a form 3.2-1 caic. no.: 10494-62-np transnuclear

j,

A Form 3.2-1 CaIc. No.: 10494-62-NPTRANSNUCLEAR Calculation Cover Sheet Rev. No.: 0

Calculation Title: Pre-Test Prediction of the Thermocouple Temperatures Page: I of 23for the HSM Thermal Testing age:

Project No.: 10494

DCR No.:

Project Name: NUHOMS 32PTH

Number of CDs attached: NoneIf original issue, is Licensing Review per TIP 3.5 required?5? No (explain) | Yes Licensing Review No.-rkic, -441 <e %F T W=° - � 'G ~ei~Software utilized: 4\T45' * NC) Version -VCalculation is completeOriginator's SiInature . I Date:3 J4-/-2cIL-Calculation has been checked for consistency, completeness, and correctnessChecker Signature: C _1, Date: 4 l osCalculation is approvdtHor use f A

Project Engineer Signature: A_ -e Met5e Date: )A-- -2co

. Form 3.1-1 Calc. No.: 10494-62-NPTRANSNUCLEAR Calculation Rev. No.: 0

Title: Pre-Test Prediction of Thermocouple Temperatures Page: 2 of 23

1- Obiective

Predict the temperatures at the location of the thermocouples for the HSM-H thermal test usingthe methodology used in the thermal analysis of NUHOMS-32PTH and NUHOMS-24PTHsystems.

2- References

4. Not Used5. Safety Analysis Report, NUHOMS-HD Horizontal Modular Storage System for Irradiated Nuclear

Fuel, rev. 0, Chapter 46. I.E. Idelchik, 'Handbook of Hydraulic Resistance", 3rd Edition, 19947. "ASHRAE Handbook, Fundamentals" - Si Edition, 19978. Rohsenow, Hartnett, "Handbook of Heat Transfer Fundamentals", 2nd Edition, 19859. ASME Boiler and Pressure Vessel Code, Section II, Part D, 'Material Properties", 1998 and 2000

addenda

16. ANSYS Computer Code and User's Manuals, Rev. 8.0. See Test Reports E-21043, Rev. 0 and E-21044, Rev. 0 for validation of computer code.

17. Amendment No.8, Addition of 24PTH DSC to NUHOMS CoC 1004, Standardized NUHOMSSystem, submitted to NRC for review and approval.

18. Computational files:

A Form 3.1-1 Calc. No.: 10494-62-NPTRANSNUCLEAR Calculation Rev. No.: 0


3- Assumptions

. Ambient Temperature is 700F

. The applied heat loads are 32.0, 36.0, 40.0, and 44.0 kW as specified in reference [1]

. The temperatures are measured at the location of thermocouples as specified inreference [2]

. Only finned side heat shields are considered in this calculation

Any deviation from the above assumptions will affect the predicted temperature values. Inorder to compare the measured and predicted values, the ambient temperature and the heatload values must be equal to the measured values at the time of testing. If the locations ofmeasurements are revised and changed from those specified in reference [2], thetemperatures must be calculated at the new locations.

4- Discussion

It is planned to perform a thermal test on a full scale mockup of the HSM-H to validate themethodology used for thermal analysis of the NUHOMS-32PTH and NUHOMS-24PTHsystems. The HSM-H mockup is a carbon steel structure, which mimics the internal geometryof the designed HSM-H with only a few changes in the shape of the inlet air channel. The innerand outer surfaces of the HSM-H mockup are covered with insulation materials to create aconductivity close to the concrete wall conductivity of the designed HSM-H.

The DSC mockup is a 0.5" thick stainless steel (SA240, type 304) shell with end plugs, whichhas a outer diameter of 69.75" and a cavit len th of 164.5". These dimensions are identical tothe NUHOMS-32PTH DSC dimenso.|

Total of 108 thermocouples are installed on the HSM-H and canister mockups. The locationsand assignments of the thermocouples are shown in references [2] and [3]. The temperaturesat the location of thermocouples are calculated using the same methodology as described toevaluate the thermal performance of the HSM-H in reference and [5]. Note that thismethodology is also identical to the one used in the evaluation of the HSM-H thermalperformance in reference [17].

