLANT ANALYSIS CONTINUATION SHEET EA-SC-93-083-22 and the following air properties which are applicable for 0°F ambient 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 Input Name Date MSB3-20 MSB3-50 Computer Input Files (No File Extension)

Analysis Description 08/02/95 08/02/95 Heat Gen. 5.97 KW, Amb o °F Heat Gen. 3.885 KW, Amb o °F 5.3.2 List of Computer Output Files Output Name.

MSB3-20.0UT MSB3-50.0UT Table 5.3.2 Computer Output Files Date 08/02/95 08/02/95 Analysis Description Heat Gen. 5.97 KW, Amb o °F 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 Sheet 11 Rev #

0 Reference/Comment

PALISADES NUCLEAR PLANT ANALYSIS CONTINUATION SHEET EA-SC-93-083-22 5.3.4 Warning Massages 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.

Sheet 12 Rev#

0 Reference/Comment

/1~JS/5 VCC THERMAL CHARACTERISTICS FOR S-* 11 R.~Jut..IS A,'ok: VSC:tl 3; !>.<t1 kW

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Attachment A

( 13 pages )

EA-SC-93-083-22 Attachment A Rev. : 0 Page Al HEAT GENERATION RATE CALCULATION

.SPENT FUEL HEAT LOAD CURVES EA-SC-93-083-22 ATTACHMENT A PAGE 1 File Name: NUREG.MCD

,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 :

2.222* 106 2.165* 106 2.173* 106 2.17* 106 2.149* 106 2.102*106 71832 77597 80557 83617 86349 90862 40350 44554 46852 49271 51423 54968 26867 30426 32266 34269 36151 39312 20814 24126 25750 27546 29293 32283 17019 20171 21648 23301 24953 27834 12243 15124 16388 17831 19333 22027 6338.7 8504.7 9406.4 10470 11630 13807

,pp.=

3100.4 4418.8 5017.8 5748 6542.7 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 261.07 415.52 511.03 630.52 740.68 899.42

,i:=O.. (rows(pp)-1) 230.62 368.66 451.74 556.l 652.07 784.54 j := 0.. (cols(pp) - 1)

.Bum-up level data:

EA-SC-93-083-22 ATIACHMENTA PAGE2 File Name: NUREG.MCD

.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

.n := 0.. 5

.m := 11 2000

/

v v

1500 soo

~

J/~

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.

[

]

H. : = linte11' RL, ~p T) 1

, 10 I

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)

3.0 Plot the afterheat power curves i := 0.. (rows( pp) - l) j.=O.. (cols(pp)- l)

EA-SC-93-083-22 ATTACHMENT A PAGE4 File Name: NUREG.MCD DRY CASK HEAT LOAD CURVES I\\\\

\\\\\\I"'-.

~\\ ~ ~~'a-._

1000 \\'~ ~

t:::-===:::::::

~

""'-.... - ~

100 5000

-+-

lOGWD/MTU 18GWD/MTU 27 GWD/MTU

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

-e-SSGWD/MTU

~

r--

--~

u*104 Time (days)

-A-r-

...--...A 2.s*104 3*104 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. *)

l,J 1,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

[

-

]

-Kn, i = linterp RL, ~ T)

, B0 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) 4 1*10

~ Kw(t, 18)

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~ Kw(t,27) j Kw(t,33)

