ML031260744

Operability Evaluation of the EDG Exhaust Piping for a Tornado Event, Rev 0, Table of Contents Through Attachment E

ML031260744
Person / Time
Site:	Monticello
Issue date:	03/16/2003
From:	Denise Wilson Nuclear Management Co
To:	Document Control Desk, Office of Nuclear Reactor Regulation
References
IR-03-002, L-MT-03-031 CA-03-030, MN03-PO22637
Download: ML031260744 (181)

Text

{{#Wiki_filter:MONTICELLO NUCLEAR GENERATING PLANT 3494 TITLE: CALCULATION COVER SHEET Revision 9 Page I of 2 Page / of 53 CALCULATION COVER SHEET Title Operability Evaluation of the EDG Exhaust CA 030 Add. Piping for a Tomado Event Vendor No. MN0I3-P027637 Associated Ref. CR 03001909 10CFR50.59ScreeningorEvaluation No: SceQ-o3-1Sj Assigned Personnel Name (Print) Sign~tureTitle Initials Scott Quiggle Mech Eng Record of Issues Total No. Last Approval Rev Description of Sheets Sheet No. Preparer Verifier Verifier Approval Date 0 Original Issue 2CJ3 __Ax_____ 3/_/4_3 1 Vendor Verification/Approval in Document Verification Method(s) E Review 0 Alternate Calculation D Test E Other 3087 (DOCUMENT CHANGE, HOLD AND COMMENT FORM) incorporated: FOR ADMINISTRATIVE Reso Suov: CNSTP Assoc Ref: AWI.05.01.25 SR: N Frea: 0 vrs USE ONLY ARMS: 3494 i Doc TvDe: 3042 i Admin Initials: Date: Approved (Signatures available in Master File)

MONTICELLO NUCLEAR GENERATING PLANT TITLE: l CALCULATION COVER SHEET 3494 Revision 9 Page 2 of 2 Page/of S3 CA 030 Design Basis Tracking (Calculation Preparer completes this section). Does this calculation: Supercede another calculation? Yes L1 No 1: CaIc. No(s): Augment another calculation? Yes aI No 3: Calc. No(s): What documents/procedures will be based on this calculation: Documents/Procedures (include revision): Operability Eval in CR 03001909 What plant procedures will be/are used to ensure inputs/assumptions/outputs are maintained: Procedures (include revision): None What Systems or components are affected? System(s): 11 & 12 Stby Diesel Generator Exhaust Pipe Component ID's (CHAMPS Equip) G-3A, G-3B DBD Section (if any): T19 External Considerations Topic Code (eg. ASME Section Xl etc): Tornado Wind Loading Other Comments: Approved (Signatures available in Master File)

Automated / Engineering Calculation Package No. 1 of 53 L/Z Services Corp. CalculationNumber: MN03-P022637-100 lRevision Number: 0 Calculation

Title:

Operability Evaluation of the EDG Exhaust Piping for a Tornado Event Client: Nuclear Management Company Project: Monticello Nuclear Generating Plant Project Number: MN03-P022637 P.O. Number: P022637

Subject:

EDG Exhaust Evals Safety Related Yes 3 No E Preparer: Scott Tradup Printed/Typed Name Reviewer: Joe Attwood Printed/Typed Name Approver: Thomas N. Vogel Printed/Typed Name

aIT Automated Engineering Services Corp. SHEET-1 of 2 REVIEWER'S CHECKLIST FOR DESIGN CALCULATIONS. PROJECT: Monticello Nuclear Generating Plant NUCLEAR SAFETY RELATED YES NO F PROJECTNO: MN03-P022637 CLIENT: Nuclear Management Company CALCULATION TITLE: Onerabilitv Evaluation ofthe EDG Exhaust Piping for a Tomado Event CALC. NO: MN03-P022637-100 CALC. REV. NO: 0 INDICATE THE DESIGN INPUT DOCUMENTS USED: TYPE OF DOCUMENT DOCUMENT ID, REV AND/OR DATE YES N/A COMMENT L General Design Basis DI No. 15, 19 X

2.

System Description

DI No. 1 X

3.

Design Information package X from related equipment vendor

4.

Electrical Discipline Input X S. Mechanical Discipline Input DI Nos. 7,14 X

6.

Coctrol Systems Discipline X Input

7.

Structural Discipline Input DI Nos. 8-13,16, 17 X

8.

Specifications DI Nos. 3,4,6 X

9.

Vendor Drawings x

10.

Design Standards DI Nos. 2, S, 18 X

11.

ClientStandards x 12 Checked Calculations X

13.

Other (specify) X PREPARER'S SIGNATURE: 5 tw DATE: 03/07/03 REVIEWER'S SIGNATURE: DATE: 03/07/03 APPROVER'S SIGNATURE: lI sJ . DATE: 03/07/03 Form 3.1-4 Rev. 2

REVIEWER'S CHECKLIST FOR DESIGN CALCULATIONS PROJECT NO: MN03-P022637 CALC. NO: MN03-P022637-100 REVIEWER TO COMPLETE THE FOLLOWING ITEMS:

1. Has the purpose of the calculation been clearly stated?

.2. Have the applicable codes, standards and regulatory requirements been: A. Properly Identified? B. Properly Applied?

3. Were the inputs correctly selected and used?

4. A. Was Design Input Log used?

B. If 4A is No, provide Project Manager's signature In Comment column to signify approval of Design Input Documents used in the calculation. S. Are necessary assumptions adequately stated?

6. Are the assumptions reasonable?

7. Was the calculation methodology appropriate?

8. Are symbols and abbreviations adequately identified?

9. Are the calculations:

A. Neat? B. Legible? C. Easy to follow? D. Presented in logical order? E. Prepared In proper format?

10. Is the output reasonable compared to the inputs?

11. If a computer program was used:

A. Have you reviewed the program validation documents for the production version of the program? B. Were codes properly verified? C. Were they appropriate for the application? D. Were they correctly used: E. Was data input correct? F. Is the computer program and revision identified? SHEET 2 of 2 Form 3.14 Rev. 2

Automated Engineering Services Corp. NO. 4 OF 53 Calculation Sheet l/i! REVISION NUMBER: 0 CLIENT: Nuclear Management Company DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:

SUBJECT:

EDG Exhaust Evals CHECKED: JvA-SAFETY RELATED YES MR NO CALC. NO.: MN03-P022637-100 Table of Contents Section 1. 2. 3. 4. 5. 6. 7. 8.. 9. 10. 11. Title -Purpose References Design Input Daughter Documents Assumptions Quality Requirements Acceptance Criteria Software Methodology Analysis Conclusion Page 5 6 .7 9 10 11 12 14 15 16 53 Attachment Title No. of Pages A B C D E F G H Stiffness Analysis for DGEH-2, -3, -5, -6 Baseplates ANSYS Input Listing for East-West Tornado Wind ANSYS Input Listing for North Tornado Wind ANSYS Input Listing for Support DGEH-1 with South Tornado Wind ANSYS Output for East-West Tornado Wind ANSYS Output for North Tornado Wind ANSYS Output for Support DGEH-1 with South Tornado Wind NPLATE Analysis for DGEH-2, -3, -5, -6 Baseplates 28 16 16 5 61 58 .17 46 Form 3.1-3 Rev. l-

I Automated Engineering Services Corp. NO.5 l[OF 53 / D JCCalculation Sheet / /REVISION NUMBER: 0 CLIENT: Nuclear Management Company DATE: 03/07/03 PROJECT: Monticello Nuclear Generatng Plant PREPARED:MAif/

SUBJECT:

EDG Exhaust Evals CHECKED:Jo SAFETY RELATED YES [o NO [] CALC. NO.: MN03-P022637-100

1.

Purpose The exhaust piping for the Emergency Diesel Generators (EDG) extends outside the EDG building. During a design basis tornado, the exhaust piping may become damaged which could lead to the EDG's becoming inoperable. Therefore, the purpose of this analysis is to evaluate the EDG exhaust piping to determine the operability of the piping-system during a design basis tornado event. The design temperature of the pipe is of little concern and the analysis is performed at 700 F. During a tornado event, the main concern isn't with the pipe but with the supports. Due to the flexibility of the piping system, thermal support loads are very small and can be neglected. In addition, an elastic-plaitic analysis of the piping system is being performed;. The bounding case for this type of analysis is when the material properties of the piping system are their largest, i.e. when the piping is cold. So, even though the maximum temperature of the piping is 950° F, the governing pipe temperature for the analysis is 70° F. Since the properties of steel have little variation between temperature of -30° F and 1000 F, using 70° F is deemed acceptable. In addition, the design basis load combinations presented in USAR section 12.2.1.4 do not consider seismic loads and tornado loads to occur simultaneously. Hence, seismic loads are also not considered. Therefore, the piping system Is evaluated for internal pressure, deadweight and tornado wind loads. It should be noted that tornado missile loads have not been applied in this evaluation. Because the wind and/or loading characteristics are different for each of the cases, the following three tornado wind load cases are evaluated:

1.

Tornado wind in the eastfWest direction

2.

Tornado wind in the north direction

3.

Tornado wind in the south direction Fonn 3.1-3 Rev. I

a Automated Engineering Services Corp. NO. 6 OF 53 Calculation Sheet REVISION NUMBER: 0 CLIENT: Nuclear Manaeement Companv DATE: 03/07/03 PROJECT: Monticello Nuclear Generatin2Plant PREPARED: f

SUBJECT:

EDG Exhaust Evals CHECKED: 3A&- SAFETY RELATED YES [X NO 2 CALC. NO.: MN03-P022637-100

2.

References

1.

Bergen Paterson Pipe Supports, Catalog No. 92

2.

Ladish Controlled Quality Fittings Catalog No. 55

3.

ASCE Paper No. 3269, Wind Forces on Structures

4.

ASME Boiler and Pressure Vessel Code, Section III, Division 1, 1977 Edition with Addenda thru Winter 1978

5.

Welding Formulas and Tables for Structural and Mechanical Engineers and Pipe Support Designers, I.V.1. Structural Design Service, Portland Oregon, 1983

6.

Not Used

7.

NPS Industries, Inc., piping and equipment supports Catalog, NPSI-81

8.

Bergen-Paterson Pipe Supports, Catalog No. 66R

9.

ASME Code Case N-318-3, 9/5/85, "Procedure for Evaluation of the Design of Rectangular Cross Section Attachments on Class 2 or 3 Piping, Section ill, Division I

10.

Marks Handbook for Mechanical Engineers, 7th Edition, McGraw Hill Book Company, 1967 Form 3.1-3 Rev. 1

i Automated Engineering Services Corp. NO.7 OF 53 Calculation Sheet REVISION NUMBER: 0 CLIENT: Nuclear Management Company DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED: 7

SUBJECT:

EDG Exhaust Evals CHECKED- ) SAFETY RELATED YES FR NO 2 CALC. NO.: MN03-P022637-100

3.

Design Input

1.

MNGP Drawing NF-36672, 'Stand-by Diesel Generators Arrangement & Piping", Rev. F .2. ANSI B31.1, "Power Piping", 1977 Edition with Addenda thru Winter 1978

3.

MNGP Specification NPD-M-38, "The Analysis of Piping and Piping Support Systems", Rev. 5

4.

MNGP Specification M-40, Piping Materials, Classification and Standards for the Monticello Nuclear Generating Plant, Rev. D-15

5.

AISC Manual of Steel Construction, gt9 Edition

6.

MNGP Specification M-43A, "Furnishing and Installing Thermal Insulation Outside the Containment Vessel", Rev. 2

7.

MNGP Drawing NX-9216-18, "Flexible Exhaust Connection", Rev. B

8.

MNGP Drawing NX-14074-2, "Support DGEH-1", Rev. 1

9.

MNGP Drawing NX-14074-3, "Support DGEH-2", Rev. 0

10.

MNGP Drawing NX-14074-4, "Support DGEH-3", Rev. 0

11.

MNGP Drawing NX-14074-5, "Support DGEH-4", Rev. 1

12.

MNGP Drawing NX-14074-6, "Support bGEH-5", Rev. 0

13.

MNGP Drawing NX-14074-7, "Support DGEH-6", Rev. 0

14.

MNGP Drawing NX-9216-19, "Exhaust Silencer', Rev. A

15.

MNGP USAR, Rev. 19

16.

NUREG-0800, Standard Review Plan for the Review of Safety Analysis Reports for Nuclear Power Plants, LWR Edition, USNRC, July 1981 Form 3.1-3 Rev. 1

z t Automated Engineering Services Corp. NO. 8 OF 53 Calculation Sheet .REVISION NUMBER: 0 CLIENT: Nuclear Management Companv DATE: 03/07/03. PROJECT: Monticello Nuclear Generating Plant PREPARED: 4/--

SUBJECT:

EDG Exhaust Evals CHECKED:iJus-SAFETY RELATED YES F NO D CALC. NO.: .MN03-P022637-100

17.

Fax from Scott Quiggle (NMC) to Joe Attwood (AES), 2-26-03, File No. MN03-P0022637-005

18.

ASME Boiler and Pressure Vessel Code, Section III, Division 1, Appendix F, 1986 Edition

19.. Fax from Mike Hippe (NMC) to Scott Tradup (AES), 2-25-03,

Subject:

Re: Engine Exhaust, File No. MN03-P0022637-005 Form 3.1-3 Rev. 1 Form 3. 1-3 Rev. I

/ Automated Engineering Services Corp. NO. 9 OF 53 Calculation Sheet _.REVISION NUMBER: 0 CLIENT: Nuclear Management Company DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED: 7'

SUBJECT:

EDG Exhaust Evals CHECKED: God SAFETY RELATED YES IXJ NO [] CALC. NO.: MN03-P022637-100

4.

Daughter Documents None Form 3.1-3 Rev. I

Automated'Engineering Services Corp. NO. 10 OF 53 Calculation Sheet REVISION NUMBER: 0 CLIENT: Nuclear Management Companv DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:

SUBJECT:

EDG Exhaust Evals CHECKED: SAFETY RELATED YES [3 NO I] CALC. NO.: MN03-P022637-100

5.

Assumptions

1.

The flexible connection near the EDG is conservatively assumed to have negligible stiffness. Therefore, the following conservative stiffness values are assumed: Kaxiaa = Kiateral = 10 lb/in Krotational = Ktorsional = 10 in Ib/rad Form 3.1-3 Rev. 1.

a Automated Engineering Services Corp. l O i1 lOF 53 Calculation Sheet REVISION NUMBER: 0 CLIENT: Nuclear Mana ement Companv DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:

SUBJECT:

EDGExhaustEvals CHECKED: SAFETY RELATED YES [RI NO CALC. NO.: MN03-P022637-l00

6.

Quality Requirements Nuclear safety related components are affected by this analysis. Therefore, the AES Quality Assurance Program will be applied to this calculation. The following QAP's were used in the preparation of this document: QAP 3-1 (Rev. 6), QAP 3-2 (Rev. 5), QAP 6-1 (Rev. 4). Form 3.1-3 Rev. I Form 3. 1-3 Rev. I

Automated Engineering Services Corp.. 12 53 /DSCaclto Sheet REVISION NUMBER: 0 CLIENT: Nuclear Management Company DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:

SUBJECT:

EDO Exhaust Evals CHECKED: J e SAFETY RELATED YES x NO [] CALC. NO.: MN03-P022637-100

7.

Acceptance Criteria The purpose of this analysis is to perform an operability evaluation of the EDG exhaust piping for a design basis tornado wind. Therefore, the following acceptance criteria will be used. Piping It is expected that the stresses in the pipe will be small. Therefore, the piping is conservatively analyzed to normal ANSI B31.1 (Dl No. 2) code allowables. The following load combination is evaluated. P + DW + Tornado Wind Pressure < Sy (@ design temperature (cons.)) Pipe Supports The following load combination is evaluated. DW + Tornado Wind Pressure Support Structural Steel The support structural steel Is analyzed using elastic-plastic methods. Members which remain elastic, i.e. stresses less than yield, are acceptable by inspection. Members which go plastic, i.e. stresses greater than yield, are acceptable provided the ductility ratio is less than 10 {guidance for this is taken from NUREG-0800 (Dl No. 16, Section 3.5.3, Appendix A). Baseplates are not analyzed using elastic-plastic methods. Therefore, the baseplates are acceptable if they meet the operability requirements of NPD-M-38 and ASME Appendix F (Dl No. 18). Form 3.1-3 Rev. I

z) Automated Engineering Services Corp. NO. 13 OF 53 Calculation Sheet REVISION NUMBER 0 CLIENT: Nuclear Management Company DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:

SUBJECT:

EDG Exhaust Eyals CHECKED: AA-SAFETY RELATED YES iR NO ] CALC. NO.: .MNO3-PO22637-100 Welds Welds are considered acceptable if the weld stress is less than the operability weld stress criteria per NPD-M-38 and ASME Appendix F (Dl No. 18)-. Manufactured Support Components Manufactured support components are considered acceptable if they meet the manufacturers Service Level D allowables (Dl No. 3, 18). Anchor Bolts Anchor bolts are considered acceptable provided the loads on the bolts are less than the operability requirements of NPD-M-38 (i.e. safety factor of 2 against ultimate). Form 3.1-3 Rev. I

Automated Engineering Services Corp. NO. 14 OF 53 Calculation Sheet REVISION NUMBER: 0 CLIENT: Nuclear Management Comanv DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED: A

SUBJECT:

EDG Exhaust Evals CHECKED: (J\\A4_ SAFETY RELATED YES 3 NO N CALC. NO.: MN03-P022637-100

8.

Software

1.

ANSYS Version 5.7

2.

NPLATE Version 1.1.0 - NPLATE is the property of the Nuclear Management Company (NMC) and is used at their request. NPLATE runs were made by NMC personnel, checked by AES personnel, and incorporated into this calculation. All computer program verification files reside with the NMC. Form 3.1-3 Rev. I Form 3.1-3 Rev. I

L) Automated Engineering Services Corp. NO. 15 OF 53 Calculation Sheet REVISION NUMBER: 0 CLIENT: Nuclear Management Comanv DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:

SUBJECT:

EDg Exhaust Evals CHECKED: JVA,- SAFETY RELATED YES [FI NO F CALC. NO.: MN03-P022637-100

9.

Methodology

1.

Create ANSYS non-linear model.

2.

Apply Deadweight and Tornado Loads

3.

Analyze South Blowing Wind

4.

Perform B31.1 analysis of piping. 5, Evaluate Supports ) Form 3.1-3 Rev. I Fonn 3. 1-3 Rev. I

Automated Engineering Services Corp. NO. 16 OF 53 Calculation Sheet _.REVISION NUMBER: 0 CLIENT: Nuclear Manaeement Comanv DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED: 7°

SUBJECT:

EDG Exhaust Evals CHECKED: JAi& SAFETY RELATED YES [ NO 2 CALC. NO.: MN03-P022637-100 10. Analysis ANSYS Model Development A. The geometry for the EDG exhaust piping is taken from Dl No. 1. The support locations are taken from Dl No. 8 - 13. From Dl No. 19, the elbows are long radius. The exhaust silencer geometry is per Dl No. 14. The flexible connection geometry is per Dl No.' 7. The flexible connection is conservatively assumed to have very small stiffnesses (see assumption 1) and therefore, very little load is transferred to the other side of the flexible connection. Therefore,.the piping is modeled from the flexible connection tithe end of the exhaust piping. B. Coordinate System X = North Y=Up Z = East C. Piping Design Conditions (see section 1) T = 700 F From Dl No. 7, the maximum operating pressure is 5" of water (0.18 psig). This value is taken as the design pressure for the entire piping system. A design pressure of 0.18 psig is considered negligible. D. Element Properties Note that the units of density for ANSYS are in lb-massfin3. The material nonlinear properties (Yield Point and Tangent Modulus) are also determined. Pipe Properties (ANSYS Material 1) Class JB Pipe is 22", 0.375" wall Material = A-106, Gr. B Sc = 15000 psi (Dl No. 1) (Dl No. 4) (Dl No. 4) (Dl No. 2) Form 3. 1-3 Rev. I

Automated Engineeng Services Corp. NO. 17 lOF 3I / D TIC ICalculation Sheet-Cl i SREVISION NUMER: 0 CLIENT: Nuclear Management Comanv DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:W 7°

SUBJECT:

EDG Exhaust Evals CHECKED: Jim-SAFETY RELATED YES b NO [j CALC. NO.: MN03-P022637-100 Sh - 15000 psi E = 27,900,000 psi v = 0.3 Sy = 35000 psi Sy = 21400 psi Tangent Modulus = 0.0 psi p = 490 Ibf/ff 3 (Dl No. 2) (DI No. 2) (Ref. 4, Table 1-2.1, 700 F) (Ref. 4, Table 1-2.1, 950° F, cons. use for pipe stress allowable) 22" Diameter Pipe - real constants 1, 3 - 5 OD=22.0in TK = 0.375 in Insulation Weight (Dl No. 6, Ref. 7, inside building only) The piping inside the EDG building is insulated. The thickness of the insulation is unknown. From Specification M-43A (Dl No. 6), insulation requirements are specified for temperatures only up to 7500 F (i.e. insulation class 1). Even though the design temperature is greater than that for insulation class i, the insulation thickness on the piping inside the EDG building is assumed to be based on insulation class 1. See Dl No. 19 for field verification. Insulation Thickness = 3" Jacketing Thickness = 0.024" Wins 11/13(21.3) + 0.024/0.016(1.6) = 20.4 lb/ft Ais= (7r14)(282 - 222) = 235.6 in2 1.636 ft2 Pins = Wins/Ains = 12.48 pcf = 0.007 lbf/in3 Elbow Parameters Long Radius Elbow - R = 33 in Calculate SIF & Flexibility i = 0.9/h213) =4.02 Form 3.1-3 Rev. I Form 3.1 -3 Rev. I

Automated Engineering Services Corp. NO.18 OF 53 Calculation Sheet REVISION NUMBER: 0 CLIENT: Nuclear Management Companv DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED: 44 7

SUBJECT:

EDG Exhaust Evals CHECKED: J VA-SAFETY RELATED YES R NO L CALC. NO.: MN03-P022637-1 00 Flex= 1.65/h= 15.588

where, h = TR/r2 = 0; 1059 T = 0.375 in R = 33 in r = 10.8125 in Exhaust Silencer - 36" Diameter Pipe - real constant 2 From Dl No. 14, the end flanges have a OD of 29.5", an ID of 22" with 20 1 3/8" diameter bolt holes and from DI No. 17 are 3/4" thick W = {(id4)[(29.52 - 222) -20 (1.375)2]}(0.75)(490/1728) = 58 Ibf The 22" pipe stubs on either end weigh 87 lb/ft (Ref. 1, 22" std pipe)