For this purpose, an equivalent loss coefficient is calculated based on the assumed ambienttemperature and the four above heat loads using the exact geometry of the mockup as shownin [2]. Similar to methodology described in [5], the HSM is divided into three regions tocalculate the equivalent loss coefficient:

Region 1 - From the air entrance opening to discharge into the HSM cavityRegion 2 - through the HSM cavityRegion 3 - From the outlet opening to exhaust to the ambient

a Form 3.1-1 Calc. No.: 10494-62-NPTRANSNUCLEAR Calculation Rev. No.: 0


Each region is divided into subsections considering entrance effects, bends, contraction,expansion, splitting, etc. The flow pattern and the subsections are shown in Figure 1. The losscoefficient in each subsection is calculated using the same correlations and diagrams as usedin reference [5]. The loss coefficient correlations and diagrams are taken from references [6]and [7]. The spreadsheets used to calculate the equivalent loss coefficients are listed in [18]. A

~ is assumed for calculation of the friction losses. The effect ofroughness value on the bulk temperatures are studied simply by changin the roughness value

M M B. It concludes that the bulk temperatures arerelatively insensitive to the roughness of the walls. This conclusion was expected because thelosses caused by flow direction changes are much higher than the friction losses. The airproperties in the spreadsheets are taken from reference [8]. The results are summarized intables 1 to 4.

The bulk temperatures within the HSM cavity are then calculated based on the assumedambient temperature, the heat load, and the corresponding equivalent loss coefficient.

A half symmetric, ANSYS [16] finite element model of the mockup is developed. Thecalculated bulk temperatures are used to apply the convection boundary conditions within theHSM cavity. Convection and radiation to ambient from the outer surface of the HSM mockupare combined together as a total heat transfer coefficient similar to reference 5]. Thecorrelations to calculate the heat transfer coefficients are described i [5].

floor. A soil temperature of 700F is considered at 7 ft below the concrete floor. As discussed in[5], the temperature distribution in the model is insensitive to soil temperature and itsthickness. This assumption is made to ease the convergence of the model solution.

The boundary conditions are applied using the same methodology as described in [5] with theexception that solar heat flux is not considered on the outer surfaces of the HSM mockup. Thethermal testing will be performed indoor. The material properties used in the model are listed insection 5. The geometry of the finite element model is shown in Figures 2 to 4. Figure 5 showstypical loads and boundary conditions applied in the model. The temperatures at the locationsof thermocouples are retrieved from the finite element model using the macro "TCs.mace listedin [18].



5- Material Properties

5.1 - Stainless Steel SA 240, type 304,DSC shell, DSC plugs - Mat 1

SA 240, Type 304 Thermal conductivityTemperature (OF) (Btulhr-ft-OF) [9] (Btu/hr-in-0F)

70 8.6 0.717100 8.7 0.725200 9.3 0.775300 9.8 0.817400 10.4 0.867500 10.9 0.908600 11.3 0.942700 11.8 0.983800 12.2 1.017900 12.7 1.0581000 13.2 1.100

An emissivity of 0.46 is considered for stainless steel surfaces, equal to the value consideredin reference [5].

5.2 - Carbon Steel - Structural Plates, Support structure - Mat 2

Carbon Steel Thermal conductivityTemperature (OF) (Btu/hr-ft-OF) [9] (Btulhr-in-OF)

70 35.1 2.925100 34.7 2.892200 3.6 2.800300 32.3 2.692400 30.9 2.575500 29.5 2.458600 28.0 2.333700 26.6 2.212800 25.2 2.100900 23.8 1.9831000 22.4 1.867

An emissivity of 0.55 is considered for carbon steel surfaces based on the data for smooth ironsheet in reference [14].

A| Form 3.1 -1 -Calc. No.: 10494-62-NPTRANSNUCLEAR . Calculation Rev. No.: 0


5.3 - Aluminum 1100 - side and top shields - Mat 3 l

Al 1100 Thermal conductivityTemperature (F) (Btu/hr-ft-0F) [9] (Btu/hr-in-OF)

70 133.1 11.092100 131.8 10.983150 130.0 10.833200 128.5 10.708250 127.3 10.608300 126.2 10.517350 125.3 10.422400 124.5 10.375

One side of the side heat shield facing the DSC is anodized. The other face and the top heatshield are not anodized. An emissivity of 0.80 is considered for anodized surfaces. Emissivityof not anodized aluminum surfaces is set to 0.1. These values are identical to the values usedin reference [5].

5.4 - Inner Insulation (Glasboard) - Mat 4

The inner surfaces of the HSM mockup are covered with _R of Glasboard insulation[15]. The conductivity of the Glasboard is taken from the manufacturer's data sheet [10]. Theemissivity of the Glasboard is measured separately in reference [11]. An average emissivityvalue of [in] is used in the model.