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i:: Kw(t,40) 1000 100
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-+- lOGWD/MTU 18GWD/MTU 27GWD/MTU
-+- 33 GWD/MTU 40GWD/MTU
.4 1*10 t
Time in days Figure A.3 Plot of interpolation function KW(t,b)
.4 l.5* 10
- ~ -
- - -V"V
.4
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 pp11 2 = 759.66 OK Kw(20*365, 33) = 948.34 PPu, 3 = 948.34 OK Kw(10-365,40) = 1.542* 103 pp10, 4 =1.542*10 3 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 LoadY ear : = 94 Cooling time prior to loading numday(month,day,year) :=(LoadMonth-month)*30+Load.Day-day+ (LoadYear-year)*365 time. :=numday(DDate. 0,DDate. 1,DDate. 2) l l,
l, l,
Heat load per cell on loading Kw(time.,BurnUp.)*Initial U.
HeatLoad. * -
1 1
1 I
1000
. i
Discharge Date
,Cell Wt(MTU)
~MWD/MTU)
.month Day
,Year
,i + 1
,Initial_ U i 0.415 30.26 2
0.415 33.027 3
0.415 33.027 4
0.387 35.117 5
0.4 12.99 6
0.386 35.333 7
0.385 35.333 8
0.387 31.414 9
0.402 13.366 IO 0.402 13.911 11 0.401 12.99 12 0.416 28.128 13 0.416 28.824 14 0.387 35.117 15 0.402 13.626 16 0.401 13.626 17 0.387 35.117 18 0.415 30.26 19 0.416 28.128 20 0.386 35.173 21 0.387 35.173 22 0.416 33.027 23 0.416 30.26 24 0.415 30.353
.Total Heat Load
.DDatei,O.DDatei, l 8
29 8
29 8
29 8
12 6
8 29 8
29 8
12 6
6 6
8 29 8
29 8
12 6
6 8
12 8
29 8
29 8
12 8
12 8
29 8
29 8
29 23
,TotalHeat := L HeatLoadi i=O
,TotalHeat = 9.034 Kw
.DDatei 2 81 81 81 83 78 81 81 83 78 78 78 81 81 83 78 78 83 81 81 83 83 81 81 81 EA-SC-93-083-22 ATIACHMENTA PAGE7 File Name: NUREG.MCD
,Cooling Time
~KW)
(Days)
,timei JieatLoadi 4677 0.425 4677 0.475 4677 0.475 3964 0.497 6005 0.133 4677 0.471 4677 0.47 3964 0.433 6005 0.134 6005 0.147 6005 0.134 4677 0.396 4677 0.411 3964 0.497 6005 0.147 6005 0.147 3964 0.497 4677 0.425 4677 0.396 3964 0.496 3964 0.497 4677 0.477 4677 0.426 4677 0.425
.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.
,7.0 Heat load *after 20 years in storage for VCC number 3
,timei *= timei + 20* 365 Kw(time.,BumUp.)*Initial U.
JleatLoad. := ---
1---
1 ----
1 I
1000 EA-SC-93-083-22 ATIACHMENTA PAGES File Name: NUREG.MCD
,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. 0 DDate. 1 l,
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
Total Heat Load after 20 years T ota!Heat : =
23 I: HeatLoad.
I i = 0 Tota!Heat = 5.97 Kw 8.0 Heat load after 50 years in storage for MSB number 3 time. :=time.+ 30-365 I
I Kw(time.,BumUp.)*Initial U.
HeatLoad. : =
1 1
1 I
1000 EA-SC-93-083-22 ATTACHMENT A PAGE9 File Name: NUREG.MCD Table A.2 Heat Load of MSB-3 after 50 years in storage Discharge Date Cell Wt(MTU) (MWDIMTU) month Day Year Cooling Time (KW)
(Days) i + 1 Initial U.
I BumUp.
I 0.415 30.26 2
0.415 33.027 3
0.415 33.027 4
0.387 35.117 5
0.4 12.99 6
0.386 35.333 7
0.385 35.333 8
0.387 31.414 9
0.402 13.366 10 0.402 13.911 11 0.401 12.99 12 0.416 28.128 13 0.416 28.824 14 0.387 35.117 15 0.402 13.626 16 0.401 13.626 17 0.387' 35;117 18 0.415 30.26 19 0.416 28.128 20 0.386 35.173 21 0.387 35.173 22 0.416 33.027 23 0.416 30.26 24 0.415 30.353 DDate. 0 I,