OD = 36 in TK 0.350 in Note: Dl No. 14 indicates that the silencer weights 1350 lbs. However, when that weight is applied to the model, the loads on the spring cans are out of the range of the spring can. Therefore, the thickness of the silencer is chosen such that the weight of the silencer will cause the loads in the spring cans to equal the as measured values (Dl No. 17). This is an iterative procedure with the final value being 0.350. This is verified by noting that the spring can displacements (nodes 39 and 49) are approximately 0.0 (See Att. E, F). Structural Steel Properties (ANSYS Material 2) Material - A-36 Steel E = 29,000,000 psi v = 0.3 Sy = 36000 psi Tangent Modulus = 0.0 psi p = 490 IbfVW 3 Form 3.1-3 Rev. I

I Automated Engineering Services Corp. NO. 19 OF 53 Calclaton Sheet Calulo Se _REVISION NUMBER: 0 CLIENT: Nuclear Management Comvany DATE: 03/07/03 PROJECT: Monticello Nuclear Generatini Plant PREPARED:

SUBJECT:

EDG Exhaust Evals CHECKED: JAA SAFETY RELATED YES [i NO f CALC. NO.: MN03-P022637-100 W4 x 13 - element type 'BEAM24" (plastic beam), real constant set 6 Point Y 7 T 7 T 1 2 3 4 5 6 7 -2.03 2.03 0.00 0.00 -2.03 0.00 2.03 1.9075 1.9075 1.9075 -1.9075 -1.9075 -1.9075 -1.9075 0.000 0.345 0.000 0.280 0.345 0.000 0.345 - C4 x 5.4 - element type "BEAM24M (plastic beam), real constant set 7 Point Y 7 T 7 T 1 1.127 2 -0.365 3 -0.365 4 1.127 1.852 1.852 -1.852 -1.852 0.000 0.296 0.184 0.296 Rigid Beam (material 3, element type 3, real constant 15) In order to model between beam centroids for gap and spring elements, a property is used. E = 29,000,000 psi v 0.3 p = 0 lbf/ft3 ANSYS Element type TBEAM4" (3-D Elastic Beam), real constant 15 A= 100.0 in2 Is = 1000 in4 IYY, = 1 000 in4 TKZ= 1.0 in TKY 1.0 in

1. = 1000 in4 rigid Form 3.1-3 Rev. 1

Automated Engineering Services Corp. N 0 Calculation Sheet A z REVISION NUMBER. 0 CLIENT: Nuclear Manazement Company DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:A 7D

SUBJECT:

EDG Exhaust Evals CHECKED: 01A 4-SAFETY RELATED YES [N] NO C] CALC. NO.: MN03-P022637-l00 E. Add Weights Add weights are modeled with the ANSYS uMass2l' element. From Dl No. 4, class JB, the flanges are slip-on flanges From Ref. 2, there is no data for 22" slip-on flanges. From Dl No. 14, the silencer 22" slip-on flanges have a OD of 29.5", a ID of 22" with 20 1 3/8" diameter bolt holes. From Dl No. 17, the flanges are 1 '/4 thick. - W = &((l4)[(29.52 - 222) - 20 (1.375)2]}(1.25)(490/1728) = 97 Ibf @ Silencer From Dl No. 7, the flexible connection 22" slip-on flanges have a OD of 29.5", a ID of 22.09" with 20 1 3/8" diameter bolt holes with a thickness of 1 12". W = {(7d4)[(29.52 - 22.092) -20 (1.375)21(1.5)(490/1728) = 115 Vbf @ Flex. Conn. F. Rigid Boundary Conditions ANSYS specifies a boundary fixity by applying a displacement of 0.0. The following degrees of freedom are permanently fixed: Node 22 (reference node for flexible, connection spring stiffnesses) x, y, z - displacements x, y, z - rotations Nodes 32, 42 (Support DGEH-2, DGEH-3, east baseplates, rigid connections) x, y, z - displacements y-rotation Form 3.1-3 II AC; VT. I

Automated Engineering Services Corp. NO. 2 1 1 OF 53 LCalculation Sheet REVISION NUMBER: 0 CLIENT: Nuclear Management Com any DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED: buff

SUBJECT:

EDG Exhaust Evals CHECKED: <JV14-SAFETY RELATED YES [i NO [CALC. NO.: MN03-P022637-100 Nodes 36, 46 (Support DGEH-2, DGEH-3, west baseplates, rigid connections) x, y, z - displacements y - rotation Nodes 50, 57 (support DGEH-1 south connections to floor steel) x, y, z - displacements x, y, z - rotations Nodes 54, 61 (support DGEH-1 north connections to floor steel) x, y, z - displacements Nodes 200 - 203 (reference nodes for supports DGEH-2, DGEH-3 baseplate spring stiffnesses) x, y, z - displacements x, y, z - rotations G. Flexible Boundary Conditions Flexible boundary conditions are modeled using the combinl4 element. The following combinl4 elements are used: Element type 7 - x-direction translation stiffness Element type 8 - y-direction translation stiffness Element type 9 - z-direction translation stiffness Element type 10 - x-direction rotation stiffness Element type 11 - x-direction rotation stiffness Element type 12 - x-direction rotation stiffness Form 3.1-3 Rev. I Form 3. 1-3 Rev. I

Automated Engineering Services Corp. .22 Calculation Sheet L//. REVISION NUMBER: 0 CLIENT: Nuclear Management Company DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED: X f

SUBJECT:

EDGExhaustEvals CHECKED: J SAFETY RELATED YES R NO [ CALC. NO.: MN03-P022637-100 The following flexible boundary conditions are specified: Flexible Connection (Dl No. 7) Elements 94-99, the following stiffnesses are used (see assumption 1) K = 10 b/in x, y, z - displacements K = 10 in Ib/rad x, y, z - rotations DGEH-2, 3 (spring cans) The spring cans are modeled using the combin37 element which allows for the input of a spring stiffness, spring force and the ability for the spring to be turned off if the positive vertical displacement is too large. For DGEH-2, the following parameters are used (Element 89) K = 363 lb/in Spring Force = 1832 lb Max. positive vertical displacement = 1.25 in For DGEH-3, the following parameters are used (Elemerit 88) K = 363 lb/in Spring Force = 1515 lb Max. positive vertical displacement = 0.375 in Baseplate Stiffnesses for both DGEH-2 and DGEH-3 (See Attachment A) K= 1000/0.0001515= 6.6 x 106 in Ib/rad (baseplate x direction) Kox= (1000/0.0001701 + 1000/0.0001726)/2 5.8 x 106 in Ib/rad (baseplate y direction) Form 3.1-3 Rev.I Fonn 3.1 -3 Rev. I

Automated Engineering Services Corp. NO.23 53 Calculation Sheet REVISION NUMBER: 0 CLIENT: Nuclear Management Comanv DATE: 03/07/03 PROJECT: MonticelloNuclearGeneratin Plant PREPARED:

SUBJECT:

EDG Exhaust Evals CHECKED: Jo SAFETY RELATED YES XI NO CALC. NO.: .MN03-P022637-100 H. Gap Elements The supports have gaps between the pipe and their support frame. These gap elements are modeled with combin40 elements. The element stiffness once the gap has closed is 1.0 x 101 lb/in. The following combin4O elements are used: Element type 5 - x-direction gap Element type 6 - z-direction gap The following gaps are specified: DGEH-1 gap = 0.5 in (x-direction, elements 83, 84) gap = 0.5 in (z-direction, elements 82, 85) DGEH-2, 3 gap = 0.125 in (z-direction, elements 74 - 77) I. Lugs (Elements 224 - 227) The lugs are modeled with a compression only LINK10 element. The area of the element is taken as the are of the lugs which equals 1.5(1.0) = 1.5 in2. J. Set solution parameters. Solution control = on Ramped loads AutoTime Stepping = on* Stress Stiffening = off Newton-Raphson Method = Auto e Time integration parameter = 1.0 Tirme integration = off (inertial effects) Large Deflections = off Form 3.1-3 Rev. 1 Form 3. 1-3 Rev. I

Automated Engineering Services Corp. NO. 24 OF 53 / / XC Calculation Sheet._._ .REVISION NUMBER: 0 CLIENT: Nuclear Management Company DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED: 7$f

SUBJECT:

EDG Exhaust Evals CHECKED: J SAFETY RELATED YES nx NO XCLC.]NO. MN03-P022637-100 K. Model Plot J rrorm J. 1-3 Rev. I

Automated Engineering Services Corp. NO.25 OF 53 / D Calculation Sheet Cal o Se REVISION NUMBER: 0 CLIENT: Nuclear Management Company DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:

SUBJECT:

EDG Exhaust Evals CHECKED: SAFETY RELATED YES [3 NO [] CALC. NO.: MN03-P022637-100 Deadweight and Tornado Loads A. Deadweight Loads Deadweight loads are accounted for by applying the acceleration due to gravity in the vertical upward direction. The acceleration due to gravity equals 386.4 in/sece. B. Tomado Loads The tornado definition is taken from USAR, Section 12.2.1.8 (Dl No. 15). Three criteria are specified.

1.

The tornado wind speed is taken as 300 mph.

2.

A differential pressure of 2 psig from inside to outside is to be considered. Since the pipe is open to the atmosphere, this requirement does not need to be considered.

3.

Torsional effects due to the tornado wind load applied to only one half the piping system. This case is bounded by the case where the entire piping system is subjected to the entire wind load. The pressure load applied to the piping is taken from ASCE paper 3269 (Ref. 3). From Ref. 3, equation 7, the pressure force equals: P = 0.002658V2 CD

Where, V = 300 mph CD = 1.81 for east/west wind on W4 x 13 (Ref. 3, p. 1146)

CD = 2.04 for north/south wind on W4 x 13 (Ref. 3, p. 1146) Pipe CD From Ref. 3, Fig. 6, the CD for a pipe is based on the Reynolds number. The Reynolds number is calculated from Ref. 3, Eq. 5 R = Vh/v = 6380Vh = 6380(300)(5280/3600)(22/12) = 5.1 x 106 CD= 0.40 for Pipe (Ref. 3, Fig. 6, R > 1.0 x 10o) Form 3.1-3 Rev. I

Automated Engineering Services Corp. NO. 26 OF 53 / D Calculation Sheet REVISION NUMBER: 0 CLIENT: Nuclear Manaaement Company DATE: 03/07/03 PROJECT: Monticello Nuclear Genemtfig Plant PREPARED:

SUBJECT:

EDO Exhaust Evals CHECKED:3A-SAFETY RELATED YES FI NO ]CALC NO.: MN03-P022637-100 For a tornado wind blowing north to south, the vertical pipe is protected by the EDG building. Therefore, the wind loads will only be applied to the portion of piping above the building. Determine load on piping above the building Load on Pipe Cross Section F = 0.062558V2CDApipe = 1627 lb

Where, V

300 mph CD = 1.0 (Ref. 10, p. 11-89, infinitely long cylinder parallel to the wind} Apip= =7(3.O)2/4 = 7.069 ft2 Load on Vertical Pipe Above Building F = 0.002558V 2CDLD. = 408 lb

Where, V = 300 mph

- CD = 0.40 L = Length above building =40 in - 22 in/2 =29 In = 2.417 ft Do= 22 in = 1.833 ft Total Load F= 1627 + 408 =2035 lb Form 3.1-3 Rev. I

Automated Engineering Services Corp. NO.27 OF 53 Calculation Sheet _L/ REVISION NUMBER: 0 CLIENT: Nuclear Management Company DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:Af e

SUBJECT:

EDG Exhaust Evals CHECKED: 4*'- SAFETY RELATED YES [5] NO CALC. NO.: MN03-P022637-100 Wind Blowing from North to South The tornado wind, which blows from north to south, impacts the open end of the exhaust line and the projected area of the silencer beyond the area of the 22" diameter pipe. The tornado wind also impacts a short run of the 22" riser, which extends above the roof elevation (i.e. height of the parapet). The magnitude of the integrated load was computed to be 2035 lbs. When this load is applied to the exhaust node of the ANSYS model, instabilities occur due to DGEH-3 spring can uplift. The spring can load oscillates between 0 lbs and 1379 lbs (i.e. minimum spring can load) and is unable to converge. A hand calculation is performed in lieu of an ANSYS run. The reaction @ DGEH-3 is taken as zero. The reactions @ DGEH-1 and DGEH-2 are computed from a static analysis. 72" .2I I- ,Support DGEH-2 2035 lb 72" 199.5" 93, C.G. (Aft. D, E) Support DGEH-1 Form 3.1-3 Rev. I

Automated Engineering Services Corp. NO.28 OF 53 Calcultion Sheet / S e t REVISION NUMBER: 0 CLIENT: Nuclear Management Company DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:

SUBJECT:

EDG Exhaust Evals CHECKED: vA,- SAFETY RELATED YES [ ] NO CALC. NO.: MN03-P022637-100 2 22 Mass := 11.4280. + 2.15954-1 + 1.3972lbse in in9+ in95 + 0.832796. lb sec - in Mass = 15.82 Ib sec in Wtot := Mass-386.4. Wtot = 61121b Xcg := 93-in Xh2 := 72-in Y:= 190.5-in .Pwind := 2035-Ib RX.hl := Pvind in 2 sec Weight of entire exhaust system (Aft. D, E) X distance from riser to CG of system (Aft. D, E) X distance from riser to DGEH-2 (Aft. B, C) Y distance from center of horizontal run to DGEH-1 (Aft. B, C) Magnitude of wind load RX.hl =2035 lb Ry.h2 = Wtot-XCg - Pwind Y Xh2 -Ry.h2 = 2510 lb Ry.hl := Wtot - Ry.h2 Ry.hl = 36021b Form 3.1-3 Rev. 1 Form 3. 1-3 Rev. I

Automated Engineering Services Corp. NO. 29 OF 53 Calculation Sheet REVISION NUMBER: 0 CLIENT: Nuclear Management Comanv. DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED: At?

SUBJECT:

EDG Exhaust Evals CHECKED: SAFETY RELATED YES M NO - CALC. NO.: .N03-P022637-100 Spring can DGEH-2 must be'evaluated for a load of Fy = 2510 lbs DGEH-1 must be evaluated for loads of F. = 2035 lbs & Fy = 3602 lbs As seen from the other two wind load cases pipe stresses are quite small and need not be considered further. Evaluation of Support DGEH-2 for South Blowing Tornado Wind The design load of 2510 lb is greater than the spring can range. However, even though the spring can has bottomed out, the spring can is acceptable for the following reason. The spring hanger housing is designed to be a 'rugged device'. This is required when a pipe is hydrostatically tested because the spring hanger is pinned so as to be rigid. The housing is designed to carry approximately twice normal operating loads. The loads on the rest of the support members are bounded by the other two tornado wind cases. Support DGEH-2 is acceptable for a South Blowing Tornado Wind Evaluation of Support DGEH-1 for South Blowing Tornado Wind An ANSYS Model of DGEH-1 is used to evaluate the loads from a south blowing tornado wind. The input listing is shown in Att. D. The output is listed in Att. G. The member forces and reaction loads are considered in the analysis of support DGEH-1 shown on pages 35 -41. Form 3.1-3 Rev. I Form 3. 1-3 I Rev. I

Automated Engineering Services Corp. NO.30 OF 53 Calculation Sheet REVISION NUMBER: 0 CLIENT: Nuclear Mana ement Companv DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:

SUBJECT:

EDG Exhaust Evals CHECKED: JVtA-SAFETY RELATED YES FI NO [I] CALC. NO.: MN03-P022637-100 Perform B31.1 Piping Analysis A. The following Code Evaluations are performed (Dl No. 2, 3, 15) Pressure + Deadweight + Tornado Wind Load < 1.2Sh (Dl No. 2, Eq. 12, cons.) a12 = PDo/4t + 0.75iM/Z

where, PDd4t = pressure stress (negligible) i = stress intensification factor (SIF, calculated below)

M = resultant moment due to deadweight + tornado Z = section modulus (calculated below) See the following page for the pipe stress summary B. SIF's Elbow SIF ieWbow = 4.02 see calculation above Flange SIF iflange= 1.9 (Dl No. 2) C. Section Modulus and Pipe Stress Check Z = 7r2t (Di No. 2, Section 104.8.4) 22" Pipe (cons. use for silencer) Do 22 in t = 0.375 in n: r = (Do - t)/2 =10.8125 in Z = 137.73 in3 Form 3.1-3 Rev. I Form 3. 1-3 Rev. I

Automated Engineering Services Corp. NO. 31 OF 53 Calculation Sheet REVISION NUMBER: 0 CLIENT: Nuclear Management Company DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:

SUBJECT:

EDG Exhaust Evals CHECKED: qVM4-SAFETY RELATED YES [RJ NO jFj CALC. NO.: MN03-P022637-100 Pipe Stresses East-West Tornado Element Node Z M IM M, lri M1121 l

• D I

ID in SIF in-lb in-lb in-lb in-lb p psi IR J 1 1 137.73 1.00 0 0 0 0 0 21400 0.00 2 137.73 1.00 0 -9630 4945 10826 79 21400 0.00 2 2 137.73 1.00 0 -9630 4945 10826 79 21400 0.00 3 137.73 1.00 0 -38521 19780 43303 314 21400 0.01 3 3 137.73 1.00 0 -38521 19780 43303 314 21400 0.01 4 137.73 1.90 0 -7413 -677 7444 77 21400 0.00 4 4 137.73 1.90 0 -7413 -677 7444 77 21400 0.00 5 137.73 1.00 0 -2488 -3400 4214 31 21400 0.00 5 5 137.73 1.00 0 -2488 -340o 4214 31 21400 0.00 6 137.73 1.00 0 25613 -19988 32489 236 21400 0.01 6 6 137.73 1.00 0 25613 -19988 32489 236 21400 0.01 7 - 137.73 1.00 0 25109 -22763 33891 246 21400 0.01 7 7 137.73 1:00 0 25109 -22763 33891 246 21400 0.01 8 137.73 1.00 0 -4002 -11727 12391 90 21400 0.00 8 8 137.73 1.00 0 -4002 -11727 12391 90 21400 0.00 9 137.73 1.00 0 -61719 13121. 63098 458 21400 0.02 9 9 137.73 1.00 0 -61719 13121 63098 458 21400 0.02 10 137.73 1.90 0 -70004 16782 71987 745 21400 0.03 10 10 137.73 1.90 0 -70004 16782 71987 745 21400 0.03 11 137.73 1.00 0 -117190 41154 124206 902 21400 0.04 11 11 137.73 1.00 0 -117190 41154 124206 902 21400 0.04 12 137.73 4.02 0 -43864 22673 49377 1081 21400 0.05 12 12 137.73 4.02 0 -22673 -43864 49377 1081 21400 0.05 13 137.73 4.02 387 -17864 37674 41697 913 21400 0.04

13.

13 137.73 4.02 387 37674 17864 41697 913 21400 0.04 14 137.73 1.00 387 59045 17864 61689 448 21400 0.02 14 14 137.73 1.00 387 59045 17864 61689 448 21400 0.02 15 137.73 1.00 387 64862 17884 67278 488 21400 0.02 15 15 137.73 1.00 387 64862 17864 67278 488 21400 0.02 16 137.73 1.00 387 55125 17864 57949 421 21400 0.02 16 16 137.73 1.00 387 55125 17864 57949 421 21400 0.02 17 137.73 1.00 387 29833 17884 34775 252 21400 0.01 l 17 17 137.73 1.00 387 29833 17864 34775 252 21400 0.01 s18 137.73 1.00 387 5467 17864 18686 136 21400 0.01 18 18 137.73 .1.00 387 447 29503. 29509 214 21400 0.01 19 137.73 4.02 387 228 29503 29506 646 21400 0.03 19 19 137.73 4.02 387 29503 -228 29506 646 21400 0.03 20 137.73 4.02 0 7617 -159 7619 167 21400 0.01 20 20 137.73 4.02 0 159 7617 7619 167 21400 0.01 21 137.73 1.90 0 0 0 0 0 21400 0.00 Maximum .~ A -0.05 Form 3.1-3 Rev. I Form 3.1-3 Rev. I

Automated Engineering Services Corp. NO. 32 ]OF 53 Calculation Sheet REVISION NUMBER: 0 CLIENT: Nuclear Management Company DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED: AR

SUBJECT:

EDG Exhaust Evals CHECKED: dJA SAFETY RELATED YES FRI NO D-CALC. NO.: _MN03-P022637-100 Pipe Stresses North Blowing Tomado Element l Node l Z l IM IMy lMzY Mr 1 u12 l 12a1l ID ID in3 SIF In-lb in-lb in-lb in-lb l psi psi IR 1 1 137.73 1.00 0 0 0 0 0 21400 0.00 2 137.73 1.00 0 0 '4945 4945 36 21400 0.00 2 2 137.73 1.00 0 0 4945 4945 36 21400 0.00 3 137.73 1.00

• 0 0

19780 19780 144 21400 0.01 3 3 137.73 1.00 0 0 19780 19780 144 21400 0.01 4 137.73 1.90 0 0 -16469 16469 170 21400 0.01 4 4 137.73 1.90 0 0 -16469 16469 170 21400 0.01 5 137.73 1.00 0 0 -22064 22064 160 21400 0.01 5 5 137.73 1.00 0 0 -22064 22064 160 21400 0.01 6 137.73 1.00 0 0 -63955 63955 464 21400 0.02 6 6 137.73 1.00 0 0 -63955 63955 464 21400 0.02 7 137.73 1.00 0 0 -92034 92034 668 21400 0.03 7 7 137.73 1.00 0 0 -92034 92034 668 21400 0.03 8 137.73 1.00 0 0 -106300 106300 772 21400 0.04 8 8 137.73 1.00 0 0 -106300 106300 772 21400 0.04 9 137.73 1.00 0 0 -106760 106760 775 21400 0.04 9 9 137.73 1.00 0 0 -106760 106760 775 21400 0.04 10 137.73 1.90 0 0 -105970 105970 1096 21400 0.05 10 10 137.73 1.90 0 0 -105970 105970 1096 21400 0.05 11 137.73 1.00 0 0 -96669 96669 702 21400 0.03 11 .11 137.73 1.00 0 0 -96669 96669 702 21400 0.03 12 137.73 4.02 0 0 -150100 150100 3286 21400 0.15 12 12 137.73 4.02 0 150100 0 150100 3286 21400 0.15 13 137.73 4.02 0 176820 0 176820 3871 21400 0.18 13 13 137.73 4.02 0 0 -176820 176820 3871 21400 0.18 14 137.73 1.00 0 0 -156920 156920 1139 21400 0.05. 14 14 137.73 1.00 0 0 -156920 156920 1139 21400 0.05 15 137.73 1.00 0 0 -121470 121470 882 21400 0.04 15 15 137.73 1.00 0 0 -121470 121470 882 21400 0.04 16 137.73 1.00 0 0 -70.458 70458 512 21400 0.02 16 16 137.73 1.00 0 0 -70458 70458 512 21400 0.02 1 17 137.73 1.00 0 0 -3894 3894 28 21400 0.00 7 17 137.73 1.00 0 0 -3894 3894 28 21400 0.00 18 137.73 1.00 0 0 50884 50884 369 21400 0.02 18 18 137.73 1.00 0 0 30096 30096 219 21400 0.01 19 137.73 4.02 0 0 30024 30024 657 21400 0.03 19 19 137.73 4.02 0 - 30024 0 30024 657 21400 0.03 20 137.73 4.02 0 7600 0 7800 171 21400 0.01 20 20 137.73 4.02 0 0 7800 7800 171 .. 21400 0.01 21 137.73 1.90 0 0 0 0 0 21400 0.00 Maximum J [ -w h [:.' 0.1 8 Form 3.1-3 Rev. 1 Fonn 3.1 -3 Rev. I