5.5 - Outer Insulation (Mineral Wool) - Mat 5

Outer surfaces of the HSM mockup are covered with _] of mineral wool "Thermafiber".The conductivity of the mineral wool is reported by the vendor in reference [12]. The emissivityof the mineral wool is measured separately in reference [13]. An average emissivity value of[ -1is used to calculate the total heat transfer coefficients on the outer surfaces.

5.6 - Concrete - Floor- Mat 6

The thermal conductivity of concrete in this analysis is set equal to the values used inreference [5], namely a conductivity of 0.0958 Btu/hr-in-OF is considered at 700F and aconductivity of 0.0479 Btu/hr-in-OF at 13820F.

5.7 - Soil - Mat 7

A thermal conductivity of 0.3 W/m-K (0.0144 Btu/hr-in-F) is considered for soil equal to thevalue in reference [5].

A Form 3.1-1 Calc. No.: 10494-62-NPTRANSNUCLEAR I Calculation Rev. No.: 0


6- Results

The predicted thermocouple temperatures are listed in tables 5 to 8. These results can becompared to the measured values at the corresponding heat loads if and only if the ambienttemperature is 700F and the location of the measurement is identical to the location specifiedin the test specification, reference [1] and the mockup drawings, reference [2].

Typical temperature distributions are shown in Figure 6 for the 44kW total heat load case.

A - Form 3.1-1 Calc. No.: 10494-62-NPTRANSNUCLEAR Calculation Rev. No.: 0


Table 1Equivalent Loss Coefficients and Bulk Temperatures for 32.0 kW Heat Load

Heat Load 32.0kW, Ambient 700F _ _

Region

1

No. ofFlawPathsTwoparallelflows

Subsection Type of Flow Resistance Ref. KEIat 70 1F

J:(KEIAE,)at 7051F

(In )e effect 171 9.26E-7

tion 16 ] 5.37E-6in entrance channel 7

Sidewall [71 7.17E-7_ A_

[71 I, . _ . . _ . _ _ _

in Section 1 for tv o Parallel Flows 1.75E-62 One

flowOneflow3parallelflowcouples

OneflowOneflow

Twoparallelflows

_

lower part [7]

[61

3.94E-1 1

3.76E-1 1

2.37E-9Friction after expansion l [71Orifice or perforated plates [6]

IOrifice or perforated plates I6] _ I

Contraction with a= 300 [6] 1

DSC as solid obiect in flow [611 2.09E-8Friction on side heat shields [71Top heat shields as louver .A 1 161 1.85E-8Splitting to outlets 1 1 0.63

t5 uivalent Losses in Section 2 for one Flow Path 4.18E-83 Entrance [71 UM 1.8E-6

Friction thru sidewall | 717 |First bend (friction included) [61 1Friction 171 3.24E-6

: I A. : _

Second bend (frictionincluded)

[6] 1 M4 4 -

Screen [71 2.OOE-6_~-* ,4I

Discharge [71 1a a . 4

Eauivalent Losses in Section 3 for two Parallel Flows 1. 76E-6Total Equivalent Losses (in4) 3.56E-6Total Equivalent Losses (ft4) 0.0738

A I Form 3.1-1 Calc. No.: 10494-62-NPTRANSNUCLEAR I Calculation Rev. No.: 0



Heat Load 36.0kW. Ambient 700FRegion

1

No. ofFlowPathsTwoparallelflows

Subsection Type of Flow Resistance Ref. KEIat 70°F

(I<E/AEJ) at 7050 F

(ink)Entrance effect [7] 1 9.26E-7Screen [7]1Contraction 1 1_ 5.37E-6Friction in entrance channel | [7L |Splitting [61 1

[71 7.1 7E-7[71 I

rivalent Losses in Section 1 for two Parallel Flows I 1. 75E-62 One


OneflowOneflow

|Two lparallelflows

Friction through lower part [71 1 _ 3.29E-1 1

3.73E-1 1[6117]

Orifice or perforated plates [6] 2.37E-9

Orifice or perforated plates [6] 1 _

[6] -l M

161 2.11E-8[71[61 1 .85E-8[61

r one Flow Path 4.20E-83 [171]

[7116]1

0.50.0062.01

1.8E-6

171 0.31 3.23E-6Second bend (frictionincluded)