DDate. 1 I,
8 29 8
29 8
29 8
12 6
8 29 8
29 8
12 6
6 6
8 29 8
29 8
12
. 1 6
6 8
12 8
29 8
29 8
12 8
12 8
29 8
29 8
29 DDate. 2 I,
81 81 81 83 78 81 81 83 78 78 78 81 81 83 78 78 83 81 81 83 83 81 81 81 time.
HeatLoad.
I I
22927 22927 22927 22214 24255 22927 22927 22214 24255 24255 24255 22927 22927 22214 24255 24255 22214 22927 22927 22214 22214 22927 22927 22927 0.185 0.205 0.205 0.208 0.06 0.202 0.202 0.183 0.06 0.066 0.06 0.173 0.179 0.208 0.066 0.066 0.208 0.185 0.173 0.207 0.208 0.205 0.185 0.185
Total Heat Load after 50 years 23 Totillleat - L i = 0 HeatLoad.
l Total.Heat = 3.885 Kw 9.0 Heat load after 20 years in storage for MSB number 4 dd : = READPRN( rnsbn4) dd<o>
Initial U : = --
106
<o>
<2>
DDate
=dd DDate<2> :=dd<4>
dd<l>
BUi:nUp : = --
1000 time. :=num.day(DDate. 0,DDate. 1,DDate. 2) + 20*365 l
l, l,
1, Heat load per cell an loading Kw(time.,BumUp.)*Initial U.
HeatLoad. : =
1 1
1 l
1000 r * - -:-93-083-22
." ' ' '\\CHMENT A PAGE10 File Name.: NUREG.MCD
EA-SC-93-083-22 A TT AC HM ENT A PAGE 11 File Name: NUREG.MCD Table A.3 Heat Load of MSB-4 after 20 years in storage Cell Wt(MTU) (MWD/MTU) i + 1 2
3 4
5 6
7 8
9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 Initial U.
I BurnUp.
I 0.415 30.343 0.415 30.26 0.416 30.585 0.387 35.117 0.402 13.626 0.416 30.585 0.415 30.343 0.387 35.117 0.401 13.626 0.404 13.366 0.401 13.11 0.415 30.353 0.414 33.629 0.388 33.517 0.401 13.366 0.387 35.333 0.387 34.93 0.415 33.629 0.415 31.787 0.387 33.517 0.387 35.173 0.415 30.26 0.416 30.26 0.401 12.99 Total Heat Load after 20 years Discharge Date month Day Year DDate. 0 I,
DDate. 1 I,
DDate. 2 l,
8 29 81 8
29 81 8
29 81 8
12 83 1
6 78 8
29 81 8
29 81 8
12 83 6
78 6
78 6
78 8
29 81 8
29 81 8
12 83 6
78 8
29 81 8
12 83 8
29 81 8
29 81 8
12 83 8
12 83 8
29 81 8
29 81 6
78 23 T otalHeat : = L HeatLoad.
I i= 0 TotalHeat = 6.035 Kw Cooling Time (KW)
(Days) time.
I 11977 11977 11977 11264 13305 11977 11977 11264 13305 13305 13305 11977 11977 -
11264 13305 11977 11264 11977 11977 11264 11264 11977 11977 13305 HeatLoad.
0.282 0.282 0.293 0.322 0.102 0.293 0.282 0.322 0.102 0.094 0.093 0.282 0.324 0.313 0.093 0.312 0.322 0.324 0.303 0.312 0.322 0.282 0.283 0.093 l
1 a.a Heat load after 50 years in storage for MSB number 4 time. :=nwnday(DDate. 0,DDate. 1,DDate. 2) + 50*365 l
1, l,
l, Heat load per cell on loading Kw(time., Burn Up.)* Initial U.
HeatLoad. : =
1 1
1 I
1000 EA-SC-93-a83-22 ATIACHMENTA PAGE12 File Name: NUREG.MCD Table A.4 Heat Load of MSB-4 after sa years in storage Cell Wt(MTU) (MWD/MTU) month Burn Up.
I DDate. 0 1,
i + l Initial U.
I 0.415 30.343 8
2 0.415 30.26 8
3 0.416 30.585 8
4 0.387 35.117 8
5 0.402 13.626 1
6 0.416 30.585 8
7 0.415 30.343 8
8 0.387 35.117 8
9 0.401 13.626 l
10 0.404 13.366 1
11 0.401 13.11 1
12 0.415 30.353 8
13 0.414 33.629 8
14 0.388 33.517 8
15 0.401 13.366 16 0.387 35.333 8
17 0.387 34.93 8
18 0.415 33.629 8
19 0:415.
31.787 8
20 0.387 33.517 8
21 0.387 35.173 8
22 0.415 30.26 8
23 0.416 30.26 8*