Automated Engineering Services Corp. NO.33 OF 53. / D Calculation Sheet. Cacuato SREVISION NUMBER: 0 CLIENT: Nuclear Management Company DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:

SUBJECT:

EDG Exhaust Evals CHECKED: J/A-SAFETY RELATED YES Fx1 NO E]. CALC NO.: MN03-P022637-100 D. Check Displacements at Flexible Connection (Node 21) East-West Tornado Wind (Att. E, Set 2) axia. = 0.0 in < 1.0 in o.k. 8iateral = 0.696 in < 1.0 in o.k. North Tornado Wind (Aft. F, Set 2) 8aiaia = 0.228 in < 1.0 in o.k.. 8lateral = 0.7085 in < 1.0 in o.k. E. Check Forces in H2 Spring Can (Element 89) East-West Tornado Wind (Aft. E, Set 2) Spring Force = 19 lb Preload = 1832 lb Total Load = 1851 lb Allowable Spring Can Range = 1379 lb 4 2240 lb o.k. North Tornado Wind (Att. F, Set 2) Spring Force = 197 lb Preload = 1832 lb Total Load = 2029 lb Allowable Spring Can Range = 1379 lb - 2240 lb o.k. F. Check Forces in H3 Spring Can (Element 88) East-West Tornado Wind (Aft. E, Set 2) Spring Force = 29 lb Preload = 1515 lb Total Load = 1544 lb Allowable Spring Can Range = 1379 lb - 2240 lb o.k. Form 3.1-3 Rev. I Form 3.1 -3 Rev. I

lAutomated Engineering Services Corp. NO.34 OF 53 Calculation Sheet _JLI/ ,REVISION NUMBER 0 CLIENT: Nuclear Management Cornan DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:

SUBJECT:

EDG Exhaust Evals CHECKED: JA-SAFETY RELATED YES i NO FII CALC. NO.: MN03-P022637-100 North Tornado Wind (Aft. F, Set 2) Spring Force = 747 lb Preload - 1515 lb Total Load = 2262 lb Allowable Spring Can Range = 1379 lb -+ 2376 lb (max) o.k. Form 3.1-3 Rev. I Form 3.1-3 Rev. I

Automated Engineering Services Corp. NO. 35 OF 53 Calculation Sheet /JL/a REVISION NUMBER: 0 CLIENT: Nuclear Management Company DATE: 03/07/03 PROJECT: Monticello Nuclear Generatine Plant PREPARED:

SUBJECT:

EDG Exhaust Evals CHECKED: 3V%- SAFETY RELATED YES i NO [ CALC. NO.: MN03-P022637-100 Perform Support Analysis A. Support Load Combinations in accordance with NPD-M-38 (Dl No. 3) and USAR (DI No. 15) are being evaluated: Deadweight + Tornado B. Support DGEH-1 (Members 50 -. 61) C4 x 5.4 members The maximum normal stress in the members is 30676 psi. This is less than the yield stress of 36000 psi. Therefore, the all members remain elastic and are acceptable by inspection. Check Shear Stress Check Shear + Torsion Stress Ay= 2bft = 2(1.584)(0.296) = 0.938 in2 A = dt = 4.00(0.184) = 0.736 in2 J = 0.04 in4 F, = 0.4FY 0.4(36000) = 14400 psi (cons.) Fymax = 1119 lb Fzmax = 1801 lb Mxmax = 1726 in lb fv = Fymax/Avy + FzmJAvz + MxmaxtfIJ = 16412 psi IR = f,/Fv = 1.14 < 1.4. o.k. Form 3.1-3 Rey. I Forin 3.1-3 Rev. I

Automated Engineering Services Corp. N36 OF 53 / D Calculation Sheet Calul SREVISION NUMBER: 0 CLIENT: Nuclear Management Comuanv DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:

SUBJECT:

EDG Exhaust Evals CHECKED: J SAFETY RELATED YES Fx NO [] CALC. NO.: MN03-P022637-100 Weld between C4 x 5.4 and C4 x 5.4 (Beam 54, J Node, Beam 55, 1 Node, Beam 56, 1 Node, Beam 57, J Node) Loads Fx:= 285-1b Fy:= 1119-lb Fz:= 1801 -Ib Properties d := 4-in t O:= 0.184-in a := d 4 b := bf -tw L := d+ a + 2-b Mx:= 1726-in:1b My := 1754-in-lb Mz:= 5208-in-lb bft:= 1.584-in tf := 0.296-in a= 3.408in b = 1.4in L = 10.208in a-tw+ 2-b-tv+ 2) L Zbar := d3 a3 2(a) -y: + - +26 1 2 12k, Zbar = 0.304in i.4 Iy = 16.762.n in Iz: d-Zbar + a:(tw Zbar) + 2-1 b +b- + - Zbar)] in4 Iz= 1.81 8-in Form 3.1-3 Rev. 1 For 3. 1-3 Rev. I

Automated Engineering Services Corp. NO.i37 lOF 53 / / .Calculation Sheet Cclo S REVISION NUMBER: 0 CLIENT: Nuclear Management Companv DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED: 7

SUBJECT:

EDG Exhaust Evals CHECKED: iJO-SAFETY RELATED YES j53 NO CALC. NO.: MN03-P022637-100 S = 2. ly d In3 S = 8.381 in in Sz :=-- lz max(bf - Zbar,Zbar) J I= l+ IZ .'3 Sz = I1.42 in in4 J = 18.58!.in lb ft = 3904. . in Stresses Fx My _ Mz ft=L +Sy Sz Fy Mx () L J Fz Mx-max(bf - Zbarzbar) L + fw: /t + f + f lb fvy = 295-in fvz = 295 lbin fw = 3927 lbin Fw:= 0.25-in-0.707-0.3-70000-psi lb Fw= 3712-in IR :=-f Fw IR = 1.06 < 1.4 o.k. Form 3.1-3 Rev. 1 Form 3.1-3 Rev. I

L t Automated Engineering Services Corp.NO. 38 OF 53 Calculation Sheet REVISION NUMBER: 0 CLIENT: Nuclear Management Companv DATE: 03/07/03 PROJECT: Monticello Nuclear Generatine Plant PREPARED:

SUBJECT:

EDG Exhaust Evals CHECKED: Add SAFETY RELATED YES i NO F] CALC. NO.: . MN03-P022637-100 Weld Between C4 x 5.4 and Floor Steel (Reactions at nodes 50, 57) Loads Fx = 687 lb Fy= 1474 lb Fz = 336 lb Mx = 1426 in lb My = 4985 in lb M. = 25473 in lb

• (ANSYS F. load)

(ANSYS Fy load) (ANSYS Fz load) (ANSYS Mx load) (ANSYS My load) (ANSYS Mz load) See the following page for weld evaluation Forrn3.1-3 Rev. I Form 3. 1-3 Rev. I

Automated Engineering Services Corp. NO. OF 53 l Calculation Sheet REVISION NO: 0 CLIENT: Nuclear Management Company DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED: 7"

SUBJECT:

EDG Exhaust Evals CHECKED: J wL-SAFETY RELATED: YES E NO O CALC NO: MN03-P022637-100

== Description:== Weld between C4 x 5.4-and Floor Steel Member: C4x5.4 Weld Type: C1 Leg Size (W): 0.2500 in Loads: Fx= Fy= Fz = Mx = MY = ,MZ= 687 lbs 1474 lbs 336 lbs 1426 in-lbs 4985 in-lbs 25473 in-lbs t f b = d = tw= ff= Weld Properties: (Ref. 5) 1.58 4.00 0.18 0.30 13.376 2.625 14.717 32.490 2.000 1.148 in in in in in in3/in in3Iin in4/in in in L = 2(2b -tW +d -t) = Swy= [lCz][(b-t)+b3)/6+d(b-Cz) 2+(d-2tt)(b-Cz-tw)2+2b(Cz-b12) 2+(112)(b-tw)(2Cz+tw-b)j = S = (1/2Cy)((d +(d-2t0 2)/6 +bd2+(b-tw)(d-2ffl1 JW= Swy(Cz) + Swz(Cy) - C= d/2b Cz b-{[2b2-tw(tw-d-2tt)]/Aw} Weld Stresses: ft= f -= f, = F/LW + MJSz + M/Swy = FY/Lw + (Mx x Cz)IJw = Fr'Lw + (M, x Cy)/Jw = (f 2 + fy + f. 2)1 1 = 3682 161 113 3687 lb/in Ib/in lb/in lb/in Allowable Stresses F,,w = Fw = 0.3*(F,,,)(0.707)(W) = - Interaction Ratio (IR) = I 70000 3712 psi lb/in (Electrode Tensile Strength) (Dl No. 5) 0.99 < 1.0 Weld is Acceptable Form 3.1-3 Rev. 1 F orm 3.1-3 Rev. 1

Automated Engineering Services Corp. NO.40 lOF 53 / D Calculation'Sheet Caclto Sheet REVISION NUMBER: 0 CLIENT: Nuclear Management Comnany DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:

SUBJECT:

EDG Exhaust Evals CHECKED: JVIA-SAFETY RELATED YES 3 NO [] CALC. NO.: MN03-P022637-100 Clip Angle Connection (Reactions at nodes 54, 61) Loads Fx = 432 lb (ANSYS Fx load) Fy = 504 lb (ANSYS Fy load) F, = 231 lb (ANSYS Fz load) From Ref. 8, p. 100, the allowable connection load for a point load is 4220/2 = 21101b. F=432+504+231 = 11671b F= 1167lb*Fyai=2110lb o.k. Evaluate Integral Welded Attachment Loads (Max. of elements 224 - 227) East-West Tomado F = 1222 lb North Tornado F = 1739 lb South Tornado F = 3602 lb (cons.) See following page for IWA Evaluation Cons. perform IWA at 9500 F. Evaluate IWA per Ref. 9 Support DGEH-1 is acceptable for a 300 mph wind load. Form 3.1-3 Rev. I Fonn 3. 1-3 Rev. I

Automated Engineering Services Corp. NO. 41 lIOF 53 / Calcultion Sheet /JJLJ. REVISION NUMBER: 0 CLIENT: Nuclear Manaaement Company DATE: 03/07/03 PROJECT: Monticello Nuclear Generatine Plant PREPARED: Ta f

SUBJECT:

EDO Exhaust Evals CHECKED: JL4A-SAFETY RELATED YES [53 NO [] CALC. NO.: - MN03-P022637-100 INTEGRAL ATTACHMENT EVALUATION PROBLEM DESCRIPTION: MODEL: EDGEXHAUST NODE: 62 - 65 MARK NO: DGEH1 TYPE: RISERCLAMP CODE CASE: N-318-3

• PROBLEM PARAMETERS:

RUN OD: 22.000 RUN THK: .375 Li: .500 L2: 2.000 KL: 3.600 E X ALPHA: .000 DELTA T: .000 A WELD: 2.386 Z-ML WELD: 1.697 Z-MN WELD:******** Z-MT WELD:******** LOADS: LOAD CASE DW DYNB DYNC DYND THMAX THMIN PIPE STRESSES: STRESS TYPE PIPE LOCAL TOTAL -ALLOWABLE RATIO OTHER STRESSES: SNL**:- SHEAR(6): WELD(7): WELD(8): W ML

0.

0.

0.

0.

0.

0.

0.

5403.

0.

0.

0.

0. MN 0. 0. 0. 0. 0. 0. EQ. 9 LEVEL C 0. 0. '0. Q1 Q2

0.

0. O. 0.

0.

0.

0.

3602.

0.

0.

0.

0. 0.. 0* MT 0.* E. ' I* O.

0.

0.

0.

.0. EQ. 11* LEVEL A

0.

0.

0.

24375. .000 EQ. 8 DESIGN Li 0. 0. 0. 4500. .000 16950. < 2401. < 6203. < 3019. < EQ. 9 EVEL B 0. 0. 0. 5400. .000 42800 21400 42800 21400 EQ. 9 LEVEL D 369. 12101. 12470. EQ. 10 LEVEL A 0. 0. 0. 19875. .000 5400. 21400. .000. - .583 (.396) (.112) (.145) (.141) OK OK OK OK Form 3.1-3 Rev. I Form 3. 1-3 Rev. I

Automated Engineering Services Corp. N. 042 li O IF 53 Calculation Sheet REVISION NUMBER: 0 CLIENT: Nuclear Management Comnany DATE: 03/07/03 PROJECT: Monticello Nuclear Generatin Plant PREPARED:A 1f

SUBJECT:

EDG Exhaust Evals CHECKED: JA4-SAFETY RELATED YES ,,- NO I] CALC. NO.: MN03-P022637-100 C. Support DGEH-2 (Members 40 - 45) W4 x 13 members The maximum normal stress in the members is 23941 psi: This is less than the yield stress of 36000 psi. Therefore, the all members remain elastic and are acceptable by inspection. Check Shear Stress -Vy 706 lb V =81 37 lb Mx = 13 in lb (negligible) Avy = 2b&tt = 2(4.06)(0.345) = 2.80 in2 Aw = dt4 = 4.16(0.28) = 1.16 in2 f, = Vy/Ay +- VA=, = 7267 psi F, = 0.4FY = 0.4(36000) = 14400 psi (cons.) IR = fI/F, = 0.50 < 1.0 o.k. Weld Between W4 x 13 and W4 x 13 (Beam 42,1 Node, Beam 43, J Node) Loads F. = 6983 lb Fy=8137 lb Fz =171 lb M= 0 in lb My = 13 in lb Mz = 115370 in lb (ANSYS F. load) (ANSYS Fz load) (ANSYS Fy !oad) (ANSYS Mx load) (ANSYS Mz load) (ANSYS My load) See the following page for weld evaluation Form 3.1-3 Rev. I Form 3.1-3 Rev.lI

Automated Engineering Services Corp. NO. 43 lOF 53 Calculation Sheet REVISION NO: 0 CLIENT: Nuclear Management Companv DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:

SUBJECT:

EDG Exhaust Evals CHECKED: Jv SAFETY RELATED: YES 0 NO O CALC NO: MN03-P022637-100

== Description:== Weld between W4 x 13 and W4 x 13 (Beam 42, I node, Beam 43, J node) Member: W4X1 3 Weld Type: Wi Leg Size (W): 0.2500 in Loads: Fx= F, = Fz= MY = .M2 = 6983 8137 171 0 13 115370 lbs lbs Ibs in-lbs in-lbs in-lbs b = d = tw= ff= 4.06 4.16 0.28 0.35 in in in in Weld Properties: (Ref. 5) Lv = SWY = Swz = .. = Jw= C = cz _ z 2(2b+d -tw-2 tf) = b2 / 3+(1 J b)[ (1 / 12)(b - tw)3+(d - 2tfW 2 + (d - 2t 2[(d -2 /3 + b - WI / d +bd = Swy(Cz) +Swz(Cy) = dJ/2 = b /2 = (1 / 4)(b - tw)(b + t) 2 = lb/in Ib/in l Ib/in lb/in 22.620 11.054 31.179 87.291 2.080 2.030 in in3/in in3/in in4/in in in Weld Stresses: ft= fv= fvz = fW= Fx/LW + M/SS, + MY/S wy = Fy/L, + (M x Cz)/Jw = FZ/LW + (Mx x Cy)/Jw = (f 2 + fY2 + f:2)112 = 401 C 36C E 402E Allowable Stresses Fw = Fw = 0.3*(Fw)(0.707)(W) = Interaction Ratio (IR) = 70000 3712 psi lblin (Electrode Tensile Strength) (Dl No. 5) 1.08 < 1.4 Weld is Acceptable Form 3.1-3 Rev. 1 Form 3.1-3 . Rev. I

l Automated Engineering Services Corp. NO. 44 lOF 53 Calculatioia Sheet a.REVISION NUMBER: 0 CLIENT: Nuclear Management Company DATE: 03/07/03 PROJECT: Monticello Nuclear Oeneratin2 Plant PREPARED:

SUBJECT:

EDG Exhaust Evals CHECKED: W SAFETY RELATED YES Fx NO. [ CALC. NO.: MN03-P022637-100 Weld Between W4 x 13 and Baseplate (Reactions at nodes 42, 46, 202, 203) Loads F. = 8182 lb Fy = 7458 lb F, = 706 lb M. = 13 in lb My = 12763 in lb Mt = 9499 in lb (ANSYS Fy load) (ANSYS F, load) (ANSYS F. load) (ANSYS My load) (ANSYS M, load) (ANSYS M. load) See the following page for weld evaluation Form 3.1-3 Rev. I

Z Automated Engineering Services Corp. NO. 45 F53 L Calculation Sheet REVISIONNO: 0 CLIENT: Nuclear Management Company DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:

SUBJECT:

EDG Exhaust Evals CHECKED: J,44-SAFETY RELATED: YES 0 NO O CALC NO: . MN03-P022637-100

== Description:== Wed between W4 x 13 and Baseplate (Nodes 42, 46, 202, 203) Member:* W4X13 Weld Type: W1 Loads: Fx= Fy = Fz = Mx=- Mr = MZ = 8182 lbs 7458 lbs .706 lbs 13 in-lbs 12763 in-lbs 9499 in-lbs Leg Size (W): 0.2500 in b = 4.06 in d = 4.16 in tw = 0.28 in tf= 0.35 -in (Ref. 5) Weld Properties: Lw 2(2b+d-tw-2ft)= Swy = b2 /-3+(1 l b)[ 11 /12)(b - tW)3+(d - 2tf)tw + (1 /4)(b - tw)(b + tw)21 = Swz = (d - 2tf)j(d - 2tf) / 3 + b - tw / d +bd= Jw Swy(Cz) +Swz(Cy) = CY d/2= Cz b/2= Weld Stresses: 22.620 11.054 31.179 87.291 2.080 2.030. - in in3/in in3/in in4/in in in f, = F-, + M,/Swz + MVSy = fW = Fy/Lw + (M, x C,)/Jw = fvz = FzIL z+ (Mx x Cy)/Jw = fw-(f.2 + f,2 + f22)"2 = Allowable Stresses 1821 330 - 32 1851 lbrin lbrin lb/in lb/in FUW = FW = 0.3*(Fw)(0.707)(W) = Interaction Ratio (IR) = I 70000 3712 psi lbfin (Electrode Tensile Strength) (Dl No. 5) D.50 < 1.0 Weld is Acceptable z'orm 3.1-3 Rev. 1 I r orm 5.1-3 Rev. I

Automated Engineering Services Corp. NO. 46 OF 53 Calculation Sheet REVISION NUMBER: 0 CLIENT: NuclearManaement Companv DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:A e

SUBJECT:

EDG Exhaust Evals CHECKED: J vA SAFETY RELATED YES 'NO [] CALC. NO.: _MN03-P022637-100 Evaluate Baseplate and Anchor Bolts (Reactions at nodes 42, 46, 202, 203) Baseplate Loads ANSYS lists reaction loads, the applied loads on the baseplate have the opposite sign of that reported in the output. The ANSYS applied loads are listed below. ANSYS East-West North East-West North Direction Nodes 42/202 Nodes 42/202 Nodes 46/203 Nodes 46/203 Fx 0 706 0 706 Fy-8182 -1074. 6212 -1074 Fz -1959 507 7458 -507 Mx7565 119 9499 -119 My 0 -13 0 13 M z 0 -12763 0 -12763 Forces are in lbs, Moments are in in-lbs The following transfer functions are'used to convert ANSYS loads to NPLATE loads: Node 42/202 XA - -YN YA eZ ZA - -XN Node 46/203 XA -+ +YN YA -+ ZN ZA - XN The NPLATE loads are listed below Form 3.1-3 Rev. I Fonn 3.1-3 Rev. I

a Automated Engineering Services Corp. NO. 47 OF 53 Calculation Sheet REVISION NUMBER: 0 CLIENT: Nuclear Management Comnanv DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:A f

SUBJECT:

EDG Exhaust Evals CHECKED: SAFETY RELATED YES f53 NO [] CALC. NO.: MN03-P022637-100 NPLATE East-West North East-West North Direction Nodes 42/202 Nodes 42/202 Nodes 46/203 Nodes 46/203 Fk 1959 -507 7458 -507 Fy0 -706 0 706 Fz -8182 -1074 6212 -1074 Mx0 12763 0 -12763 My -7565 -119 9499 -119 Mz0 -13** 0 13**

• • Negligible Load Forces are in 'lbs, Moments are in in-lbs Baseplate Parameters t=0.375 in Es = 29,000,000 psi v, = 0.3 Ec = 3,122 psi v, = 0.15 Su = 58,000 psi Sy = 36,000 psi SSY = 1.61 Pall = 1.167(Su/Sy)(O. 75)(Sy) = 50765 psi (Dl No. 18)

Anchor Bolt Allowables (Ref. 1) Dl No. 9,12, the anchor bolts are 5/8" conc. fasteners. From Ref. 1, the concrete fasteners are Phillips Red Head Self Drilling Anchors. The operability allowable is based on a safety factor of 2 on ultimate. Tall = (3/3.5)(4)(2925)/2 = 5014 lb Vaul = (3/3.5)(4)(2975)/2 = 5100 lb Forin3.l-3 Rev. I Form 3.1-3 Rev. I

Automated Engineering Services Corp. 48 Calculation Sheet z/JL REVISION NUMBER: 0 CLIENT: Nuclear Management Company DATE: 03/07/03 PROJECT: Monticello Nuclear Generathig Plant PREPARED:

SUBJECT:

EDG Exhaust Evals CHECKED: JAo SAFETY RELATED YES [E] NO CALC. NO.: MN03-P022637-100 Baseplate Analysis Results (Aft. H, L. C. 1 - 4) Plate Bending IR= 0.53 < 1.0 Anchor Bolts IR = 0.98 o.k. o.k. < 1.0 Form 3.1-3 Rev. I Fonn 3.1 -3 Rev. I

Automated Engineering Services Corp. .49 / / DzCCalculation Sheet E o Sheet REVISION NUMBER. 0 CLIENT: Nuclear Management Company DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED: 7"f

SUBJECT:

EDG Exhaust Evals CHECKED: J SAFETY RELATED YES NO CALC. NO.: MN03-P022637-100 D. Support DGEH-3 (Members 30 - 35) W4 x 13 members The maximum normal stress in the members is 14119 psi. This is less than the yield stress of 36000 psi. Therefore, the all members remain elastic and are acceptable by inspection. Check Shear Stress Vy = 706 lb V, = 5201 lb Mx = 13 in lb (negligible) Al, = 2bt = 2(4.06)(0.345) = 2.80 in2 A,, = dti, = 4.16(0.28) = 1.16 in2 fv = Vy/Ay + V/Avz = 4736 psi F, = 0.4Fy = 0.4(36000) = 14400 psi IR = fIF, = 0.33 < 1.0 o.k. (cons.) Form 3.1-3 Rev. 1 Formn 3. 1-3 Rev. I

Automated Engineering Services Corp. NO. 50 OF 53 / Calculation Sheet ZJL~f _REVISION NUMB3ER: 0 CLIENT: Nuclear Management Company DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:

SUBJECT:

EDG Exhaust Evals CHECKED:.3 SAFETY RELATED YES [3 NO CALC. NO.: MN03-PO22637-100 Weld Between W4 x 13 and W4 x 13 (Beam 32, I Node, Beam 33, J Node) Loads F. = 3885 lb Fy = 5201 lb Fz= 171 lb M.= 0 in lb My= 13 in lb Mz= 71175 in lb (ANSYS F. load) (ANSYS F. load) (ANSYS Fy load) (AN SYS M. load) (ANSYS M, load) (ANSYS My load) The weld is identical to the DGEH-H2 weld and the loads are bounded by the DGEH-2 weld, therefore, this weld is o.k. by inspection. Weld Between W4 x 13 and Baseplate (Reactions at nodes 32, 36,200, 201) Loads F. = 5246 lb Fy = 4359 lb Fz = 706 lb M.= 13 in lb My = 12763 in lb Mz = 5822 in lb (ANSYS Fy load) (ANSYS F. load) (ANSYS F. load) (ANSYS My load) (ANSYS M. load) (ANSYS Mx load) The weld is identical to the DGEH-H2 weld and the loads are bounded by the DGEH-2 weld, therefore, this weld is o.k. by inspection. Form 3.1-3 Rev. I Form 3. 1-3 Rev. I

/ Automated Engineering Services Corp. NO. 51lIOF 53 Calculation Sheet REVISION NUMBER: 0 CLIENT: Nuclear Mana ement Company DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:

SUBJECT:

EDG Exhaust Evals CHECKED: Ji SAFETY RELATED YES N NO CALC. NO.: MN03-P022637-100 Evaluate Baseplate and Anchor Bolts (Reactions at nodes 32, 36, 200, 201) Baseplate Loads ANSYS lists reaction loads, the applied loads on the baseplate have the opposite sign of that reported in the output. The ANSYS applied loads are listed below. ANSYS East-West North East-West North Direction Nodes 32/200 Nodes 32/200 Nodes 36/201 Nodes 36/201 Fx 0 706 0 -706 Fy-5246 -1190 3583 -1190 Fz -800 565 4359 -565 Mx4770 132 5822 -132 My 0 -13 0 13 Mz0 -12763 0 -12763 Forces are in lbs, Moments-are in in-lbs The following transfer functions are used to NPLATE loads: convert ANSYS loads to Node 32/200 XA -+ -YN YA - ZN ZA - -XN Node 36/201 XA -+ +YN YA -+ ZN ZA-XN The NPLATE loads are listed below Form 3.1-3 Rev. I Fonn 3.1 -3 Rev. I

Automated Engineering Services Corp. NO. 52 53 Calculation Sheet /E .k REVISION NIMMER: 0 CLIENT: Nuclear Management Comuanv DATE: 03/07/03 PROJECT: Monticello Nuclear Generatine Plant PREPARED: -°

SUBJECT:

EDG Exhaust Evals CHECKED: By SAFETY RELATED YES I NO [ CALC. NO.: MN03-P022637-100 NPLATE East-West North East-West North Direction Nodes 32/200 Nodes 32/200 Nodes 36/201 Nodes 36/201 Fx 800 -565 4359 -565 Fy 0 -706 0 706 Fz -5246 -1190 3583 -1190 Mx0 12763 0 -12763 My -4770 -132 5822 -132 Mz 0 -1 3** 0 13**

• • Negligible Load The east-west loads are bounded by DGEH-2, Therefore, the north loads.

Forces are in lbs, Moments are in in-lbs only evaluate Baseplate Parameters/Anchor Bolt Allowables See Support DGEH-2 for development of the baseplate parameters and anchor bolt allowables. Baseplate Analysis Results (Aft. H, L. C. 1 - 6) Plate Bending IR=0.53 <- 1.0 o.k. Anchor Bolts IR = 0.98 < 1.0 o.k. Form 3.1-3 Rev. I Form 3.1-3 Rev. I

a Automated Engineering Services Corp. NO.53 Calculation Sheet REVISION NUMBER: 0 CLIENT: Nuclear Management Comanv DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED: 4 70

SUBJECT:

EDG Exhaust Evals CHECKED: SAFETY RELATED YES IxJ NO [] CALC. NO.: MN03-P022637-100

11.

Conclusion The EDG exhaust piping and supports meet the operability requirements of NPD-M-38 and ASME Appendix F for a Design Basis Tornado wind of 300 mph. Form 3.1-3 Rev. 1 Form 3.1-3 Rev. I

Automated Engineering Services Corp. NO. Al OF A28 / I Calculation Sheet REVISION NUMBER: 0 CLIENT: Nuclear Management Company DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:,A 7°

SUBJECT:

ED GExhaust Evals CHECKED: Vl'l-SAFETY RELATED YES [5] NO ] CALC. NO.: MN03-P022637-100 Attachment A Stiffness Analysis for DGEH-2, -3, -5, -6 Baseplates Form 3.1-3 Rev. I

Automated Engineering Services Corp. NO. A2 OF A28 Calculation Sheet REVISION NUMBER: 0 CLIENT: Nuclear Management Comvanv DATE: 03/07/03 PROJECT: Monticello Nuclear GeneratinPlant PREPARED:

SUBJECT:

EDG Exhaust Evals CHECKED: JVA-SAFETY RELATED YES i N [] CALC. NO.: MN03-P022637-100 121 122 123 124 125 127 12R 129 130 131n 126 1321 I109 97 95 73 61 49 37 25 13 1 12 127 ¶ 27 ii -I-120 'as 96 84 72 60 48 24 2 3 4 5 6 7 8 9 10 11 12 Form 3.1-3 Rev. I

• • • • • Pacific Nuclear NPLATE v. 1.1.0 Supports DGEH-2, 3, 5, 6 -

Stiffness CLIENT Nuclear Management Company PROJECT NAME Monticello Nuclear Generating Plant JOB NUMBER FILENUMBER MN03-P022637-100 RUN NUMBER NEC-3E68DClC RUN DATE FRI MAR 07 12:51:24 2003 PREPARED BY/DATE: CHECKED BY/DATE: -7 Scott Tradup -- a-t-" Joe Attwood NPLATE DIRECTORY : C:\\NPLATE\\ CURRENT DIRECTORY : C:\\NPLATE INPUT FILE

C:\\NPLATE\\H2STIFF.NPL PAGE it OF

• • • • • Pacific Nuclear ****

NEC-3E68DC1C FRI MAR 07 12:51:24 2003 PROJECT : Monticello Nuclear Generating Plant CLIENT

Nuclear Management Company PAGE A004 of A028 NPLATE v. 1.1.0 MN03-P022637-100 Supports DGEH-2, 3, 5, 6 -

Stiffness PROBLEM SIZE : Number of Nodes 132 Number of Plate Elements 110 Number of Bolts 4 Number of Bolt Types. 1 Number of Column Segments 13 Number of Stiffener Types 0 Number of Stiffeners 0 Number of Beam Types 0 Number of Beams 0 Number of Boundary types 0 Number of Weld thickness 0 Number of'Weld Segments 0 Number of Fixed joints 0 Number of Applied Loads 3 Number of Applied Inloads 0 Number of Loading Cases 3 Number of Equations 396 Half-Bandwidth of System 42 STEEL PROPERTIES Young's Modulus Poisson's Ratio 29000.0000 ksi 0.3000 CONCRETE PROPERTIES : Young's Modulus Poisson's Ratio 3122.0000 ksi 0.1500 BASEPLATE DATA : Base Plate thickness Allowable Bending Stress Concrete Mat Stiffness Baseplate Aspect Ratio Max. El. Aspect Ratio Additional pages before page 1 0.3750 in 27.0000 ksi 373.5511 k/inA3 1.0000 2.0000 for el. 24 33

• • • • • Pacific Nuclear ****

FRI MAR 07 12:51:24 2003 NEC-3E68DC1C PAGE A005 of A028 NPLATE v. 1.1.0 PROJECT : Monticello Nuclear Generating Plant CLIENT

Nuclear Management Company MN03-P022637-100 Supports DGEH-2, 3,

5, 6 - Stiffness NODAL COORDINATES

(UNITS:

INCHES) NODE 1 2 .3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 -X-1.000000 1.000000 1.500000 2.250000 3.000000 4.000000 5.000000 6.000000 6.750000 7.500000 8.250000 9.000000

0. 000000 1.000000 1.500000 2.250000 3.000000 4.000000 5.000000 6.000000 6.750000 7.500000 8.250000 9.000000 0.000000 1.000000 1.500000 2.250000 3.000000 4.000000 5.000000 6.000000 6.750000 7.500000 8.250000 9.000000

0. 000000.

1.000000 1.500000 -y_

0.

.000000 0.000000

0. 000000 0.000000 0.000000 O.000000 0.000000 0.000000 0.000000

0. 000000

0. 000000 0.000000 0.750000 0.750000 0.750000 0.750000 0.750000 0.750000 0.750000 0.750000 0.750000 0.750000 0.750000 0.750000 1.500000 1.500000 1.500000 1.500000 1.500000 1.500000 1.500000 1.500000 1.500000 1.500000 1.500000 1.500000 2.500000

-2.500000 2.500000 NODE 67 68 69 70 71 72 73 74 75 76 77 78 79 80 81 82 83 84 85 86 87 88 89 90 91 92 93 94 95 96 97 98 99 100 101 102 103 104 105 -X-5.000000 6:000000 6.750000 7.500000 8.250000 9.000000

0. 000000 1.000000 1.500000 2.250000 3.000000 4.000000 5.000000 6.000000 6.750000 7.500000 8.250000 9.000000 0.000000 1.000000 1.500000 2.250000 3.000000 4.000000 5.000000 6.000000 6.750000 7.500000 8.250000 9.000000 0.000000 1.000000 1.500000 2.250000 3.000000 4.000000 5.000000 6.000000 6.750000 5y0 4.500000 4;500000 4.500000 4.500000 4.500000 4.500000 5.500000 5.500000 5.500000 5.500000 5.500000 5.500000 5.500000 5.500000 5.500000 5.500000 5.500000 5.500000 6.500000 6.500000 6.500000 6.500000 6.500000 6.500000 6.500000 6.500000 6.500000

-6.500000 6.500000 6.500000 7.500000 7.500000 7.500000 7.500000 7.500000 7.500000 7.500000 7.500000 7.500000

• • • • • Pacific Nuclear ****

FRI MAR 07 12:51:24 2003 NEC-3E68DC1C PAGE A006 of A028 NPLATE v. 1.1.0 PROJECT : Monticello Nuclear Generating Plant CLIENT

Nuclear Management Company i MN03-P022637-100 Supports DGEH-2, 3,

5, 6 - Stiffness NODAL COORDINATES

(UNITS:

INCHES) NODE 40 41 42 43 44 45 46 47 48 49 50 5,1 52 53 54 55 56 57 58 59 60 61 i62 63 64 65 66 -X-2.250000 3.000000 4.000000 5.000000 6.000000 6.750000 7.500000 8.250000 9.000000 0.000000 1.000000 1.500000 2.250000 3.000000 4.000000 5.000000 -6.000000 6.75Q000 7.500000 8.250000 9.000000 0.000000 1.000000 1.500000 2.250000 3.000000 4.000000 .y0 2.500000 2.500000 2.500000 2.500000 2.500000 2.500000 2.500000 2.500000 2.500000 3.500000 3.500000 3.500000 3.500000 3.500000 3.500000 3.500000 3.500000 3.500000 3.500000 3.500000 3.500000 4.500000 4.500000 4.'500000 4.500000 4.500000 4.500000 I NODE 1 106 1 107 108 109 110 111 112 113 114 115 I116 117 118 119 120 121 122 I123 124 125 126 127 128 129 130 131 132 ,-X-7,500000 8.25.0000 9.000000 0.000000 1.000000 1.500000 2.250000 3.000000 4.000000 5.000000 6.000000 6.750000 7.500000 8.250000 9.000000 0.000000 1.000000 1.500000 2.250000 3.000000 4.000000 5.000000 6.000000 6.750000 7.500000 8.250000 9.000000 7 Y0 7.500000 7.500000 7.500000 8.250000 8.250000 8.250000 8.250000 8.250000 8.250000 8.250000 8.250000 8.250000 8.250000 8.250000 8.250000 9.000000 9.000000 9.000000 9.000000 9.000000 9.000000 9.000000 9.000000 9.000000 9.000000 9.000000 9.000000 PLATE CONNECTIVITY : PLATE NODE1 NODE2 1 1 13 2 2 14 3 3 15 4 4 16 5 5 17 6 6 18 NODE3 2 3 4 5 6 7 NODE4 I 14 1 15 1 16 1 17 1 18 1 19 1 PLATE 56 57 58 59 60 61 NODE1 61 62 63 64 65 66 NODE2 73 74 75 76 7. 78 NODE3 62 63 64 65 66 67 NODE4 74 75. 76 77 78 79

• t**
  • • • • Pacific Nuclear ****

NEC-3E68DC1C FRI MAR 07 12:51:24 2003 PROJECT : Monticello Nuclear Generating Plant CLIENT

, Nuclear Management Company PAGE A007 of A028 NPLATE v.

1.1.0 MN63-P022637-100 Supports DGEH-2, 3, 5, 6 - Stiffness PLATE CONNECTIVITY PLATE 7 8 9 10 11-12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 '37 38 39 40 41 42 43 44 45 NODEl 7 8 9 10 11 13 14 15 16 17 18 19 20 21 22 23 25 26 27 28 29 30 31 32 33 34 35 37 38 39 40 41 42 43 44 45. 46 47 49 NODE2. 19 20 21 22 23 25 26 27 28 29 30 31 32 33 34 35 37 38 39 40 41 42 43 44 45 46 47 49 50 51 52 53 54 55 56 57 58 59 61 NODE3 8 9 10 11 12 - 14 15 16 17 18 19 20 21 22 23 24 26 27 28 29 30 31 32 33 34 35 36 38 39 40 41 .42 43 44 45 46 47 48 50 NODE4 20 21 22 23 24 26 27 28 29 30 31 32 33 34 35 36 38 39 40 41 42

• 43 44 45 46 47 48 50 51 52 53 54 55 56 57 58 59 60 62 I PLATE I

62 1 63 I 64 1 65 1 66 I 67 1 68 I 69 70 I 71 1 72 1 73 i 74 1 75 1 76 1 77 78 79 I 80 1 81 1 82 1 83 1 84 I 85 1 86 1 87 l 88 1 89 1 90 1 91 I 92 1 93 94 95 I 96 1 97 1 98 1 99 1 100 NODEl 67 68 69 70 71 73 74 75 76 77 78 79 80 81 82 83 85 86 87 88 89 90 91 92 93 94 95 97 98 99 100 101 102 103 104 105 106 107 109 NODE2 79 80 81 82 83 85 86 87 88 89 90 91 92 93 94 95 97 98 99 100 101 102 103 104 105 106 107 109 110 111 112 113 114 115. 116 117 118 119 121 NODE3 68 69 70 71 72 .74 75 76 77 78 79 80 81 82 83 84 86 87 88 89 90 91 92 93 94 9.5 96 98 99 100 101 102 103 104 105 106 107 108 110 NODE4

• 80 81 82 83 84 86 87 88.

89 90 91 92 93 94 95 96 98 99 100 101 102 103 104 105 106 107 108 110 111 112 113 114 115 126 117 118 119 120 122

• • • • • Pacific Nuclear
• NEC-3E68DC1C FRI MAR 07 12:51:24 2003 PAGE A008 of A028 NPLATE v. 1.1.0.

PROJECT : Monticello Nuclear Generating Plant CLIENT

Nuclear Management Company MN03-P022637-100 Supports DGER-2, 3, 5, 6 -

Stiffness PLATE CONNECTIVITY PLATE NODEl NODE2 NODE3 NODE4 I PLATE NODEl NODE2 NODE3 NODE4-46 50 62 51 63 1101 110 122 111 123 47 51 63 52 64 1 102 111 123 112 124 48 52 64 53 65 1 103 112 124 113 125 49 53 65 54 66 1 104 113 125 114 126 50 54 66 55 67 1 105 114 126 115 127 51 55 67 56 68 l 106 115 127 116 128 52 56 68 57 69 1 107 116 128 117 129 53 57 69 58 70 1 108 117 129 118 130 54 58 70 59 71 I 109 118 130 119 131 55 59 71 60 72 110 119 131 120 132 BOLT PROPERTIES BOLT TYPE 1 Bolt Diameter 0.6250 in Cross Section 0.3068 in12 Axial Stiffness 300.0000 k/in Allowable Tension 5.0140 k Allowable Shear 5.1000 k BOLT LOCATIONS BOLT TYPE NODE 1 1 34 2 1 106 3 1 99

4.

1 27 COLUMN SEGMENTS NO. FROM TO 1 86 74 2 74 62 3 62 50 4 50 38

• • • • • .Pacific Nuclear ****

FRI MAR 07 12:51:24 2003 NEC-3E68DC1C PAGE A009 of A028 NPLATE v. 1.1.0 PROJECT : Monticello Nuclear Generating Plant CLIENT : Nuclear Management Company MN03-P022637-100 Supports DGEH-2, 3, 5, 6 - Stiffness COLUMN SEGMENTS NO. 5 6 . 7 8 9 10 11 12 13 FROM 67 66 65 64 63 91 79 67 55 TO 66 65 64 63 62 79 67 55 .43 V,

• • • • • Pacific Nuclear ****

NEC-3E68DClC FRI MAR 07 12:51:24 2003 PAGE A010 of A028 NPLATE v. 1.1.0 MN03-P022637-100 PROJECT : Monticello Nuclear Generating Plant CLIENT : Nuclear Management Company Supports DGEH-2, 3, 5, 6-- Stiffness LOAD CASE 1 POINT LOADS : (UNITS: KIPS AND IN-KIPS) NODE P 65 +0.000 rx Fy +0.000 +0.000 +1.000 My T +0.600 +0.000 EQUILIBRIUM CHECK : (UNITS: KIPS AND IN-KIPS) NODE _P_ _Mx- -MY-65 -1.092E-14 +1.OOOE+00 +1.886E-14 I NODE -Mx- -My-NODAL DISPLACEMENTS : (UNITS: INCHES AND RADIANS) 7---------- NODE 1 2 3 4 5 6 7 8 9 10 'll 12 13 14 is 16 17 18 19 20 21 .22 23 24 25 26 .27 28 _W_ +9.185E-07 +5.018E-06 +6.820E-06 +7.862E-06 +5.967E-06 -3.652E-07 -4.915E-06 -4.113E-06 -1.495E-06 +2.343E-07 +1.849E-07 117E-06 -2.696E-05 118E-05 -1. 659E-05 059E-05 -9.850E-06 -1.800E-05 -2.428E-05 -1.733E-05 -8.405E-06 -2.803E-06 66BE-06 386E-06 -5.244E-05 032E-05 -3.946E-05 -2.317E-05 .- THETAx- -3.643E-05 -3.419E-05 -3.119E-05 -2.587E-05 -2.27sE-05 -2.346E-05 -2.396E-05 -1.734E-05 -1.026E-05 -5.306E-06 -3.250E-'06 -3.293E-06 -3.817E-05 -3.722E-05 -3.158E-05 -2.260E-05 -1. 814E-05 -2.326E-05 -2.924E-05 -1.7-75E-05 7.17SE-06 -1. 679E-06 -1. 112E-06 -2.792E-06 -2.207E-05 -4.049E-05 -2.754E-05 -7.393E-D6 -THETAy- -3.792E-06 -4.205E-06 -2.855E-06 +3.170E-07 +4.609E-06 +6.939E
-06 +1. 955E-06 -3.267E-06 -3.352E-06 -1.11SE-06 +1. 15BE-06 +2.13BE-06 -3.831E-06 -8.044E-06 -9.577E-06 -5.268E-06 +3.550E-06 +1. 037E-05 -1. 174E-07 -1:192E-05 -1. 040E-05 -4.321E-06 +8.966E-07 +3.036E-06 -2.322E-08 -1. 634E-05 -2.486E-05 -1.-592E-05 I NODE 1 67 1 68 1 69 1 70 1 71 1 72 73 74 75 76 17 78 179 80 81 .82 83 84 85 - 86 87 as 89 90 91. 92 93 ' 94 . _W_ +2.298E-04. +2. 08 1E-0 4 +1. 676E-04 +1. 170E-04 +6.323E-05 +9. 943E-D6 +3.533E-04 +3.423E-04 +3.479E-04 +3.511E-04 +3.550E-04 +3.634E-04 +3. 640E-04 +3.213E-04 +2.462E-04 +1. 61BE-04 +8.094E-05 +6.372E-06 +4.670E-04 +4. 682E-04 +4.5i9E-04 +4.316E-04 +4. 414E-04 +4.734E-04 +4. 95SE-0 4 +4. 060E-04 +2.920E-04 +1.779E-04 -THETAX- +1.360E-04 +1.181E-04 +8. 68SE-05 +5.369E-05 +2.551E-05 +2.959E-06 +1. 417E-04 +1. 27SE-04 +1.289E-04 +1. 153E-04 +1.135E-04 +1.288E-04 +1.327E-04 +1. 052E-04 +3.222E-05 +7.880E-06 -1. 009E-G5 +5.081E-05 +1. 250E-04 +3.712E-05 +3.745E-05 +5. 816E-05 +7.781E-05 +1. 312E-04 +4.873E-05 +2.577E-05 -9.806E-07 -THETAy- -3.155E-06 +4.301E-05. +6.259E-05 +7.079E-05 +7;188E-05 +7. OOOE-05 +1. 922E-05 -4.104E-06 -9.'693E-06 -2.813E-06 -8.068E-06 -4.811E-06 -2.444E-06 +8.297E-05 +1.107E-04 +1.118E-04 +1. 033E 04 +9.669E-05 +8. 072E-06 -3.719E
06 +4.452E-05 +5.476E-06 -2.598E-05 -3.383E-05 -2.029E-06 +1.415E-04 +1. 572E-04 +1. 436E-04 I I I I I I I I I I I I I I