[6] 0.82

Screen [7] 0.58 2.OOE-6Discharge 717 1

Equivalent Losses in Section 3 for two Parallel Flows 1. 76E-6Total Equivalent Losses (In4) II 3.55E-6Total Equivalent Losses (ft 4) 0.0737

A | Form 3.1-1 CaIc. No.: 10494-62-NPTRANSNUCLEAR Calculation Rev. No.: 0



Heat Load 40.0kW, Ambient 700FRegion

1

No. of SubsectionFlowPaths

Twoparallelflows

Type of Flow Resistance Ref. KEIat 70°F

1 (KEVAEI')at 705IF

(In-49.26E-7

4 4

Entrance effect i71 M4 .~ .

Screen 171 1 _______ - - - - 4 .&A � 4.

Contraction [61 _ 5.37E-6_ Friction in entrance channel | 717 |Splitting [6] 1 _Friction thru Sidewall [7] | M 7.17E-7Discharae fi7 I

Losses in Section 1 for two Parallel Flows j1.75E-62 One


OneflowOneflow

Twoparallelflows

:tion through lower part [7]

- I _- .

[61

3.90E-1 1

3.72E-1 1

2.37E-9Friction after expansion 17Orifice or perforated plates [6]

IOrifice or perforated plates [6] _

Contraction with a= 300 [6] 1

I 4

DSC as solid obiect in flow 161 _ - 2.12E-8_ _ _ _ ; _

Friction on side heat shields 171- 4-W*- 4

ToD heat shields as louver 161 1 .85E-8I . ...................

Splitting to outlets 161Losses in Section 2 for one Flow Path 4.22E-8

3 7 _ i779E-6thru sidewall [71nd (friction included) 161

171 3.23E-6_:bend (friction [6]

included) 4

Screen 171 2.OOE-6__._. A.1 _ _

Discharge [7] IEquivalent Losses in Section 3 for two Parallel Flows 1.76E-6

Total Equivalent Losses (in) 3.55E.6Total Equivalent Losses (ft 4) 0.0736




Heat Load 44.0kW, Ambient 70IFRegion No. of Subsection Type of Flow Resistance Ref. KEI E(KEVAEI')

Flow at 70DiF at 705onfPaths (i4)

1 Two _Entrance effect 717 9.26E-7parallel Screen 717flows Contraction _[61 5.37E-6

Friction in entrance channeld [71Splitting to s1Friction thru Sidewall [17.17E-7Discharge[7

E uivalent Losses in Section 1 for two Parallel Flows 1. 75E-62 Onel Friction through lower part L7] 3.88E-11

flofdOn pansion 16 1 3.70E11floS friction af6er expansion 7

icee or perforated plates n6] 2.37E-9pariaellflow Oiceor perforated plates [6]_coupless

Cotrcto with ca= 300 [6]_

On, DSC as solid object in flow [61 M 2.14-8flow Friction on side heat shields [ 71IOne _Top heat shields as louver [61 1.85E-8flow Splitting to outlets _[6]

Equivalent Losses in Section 2 fort one Flow s 4.23E-8Two E ntrance L Ise 1 3.79E-6

parallel Friction thru sidewall [7flows First bend (friction included) [ 61 _

Friction i-71 _ 3.22E-6Second bend (friction [6]included)

_Screen 11[71 IM .OE-66 Discharge [71 1

Equivalent Losses in Section 3 for two Parallel Flows 1.75E-6Total Equivalent Losses (In )3.55E-6Total Equivalent Losses (ft )I 0.0736

I A Form 3.1-1 Calc. No.: 10494-62-NPTRANSNUCLEAR Calculation Rev. No.: 0


Table 5Thermocouple Temperatures for 32kW, 70°F Ambient

Resultant Temperatures from FE Model of Mockup (MK32kW) with Finned Side Heat Shields.Assumptions: Heat Load = 32kW, Ambient Temp = 70F

Note: The assumed values for the heat load and the ambient temperature as well as the exact location of thethermocouples are subject to change based on the actual measured values and the location of measurements.