24 0.401 12.99 Discharge Date Day Year DDate. 1 I,
DDate. 2 1,
29 81 29 81 29 81 12 83 6
78 29 81 29 81 12 83 6
78 6
78 6
78 29 81 29 81 12 83 6
78 29 81 12 83 29 81 29 81 12 83 12 83 29 81 29 81 6
78 Cooling Time (KW)
(Days) time.
HeatLoad.
I 22927 22927 22927 22214 24255 22927 22927 22214 24255 24255 24255 22927 22927 22214 24255 22927 22214 22927 22927 22214 22214 22927 22927 24255 0.185 0.185 0.192 0.208 0.066 0.192 0.185 0.208 0.066 0.061 0.06 0.185 0.211 0.202 0.06 0.203.
0.208 0.211 0.198 0.202 0.208 0.185 0.185 0.06 I
Total Heat Load after 50 years 11.0 Result Summary 23 Tota!Heat := 2: HeatLoad.
I i = 0 Tota!Heat = 3.925 Kw 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 A PAGE13 File Name: NUREG.MCD
Attachment B (4 pages)
FUEL DATA EA-SC-93-083-22 Attachment B Rev.: 0 Page Bl
VSC-24 STORAGE SHEET VCC Number:
1 EA-SC - q 3 _ 08'~ _ 2 2-
/+TT ACH AA ENT I;
PA-<iE r;2 MSB Number:
1 Date MSB Loaded: oS"-07-93@003'-f Isl asse"'"f Storage Pad Position:
.1.
Placement Date: M0.1 I 2 1 l'1Cf3 Comments:
FUEL ASSEMBLY LISTING
~
Fuel Assembly Parameters ID No Initial u Initial U Burn up 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
G-06 3.00 387,248 33,997.0 n
09-25-92 7
G-07 3.00 387,815 33,997.0 II 09-25-92 8
G-08 3.00 387,372 33,997.0 II 10-05-92 9
G-09 3.00 388,101 33,516.6 II 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 20 G-21 3.00 385,931 30,972.2 n
10-09-92 21 G-22 3.00
_-387,641 32,410.2 II 10-09-92 22 G-23 3.00 387,841 32,410.2 II 10-09-92 23 G-24
3. 00.
387,677
3 0, 9 72. 2 II 10-09-92 24 G-25 3.00 387,993 32,722.6 II 10-09-92
C:A,SC-q~- 08 ~ - 2. 2 A-TTlrCH MEN7
.g VSC-24 STORAGE SHEET PA-G-E e,~
MSB Number:
Z VCC Number:
z..
Date MSB Loaded: 5-JlJ-Cf 3 Storage Pad Position:
2 Placement Date: 5--16-93 Comments:
PUEL ASSEMBLY LISTING
~
Fuel Assembly Parameters ID No Initial U Initial U Burn up 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
G-33 3.00 388,150 33,516.6 n
10-09-92 7
G-34 3.00 387,834 33,516.6
n 10-09-92 8
G-37 3.00 387,458
.31,413.8 n
09-25-92 9
G-38 3.00 386,736 34,929.8 II 10-09-92 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 20 G-54 3.00 386,371 34,929.8 n
10-14-92 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
VCC Number:
Date MSB Loaded:
Storage Pad Position:
Comments:
MSB Cell No.
ID No 1
EFOOOO 2
EF0001 3
EF0002 4
G026 5
XF02 6
D102 7
E014 8
G068 9
XF08 10 XF09 11 XF10 12 EF0011 13 EF0013 14 G047 15 XF15 16 XF16 I
17 G051 I
18 EF0014 19 EF0016 I
20 GOSS 21 G056 22 EF0018 23 EF0019 24 EFOOOH VSC-24 STORAGE SHEET 3
MSB Number:
6/20-6/21 /94 EA-sc_q3_ Of?-2.2-A-TT AC..tf A.I E: N 7
(~
PMiE &If 3
3 Placement Date:
6/30/94 FUEL ASSEMBLY LISTING Fuel Assembly Parameters Initial U Initial U Burn up Discharge Visual Enr (w/o)
Wt <al lMWD/MTlJ)
Date Exam Date 2.74 415,213 30,260 08/29/81 04/07/94 2.74 415,470 33,027 08/29/81 04/11/94.
2.74 415,208 33,027 08/29/81 04/11/94 "
3.00 386,826 35,117 08/12/83 01/24/94.
1.51 400,106 12,990 01/06/78 04/07/94 :