t**** Pacific Nuclear FRIMAR*

• • • 15*2** ****

FRI MAR 07 12:51:24 2003 NEC-3E68DClC PAGE A011 of A028 NPLATE v. 1.1.0 PROJECT : Monticello Nuclear Generating Plant CLIENT : Nuclear Management Company MN03-P022637-100 Supports DGEH-2, 3, 5, 6 - Stiffness LOAD CASE 1 NODAL DISPLACEMENTS (UNITS: INCHES AND RADIANS) NODE -W-29 -1.786E-05 30 -3.181E-05 31 -4.826E-05 32 -2.758E-05 33 -9.445E-06 34 -8.847E-07 35 -5.256E-07 36 -4.908E-06 37 -3.329E-05 38 -4.512E-05 39 -2.957E-05 40 -3.696E-06 41 +5.660E-06 42 -8.412E-06 43 -3.44BE-05 44 -2.497E-06 45 +1.543E-05 46 +l.853E-05 47 +1.070E-05 48 -3.250E-06 49 +7.065E-05 50 +8.209E-05 51 +8.179E-05 52 +8.556E-05 53 +8.957E-05 54 +9.047E-05 55 +9.608E-05 56 +9.076E-05 57 +8.093E-05 58 +6.186E-05 59 +3.477E-05 60 +3.559E-06 61 +2.094E-04 62 +2.124E-04 63 +2.147E-04 64 +2.183E-04 65 +2.218E-04 -THETAX- -3.049E-07 -8.271E-06 -3.397E-05 -4.430E-06 +7. l10E-06 +8.219E-06 +4.961E-06 -1.101E-06 +5.091E-05 +1.265E-04 +6.707E-05 +5.447E-05 +5.417E-05 +5.586E-05 +1.298E-04 +5.418E-05 +4.670E-05 +3.175E-05 +1. 81OE-05 +4.602E-06 +1. 312E-04 +1.285E-04 +1.289E-04 +1. 171E-04 +1. 120E-04 +1. 244E-04 +1.318E-04 +1.131E-04 +8.147E-05 +5.250E-05 +2.850E-05 +8.248E-06 +1. 431E-04 +1.326E-04 +1.373E-04 +1.444E-04 +1.515E-04 -THETAy- +2.617E-06 +2.254E-05 -1.729E-06 -2.840E-05 -1.818E-05 -5.279E-06 +3.531E-06 +7.229E-06 +1.150E-05 -4.848E-06 -4.139E-05 -2.486E-05 -4.907E-07 +2.948E-05 -3.117E-06 -3.559E-05 -1.338E-05 +4.131E-06 +1.562E-05 +2.040E-05 -1. 538E-05 -4.703E-06 -4.253E-07 -6.762E-06 -3.108E-06 -2.066E-06 -3.120E-06 +9.406E-06 +1.893E-05 +3.154E-05 +3. 978E-05 +4.251E-05 -2.485E-06 -4.555E-06 -4.699E-06 -4.738E-06 -4.572E-06 I NODE -W-I 95 +7.861E-05 1 96 -8.!02E-06 1 97 +4.821E-04 1 98 +4.419E-04 I.99 +4.192E-04 1 100 +4.344E-04 1 101 +4.724E-04 1 102 +5.247E-04 1 103 +5.318E-04 1 104 +4.304E-04 1 105 +3.040E-04 1 106 +1.717E-04 1 107 +6.921E-05 1 108 -2:252E-05 1 109 +4.398E-04 I 110 +4.047E-04 I 111 +4.000E-04 1 112 +4.251E-04 1 113 +4.740E-04 1 114 +5.308E-04 1 115 +5.272E-04 1 116 +4.304E-04 1 117 +3.110E-04 1 118 +1.840E-04 1 119 +7.355E-05 1 120 -2.426E-05 1 121 +3.958E-04 1 122 +3.754E-04 1 123 +3.808E-04 1 124 +4.153E-04 1 125 +4.711E-04 I 126 +5.341E-04 1 127 +5.307E-04 1 128 +4.364E-04 1 129 +3.215E-04 1 130 +1.969E-04 1 131 +8.228E-05 -THETAx- -1.037E-05 -1.765E-05 -3.879E-05 -6. 694E-05 -4. 908E-05 -1. 382E-05 +1.019E-O5 +2.087E-05 -5. 967E-06 +3.043E-06 +7.079E-06 +4.103E-06 -1. 930E-06 -7.972E-06 -6.093E-05 -3. 992E-05 -1.931E-05 -1.105E-05 -2.954E-06 +2.052E-06 -3.339E-06 +1.815E-06 +1.196E-05 +1.998E-05 +1.102E-05 +2.981E-06 -5.751E-05 -4.201E-05 -3.131E-05 -1. 682E-05 -3.811E-06 +9.587E-06 +1. 407E-05 +1. 492E-05 +1.579E-05 +1.494E-05 +l.046E-05 -THETAy- +1.221E-04 +1.140E-04 +4.207E-05 +5.493E-05 +2.116E-05 -4.362E-05 -5. 611E-05 -4.120E-05 +4.802E-05 +1.486E-04 +1.814E-04 +1.582E-04 +1.246E-04 +1.217E-04 +3.891E-05 +2.272E-05 -7.358E-06 -5.526E-05 -6. 856E-05 -3.567E-05 +4.881E-05 +1. 391E-04 +1.716E-04 +1.606E-04 +1. 359E-04 +1.284E-04 +2.832E-05 +3.567E-06 -2.522E-05 -6.473E-05 -7.749E-05 -3.761E-05 +4.886E-05 +1.344E-04 +1.657E-04 +1. 620E-04 +1. 429E-04

• • c**a********

Pacific Nuclear *** NEC-3E68DClC FRI MAR 07 12:51:24 2003 PROJECT : Monticello Nuclear Generating Plant CLIENT

Nuclear Management Company PAGE A012 of A028 NPLATE v. 1.1.0 MN03-P022637-100 Supports DGEH-2, 3, 5, 6 - Stiffness LOAD CASE 1 NODAL DISPLACEMENTS : (UNITS: INCHES AND RADIANS)

NODE -W- -THETAx- -THETAy-66 +2.262E-04 +1.438E-04 -4.041E-06 PLATE ELEMENT STRESSES : I NODE 1 132 -W- -THETAx- -THETAy- -2.006E-05 +6.563E-06 +1.332E-04 El. 1 2 3 4 5 6 7 .8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 -Mx- +1.9038E-04 -7.0220E-05 -6.1779E-04 -1.0022E-03 -5.0493E-04 +9.4098E-04 +1.0330E-03 -5. 9247E-05 -5.9378E-04 -5.4366E-04 -2.1732E-04 +1.7975E-03 +1.4285E-03 -6.9723E-04 -1.6288E-03 -9.5338E-04 +2.7210E-03 +2.9346E-03 -3.2262E-04 -1.0892E-03 -8.5670E-04 -3.2758E-04 +7.3281E-03 +1.1804E-02 +9.0966E-04 -1.5619E-03 -1.0019E-03 +8.7690E-03 +8.8126E-03 -9.6412E-04 -1.5139E-03 -My- -3.4815E-04 -3.1198E-04 +5.9510E-05 +3.7184E-04 +2.5993E-04 -1.4900E-04 -1.7308E-04 +2.0963E-04 +3.7501E-04 +3.0977E-04 +1.5908E-04 +1.6300E-03 +4.9431E-04 +1.4262E-03 +2.3184E-03 +2.5023E-03 +1.6877E-03 +1.6103E-03 +2.2488E-03 +1.7451E-03 +1.1169E-03 +5.6135E-04 +1.7488E-02 +2.0209E-02 +1.0243E-02 +6.9446E-03 +7.2572E-03 +1.7152E-02 +1.6814E-02 +5.9681E-03 +3.5679E-03 -Mxy- -1. 9867E-04 -7.9373E-04 -8.7416E-04 -4.6841E-04 +2.0184E-04 +1.8001E-04 -7.8509E-04 -1.0805E-03 -6.6537E-04 -2.0443E-04 +8.1849E-05 +8.5482E-05 -1.7267E-03 -1.8036E-03 -7.1660E-04 +6.1821E-04 +9.1358E-04 -1.3983E-03 -1.4257E-03 -4.7429E-04 +1.3709E-04 +4.8790E-04 -3.0412E-03 +5.2278E-03 -4.8851E-04 -5.0496E-04 +4.8315E-04 -3.0359E-03 +2.9467E-03 -4.0916E-04 +8.8613E-04 +S1 -S2 TOP BOT +1.7643E-02 +4.2410E-02

• +5.1909E-02

+4.8927E-02 +2.3677E-02 +7.5928E-03 +2.3893E-02 +4.3248E-02 +3.9783E-02 +2.5178E-02 +9.9987E-03 -6.8012E-02 +3.5303E-02 +7.3746E-02 +7.4877E-02 +4.5254E-02 -4.9272E-02 -3.0944E-02 +4.0819E-02 +4.9768E-02 +3.6957E-02 +2.3173E-02 -2.7679E-01 -3.9675E-O1 -3.7724E-02 +6.7917E-02 +4.3951E-02 -3.3216E-01 -3.3470E-01 +4.2162E-02 +7.0997E-02 +S2 -S1 TOP BOT -1.0912E-02 -2.6103E-02 -2.8089E-02 -2.2030E-02 -1.3223E-02 -4.1384E-02 -6.0584E-02 -4.9665E-02 -3.0448E-02 -1.5199E-02 -7.5138E-03 -7.8224E-02 -1.1734E-01 -1.0485E-01 -1.0430E-01 -1.1134E-01 -1.3883E-01 -1. 6297E-01 -1.2300E-01 -7.7754E-02 -4.8057E-02 -3.3147E-02 -7.8202E-01 -9.6912E-01 -4.3813E-01 -2.9758E-01 -3.1084E-01 -7.7381E-01 -7.5869E-01 -2.5566E-01 -1.5863E-01

• Pacifi * **N*
  • l*ear****

Pacific Nuclear NEC-3E68DC1C FRI MAR 07 12:51:24 2003 PAGE A013 of A028 NP7DTF'P. 1 1 n PROJECT : Monticello Nuclear Generating Plant CLIENT : Nuclear Management Company MN03-P022637-100 Supports DGEH-2, 3, 5, 6 - Stiffness LOAD CASE 1 PLATE ELEMENT STRESSES El. -Mx-32 -1.1249E-03 33 -3.9610E-04 34 +2.1257E-03 35 +5.8580E-03 36 +1.6633E-03 37 -8.5153E-05 38 +4.8313E-04 39 +3.8385E-03 40 +2.6770E-03 41 -9.9425E-04 42 -1.6457E-03 43 -1.1882E-03 44 -4.0617E-04 45 -2.6639E-04 46 -3.1458E-04 47 +1.3455E-03 48 +1.0473E-03 49 +1.1275E-03 50 +5.0666E-04 51 -3.9155E-03 52 -2.4982E-03 53 -1.8046E-03 54 -9.0977E-04 55 -2.5347E-04 56 +1.6420E-03 57 +5.4738E-04 58 -1.4455E-03 59 -9.3566E-04 60 -1.3780E-03 61 -6.1035E-04 62 -9.5548E-03 63 -5.1270E-03 64 -1.7589E-03 65 -1.2953E-04 66 +1.4410E-04 67 +4.9699E-04 68 -7.9259E-03 69 -5.7933E-04 -My- +1.9994E-03 +1.0817E-03 +5.8806E-03 +5.8227E-03 +8.4308E-03 +7.6514E-03 +8.1964E-03 +5.6484E-03 +4.6869E-03 +5.6720E-03 +3.0440E-03 +1. 6285E-03 +7.7339E-04 +9.3986E-04 +7.0745E-04 +2.6794E-03 +4.5729E-03 +4.0922E-03 +1.6532E-03 -5.8597E-04 -8.5494E-05 -1.2264E-04 -3.8812E-04 -6.0375E-04 +8.0448E-05 -6.9549E-04 -2.8245E-03 -4.5600E-03 -3.7886E-03 -1.3436E-03 -3.9018E-03 -3.7006E-03 -3.2316E-03 -2.5303E-03 -1.9118E-03 -5.8012E-03 -8.3873E-03 -1.0983E-02 -Mxy- +1.0892E-03 +1.2658E-03 -2.5981E-03 +4.6905E-03 +1.5956E-03 +4.1636E-04 -8.9820E-04 -2.4283E-03 +3.1724E-03 +2.7175E-03 +2.8991E-03 +2.4705E-03 +2.2183E-03 +4.5848E-04 -1.9268E-04 +1.6800E-04 -1. 6847E-P4 -5.7797E-05 -2.7669E-04 +1.8313E-03 +3.8991E-03 +4.0031E-03 +3.4152E-03 +2.8325E-03 +9.1302E-04 -1.7598E-04 +2.1583E-04 -3.7342E-04 -1.8165E-04 -1.1145E-04 +2.1671E-03 +4.3968E-03 +4.3076E-03 +3.4459E-03 +2.7134E-03 -2.2694E-03 +6.8492E-03 +8.8375E-04 +S1 -S2 TOP BOT +6.2595E-02 +4.7909E-02 -3.4036E-02 -4.9059E-02 -5.5720E-02 +4.5865E-03 -1.6210E-02 -9.1816E-02 -1.5111E-02 +8.3698E-02 +1.2926E-01 +1.1194E-01 +9.0102E-02 +1.7957E-02 +1.4921E-02 -5.6521E-02 -4.4341E-02 -4.8057E-02 -1.8918E-02 +2.0163E-01 +2.2926E-Ol +2.1564E-01 +1.7383E-01 +1.3937E-01 +1.4511E-02 +3.0717E-02 +1.2192E-01 +1.9618E-Ol +1.6223E-01 +5.8035E-02 +4.3904E-01 +3.7837E-01 +2.9292E-01 +2.1243E-01 +1.6151E-01 +2.7877E-01 +6.4041E-01 +4.7180E-01 +S2 -Si TOP BOT -9.9909E-02 -7.7163E-02 -3.0756E-01 -4.4932E-01 -3.7496E-01 -3.274lE-01 -3.5412E-Q1 -3.1296E-01 -2.9908E-01 -2.8328E-01 -1.8892E-01 -1.3073E-01 -1.0577E-01 -4.6692E-02 -3.1683E-02 -1.1521E-01 -1.9545E-01 -1.7465E-01 -7.3237E-02 -9.5641E-03 -1.1902E-O1 -1.3341E-01 -1.1845E-01 -1.0280E-01 -8.8004E-02 -2.4397E-02 +6.0266E-02 +3.8297E-02 +5.8213E-02 +2.5335E-02 +1.3511E-01 -1.7271E-03 -7.9989E-02 -9.8947E-02 -8.6089E-02 -5.2459E-02 +5.5618E-02 +2.1538E-02

• • • • • Pacific Nuclear ****

NEC-3E68DClC FRI MAR 07 12:51:24 2003 PROJECT : Monticello Nuclear Generating Plant CLIENT

Nuclear Management Company PAGE A014 of A028 NPLATE v. 1.1.0 MN03-P022637-100 4------------------------------

Supports DGEH72, 3, 5, 6 - Stiffness LOAD CASE 1 PLATE ELEMENT STRESSES : El. 70 71 72 73 74 75 76 77 78 79 80 81 82 83 84 85 86 87 88 89 90 91 92 - 93 94 95 . 96 97 98 99 I. 100 101 102 103 104 105 106 107 _Mx- +6.3023E-04 -1.9131E-03 !-3.4973E-03 -1.7249E-02 -6.0825E-03 -3.7195E-04 +1.7170E-03 +8.2772E-04 -5.9899E-03 -7.8692E-03 +6.8060E-03 +2.0180E-03 -2.6984E-03 -1.2551E-02 -2.0935E-02 -5.8806E-03 +3il485E-03 +5.4267E-03 +1.4066E-03 +3.6879E-04 +17.0533E-02 +1:.1432E-02 .+2.1169E-03 -4.2424E-03 -1.2616E-02 -1.3327E-02 -5.9961E-03 +3.7767E-03 +6.2521E-03 +1.6326E-03 +2.9040E-03 +7.8494E-03 +7.6623E-03 +2.2483E-03 -4.9090E-03 -1.1271E-02 -1.1456E-02 -5.4844E-03 MY- -8.2972E-03 -7.3513E-03 -4.4005E-03 -8.8722E-03 -7.9777E-03 -4.7835E-03 -2.7634E-03 -1.3960E-03 -1.9738E-02 0085E-02 -6.7180E-03 -5.71BOE-03 -7,4944E-03. -1.61M-02 -1.7930E-02 -5.8661E-03 +7.7557E-05 +2.4899E-03 +1.5763E-03 +5.2529E-04 +7.9856E-03 +6.1947E-03 -2.4684E-04 -3.9884E-03 -5.1602E-03 -3.8792E-03 -1.488BE-03 +2.8960E-03 +4.3248E-03 +2.5208E-03 +9.8433E-04 +1.1574E-03 +7.8809E-04 +1.1127E-04 -9.0527E-04 -1.261SE-03 -8.4394E-04 -2.0607E-04 -Mxy- -9.4609E-04 -1.7009E-03 -2.0733E-03 +3.6622E-03 +4.1357E-03 +3.9159E-03 +2.2784E-03 +1.7469E-03 -1.7679E-03 +7.3389E-03 -i..2436E-03 -3.1101E-03 1.3361E-03 -7.1044E-04 +5.2667E-03 +1.1453E-03 +1.4695E-03 +1.4339E-03 +8.0459E-04 -1.2924E-03 -3.0162E-03 -3.7455E-03 -1.7906E
03 -6.2226E-04 +5'
003E-04 -6:6286E-04 -9.6557E-04 +1.0442E-04 +4.7078E-04 +l.O.j55E-03 .- I.8166E-03 -2.8570E-03 -1.6359E-03 -1.369BE-03 -8.0806E-04 -4.4j52E-05 -2.6844E-04 -6.3675E-04 +Sl -S2 TOP BOT +3.5825E-01 +3.3448E-01 +2.5902E-01 +7.946SE-01 +4.809SE-01 +3.0174E-01 +1.5865E-01 +1.0047E-01 +8.516BE-01 +1.0037E+00 +2.9147E-01 +2.9070E-01 +3.3457E-01 .+6.9410E-01 +1.0628E+00 +2.9946E-01 +2.1860E-02 -8.1318E-02 -2.9115E-02 +3.6168E-02 -2.5537E-bl -1.8104E-01 +5.1645E-02 '+2.0269E-01 +5.4028E-02 +5.7061E-01 +2.6429t-01 -1.2304E-01 -1.798BE-01 -4.0532E-02 +4.7122E-03 -4.4184E-03 -1.7863E-02 +2.'3787E-02 +2.1615E-01 +4.8091E-01 +4.896SE-01 +2.3723E-01 +S2 -Sl TOP BOT -3.1121E-02 +6.079BE-02 +7.7954E-02 +3.1987E-01 +1.1892E-01 -8.1778E-02 -1.1401E-01 -7.6227E-02 +2.4603E-01 +1.8897E-01 -2.9523E-01 -1.3283E-01 +1.0032E-01 +5.2973E-01 +5.954SE-01 +2.0173E-01 -1.5951E-01 -2.5646E-01 -9.8154E-02 -7.4316E-02 -5.3476E-01 -5.7104E-01 -1.3144E-01 +1.4849E-01 +2.1819ErOl +1.6354E-01 +5.5066E-02 -1.6166E-01 -2.7140E-01 -1.3668E-01 -1.7061E-01 -3.7987E-01 -3.4269E-01 -1,2446E-01 +3.1929E-.02 +5.3827E-02 +3.5719E-02 +5.5611E-03

• • • • • Pacific Nuclear NEC-3E68DC1C FRI MAR 07 12:51:24 2003 PAGE A015 of A028 NPLATE v. 1.1 A PROJECT : Monticello Nuclear Generating Plant CLtENT : Nuclear Management Company MN03-P022637-100 Supports DGEH-2, 3, 5, 6 -

Stiffness LOAD CASE 1 PLATE ELEMENT STRESSES E1. '108 109 110 -Mx- +1.3394E-03 +3.9320E-03 +1.6819E-03 -My- +2.9964E-04 +7.0359E-04 +7.6088E-04 -Mxy- -3.4701E-04 +7.1165E-04 +7.6441E-04 +Sl -S2 TOP BOT -8.2973E-03 -2.3624E-02 -1.4036E-02 +S2 -S1 TOP BOT -6.1636E-02 -1.7416E-01 -9.0187E-02 MAX. BENDING STRESS - +1.063 ksi AT EL.