Thermocouple PredictedNo. Value (°F)

Thermocouple(1) 345Thermocouple(2) 313Thermocouple(3) 296Thermocouple(4) 279Thermocouple(5) 299Thermocouple(6) 279Thermocouple(7) 296Thermocouple(8) 313Thermocouple(9) 413

Thermocouple(10) 361Thermocouple(1 1) 340Thermocouple(12) 322Thermocouple(13) 357Thermocouple(14) 416Thermocouple(1 5) 337Thermocouple(1 6) 341Thermocouple(17) 324Thermocouple(18) 358Thermocouple(19) 324Thermocouple(20) 341Thermocouple(21) 337Thermocouple(22) 414

Thermocouple(23) 362Thermocouple(24) 340Thermocouple(25) 322Thermocouple(26) 357Thermocouple(27) 346Thermocouple(28) 313Thermocouple(29) 296Thermocouple(30) 279Thermocouple(31) 299Thermocouple(32) 279Thermocouple(33) 296

Thermocouple PredictedNo. Value (OF)

Thermocouple(34) 313Thermocouple(35) 108

Thermocouple(36) 105Thermocouple(37) 110Thermocouple(38) 123Thermocouple(39) 107Thermocouple(40) 108Thermocouple(41) 105Thermocouple(42) 110Thermocouple(43) 123Thermocouple(44) 107Thermocouple(45) 118Thermocouple(46) 110Thermocouple(47) 111Thermocouple(48) 107Thermocouple(49) 114Thermocouple(50) 118Thermocouple(51) 110Thermocouple(52) 111Thermocouple(53) 107Thermocouple(54) 114Thermocouple(55) 112Thermocouple(56) 101Thermocouple(57) 102Thermocouple(58) 123Thermocouple(59) 105Thermocouple(60) 112Thermocouple(61) 101Thermocouple(62) 102Thermocouple(63) 123Thermocouple(64) 105Thermocouple(65) 137Thermocouple(66) 134


Thermocouple(67) 116Thermocouple(68) 121Thermocouple(69) 135Thermocouple(70) 132Thermocouple(71) 116Thermocouple(72) 119Thermocouple(73) 135Thermocouple(74) 132Thermocouple(75) 135Thermocouple(76) 95Thermocouple(77) 102Thermocouple(78) 95Thermocouple(79) 138Thermocouple(80) 132Thermocouple(81) 138Thermocouple(82) 107Thermocouple(83) 108Thermocouple(84) 107Thermocouple(85) 132Thermocouple(86) 131Thermocouple(87) 132Thermocouple(88) 101Thermocouple(89) 101Thermocouple(90) 101Thermocouple(91) 137Thermrocouple(92) 137Thermocouple(93) 136Thermocouple(94) 119Thermocouple(95) 119Thermocouple(96) 129Thermocouple(97) 129Thermocouple(98) 118Thermocouple(99) 118

*For the location and numbering the thermocouples see references [1 I and 12]



Table 6ThermocouDle Temperatures for 36kW. 70°F Ambient




Thermocouple(1) 370Thermocouple(2) 335Thermocouple(3) 317Thermocouple(4) 299Thermocouple(5) 321Thermocouple(6) 299Thermocouple(7) 317Thermocouple(8) 335Thermocouple(9) 443

Thermocouple(10) 386Thermocouple(1 1) 364Thermocouple(12) 345Thermocouple(13) 383Thermocouple(14) 446Thermocouple(1 5) 362Thermocouple(16) 365Thermocouple(17) 347Thermocouple(18) 385Thermocouple(19) 347Thermocouple(20) 365Thermocouple(21) 362Thermocouple(22) 444Thermocouple(23) 387Thermocouple(24) 364Thermocouple(25) 345Thermocouple(26) 384Thermocouple(27) 371Thermocouple(28) 335Thermocouple(29) 317Thermocouple(30) 299Thermocouple(31) 322Thermocouple(32) 299Thermocouple(33) 317


Thermocouple(34) 335Thermocouple(35) 113Thermocouple(36) 109Thermocouple(37) 114Thermocouple(38) 129Thermocouple(39) 112Thermocouple(40) 113Thermocouple(41) 109

Thermocouple(42) 114Thermocouple(43) 129Thermocouple(44) 112Thermocouple(45) 125Thermocouple(46) 115Thermocouple(47) 116Thermocouple(48) 111Thermocouple(49) 119Thermocouple(50) 125Thermocouple(51) 115Thermocouple(52) 116Therrmocouple(53) 111Thermocouple(54) 119Thermocouple(55) 116Thermocouple(56) 105Thermocouple(57) 106Thermocouple(58) 129Thermocouple(59) 109Thermocouple(60) 116Thermocouple(61) 105Thermocouple(62) 106Thermocouple(63) 129Thermocouple(64) 109Thermocouple(65) 144Thermocouple(66) 141