3.05 385,792 35,333 08/29/81 01/19/94 3.05 385,292 35,333 08/29/81 04/06/94 3.00 387,137 31,414 08/12/83 03/18/93 1.5 401,697 13,366 01/06/78 01/19/94 1.5 401,583 13,911 01/06/78.
04/06/94 1.5 400,690 12,990 01/06/78 04/08/94 2.74 415,913 28,128 08/29/81 03/21/94 2.74 416,121 28,824 08/29/81 03/21/94 3.00 387,028 35, 117
08/12/83 04/07/94 1.5 401,962 13,626 01/06/78 04/05/94 1.51 401,039 13,626 01/06/78 04/08/94 3.00 386,875 35,117 08/12/83 03/30/94 2.74 415,481 30,260 08/29/81 03/21/94 2.74 415,795 28,128 08/29/81 03/25/94 3.00 386,489 35,173 08/12/83 03/31/94.
3.00 386,901 35,173 08/12/83 04/04/94 2.74 415,751 33,027 08/29/81 01/13/94 2.74 415,660 30,260 08/29/81 04/05/94 2.74 415432 30353 08/29/81 04/11/94
VCC Number:
Date MSB Loaded: -
Storage Pad Position:
Comments:
MSB Cell No.
ID No 1
EFOOOC 2
EFOOOX 3
EFOOOY 4
G061 5
XF20 6
EFOOOZ 7
EF001G 8
G062 9
XF22 10 XF30 11 XF46 12 EF001H 13 EF001J 14 G065 15 XF51 16 E065 17 G066 18 EF001K 19 EF001R 20 G067 21 G030 22 EF0006 23 EF0010 24 XF53
.eA- - s c -. q? -
0.v.; - 2 z.,
VSC-24 STORAGE SHEET
~Tl.+uf A.I ENT
~
p~ &5 4
MSB Number:
Placement Date:
FUEL ASSEMBLY LISTING Fuel Assembly Parameters Initial U Enr (w/o) 2.74 2.74 2.75 3.00 1.50 2.73 2.74 3.00 1.51 1.50 1.50 2.74 2.73 3.00 1.50 3.05 3.00 2.73 2.74 3.00 3.00 2.74 2.74 1.51 Initial U wt (a) 415,192 415,199 415,810 387,249 401,817 415,647 415,453 387,358 401,013 404,306 401,473 415,333 414,477 387,876 401,056 386,524 386,896 415,010 414,830 387,422 386,654 415,135 415,726 400975 EAvg XFAvg
. GAvg Burn up (MWD/MTU) 30,343 30,260 30,585 35, 117 13,626 30,585 30,343 35,117 13,626 13,366 13, 110 30,353 33,629 33,517 13,366 35,333 34,930 33,629 31,787 33,517 35,173 30,260 30,260 12 990 29585 17071 34562 Heat Discharge Visual Load Date Exam Date (KW) 08/29/81 03/30/94 0.4152 08/29/81 03/31/94 0.4152 08/29/81 01/10/94 0.4158 08/12/83 04/08/94 0.5034 01/06/78 01/18/94 0.2009 08/29/81 04/04/94 0.4156 08/29/81 04/11/94 0.4155 08/12/83 01/20/94 0.5036 01/06/78 03/31/94 0.2005 01/06/78 04/07/94 0.2022 01/06/78 01/14/94 0.2007 08/29/81 04/11/94 0.4153 08/29/81 04/11/94 0.4559 08/12/83 03/28/94 0.5042 01/06/78 04/06/94 0.2005 08/29/81 04/05/94 0.4638 08/12/83 01/21/94 0.5030 08/29/81 04/11/94 0.4565 08/29/81 04/05/94 0.4563 08/12/83 03/30/94 0.5036 08/12/83 04/08/94 0.5027 08/29/81 04/11/94 0.4151 08/29/81 04/11/94 0.4157 01/06/78 01/18/94 0.2005 Total Ht I 9.381
EA-SC-93-083-22 Attachment C Rev.: 0 Page Cl Attachment C (2.~pages )
ANSYS INPUT DECK
/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 11TOAS" 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 C2
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 C3
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 C4
I.
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 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 cs
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 C6
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 C7
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 C8
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 I 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 t