84. STRESS RATIO - +0.03936.

BOLT TENSION AND SHEAR : (UNITS: KIPS/BOLT) BOLT 1 2 3 4 TENSION -0.0003 +0. 0515 +0.1258 -0.011B +0.1258 SHEAR +0. 0000 +0.0000 +0.0000 +0.0000 +0.0000 INTERACTION O.0000 0.0103 Q.0251 O.0000 0.0251 at bolt 3 MSk (+) I1NTERACTION - (T/Tallow)**(1.000) + (V/Vallow)**(1.0001

• • • • • Pacific Nuclear ****

NEC-3E68DClC FRI MAR 07 12:51:24 2003 PAGE A016 of A028 1..TIrF .v 1 1 n PROJECT : Monticello Nuclear Generating Plant CLIENT

Nuclear Management Company MN03-P022637-100 Supports DGEH-2, 3, 5, 6 -

Stiffness LOAD CASE 2 POINT LOADS : (UNITS: KIPS AND IN-KIPS) NODE P 65 +0.000 Fx Fy Mx ,+0.000 +0.000 +0.000 My T +1.000 +0.000 EQUILIBRIUM CHECK : (UNITS: KIPS AND IN-KIPS) NODE -P- -Mx- -My-I NODE 65 -2.243E-13 +3.683E-15 +1.OOOE+00 I NODAL DISPLACEMENTS : (UNITS: INCHES AND RADIANS) -Mx- -My-NODE -W-1 +4.221E-04

• 2 +2.347E-04 3 +1.568E-04 4 +7.009E-05 5 +1.872E-05 6 -1.222E-05 7 -1.882E-05 8 -1.184E-05 9 -1.144E-06 10 +1.318E-05 11 +3.033E-05 12

+4.904E-05 13 +5.537E-04 14 +3.518E-04 15 +2.628E-04 16 +1.612E-04 17 +9.157E-05 18 +2.853E-05 19 -6.836E-06 20 -1.403E-05 21 -5.716E-06 22 +9.072E-06 23 +2.726E-05 24 +4.681E-05 25 +6.840E-04 26 +4.772E-04 27 +3.701E-04 28 +2.532E-04 -THETAx- +1.743E-04 +i.589E-04 +1.468E-04 +1.263E-04 +1.004E-04 +5. 680E-05 +1.911E-05 -2.143E-07 -4.541E-06 -4.734E-06 -3.899E-06 -3.113E-06 +1.778E-04 +1.574E-04 +1.360E-04 +1.195E-04 +9.546E-05 +5.211E-05 +1.101E-05 -7.655E-06 -8.359E-06 -6.326E-06 -4.166E-06 -2.585E-06 +1. 574E-04 +1.837E-04 +1.658E-04 +1.264E-04 -THETAy- +1. 950E-04 +1.708E-04 +1.404E-04 +9.046E-05 +4. 917E-05 +1.676E-05 -1. 470E-06 -1.230E-05 -1. 681E-05 -2.128E-05 -2.425E-05 -2.527E-05 +2.053E-04 +1. 905E-04 +1.623E-04 +1.109E-04 +7.786E-05 +4. 947E-05 +2.190E-05 -4.461E-06 -1. 638E-05 -2.246E-05 -2.555E-05 -2.622E-05 +2.080E-04 +2.222E-04 +1. 933E-04 +1.328E-04 I NODE 1 67 1 68 69 70 71 72 1 73 74 75 76 77 78 79 80 81 82 83 1 84 85 86 87 88 89 90 91 92 93 94 -W- -THETAx- -THETAy- -1.709E-05 -6.397E-05 -3.765E-05 -7.072E-06 +2.047E-05 +4.644E-05 +8.104E-04 +6.303E-04 +5.493E-04 +4.191E-04 +2.906E-04 +1. 337E-04

• -1.598E-05

-6.193E-05 -3.561E-05 -6.040E-06 +2.066E-05 +4.593E-05 +7. 917E-04 +6.239E-04 +5.219E-04 +3.684E-04 +2.447E-04 +1. 114E-04 -1. 376E-05 -5. 041E-05 -2.743E-05 -2.318E-06 -1. 554E-17 -9.314E-18 -3.848E-18 -3.458E-19 +1.797E-18 +3.367E-18 +5.057E-06 -4.901E-06 -4.955E-06 -2.183E-05 -2.576E-05 -1. 155E-05 +1;859E-06 +5.306E-06 +4.480E-06 +2.240E-06 +4.651E-07 -8.564E-07 -7.537E-05 -7.264E-06 -8.838E-05 -8.703E-05 -6. 676E-05 -3.426E-05 +2.397E-06 +2.129E-05 +1.179E-05 +5.221E-06 +1.521E-04 -2.030E-05 -4.214E-05 -3.877E-05 -3.522E-05 -3.439E-05 +1. 883E-04 +1. 645E-04 +1. 663E-04 +1.756E-04 +1. 649E-04 +1.501E-04 +1. 504E-04 -2.162E-05 -4.103E-05 -3.744E-05 -3.426E-05 -3.346E-05 +1.764E-04 +1. 649E-04 +2.189E-04 +1.850E-04 +1. 484E-04 +1.220E-04 +1.496E-04 -2.243E-05 -3.444E-05 -3.268E-05 I I I I I I I I I I I I

Paf**** Nu****

• • • • • Pacific Nuclear NEC-3E68DC1C FRI MAR 07 12:51:24 2003 PROJECT : Monticello Nuclear Generating Plant CLIENT : Nuclear Management Company PAGE A017 of A028 NPLATE v. 1.1.0 MN03-P022637-100 Supports DGEH-2, 3, 5, 6 -

Stiffness LOAD CASE 2 NODAL DISPLACEMENTS : (UNITS: INCHES AND RADIANS) NODE 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 '61 62 63 64 65 -W- +1.626E-04 +6.633E-05 -4.224E-06 -2.504E-05 -1.402E-05 +3.898E-06 +2.432E-05 +4.538E-05 +7.917E-04 +6.239E-04 +5.219E-04 +3.684E-04 +2.447E-04 +1.114E-04 -1.376E-05 -5.041E-05 -2.743E-05 -2.318E-06 +2.170E-05 +4.51lE-05 +8.104E-04 +6.303E-04 +5. 493E-04 +4.191E-04 +2.906E-04 +1.337E-04 -1.598E-05 -6.193E-05 -3.561E-05 -6.04OE-06 +2.066E-05 +4.593E-05 +8.062E-04 +6.329E-04 +5.511E-04 +4.278E-04 +3.020E-04 -THETAx- +9.268E-05 +4.958E-05 -5.301E-06 -2.218E-05 -1. 325E-05 -7.004E-06 -3.482E-06 -1.188E-06 +7.537E-05 +7.264E-06 +8.838E-05 +8.703E-05 +6.676E-05 +3.426E-05 -2.397E-06 -2.129E-05 -1. 179E-05 -5.221E-06 -1.766E-06 +4.537E-07 -5.057E-06 +4.901E-06 +4.955E-06 +2.183E-05 +2.576E-05 +1.155E-05 -1.859E-06 -5.306E-06 -4.480E-06 -2.240E-06 -4.651E-07 +8.564E-07 -3.032E-17 -2.686E-17 -2.549E-17 -2.331E-17 -2.115E-17 -THETAy- +1.090E-04 +8.531E-05 +3.978E-05 -4.002E-06 -2.132E-05 -2.599E-05 -2.796E-05 -2.802E-05 +1.764E-04 +1. 649E-04 +2.189E-04 +1.850E-04 +1. 484E-04 +1.220E-04 +1. 496E-04 -2.243E-05 -3.444E-05 -3.268E-05 -3.152E-05 -3. IOIE-05 +1.883E-04 +1.645E-04 +1.663E-04 +1.756E-04 +1. 649E-04 +1.501E-04 +1.504E-04 -2.162E-05 -4.103E-05 -3.744E-05 -3.426E-05 -3.346E-05 +1.776E-04 +1.639E-04 +1.638E-04 +1. 657E-04 +1.701E-04 NODE -W-95 +2.170E-05 96 +4.511E-05 97 +6.840E-04 98 +4.772E-04 99 +3.701E-04 100 +2.532E-04 101 +1.626E-04 102 +6.633E-05 103 -4.224E-06 104 -2.504E-05 105 -1.402E-05 106 +3.898E-06 107 +2.432E-05 108 +4.538E-05 109 +5.537E-04 110 +3.518E-04 111 +2.628E-04 112 +1.612E-04 113 +9.157E-05 114 +2.853E-05 115 -6.836E-06 116 -l.403E-05 117 -5.716E-06 118 +9.072E-06 119 +2.726E-05 120 +4.681E-05 121 +4.221E-04 122 +2.347E-04 123 +1.568E-04 124 +7.009E-05 125 +1.872E-05 126 -1.222E-05 127 -1.882E-05 128 -1.184E-05 129 -1.144E-06 130 +1.318E-05 131 +3.033E-05 -THETAx- +1.766E-06 -4.537E-07 -1.574E-04 -1.837E-04 -1. 658E-04 -1. 264E-04 -9.268E-05 -4. 958E-05 +5.301E-06 +2.218E-05 +1.325E-05 +7.004E-06 +3.482E-06 +1. 188E-06 -1.778E-04 -1.574E-04 -1. 360E-04 -1. 195E-04 -9.546E-05 -5.211E-05 -1. 101E-05 +7.655E-06 +8.359E-06 +6. 326E-06 +4.166E-06 +2.585E-06 -1.743E-04 -1. 589E-04 -1.468E-04 -1.263E-04 -1. 004E-04 -5. 680E-05 -1. 911E-05 +2.143E-07 +4.541E-06 +4.734E-06 +3.899E-06 -THETAy- -3.152E-05 -3.101E-05 +2.080E-04 +2.222E-04 +1. 933E-04 +1.328E-04 +1.090E-04 +8.531E-05 +3.978E-05 -4.002E-06 -2.132E-05 -2.599E-05 -2.796E-05 -2.802E-05 +2.053E-04 +1.905E-04 +1. 623E-04 +1.109E-04 +7.786E-05 +4.947E-05 +2.190E-05 -4.461E-06 -1. 638E-05 -2.246E-05 -2.555E-05 -2.622E-05 +1. 950E-04 +1.708E-04 +1. 404E-04 +9.046E-05 +4. 917E-05 +1. 676E-05 -1.470E-06 -1.2303-05 -1.681E-05 -2.128E-05 -2.425E-05

Pacific Nuclear *** NEC-3E68DC1C FRI MAR 07 12:51:24 2003 PAGE A018 of A028 NPLATE v. 1.1.0 PROJECT : Monticello Nuclear Generating Plant CLIENT

Nuclear Management Company MN03-P022637-100 Supports DGEH-2, 3,

5, 6 - Stiffness LOAD CASE 2 NODAL DISPLACEMENTS

(UNITS:

INCHES AND RADIANS) NODE -W - -THETAx- -THETAy-66

• 1.380E-04 -1.835E-17 +1.589E-04 PLATE ELEMENT STRESSES :

I NODE -W- -THETAx- -THETAy-I 132 +4.904E-05 +3.113E-06 -2.527E-05 El. 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 -18 19 20 21 22 23 24 25 26 27 28 29 30 31 -Mx- +2.7882E-03 +7.8590E-03 +8.9738E-03 +6.6076E-03 +3.9868E-03 +2.8491E-03 +2.1690E-03 +1.2181E-03 +8.3401E-04 +5.1325E-04 +1.6533E-04 +2.0417E-04 +9.5749E-03 +1.1482E-02 +5.4182E-03 +3.4975E-03 +4.5901E-03 +4.0480E-03 +2.1856E-03 +8.4838E-04 +4.7171E-04 +1.2646E-04 -5.6175E-03 -8.8464E-03 +6.3627E-03 +4.2662E-03 +2.6383E-03 +9.9602E-04 +1.5190E-02 +2.7873E-03 +3.4045E-04 -My- +1.0017E-03 +1.3176E-03 +1.1978E-03 +9.8022E-04 +3.75i6E-04 -2.3122E-04 -6.6931E-04 -5.9120E-04 -2.0943E-04 -3.9105E-06 +7.1792E-05 +5.6688E-04 +7.6405E-03 +6.5620E-03 +1.9772E-03 +5.9812E-04 -2.2416E-04 -1.4057E-03 -9.9432E-04 -2.1869E-04 +1.4200E-04 +2.1470E-04 -1.8155E-02 -1.8833E-02 -5.5372E-03 -2.8829E-03 -1.8362E-03 -4.9202E-04 +4.7992E-03 +9.8659E-04 +3.0890E-04 -Mxy- +1.8258E-03 +3.0848E-03 +2.5924E-03 +3.2983E-03 +4.0795E-03 +3.7669E-03 +2.0490E-03 +4.5468E-04 -8.7833E-05 -1.7827E-04 -1.5521E-04 +1.3038E-03 +3.2353E-03 +4.4376E-03 +3.5796E-03 +4.2722E-03 +3.6156E-03 +1.1606E-03 -3.6055E-04 -5.4896E-04 -3.7008E-04 -2.6511E-04 +1.5093E-03 -6.7599E-03 +1.6951E-03 +3.7067E-03 +3.7967E-03 +6.3157E-03 +4.6793E-03 -1.1875E-03 -8.6793E-04 +S1 -S2 TOP BOT +5.8726E-03 -3.9387E-03 -1.7614E-02 +2.3103E-02 +9.7275E-02 +1.1779E-01 +7.4352E-02 +2.9825E-02 +9.2490E-03 +2.5348E-03 +1.8578E-03 +3'.9716E-02 -2.2319E-01 -1.6846E-01 +1.1686E-02 +1.0511E-01 +9.2186E-02 +7.0077E-02 +4.4147E-02 +1.9229E-02 +4.1935E-03 +4.1888E-03 +7.8226E-01 +9.4908E-01 +2.4636E-01 +1.9020E-01 +1.7091E-01 +2.6058E-01 -1.2811E-01 -1.6926E-02 +2.318SE-02 +S2 -S1 TOP BOT -1.6758E-01 -3.8759E-01 -4.1638E-01 -3.4685E-01 -2.8341E-01 -2.2948E-01 -1.3834E-01 -5.6573E-02 -3.5897E-02 -2.4266E-02 -1.1975E-02 -7.2614E-02 -5.1134E-01 -6.0143E-01 -3.2722E-01 -2.7986E-01 -2.7847E-01 -1.8282E-01 -9.4973E-02 -4.6096E-02 -3.0378E-02 -1.8745E-02 +2.3204E-01 +2.3192E-01 -2.8158E-01 -2.4922E-01 -2.0514E-01 -2.8209E-01 -7.2476E-01 -1.4409E-01 -5.0891E-02

• • • • • Pacific Nuclear NEC-3E68DClC FRI MAR 07 12:51:24 2003 PROJECT :

CLIENT Monticello Nuclear.Generating Plant Nuclear Management Company PAGE A019 of A028 NPLATE v. 1.1.0 MN03-P022637-100 r------------------- Supports DGEH-2, 3, 5, 6 - Stiffness LOAD CASE 2 PLATE ELEMENT STRESSES : El: ' 32 33 34 35 36 37 38
q 40 41 .42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 '60 61 62 63 64 65 66 67 68 69 _Mx- +1.4816E-04' +2.8726E-05 +7.4037E-04 -9.63OOE-03 -8.1901E-04 +2.189BE-03 +1.5438E-03 -2.4222E-03 +2.4439E-02 +3.4221E-03 -2.8281E-04 -3.1574E-04 -8.6761E-05 -k2.6328E-03 -4.5202E-04 -1.6062E-03 -4.0985E-04 +1.0381E-03 +2.5165E-04 +2.4267E-02 +4.0569E-03 -5.0836E-04 -5.7113E-04 -1.6081E-04 +2.632BE-03 -4.5202E-04 1.6062E-03 -4.0985E-04 +1.0381E-03 +2.5165E-04 +2.4267E-02 +4.0569E-03 -5.0836E-04. -5.7113E-04 -1.6081E-04 +7.4037E-04 -9.63DOE-03 -8.1901E-04 -My- +2.6737E-04 +2.2256E-04 -5.0532E-03 -8.3552E-03 -0.7158E-03 -6.1104E-03 -3.5971E-03 -2.139BE-03 +8.3843E-03 +2.5106E-03 +5.7081E-04 +1.7814E-04 +8.2532E-05 +7.9981E-04 -7.6363E-04 -2.1885E-03 -3.1551E-03 -2.0558E-03 -5.4198E-04 +7.7366E-03 +1.8407E-03 +2.7572E-04 +1.0366E-06 -7.3177E-05 +7.9981E-04 -7.6363E-04 -2.1885E-03 -3.15SlE-03 -2.0658E-03 -5.4198E-04 +7-.7366E-03 +1.8407E-03 +2.7572E-04 +1.0366E-06 -7.3177E-05 -5.0532E-03 -8.3552E-03 -9.715SE-03 I -Mxy- -4.8932E-04 -3.0735E +2.2069E-03 -6.4247E-03 -1.001BE-01 +7.6951E-04 +2.1691E-03 +1.4692E-03 +2.6579E-04 -5.2097E-04 -5.4978E-04 -3.5897E-04 -2.4244t-04 -3A512E-04 -3.3022E-04 -8.1926E-04 -1.1187E-04 +6.8294E-04 +6.42SIE-04 +2.2099E-04 -4.2081E-05 -1.345SE-04 -1.2,732E-04 -8.9457E-05 +3.6512E-04 +3.3022E-04 +8.1926E-04 +1.1187E-04 -6.8294E-04 -6.4251E-04. -2.2099E-04 +4.20SIE-05 +1.3455E-04 +1.1732E-04 +8.9457E-05 -2.2069E-03 +6.4247E-03 +1.0018E-03 +SI -S2 TOP BOT +1.2167E-02 +8.3894E-03 +2.4739E-01 +6.591SE-01 +4.1930E-01 +2.6373E-01 +1.8731E-01 +1.6030E-01 -3.5754E-01 -9.7032E-02 +2.3552E-02 +2.1526E-02 +1.1047E-02 -3.1136E-02 +4.1513E-02 +1.1805E-01 +1.3481E-01 +9.4267E-02 +3.8414E-02 -3.2997E-01 -7.8501E-02 +2.264BE-02 +2.5355E-02 +9.2417E-03 -3.1136E-02 +4.1513E-02 +1.1805E-01 +1.3481E-01 +9.4267E-02 +3.8414E ;--3.2997E-01 -7.8501E-02 +2.2648E-02 +2.535SE-02 +9.2417E-03 +2.4739E 01 +6.5915E-01 +4.1930E-01 +S2 -SI TOP BOT -2.9896E-02 -1.0111E-02 -6.3371E-02 +1.0822E-01 +3.0191Z-02 -9.6450E-02 -9.97OOE-02 +3.434SE-02 -1.0429E+00 -1.5610E-01 -3.5840E-02 -1.5654E-02. -1.0866E-02 -1.1532E-01 +1.0355E-02 +4.3856E-02 +1.7293E-02 -5.0422E-02 -2.6027E-02 -1.0355E+00 -1.7313E-01 -1.2722E-02 -1.0307E-03 +7.4162E-04 -1.1532E-01 +1.0355E-02 +4.3856E-02 +1.7293E-02 -5.0422E-02 -2.6027E-02 -1.0355E+00
-1.7313E-01 -1.2722E-02 -1.0307E-03 +7.4i62E-04 -6.3371E-02 +1.0822E-01 +3'.0191E-02

Pacific Nuclear NEC-3E68DC1C FRI MAR 07 12:51:24 2003 PAGE A020 of A028 NPLA.TE v. I_1.0 PROJECT : Monticello Nuclear Generating Plant CLIENT : Nuclear Management Company MN03-P022637-100 Supports DGEH-2, 3, 5, 6 - Stiffness LOAD CASE 2 -PLATE ELEMENT STRESSES : El. -Mx-70 +2.1898E-03 71 +1.5438E-03 72 -2.4222E-03 73 +2.4439E-02 74 43.4221E-03 75 -2.8281E-04 76 -3.1574E-04 77 -8.6761E-05 78 -5.6175E-03 79 -8.8464E-03 80 +6.3627E-03 81 +4.2662E-03 82 +2.6383E-03 83 +9.9602E-04 84 +1.5190E-02 85 +2.7873E-03 86 +3.4045E-04 87 +1.4816E-04 88 +2.8726E-05 89 +2.0417E-04 90 +9.5749E-03 91 +1.1482E-02 92 +5.4182E-03 93 +3.4975E-03 94 +4.5901E-03 95 +4.0480E-03 96 +2.1856E-03 97 +8.4838E-04 98 +4.7171E-04 99 +1.2646E-04 100 +2.7882E-03 101 +7.8590E-03 102 +8.9738E-03 103 +6.6076E-03 104 +3.9868E-03 105 +2.8491E-03 106 +2.1690E-03 107 +1.2181E-03 -My- -6.1104E-03 --3.5971E-03 -2.1398E-03 +8.3843E-03 +2.5106E-03 +5.7081E-04 +1.7814E-04 +8.2532E-05 -1.8155E-02 -1.8833E-02 -5.5372E-03 -2.8829E-03 -1.8362E-03 -4.9202E-04 +4.7992E-03 +9.8659E-04 +3.0890E-04 +2.6737E-04 +2.2256E-04 +5.6688E-04 +7.6405E-03 +6.5620E-03 +1.9772E-03 +5.9812E-04 -2.2416E-04 -1.4057E-03 -9.94.32E-04 -2.1869E-04 +1.4200E-04 +2.1470E-04 +1.0017E-03 +1.3176E-03 +1.1978E-03 +9.8022E-04 +3.7576E-04 -2.3122E-04 -6.6931E-04 1-5.9120E-04 -Mxy- -7.6951E-04 -2.1691E-03 -1.4692E-03 -2.6579E-04 +5.2097E-04 +5.4978E-04 +3.5897E-04 +2.4244E-04 -1.5093E-03 +6.7599E-03 -1.6951E-03 -3.7067E-03 -3.7967E-03 -6.3157E-03 -4.6793E-03 +1.1875E-03 +8.6793E-04 +4.8932E-04 +3.0735E-04 -1.3038E-03 -3.2353E-03 -4.4376E-03 -3.5796E-03 -4.2722E-03 -3.6156E-03 -1.1606E-03 +3.6055E-04 +5; 4896E-04 +3.7008E-04 +2.6511E-04 -1.8258E-03 '-3.0848E-03 .-2.5924E-03 -3.2983E-03 -4.0795E-03 -3.7669E-03 -2.0490E-03 -4.5468E-04 +S1 -S2 TOP BOT +2.6373E-01 +1.8731E-01 +1.6030E-01 -3.5754E-01 -9.7032E-02 +2.3552E-02 +2.1526E-02 +1.1047E-02 +7.8226E-01 +9.4908E-01 +2.4636E-Q1 +1.9020E-01 +1.7091E-01 +2.6058E-01 -1.2811E-01 -1.6926E-02 +2.3185E-02 +1.2167E-02 +8.3894E-03 +3.9716E-02 -2.2319E-01 -1.6846E-01 +1.1686E-02 +1.0511E-01 +9.2186E-02 +7.0077E-02 +4.4147E-02 +1.9229E-02 +4.1935E-03 +4.1888E-03 +5.8726E-03 -3.9387E-03 -1.7614E-02 +2.3103E-02 +9.7275E-02 +1.1779E-01 +7.4352E-02 +2.9825E-02 +S2 -SI TOP BOT -9.6450E-02 -9.9700E-02 +3.4348E-02 -1.0429E+00 -1.5610E-01 -3.5840E-02 -1.5654E-02 -1.0866E-02 +2.3204E-01 +2.3192E-01 -2.8158E-01 -2.4922E-01 -2.0514E-01 -2.8209E-01' -7.2476E-01 -1.4409E-01 -5.0891E-02 -2.9896E-02 -1.9111E-02 -7.2614E-02 -5.1134E-01 -6.0143E-01 -3.2722E-01 -2.7986E-01 -2.7847E-01 -1.8282E-01 -9.4973E-02 -4.6096E-02 -3.0378E-02 -1.8745E-02 -1.6758E-01 -3.8759E-01 -4.1638E-01 -3.4685E-01 -2.8341E-01 -2.2948E-01 -1.3834E-01 -5.6573E-02

• • • k*

Pacific Nuclear **** NEC-3E68DC1C FRI MAR 07 12:51:24 2003 PROJECT : Monticello Nuclear Generating Plant CLIENT

Nuclear Management Company PAGE A021 of A028 NPLATE v. 1.1.0 MN03-P022637-100 Supports DGEH-2, 3, 5, 6 - Stiffness LOAD CASE 2 PLATE ELEMENT STRESSES :

El. 108 109 110 -Mx- +8.3401E-04 +5.1325E-04 +1.6533E-04 .-My- -2.0943E-04 -3.9105E-06 +7.1792E-05 -Mxy- +8.7833E-05 +1.1827E-04 +1.5521E-04 +Sl -S2 TOP BOT +Y.2490E-03 +2.5348E-03 +1.8578E-03 +S2 -Sl TOP BOT -3.5897E-02 -2.4266E-02 -1.1975E-02 MAX. BENDING STRESS - +1.043 ksi AT EL.