Thermocouple(67) 120Thermocouple(68) 126Thermocouple(69) 141Thermocouple(70) 138Thermocouple(71) 120Thermocouple(72) 124Thermocouple(73) 142Thermocouple(74) 138Thermocouple(75) 142Thermocouple(76) 98Thermocouple(77) 105Thermocouple(78) 98Thermocouple(79) 145Thermocouple(80) 139Thermocouple(81) 145Thermocouple(82) 111Thermocouple(83) 113Thermocouple(84) 111Thermocouple(85) 138Thermocouple(86) 137Thermocouple(87) 138Thermocouple(88) 104Thermocouple(89) 105Thermocouple(90) 104Thermocouple(91) 142Thermocouple(92) 143Thermocouple(93) 142Thermocouple(94) 124Thermocouple(95) 124Thermocouple(96) 136Thermocouple(97) 136Thermocouple(98) 124Thermocouple(99) 124

'For the location and numbering the thermocouples see references [1] and [2]

l A Form 3.1-1 Calc. No.: 10494-62-NPTRANSNUCLEAR Calculation Rev. No.: 0


Table 7Thermocouple Temperatures for 40kW, 70°F Ambient I

Resultant Temperatures from FE Model of Mockup (MK4OkW) with Finned Side Heat Shields.Assumptions: Heat Load = 40kW, Ambient Temp = 70F



Thermocouple(1) 394Thermocouple(2) 356Thermocouple(3) 337Thermocouple(4) 318Thermocouple(5) 343Thermocouple(6) 318Thermocouple(7) 337Thermocouple(8) 356Thermocouple(9) 472Thermocouple(10) 409Thermocouple(1 1) 386Thermocouple(12) 366Thermocouple(13) 408Thermocouple(14) 475Thermocouple(15) 386Thermocouple(16) 387Thermocouple(17) 369Thermocouple(18) 410Thermocouple(19) 369Thermocouple(20) 387Thermocouple(21) 386Thermocouple(22) 472Thermocouple(23) 410Thermocouple(24) 386Thermocouple(25) 367Thermocouple(26) 408Thermocouple(27) 396Thermocouple(28) 357

Thermocouple(29) 337

Thermocouple(30) 318Thermocouple(31) 343Thermocouple(32) 318Thermocouple(33) 337





Thermocouple(38) 136Thermocouple(39) 117Thermocouple(40) 118Thermocouple(41) 114Thermocouple(42) 120

Thermocouple(43) 136Thermocouple(44) 114Thermocouple(45) 132Thermocouple(46) 121Thermocouple(47) 123





Thermocouple(54) 125Thermocouple(55) 122Thermocouple(56) 109Thermocouple(57) 111Thermocouple(58) 136Thermocouple(59) 114Thermocouple(60) 122Thermocouple(61) 109







Thermocouple(67) 125Thermocouple(68) 132Thermocouple(69) 149Thermocouple(70) 145Thermocouple(71) 125Themmocouple(72) 130













Thermocouple(85) 145Thermocouple(86) 144Thermocouple(87) 145Thermocouple(88) 108Thermocouple(89) 109Thermocouple(90) 108Thermocouple(91) 148Thermocouple(92) 149Thermocouple(93) 148Thermocouple(94) 131


Thermocouple(96) 144Thermocouple(97) 144Thermocouple(98) 130Thermocouple(99) 130

For the location and numbering the thermocouples see references [1 J and [2]



Table 8ThermocouDle TemDeratures for 44kW. 70°F Ambient I




Thermocouple(1) 418Thermocouple(2) 377Thermocouple(3) 356Thermocouple(4) 336Thermocouple(5) 363Thermocouple(6) 336Thermocouple(7) 356Thermocouple(8) 377Thermocouple(9) 500Thermocouple(10) 432Thermocouple(l 1) 406Thermocouple(12) 387Thermocouple(13) 432Thermocouple(14) 504Thermocouple(15) 409Thermocouple(16) 408Thermocouple(17) 390Thermocouple(18) 434Thermocouple(19) 390Thermocouple(20) 408Thermocouple(21) 409Thermocouple(22) 501Thermocouple(23) 433Thermocouple(24) 407Thermocouple(25) 388Thermocouple(26) 433Thermocouple(27) 420Thermocouple(28) 377Thermocouple(29) 356Thermocouple(30) 336Thermocouple(31) 364Thermocouple(32) 336Thermocouple(33) 356