EA-SC-93-083-22 ATTACHMENT C Page C9
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 C10
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 C11
L 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 EA-SC-93-083-22 ATTACHMENT C Page C12
/INPUT,27 FINISH EA-SC-93-083-22 ATTACHMENT C Page C13
/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
Total Heat Generation of MSB assembly K'J/MSB AAAA=0.00
Ant>ient Air Tell1)erature 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
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 11TOAS 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 C14
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 C15
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 C16
L 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 EA-SC-93-083-22
- ATTACHMENT C Page C17
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 C18
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 C19
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 I 1 EN,78,177,178,185,185,476,477,484,484 EA-SC-93-083-22 ATTACHMENT C Page C20
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 C21
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 C22
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 C23
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 C24
/INPUT,27 FINISH
~
EA*SC-93-083-22 ATTACHMENT c Page C25
ATTACHMENT D
( q pages)
ANSYS OUPUT EA-SC-93-083-22 ATTACHMENT D Page Dl
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 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
/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
r
!\\~
PARAMETER= TOAS 29.85 TOCA~*.,'\\.
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 PARAMETER= CPAI PARAMETER=.MFLO PARAMETER= *DENA*
0.2037E+05 0.2390 0.7932 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
9.2863 AUG PARA IUETC.ll. s OtJTPUT MSB 3_ 2a. ovT
PARAMETER= DELT 29.98
e.A - S C _ q S _ O 8 ~ - L L Jr. IT Jr<.,t-1 Ai f NT D PAU'!
D ?J C*** ********************************************************************
C*** Calculated Air outlet teq:> TOCA llPJSt be equal to assi.med value TOAS C*** ********************************************************************
PARAMETER= TOCA 29.98 PARAMETER= Q016 1562.
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 5.870 PARAMETER= T048 9.849 PARAMETER= T064 13.80 PARAMETER= TOSO 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 INOPR= 0 NUMBER OF NODES=
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 INOPR= 0 NUMBER OF NODES=
RADIATION LINK 0
8 0
2 0
0 0
0 0
0 0
0 0
0 p Ji./LA Lt e.T ER.~ o tJf PuT
~~~?-20. OUT
t:-M--
Q 7~ PE/l.A-IVA,E.
tJu7 Pu T AIS'8 3 _ 2.Q. OUT J;rT A-c.ff M 6 NT D 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
~ S 8 3 - 2. D. O UT A,.iT lrCH 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 13.733 233 7.4558 234 13.619 235 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 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
/SHOW SWITCH PLOTS TO FILE BNCHVCC2.GEO