73. STRESS RATIO - +0.03863.

BOLT TENSION AND SHEAR : (UNITS: KIPS/BOLT) BOLT TENSION SHEAR INTERACTION 1 +0.0012 +0.0000 0.0002 2 +0.0012 +0.0000 0.0002 3 +0.1110 +0.0000 0.0221 4 +0.1110 +0.0000 0.0221 MAX (+) +-0.1110 +0.0000 0.0221 at bolt 4 INTERACTION - (T/Tallow)**(1.000) +. (V/Vallow)*"{1.000)

• • • • • Pacific Nuclear ****

NEC-3E68DClC FMI MAR 07 12:51:24 2003 PAGE A022 of A028 NPLATE v 1 1 A PROJECT : Monticello Nuclear Generating Plant CLIENT : Nuclear Management Company MN03-P022637-100 Supports DGEH-2, 3, 5, 6 - Stiffness LOAD CASE 3 POINT LOADS

(UNITS: KIPS AND IN-KIPS)

NODE P 65 +0.000 Fx +0.000 Fy Mx MNy +0.000 +0.000 -1.000 +0. 000 EQUILIBRIUM CHECK : (UNITS: KIPS AND IN-KIPS) NODE -P- -Mx- -My-65 -2.900E-13 +3.489E-16 -1.OOOE+00 I NODE -P- -Mx- -My-NODAL DISPLACEMENTS

(UNITS: INCHES AND RADIANS)

NODE -W- -THETAx-1 -1.960E-05 -3.041E-05 2 +6.306E-05 -2.680E-05 3 +1.146E-04 -2.183E-05 4 +2.067E-04 -1.059E-05 5 +3.063E-04 +2.470E-06 6 +4.146E-04 +2.463E-05 7 +4.455E-04 +5.137E-05 8 +3.691E-04 +7.171E-05 9 +2.559E-04 +7.680E-05 10 +1.282E-04 +7.568E-05 11 +1.136E-05 +7.371E-05 12 -9.053E-05 +6.709E-05 13 -4.404E-05 -3.607E-05 14 +4.008E-05 -3.483E-05 15 +9.535E-05 -2.985E-05 16 +1.977E-04 -1.286E-05 17 +3.095E-04 +5.431E-06 18 +4.386E-04 +3.707E-05 19 +4.937E-04 +7.722E-05 20 +4.314E-04 +9.619E-05 21 +3.172E-04 +8.929E-05 22 +1.843E-04 +7.448E-05 23 +6.645E-05 +7.679E-05 24 -3.874E-05 +7.343E-05 25 -7.400E-05 -4.301E-05 26 +1.218E-05 -3.822E-05 27 +7.299E-05 -2.345E-05 28 +1.893E-04 -7.791E-06 -THETAy- -7.569E-05 -9.448E-05 -1.116E-04 -1.316E-04 -1.290E-04 -7.779E-05 +2.168E-05 +1.264E-04 +1. 681E-04 +1. 666E-04 +1.439E-04. +1.321E-04 -7.605E-05 -9.983E-05 -1.223E-04 -1.470E-04 -1. 465E-04 -1.023E-04 -5.556E-07 +1.203E-04 +1.746E-04 +1.708E-04 +1. 453E-04 +1.390E-04 -7.500E-05 -1.024E-04 -1.387E-04 -1.644E-04 I NODE -W-1 67 +6.382E-04 1 68 +6.942E-04 1 69 +6.307E-04 1 70 +5.188E-04 1 71 +3.917E-04 I 72 +2.689E-04 1 73 -1.241E-04 1 74 -1.808E-05 1 75 +6.245E-05 1 76 +1.864E-04 1 77 +3.139E-04 I 78 +4.806E-04 1 79 +6.365E-04 1 80 +6.797E-04 1 81 +6.019E-04 1 82 +4.825E-04 1 83 +3.531E-04 84 +2.299E-04 1 85 -1.115E-04 1 86 -1.594E-05 1 87 +6.296E-05 1 88 +1.865E-04 1 89 +3.154E-04 1 90 +4.817E-04 1 91 +6.326E-04 i 92 +6.238E-04 1 93 +5.142E-04 1 94 +3.801E-04 -THETAx- -THETAy- +3.649E-18 -1.564E-04 +2.479E-18 +3.441E-05 +2.108E-18 +1.257E-04 +1.548E-18 +1.651E-04 +8.955E-19 +1.695E-04 +2.088E-19 +1.561E-04 +4.108E-06 -7.878E-05 +1.749E-06 -1.599E-04 +6.797E-07 -1.624E-04 +1.225E-06 -1.682E-04 +2.884E-06 -1.700E-04 +3.708E-06 -1.603E-04 -3.068E-06 -1.548E-04 -3.129E-05 +5.552E-05 -5.822E-05 +1.404E-04 -7.199E-05 +1.710E-04 -7.510E-05 +1.703E-04 -7.460E-05 +1.576E-04 +2.849E-05 -6.933E-05 +2.352E-06 -1.594E-04 +2.254E-06.-l.592E-04 -2.169E-07 -1.699E-04 +6.952E-07 -1.719E-04 -9.069E-06 -1.587E-04 -4.431E-06 -1.538E-04 -9.219E-05 +1.113E-04 -1.128E-04 +1.716E-04 -1.292E-04 +1.793E-04

Pacific Nuclear *** NEC-3E68DC1C FRI MAR 07 12:51:24 2003 PAGE A023 of A028 NPLATE v. 1.1.0 PROJECT : Monticello Nuclear Generating Plant CLIENT

Nuclear Management Company MN03-P022637-100 Supports DGEH-2, 3,

5, 6 - Stiffness LOAD CASE 3 NODAL DISPLACEMENTS (UNITS: INCHES AND RADIANS) NODE -W- -THETAx- -THETAy-29 +3.133E-04 +3.948E-06 -1.639E-04 30 +4.658E-04 +3.038E-05 -1.352E-04 31 +5.593E-04 +9.659E-05 -2.211E-05 32 +5.130E-04 +1.184E-04 +1.199E-04 33 +3.933E-04 +1.148E-04 +1.896E-04 34 +2,484E-04 +1.096E-04 +1.772E-04 35 +1.327E-04 +1.037E-04 +1.441E-04 36 +2.381E-05 +9.583E-05 +1.473E-04 37 -1.115E-04 -2.849E-05 -6.933E-05 38 -1.594E-05 -2.352E-06 -l.594E-04 39 +6.296E-05 -2.254E-06 -1.592E-04 40 +1.865E-04 +2.169E-07 -1.699E-04 41 +3.154E-04 -6.952E-07 -1.719E-04 42 +4.817E-04 +9.069E-06 -1.587E-04 43 +6.326E-04 +4.431E-06 -1.538E-04 44 +6.238E-04 +9.219E-05 +1.113E-04 45 +5.142E-04 +1.128E-04 +1.716E-04 46 +3.801E-04 +1.292E-04 +1.793E-04 47 +2.510E-04 +1.209E-04 +1.644E-04 48 +1.315E-04 +1.124E-04 +1.566E-04 49 -1.241E-04 -4.108E-06 -7.878E-05 50 -1.808E-05 -1.749E-06 -1.599E-04 51 +6.245E-05 -6.797E-07 -1.624E-04 52 +1.864E-04 -1.225E-06 -1.682E-04 53 +3.139E-04 -2.884E-06 -1.700E-04 54 +4.806E-04 -3.708E-06 -1.603E-04 55 +6.365E-04 +3.068E-06 -1.548E-04 56 +6.797E-04 +3.129E-05 +5.552E-05 57 +6.019E-04 +5.822E-05 +1.404E-04 58 +4.825E-04 +7.199E-05 +1.710E-04 59 +3.531E-04 +7.510E-05 +1.703E-04 60 +2.299E-04 +7.460E-05 +1.576E-04 61 -1.255E-04 +2.426E-18 -7.975E-05 62 -1.910E-05 +3.416E-18 -1.607E-04 63 +6.161E-05 +3.469E-18 -1.624E-04 64 +1.848E-04 +3.514E-18 -1.665E-04 65 +3.118E-04 +3.564E-18 -1.726E-04 I NODE I 95 1 96 1 97 I 98 1 99 1 100 1 101 i 102 1 103 1 104 105 1 106 1 107 1 108 1 109 I 110 I 1l1 1 112 113 1 114 1 115 1 116 117 1 118 1 119 1 120 121 1 122 1 123 124 1 125 1 126 127 1 128 1 129 1 130 131 -W- -THETAx- +2.510E-04 -1.209E-04 +1.315E-04 -1.124E-04 -7.400E-05 +4.301E-05 +1.218E-05 +3.822E-05 +7.299E-05 +2.345E-05 +1.893E-04 +7.791E-06 +3.133E-04 -3.948E-06 +4.658E-04 -3.03BE-05 +5.595E-04 -9.659E-05 +5.130E-04 -1.184E-04 +3.933E-04 -1.148E-04 +2.484E-04 -1.096E-04 +1.327E-04 -1.037E-04 +2.381E-05 -9.583E-05 -4.404E-05 +3.607E-05 +4.008E-05 +3.483E-05 +9.535E-05 +2.985E-05 +1.977E-04 +1.286E-05 +3.095E-04 -5.431E-06 +4.386E-04 -3.707E-05 +4.937E-04 -7.722E-05 +4.314E-04 -9.619E-05 +3.172E-04 -8.929E-05 +1.843E-04 -7.448E-05 +6.645E-05 -7.679E-05 -3.874E-05 -7.343E-05 -1.960;-05 +.3.041E-05 +6.306E-05 +2.680E-05 +1.146E-04 +2.183E-05 +2.067E-04 +1.059E-05 +3.063E-04 -2.470E-06 +4.146E-04 -2.463E-05 +4.455E-04 -5.137E-05 +3.691E-04 -7.171E-05 +2.559E-04 -7.680E-05 +1.282E-04 -7.568E-05 +1.136E-05 -7.371E-05 -THETAy- +1.644E-04 +1.566E-04 -7.50OE-05 -1.024E-04 -1.387E-04 -1. 644E-04 -1. 639E-04 -1.352E-04 -2.211E-05 +1. 199E-04 +1. 896E-04 +1.772E-04 +1.441E-04 +1.473E-04 -7. 605E-05 -9. 983E-05 -1.223E-04 -1. 470E-04 -1.465E-04 -1. 023E-04 -5.556E-07 +1.203E-04 +1. 746E-04 +1.708E-04 +1. 453E-04 +1.390E-04 -7.569E-05 -9.44BE-05 -1.116E-04 -1. 316E-04 -1.290E-04 -7.779E-05 +2.168E-05 +1.264E-04 +1. 681E-04 +1.666E-04 +1.439E-04

• • • • • Pacific Nuclear ****

NEC-3E68DC1C FRI MAR 07 12:51:24 2003 PAGE A024 of A028 NPLATE v. 1.1.0 PROJECT : Monticello Nuclear Generating Plant CLIENT

Nuclear Management Company MN03-P022637-100 Supports DGEH-2, 3,

5, 6 - Stiffness LOAD CASE 3 NODAL DISPLACEMENTS (UNITS: INCHES AND RADIANS) NODE -W- -THETAx- -THETAy-66 +4.790E-04 +3.614E-18 -1.627E-04 I NODE -W-I 132 -9.053E-05 -THETAx- -THETAy- -6.709E-05 +1.321E-04 PLATE ELEMENT STRESSES : El. 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23. 24 25 26 27 28 29 30 31 -Mx- +2.5976E-03 +5.0944E-03 +3.8854E-03 -2.6826E-04 -6.2510E-03 -1.3017E-02 -1.4388E-02 -7.9172E-03 +8.0821E-04 +4.5428E-03 +1.9600E-03 +3.2940E-03 +8.3101E-03 +5.0254E-03 +1.6328E-05 -5.3363E-03 -1.4689E-02 -1.7243E-02 -1.0233E-02 +3.2022E-03 +7.2089E-03 +1.6772E-03 +9.2853E-03 +6.2521E-03 +4.0089E-03 +2.1272E-04 -3.4766E-03 -1.0646E-02 -3.0994E-02 -1.2724E-02 +7.9693E-04 -My- -3.8430E-04 +1.6421E-04 +2.9107E-04 -2.2145E-05 -5.6677E-04 -6.5168E-04 -4.0497E-05 +7.6503E-04 +1.2013E-03 +1.5225E-03 +1.3880E-03 +1.1060E-04 +2.7489E-03 +2.4820E-03 +3.0985E-04 -2.2954E-03 -3.3295E-03 -1.6404E-03 +9.8521E-04 +6.1112E-03 +7.4349E-03 +4.6960E-03 +5.9963E-03 +5.5116E-03 +3.0635E-03 +2.7824E-04 -2:6967E-03 -1.0424E-02 -1.6841E-02 -5.6179E-03 +1.3558E-03 -Mxy- -4.2082E-04 -1.0441E-03 -1.7551E-03 -2.0704E-03 -2.6847E-03 -3.1647E-03 -1.9394E-03 -2.3980E-05 +8.2654E-04 +1.7393E-04 +6.2225E-04 -1. 2467E-.04 -1.7310E-03 -1. 9177E-03 -2.1124E-03 -3.0592E-03 -3.7227E-03 -1.3700E-03 +6.7758E-04 +6.1344E-04 +9.4992E-04 +5.5219E-04 -3.1115E-03 -1.7125E-03 -1.5146E-03 -7.2006E-04 -1.9729E-03 -5.0262E-03 -8.5502E-03 -1.0939E-03 -9.1143E-05 +S1 -S2 TOP BOT +1.8882E-02 +2.038BE-03 +1.8082E-02 +9.4689E-02 +3.1226E-01 +5.8795E-01 -+6.2488E-01 +3.378OE-01 --6.6197E-03 -6.4532E-02 -4.2202E-02 -4.5110E-03 -9.6175E-02 -6.1982E-02 +8.3389E-02 +3.0857E-01 +6.7413E-01 +7.4078E-01 +4.3834E-01 -1.3133E-01 -2.7159E-01 -6.7386E-02 -1.7585E-01 -1.7620E-01 -8.3182E-02 +2.0281E-02 +2.1750E-01 +6.6399E-01 +1.4940E+00 +5.4993E-01 -3.3384E-02 +S2 -Sl TOP BOT -1.1332E-01 -2.2641E-01 -1.9628E-01 -8.2298E-02 -2.1365E-02 -4.7445E-03 -9.2606E-03 -3.2644E-02 -7.9118E-02 -1.9425E-01 -1.0064E-01 -1.4075E-01 -3.7567E-01 -2.5834E-01 -9.7306E-02 +1.7052E-02 +9.4641E-02 +6.4895E-02 -4.3775E-02 -2.6604E -3.5322E-01 -2.0454E-01 -4.7617E-01 -3.2571E-01 -2.1858E-01 -4.1228E-02 +4.5891E-02 +2.3499E-0l +5.4692E-01 +2.3268E-0l -5.8466E-02

• • • • • • • • • • • • • • • • • • Pi Pacific Nuclear
    • t****

NEC-3E68DClC FRI MAR 07'12:51:24 2003 PROJECT : Monticello Nuclear Generating Plant CLIENT

Nuclear Management Company PAGE A025 of A028 NPLATE v. 1.1.0 MN03-P022637-100 Supports DGEH-2, 3, 5, 6 -

Stiffness LOAD CASE 3 PLATE ELEMENT STRESSES : El. 32 33 34 35 36 37 38 .39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 65 66 67 68 69 -Mx- +5.2578E-03 +1.1342E-03 +1.2512E-02 +3.6342E-04 +1.5505E-03 +2.7813E-04 -1.9221E-03 -1.0244E-03 -3.4595E-02 -1.5984E-02 -5.9217E-03 -7.0826E-04 +1.5769E-04 +1.147OE-02 +6.3-587E-04 +9.7203E-04 +8.1987E-04 -1.2357E-03 -8.1346E-04 -2.8808E-02 -1.8330E-02 -9.2735E-03 -3.4338E-03 -7.0986E-04 +1.1470E-02 +6.3587E-04 +9.7203E-04 +8.1987E-04 -1.2357E-03 -8.1346E-04 -2.8808E-02 -1.8330E-02 -9.2735E-03 -3.4338E-03 -7.0986E-04 +1.2512E-02 +3.6342E-04 +1.5505E-03 -My- +3.9158E-03 +2. 4844E-03 +5.3458E-03 +2.4777E-04 +4.7362E-04 -1.4792E-04 -1.5303E-03 -1.2084E-03 -1.4346E-02 -1.2150E-02 -8. 8944E-03 -6.7713E-03 -5.2746E-03 +3.8144E-03 +3.4553E-04 +4.1296E-04 +5.078OE-04 +4.9368E-05 -2.0325E-04 -1.0832E-02 -1.1203E-02 -1,1079E-02 -1.0403E-02 -9.7521E-03 +3.8144E-03 +3.4553E-04 +4.1296E-04 +5.0780E-04 +4.9368E-05 -2.0325E-04 -1.0832E-02 -1.1203E-02 -1.1079E-02 -1.0403E-02 -9.7521E-03 +5.3458E-03 +2.4777E-04 +4.7362E-04 -Mzcy- +2.6351E-04 +1.1401E-03 -8.5793E-04 +3.0211E-05 -1.5143E-04 +1.5287E-04 -3.7741E-04 +2.6850E-04 -3.3678E-03 -3.2114E-03 -1.9857E-03 +1.9432E-04 +4.4299E-04 -1.6404E-04 -1.1297E-04 +2.2207E-05 +5.6173E-07 -1.4798E-04 -2.1414E-04 -1.2442E-03 -1.6542E-03 -9.2280E-04 -2.4259E-04 -2.4046E-05 +1.6404E-04 +1.1297E-04 -2.2207E-05 -5.6173E-07 +1.4798E-04 +2.1414E-04 +1.2442E-03 +1.6542E-03 +9.2280E-04 +2.4259E-04 +2.4046E-05 +8.5793E-04 -3.0211E-05 +1.5143E-04 +S1 -S2 TOP BOT -1.6494E-01 -2.0662E-02 -2.2377E-01 -1.0255E-02. -1.9317E-02 +8.4092E-03 +9.1796E-02 +5.9741E-02 +1.4993E+00 +7.5976E-01 +4.2191E-01 +2.8918E-01 +2.2658E-01 -1.6260E-Ol -1.3088E-02 -1.7582E-02 -2.1666E-02 +5.3442E-02 +3.7594E-02 +1.2328E+00- +7.9765E-0l +4.8928E-01 +4.4423E-01 +4.1609E-01 -1.6260E-01 -1.3088E-02 -1.7582E-02 -2.1666E-02 +5.3442E-02 +3.7594E-02 +1.2328E+00 +7.9765E-01 +4.8928E-01 +4.4423E-01 +4.1609E-01 -2.2377E-01 -1.0255E-02 -1.9317E-02 +S2 -Si TOP BOT -2.2646E-01 -1.3373E-01 -5.3816E-01 -1.5822E-02 -6.7044E-02 -1.3965E-02 +5.5510E-02 +3.5521E-02 +5.8881E-01 +4.4063E-01 +2.1025E-01 +2.9954E-02 --8.2593E-03 -4.8956E-01 -2.8785E-02 -4.1511E-02 -3.4981E-02 -2.8240E-03 +5.7855E-03 +4.5850E-01 +4.6240E-01 +3.7911E-01 +1.4615E-01 +3'.0284E-02 -4.8956E-01 -2.8785E-02 -4.1511E-02 -3.4981E-02 -2.8240E-03 +5.7855E-03 +4.5850E-01 +4.6240E-01 +3.7911E-01 +1.4615E-01 +3.0284E-02 -5.3816E-01 -1.5822E-02 -6.7044E-02

• • • • i**c**

Pacific Nuclear **** NEC-3E68DClC FRI MAR 07 12:51:24 2003 PAGE A026 of A028 NPT.PLA. v. 1. 1 PROJECT : Monticello Nuclear Generating Plant CLIENT

Nuclear Management Company kMN03-P022637-100 Supports DGEH-2, 3, 5, 6 -

Stiffness LOAD CASE 3 PLATE ELEMENT STRESSES : El. 70 71 72 73 74 75 76 77 78 79 80 '81 82 83 84 85 86 87 88 89 90 91 - 92 93 94 95 96 97 98 99 100 101 102 103 104 105 106 107 -Mx- +2.7813E-04 -1.9221E-03 -1.0244E-03 -3.4595E-02 -1.5984E-02 -5.9217E-03 -7.0826E-04 +1.5769E-04 +9.2853E-03 +6.2521E-03 +4.0089E-03 +2.1272E-04 -3.4766E-03 -1.0646E-02 -3.0994E-02 -1.2724E-02 +7.9693E-04 +5.2578E-03 +1.1342E-03 +3.2940E-03 +8.3101E-03 +5.0254E-03 +1.6328E-05 -5.3363E-03 -1.4689E-02 -1.7243E-02 -1.0233E-02 +3.2022E-03 +7.2089E-03 +1.6772E-03 +2.5976E-03 +5.0944E-03 +3.8854E-03 -2.6826E-04 -6.2510E-03 -1.3017E-02 -1.4388E-02 -7.9172E-03 -My- -1.4792E-04 -1.5303E-03 -1.2084E-03 -1.4346E-02 -1.2150E-02 -8.8944E-03 -6.7713E-03 -5.2746E-03 +5.9963E-03 +5.5116E-03 +3.0635E-03 +2.7824E-04 -2.6967E-03 -1.0424E-02 -1.6841E-02 -5.6179E-03 +1.3558E-03 +3.9158E-03 +2.4844E-03 +1.1060E-04 +2.7489E-03 +i.4820E-03 +3.0985E-04 -2.2954E-03 -3.3295E-03 -1.6404E-03 +9..8521E-04 +6.1112E-03 +7.4349E-03 +4.6960E-03 -3.8430E-04 +1.6421E-04 +2.9107E-04 -2.2145E-05 -5.6677E-04 -6.5168E-04 -4.0497E-05 +7.6503E-04 -Mxy- -1.5287E-04 +3.7741E-04 -2.6850E-04 +3.3678E-03 +3.2114E-03 +1.9857E-03 -1.9432E-04 -4.4299E-04 +3.1115E-03 +1.7125E-03 +1.5146E-03 +7.2006E-04 +1.9729E-03 +5.0262E-03 +8.5502E-03 +1.0939E-03 +9.1143E-05 -2.6351E-04 -1.1401E-03 +1.2467E-04 +1.731OE-03 +1.9177E-03 +2.1124E-03 +3.0592E-03 +3.7227E-03 +1.3700E-03 -6.7758E-04 -6.1344E-04 -9.4992E-04 -5.5219E-04 +4.2082E-04 +1.0441E-03 +1.7551E-03 +2.0704E-03 +2.6847E-03 +3.1647E-03 +1.9394E-03 +2.3980E-05 +S1 -S2 TOP BOT +8.4092E-03 +9.1796E-02 +5.9741E-02 +1.4993E+00 +7.5976E-01 +4.2191E-01 +2.8918E-01 +2.2658E-01 -1.7585E-Ol -1.7620E-01 -8.3182E-02 +2.0281E-02 +2.1750E-01 +6.6399E-01 +1.4940E+00 +5.4993E-01 -3.3384E-02 -1.6494E-01 -2.0662E-02 -4.5110E-03 -9.6175E-02 -6.1982E-02 +8.3389E-02 +3.0857E-01 +6.7413E-01 +7.4078E-01 +4.3834E-01 -1.3133E-01 -2.7159E-01 -6.7386E-02 +1.8882E-02 +2.0388E-03 +1.8082E-02 +9.4689E-02 +3.1226E-01 +5.8795E-01 +6.2488E-01 +3.3780E-01 +S2 -Sl TOP BOT -1.3965E-02 +5.5510E-02 +3.5521E-02 +5.8881E-01 +4.4063E-01 +2.1025E-01 +2.9954E-02 -8.2593E-03 -4.7617E-01 -3.2571E-01 -2.1858E-01 -4.1228E-02 +4.5891E-02 +2.3499E-0l +5.4692E-01 +2.3268E-0l -5.8466E-02 -2.2646E-01 -1.3373E-01 -1.4075E-01 -3.7567E-01 -2.5834E-01 -9.7306E-02 +1.7052E-02 +9.4641E-02 +6.4895E-02 -4.3775E-02 -2.6604E-01 -3.5322E-01 -2.0454E-01 -i.1332E-01 -2.2641E-01 -1.9628E-01 -8.2298E-02 -2.1365E-02 -4.7445E-03 -9.2606E-03 -3.2644E-02

• • • • • Pacific Nuclear NEC-3E68DC1C FRI MAR 07 12:51:24 2003 PAGE A027 of A028 NPLATE v. 1.1.0 PROJECT : Monticello Nuclear Generating Plant CLIENT

Nuclear Management Company MN03-P022637-100 Supports DGEH-2, 3,

5, 6 - Stiffness LOAD CASE 3 PLATE ELEMENT STRESSES : El. 108 109 110 -Mx- +8.0821E-04 +4.5428E-03 +1.9600E-03 -My- +1.2013E-03 +1.5225E-03 +1.388OE-03 -Mxy- -8.2654E-04 -1.7393E -6.2225E-04 +S1 -S2 TOP BOT -4.6197E-03 -6.4532E-02 -4.2202E-02 +S2 -Sl TOP BOT -7.9118E-02 -1.9425E-01 -1.0064E-01 MAX. BENDING STRESS - +1.499 ksi AT EL.