Thermocouple(34) 377Thermocouple(35) 123Thermocouple(36) 119Thermocouple(37) 125Thermocouple(38) 141Thermocouple(39) 121Thermocouple(40) 123Thermocouple(41) 119Thermocouple(42) 125Thermocouple(43) 141Thermocouple(44) 121Thermocouple(45) 138Thermocouple(46) 127Thermocouple(47) 128Thermocouple(48) 121Thermocouple(49) 130Thermocouple(50) 138Thermocouple(51) 127Thermocouple(52) 128Thermocouple(53) 121Thermocouple(54) 130Thermocouple(55) 127Thermocouple(56) 113Thermocouple(57) 114Thermocouple(58) 141Thermocouple(59) 118Thermocouple(60) 127Thermocouple(61) 113Thermocouple(62) 114Thermocouple(63) 141Thermocoupie(64) 118Thermocouple(65) 159Thermocouple(66) 154


Thermocouple(67) 129Thermocouple(68) 137Thermocouple(69) 156Thermocouple(70) 152Thermocouple(71) 129Thermocouple(72) 135Thermocouple(73) 157Thermocouple(74) 152Thermocouple(75) 157Thermocouple(76) 105Thermocouple(77) 113Thermocouple(78) 105Thermocouple(79) 160Thermocouple(80) 152Thermocouple(81) 160Thermocouple(82) 120Thermocouple(83) 122Thermocouple(84) 120Thermocouple(85) 152Thermocouple(86) 150Thermocouple(87) 152Thermocouple(88) 112Thermocouple(89) 112Thermocouple(90) 112Thermocouple(91) 155Thermocouple(92) 156Thermocouple(93) 155Thermocouple(94) 136Thermocouple(95) 136Thermocouple(96) 151Thermocouple(97) 151Thermocouple(98) 136Thermocouple(99) 136

'For the location and numbering the thermocouples see references [1] and [2]

, R | Form 3.1-1 Calc. No.: 10494-62-NPTRANSNUCLEAR Calculation Rev. No.: 0


Hot Air to AnIblert

Cold Airet AmbiertTemperoture

Exhaust Bend +into Cavity Contraction

Contraction EntranceEffect +Screen

Bends

Insulation on the side isremoved for clearance

Splitting

Contraction

PerforatedPlate /

Expansion -

Inlet Opening

Figure 1Air Flow Path

A Form 3.1-1 CaIc. No.: 10494-62-NPTRANSNUCLEAR Calculation Rev. No.: 0


Outer Insulation

Heat Shields

DSC Mockup

Inner Insulation

Concrete Floor

IreSupport StructuA. _

OutDetail A

Inner Insulation

ter Insulation

Carbon Steel Structure

Figure 2Finite Element Model of the Mockup

A | Form 3.1-1 Calc. No.: 10494-62-NP_TRANSNUCLEAR Calculation Rev. No.: 0


Figure 3Finite Element Model of the HSM Mockup

DSC is removed to show the Support Structure

A Form 3.1-1 Caic. No.: 10494-62-NPTRANSNUCLEAR Calculation Rev. No.: 0


Figure 4Mesh Map of the Mockun Finite Element Model

A Form 3.1-1 Calc. No.: 10494-62-NP|TRANSNUCLEAR Calculation | Rev. No.: 0 J


ALNSYS 8.0CO)IV-HCOE

EYnI -14.2223.073 144

m 10.666

Jij C~onvectioniInside HSHeat Flux and Fixed Temp

AKTS8.08

,.5 :, upprt Srucure CO11V-HCOE

Convection ond Rad Shel

-34 FiguFlux

MASTS 9.0

CONY-UCOSE

SuportStuctre-25 S

-248211

Ann -22.333

-1-11.111

-3. 5Figure85

Convection andlRaoatndnrouCsnditions

a A Form 3.1-1 Calc. No.: 10494-62-NPTRANSNUCLEAR Calculation Rev. No.: 0


A Form 3.1 -1 Calc. No.: 10494-62-NPTRANSNUCLEAR I Calculation Rev. No.: 0


a Form 3.1-1 Calc. No.: 10494-62-NPTRANSNUCLEAR Calculation Rev. No.: 0


I B. E-mail from Mr. Mike Battaalia. Ionics. Inc. I

a form 3.2-1 caic. no.: 10494-62-np transnuclear

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