- RASTER MOOE.
SHRINK SET TO ANALYSIS TYPE= -1 PARAMETER= GGGG PARAMETER= AAAA PARAMETER= SOTO PARAMETER= SOS!
PARAMETER= SOCO PARAMETER= SUMK PARAMETER= TOAS PARAMETER= DRHI PARAMETER= TOOO PARAMETER= TAVE 0.3000 (THERMAL ANALYSIS) 3.885 O.OOOOE+OO O.OOOOE+OO O.OOOOE+OO O.OOOOE+OO 0.6194 22.25
~ ToCP.. =L.:..?,~
13.69 O.OOOOE+OO 11.13 C*** ******************************************************
C*** CALCLATIONS ARE VALID FOR 0 < TAVE <32 F C*** ******************************************************
PARAMETER= HEAT PARAMETER= CPAI PARAMETER= MFLO PARAMETER= OED 0.1326E+05 0.2390 0.6923 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 9.3978 AUG M~B; _ ~- ovr
PARAMETER= DELT 22.34 C*** ********************************************************************
C*** Calculated.Air outlet t~ TOCA rrust be equal to assuned value TOAS C*** ********************************************************************
EA-SC-q)_,_ oK~ _i,,z_,
JrTilt<-HM £NT 0 P.+t;.t D 7 PARAMETER= TOCA PARAMETER= Q016 22.34 1016.
PA-11-1+ A.4 E.TER.. <;
O()/ Pi.Ji 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 4.377 PARAMETER= T048 7.344 PARAMETER= T064 10.29 PARAMETER= TOSO 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..,
hrfT A-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 2,1995 CP=
378.330
TEMPERATURE ITER.=
72 NOOE TEMP TEMP
13. 165 8.3765 6
7. 7927 9.1846 11 9.0811 0.94010 13.26D 21 11.589 15.424 26 13.582 4.m9 31 0.96313
13. 743 36 13.588 0.98226 41 15.403 10.944 46 4.8028 15.767 51 14.429 4.8125 56 0.98621 10.980 61 10.866 17.444 66
15. 738 10.674 71 4.8419 14.705 76 10.647 81 72.745 9.5939 86 9.6217 21.411 91 21.301 1.0166 32.670 101
. 10.653 106 32.668 5.5955 111 1.1344 38.550 116 38.351 1.3n9 13.553 126 6.6143 131 42.475 8.6229 136 1.6946 17.657 141 17.616 89.937 SOLUTION *****
TIME =
NOOE TEMP 2
12.134 7
4.6270 12 8.3765 17 16.349 22 11.110 27 13.260 37 11.286 42 13.743 47 0.98232 52 14.038 57 15.767 62 4.8125 67 14.558 72 0.98659 n
10.674 87 4.9654 92 9.5928 97 90.290 102 10.635 107 32.498 117 13.597 122 38.334 127 1.3780 132 42.334 142 8.6231 O.OOOOOE+OO LOAD STEP=
NOOE TEMP 3
9.1846 8 0.94004 13 7.7926 18 15.424 23 4.m9 28 11.589 33 16.454 38 10.944 43 13.588 53 10.980 58 14.431 63 0.98627 68 14.709 73
15. 738 78 4.8419 83 21.564 88 1.0166 93 9.6211 103 5.5953 108 10.651 113 98.578 118 13.554 123 38.158 133 17.659 138 42.279 143 1.6947 9.5000 AUG 3
ITERATION=
NOOE TEMP 4
9.0812 9
12.134 14 4.6270 19 13.582 24 0.96308 29 11.110 34 15.403 39 4.8027 44 11.286 49 17.352 54 10.867 59 14.038 69 10.647 74 14.560 79 0.98665 84 21.437 94 4.9655 99 32.859 104 1.1344 109 10.634 119 6.6140 124 13.595 129 102.86 134 17.617 139
42. 157 144 O.OOOOOE+OO 40 CUM.
NOOE 5
10 15 20 25 30 35 40 45 50 55 60 65 70 75 85 90 95 100 110 115 120 125 135 140 145
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 C) 20.395 151 9.8200 152 1.8997 154 42.326 155 42.019 156 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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