73.

STRESS RATIO = +0.05553. BOLT TENSION AND SHEAR : (UNITS: KIPS/BOLT) BOLT TENSION 1 +0.0745 2 +0.0745 3 .+0.0219 4 +0.0219 SHEAR +0.0000 +0.0000 +0: 0000 +0.0000 +0.0000 INTERACTION 0.0149 0.0149 0.0044 0.0044 0.0149 at bolt 2 mX (+) +0.0745 INTERACTION - (T/Tallow)**(1.000) + (V/Vallow)**(1.000) S-U-M-M-A-R-Y MAXIMUM PLATE BENDING: S t r e s s _ _ _ _ _ - 1 9f o l n 3 t 7 8 I LOAD CASE 3 Stress 1.499 ksi for element #73 (its. 79, 80, 91,.921 Interaction - 5.553% of bending allowable ( 27 ksi) MAXIMUM BOLT LOADS: Tension .- 0.1258 k (Jt. Shear 0 k (Jt. Interaction - 0.02508 (Jt.

99) 1

27)

I

99) I LOAD CASE 1 LOAD CASE 3 LOAD CASE 1 I

S ************ Pacific Nuclear A****** NEC-3E68DC1C FRI MAR 07 12:51:24 2003 PAGE A028 of A028 NPLATE V. 1.1.0 PROJECT : Monticello.Nuclear Generating Plant CLIENT : Nuclear Management Company MN03-P022637-100 Supports DGEH-2, 3, 5, 6 - Stiffness -END

z) Automated Engineering Services Corp. NO. B I OF B16 Calculation Sheet REVISION NUMBER: 0 CLIENT: Nuclear Management Companv DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPAED:

SUBJECT:

EDG Exhaust Evals CHECKED: .44 SAFETY RELATED YES i NO [] CALC. NO.: MNO3-P022637-100 Attachment B ANSYS Input Listing for East-West Tornado Wind Form 3.1-3 Rev. I

Automated Engineering Services Corp. NO. B2 lOF B16 Calculation Sheet REVISION NUMBER:. 0 CLIENT: Nuclear Management Companv DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED: 4 7°

SUBJECT:

EDG Exhaust Evals CHECKED:. SAFTY RELATED YES [R] NO CALC. NO.: MN03-P022637-100 /filnam, exhaust /title, EDG Exhaust Piping ! Units are pounds and inches /prep7 tref, 0.0 Material Properties Material 1 - A-106 GR. B

mnp, ex, 1, 27900000.

mp, nuxy, 1, 0.3 mp, dens,. 1, 490/1728/386.4 !-Material 2 - A-36 mp, ex, 2, 29000000. mp, nuxy, 2, 0.3 mp, dens, 2, 490/1728/386.4 tb, bkin, 2, 1 tbtemp, 0.0 tbdata, 1, 36000.0, 0.0 Material 3 - rigid mp, ex, 3, 29000000. mp, nuxy, 3, 0.3 mp, dens, 3, 0.0 ! element types et, 1, pipel6 et, 2, pipel8 et, 3, beam4 et, 4, mass2l keyopt, 4, 3, 2 et, 5, combin40 ! Gap Elei keyopt, 5, 3, 0 et, 6, combin40 ! Gap Elei keyopt, 6, 3, 3 et, 7, combinl4 ! Spring I keyopt, 7, 2, 1 et, 8, combinl4 ! Sorina I I nent in the x-direction nent in the z-direction Element in the x-direction Element in the y-direction Form 3.1-3 Rev. I

Automated Engineering Services Corp. NO. B3 OF B16 Calculation Sheet Z REVISION NUMBER: O CLIENT: NuclearManaeementCompanv DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:,/7

SUBJECT:

EDG Exhaust Evals CHECKED: J A-SAFETY RELATED YES FRI NO [] CALC. NO.: MN03-P022637-100 keyopt, 8, 2, 2 et, 9, combinl4 keyopt, 9, 2, 3 et, 10, combinl4 keyopt, 10, 2, 4 et,. 11, combinl4 keyopt, 11, 2, 5 et, 12, combinl4 keyopt, 12, 2, 6 et, 13, beam24 keyopt, 13, 1, 1 et, 14, combin37 keyopt, 14, 2, 2 keyopt, 14, 3, 2 keyopt, 14, 4, 1 et, 15, linklO keyopt, 15, 3, 1 Member Properties ! Spring Element in the z-direction ! Spring Element in the x-rotation ! Spring Element in the y-rotation ! Spring Element in the z-rotation ! non-linear beam ! Spring Can r, 1, r, 2, r, 3,

rmore, r,

4,

rmore, r, 5,

rmore, r, 6,

rmore, rmore,

rmore, r, 7,

rmore, r, 8, r, 10, r, 11, r, 12, r, 13, r, 14, r, 15,

rmore, r, 17, r, 18, r, 19, 22.00, 36.00, 22.00, 0.375 0.350 0.375, 33.0, 4.02, 4.02, 15.588 22.00, 0.375 0.007/386.4, 3.0 22.00, 0.375, 33.0,

, 0.007/386.4, 3.0, -2.03, 0.0, -2.03, 2.03, 1.127, -0. 365, 0.0, 1.9075, 1.9075, -1.9075, -1.9075, 1.852, -1.852, 0.0, 0.0, 0.0, 0.345, 0.345 0.0, 0.184, 0.0, 4.02, 2.03, 0.0, 0.0, -0.365, 1.127, 0.125, 4.02, 1.9075, -1.9075, -1.9075, 1.852, -1.852, ,15.588 15.588

15. 588 0.345 0.280 0.0 0.296 0.296

! 22" Pipe ! 36" Pipe ! Elbow ! 22" Pipe w/ insul ! Elbow w/ insul ! W4 x 13 1 C4 x 5.4 155.0/386.4 230.0/386.4 0.0, 0.0, 1.OE10 10.0 100.0, 1000.0, 0.000, 1000.0 6.6E6

• 5.8E6
• 0.0, 0.0, 0.0, 0.5, 0.0, 1.OE10 ! Gap Element

!Flange Weight ! Flange Weight 0.0, 1.OE10 ! Gap Element !Rigid Stiffness !Bellows Stiffness 1.0 ! Rigid Beam ! Kz Rotational Stiffness !.Kx Rotational Stiffness 0.0, 1.OE10 ! Gap Element 1000.0, 1.0, 0.0, 0.5, Form 3.1-3 Rev. 1 Form 3. 1-3 Rev. I

Automated Engineering Services Corp. NO. B4 OF B16 / D XCCalculation Sheet REVISION NUMBER: 0 CLIENT: Nuclear Management Companv DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED: 4

SUBJECT:

EDG Exhaust Evals CHECKED: J SAFETY RELATED YES [] NO z CALC. NO.: MN03-P022637-100 r, 20, r, 21, r, 22, r,- 23, r, 24, r, 25, r, 26, r, 27, csys, 0 10.0 10.0 10.0 10..0 10.0 363.0, 363.0, 1.5 ! Bellows ! Bellows ! Bellows ! Bellows -Bellows 0.0, 0.0, 0.375, -10, 1515.0 ! DGEH-3 0.0, 0.0, 1.250, -10, 1832.0 ! DGEH-2 Stiffness Stiffness Stiffness Stiffness Stiffness ! 22" Pipe n, 1, 0.0, n, 2, -37.0, n, 3, -74.0, n, 4, -96.0, n, 5, -100.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0 0.0 0.0 0.0 0.0 ! 36" Pipe n, 6, -135.25, n, 7, -170.50, n, 8, -205.75, n, 9, -241.0, ! 22" Pipe n, 10, -245.0, n, 11, -266.0, n, 12, -305.0, n, 13, -338.0, n, 14, -338.0, n, 15, -338.0, n, 16, -338.0, n, 17, -338.0, n, 18, -338.0, n, 19, -338.0, n, 20, -371.0, n, 21, -394.0, n, 22, -394.0, Support DGEH-3 n, 30, -74.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, -33.0, -66.25, -99.5, -132.75, -166.0, -190.5, -222.25, -255.25, -255.25, -255.25, 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 O, 0 0.0 0.0 0.0 ! for bellows stiffnesses 0.0, 13.125 Form 3.1-3 Rev. I

Automated Engineering Services Corp. NO. B5 OF B16 Calculation Sheet Lt REVISION NUMBER.: 0 CLIENT: Nuclear ManaanementyCoran DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:X& /

SUBJECT:

EDG Exhaust Evals CHECKED: SAFETY REILATED YES [R NO CALC. NO.: MN03-P022637-100 rn, 31, n, 32, n, 33, n, 34, n,. 35, n, 36, n, 37, n, 38, n, 39, n, 200, n, 201, -74.0, -74.0, -74.0, -74.0, -74.0, -74.0, -74.0, -74.0, -74.0, -74.0, -74.0, ! Support DGEH-2 n, 40, -266.0, n, 41, -266.0, n, 42, -266.0, n, 43, -266.0, n, 44, -266.0, n, 45, -266.0, n, 46, -266.0, n, 47, -266.0, n, 48, -266.0, n, 49, -266.0, n, 202, -266.0, n, 203, -266.0, Support DGEH-1 -30.5, -41.0, -30.5, 0.0, -30.5, -41.0, 0.0, 0.0, -30.5, -41.0, -41.0,

0. 0,

-30.5, -41.0, -30.5, ' 0.0, -30.5, -41.0, 0.0, 0.0, -30.5, -41.0, -41.0, -190. 5, -190. 5, -190. 5, -190.5, -190. 5,. -190.5, -.190. 5, -190.5, -190.5, -190. 5, -190.5, -190. 5, -190.5, -190. 5, -190. 5, -190. 5,

13. 125

13. 125 0.0

-13.125 -13.125 -13.125 13.125 -13.125 0.0 13.125 -13.125 13.125 i3.125 13.125 0.0 -13.125 -13.125 -13.125 13.125 -13.125 0.0 13.125 -13.125 -11. 957 -11.957 -11.957 -11. 957 -11.957 0.0 0.0 11.957 11.957

11. 957

11. 957 11.957

-11. 957 0.0 0.0 11.957 ! for ! for ! for ! for ! for ! for -! for ! for ! for ! for ! for ! for ! for ! for lateral gap lateral gap spring can bp stiffnesses bp stiffnesses lateral gap lateral gap spring can bp stiffnesses bp stiffnesses n, n, n, n, n, n, n, n, n, n, n, n, n, n, -n, n, 50, 51, 52, 53, 54, 55, 56, 57, 58, 59, 60, 61, 62, 63, 64, 65, -377.0, -349. 957, -338.0, -326.043, -306.0, -34 9. 957, -326.043, -377.0,. -34 9.957, -338.0, -326.043, -306.0, -338.0, -349.957, -326. 043, -338.0, ] Lateral Lateral Lateral Lateral gap gap gap gap Form 3.1-3 Rev. I

Automated Engineering Services Corp. NO. B6 OF B16 Calclaton Sheet REVISION NUMBER: 0 CLIENT: Nuclear Mana ement CoQ anv DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:

.)/

SUBJECT:

EDG Exhaust Evals CHECKED: )1 SAFETY RELATED YES [x] NO FlI CALC. NO.: MN03-P022637-100 n, 72, -338.0, -186.5, - n, 73, -349.957, -186.5, n, 74, -326.043, -186.5, n, 75, -338.0, -186.5, !Reference Nodes for Elbows 11.957 0.0 0.0 11.957 ! for ! for ! for ! for vertical vertical vertical vertical support support support support n, 100, n, 101, I -305.0, -33.0, -371.0, -222.25, 0.0 0.0 ! Reference Nodes for Beams n, 102, -349.957, n, 103, -326.043, ! 22" Pipe -180.5, -11.957 -180.5, 11.957 mat, 1 type, 1 real, 1 EN, 1, EN, 2, EN, 3, : EN, 4, ! 36' Pipe real, 2 EN, 5, EN, 6, EN, 7, EN, 8, I 1,- 2 2, 3 3, 4 4, 5 5, 6, 7, B, 6 7 8 9 ! 22" Pipe real, 1 EN, 9, 9, 10 EN, 10, 10, 11 EN, 11, 11, 12 type, 2 real, 3 EN, 12, 12, 13, 100 type, 1 real, 1 EN, 13, 13, 14 Form 3.1-3 Rev. I

Automated Engineering Services Corp. NO. B7 OF B16 / Calculation Sheet /REVISION NUMBER: 0 CLIENT: Nuclear Management Company DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:,j

SUBJECT:

EDG Exhaust Evals CHECKED: iA-SAFETY RELATED YES [RI NO LI CALC. NO.: MN03-P022637-100 EN, 14, 14, 15 EN, 15, 15, 16 EN, 16, 16, 17

real, 4

EN, 17, 17, 18 EN, 18, 18, 19

type, 2

real, 5 EN, 19, 19, 20

type, 1

real, 4

EN, 20, 20, 21 I 101 l Support DGEH-3

mat, 2

real, 6

type, 13.

en, 30, 30, 3 en, 31, 31, 3 en, 32, 31, 3 en, 33, 33, 3 en, 34, 34, 3 en, 35, 35, 3 ! Support DGEH-2 1, 2, 3, 5, 5, 6, 3 .3 3 3 3 3 en, en, en, en, en, en, 40, 40, 41, 11 41, 41, 42, 11

• 42, 41, 43, 11 43, 43, 45, 11 44, 44, 45, 11 45, 45, 46, 11

! Support DGEH-1 real, 7 en, 50, en, 51, en, 52, en, 53, en, 54, en, 55, en, 56, en,- 57, 50, 51, 52, 53, 55,. 58, 53, 56, 51, 52, 53, 54, 51, 55, 56, 60, 102 102 102 102 102 102 103 103 Form 3.1-3 Rev. I

Automated Engineering Services Corp. No. B8 OF B16 / / Calculation Sheet REVISION NUMBER: 0 CLIENT: Nuclear Management Companv DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:

SUBJECT:

EDG Exhaust Evals CHECKED: JA-SAFETY RELATED YES NO I CALC. NO.: MN03-P022637-100 en, 58, 58, 57, 103 en, 59, 59, 58, 103 en, .60, 60, 59, 103 en, 61, 61, 60, 103 Gap Elements

mat, 3

type, 3 real, 15. en, 70, 3, 37 en, 71, 3, 38 en, 72, 11, 47 en, 73, 11, 48 type, 6 real, 8 en, 74, 37, 30 en, 75, 34, 38 en, 76, 47, 40 en, 77, 44, 48 type, 3 real, 15 en, 78, 18, 62 en, 79, 18, 63 en, 80, 18, 64 en, 81, 18, 65 type, 6 real, 12 en, 82, 52, 62 en, 85, 65, 59 type, 5 real, 19 en, 83, 63, 55 en, 84, 56, 64 Spring Elements type, 3 real, 15 en, 86, .3, 39 en, 87, 11, 49 type, 14 real, 25 en, 88, 39, 33, 39, 33 real, 26 Form 3. 1-3 Rev. 1 Form 3.1 -3 Rev. I

Automated Engineering Services Corp. No. Bi l iOF B16 / D ACalculation Sheet REVISION NUMBER 0 CLIENT: Nuclear Management Company DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:

SUBJECT:

EDG Exhaust Evals CHECKED: JoA4-SAFETY RELATED YES [ NO CALC. NO.: MN03-P022637-100 en, 89, 49, -43, 49, 43 Bellows - type, 7 real, 14 en, 94, 21, 22 type, 8 real, 20 en, 95, 21, 22 type, 9 real, 21 en, 96, 21, 22 type, 10 real, 22 en, 97, 21, 22 type, 11 real, 23 en, 98, 21, 22 type, 12 real, 24 en, 99, 21, 22 Add Weights type, 4 real, 10 en, 100, 4 en, 101, 10 real, 11 en, 102, 21 Baseplate Stiffnesses type, 10 real, 18 en, 200, 32, 200 en, 203, 36, 201 en, 205, 42, 202 en, 208, 46, 203 type, 12 real, 17 en, 201, 32, 200 en, 204, 36, 201 en, 206, 42, 202 Form 3.1-3 Rev. I

Automated Engineering Services Corp. NO. Bs0 OF B16 Calculation Sheet REVISION NUMBER: 0 CLIENT: Nuclear Management Companv DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED::,A

SUBJECT:

EDO Exhaust Evals CHECKED: t-SAFETY RELATED YES [ER NO [] CALC. NO.: MN03-PO22637-100 en, 209, 46, 203 ! Lugs type, 3 real, 15 en, 220, 18, 72 en, 221, 18, 73 en, 222, 18, 74 en, 223, 18, 75 type, 15 real, 27 en, 224, 72, *52 en, 225, 73, 55 en, 226, 74,. 56 en, 227, 75, 59 ! Boundary Conditions d, 22, all, 0.0 d, 32, ux, 0.0,, , uy,. uz, roty d, 36, ux, 0.0,, ,, uy, uz, roty d, 42, ux, 0.0,, , uy, uz, roty d, 46, ux, 0.0,, , uy, uz, roty d, 50, all, 0.0 d, 54, ux, 0.0,, , uy, uz d, 57, all, 0.0 d, 61, ux, 0.0,,,, uy, uz d, 200, all, 0.0,,-203 nlist, all mplist, all etlist, all rlist, all elist, all tblist, all, all finish /solu antype, trans, new solcontrol, on timint, off nlgeom, off outres, all, all time, 1.0 nsubst, 1000, 10, 10000 Form 3.1-3 Rev. I

r~ lAutomated Engineering Services Corp. NO. BB16 / Calculation Sheet p O 1 C i SREVISION NUMBER: 0 CLIENT: Nuclear Manaement Company DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:

SUBJECT:

EDG Exhaust Evals CHECKED; JM.- SAFETY RELATED YES M NO [] CALC. NO.: MN03-P022637-100 Apply Gravity Force acel, 0.0, 386.4, 0. solve

time, 2.0 nsubst, 1000, 10, 10000 Apply Gravity Force acel, 0.0, 386.4, 0.

Apply Tornado Load wind - 300 pressure - (0.40*0.002558*wind**2)/144 pressw4 - (1.81*0.002558*wind**2)/144 esel, s, elem,, 1, 4 esel, a, elem,, 9, 16 sfe, all, 4, pres,, 2 2*pressure esel, s, elem,, 5, 8 sfe, all, 4, pres,, 3 6 *pressure esel, s, elem,, 30, 31 esel, a, elem,, 40, 41 sfbeam, all, 1, pres, 4*pressw4, 4*pro esel, s, elem,, 34, 35 esel, a, elem,, 44, 45 sfbeam, all, 1, pres, -4*pressw4, -4*pj esel, all solve finish /postl file, exhaust, rst set, 1, last ! Nodal Displacements prnsol, u Reaction Forces prrsol set, 2, last Nodal Displacements essw4 ressw4 Form 3.1-3 Rev. I

Automated Engineering Services Corp. NO. s2 OF B16 / / SCCalculation Sheet /_.REVISION NUMBER: 0 CLIENT: Nuclear Management ComRanv DATE: 03/07/03 PROJECT: Monticello Nuclear Genefatinj Plant PREPARED:

e

SUBJECT:

EDG Exhaust Evals CHECKED: SAFETY RELATED YES Fx NO M CALC. NO.: MN03-P022637-100 prnsol, u Pipe Forces esel, s, type, etable, xfori, etable, yfori, etable, zfori, etable, xmomi, etable, ymomi, etable, zmomi, -etable, xforj, etable, yforj, etable, zforj, etable, xmomj, etable, ymomj, etable, zmomj, pretab, xfori, pretab, xforj, , 1, 2

smisc, 1

smisc, 2

smisc, 3

smisc, 4

smisc, 5

smisc, 6

smisc, 7

smisc, 8

smisc, 9

smisc, 10 smisc, 11 smisc, 12 yfori, zfori, yforj, zforj, xmomi, ymomi, zmomi xmomj, ymomj, zmomj ,I Support DGEH W4 x 13 ! Plastic Strains esel, s, elem,

etable, plstrl, I

etable, plstr2, I

etable, plstr3, 3

etable, plstr4, I

etable, plstrS, 3

etable, plstr6, 3

etable, plstr7, 3 etable, plstr2l, I etable, plstr22, l etable, plstr23, I etable, plstr24, I etable, plstr25, 1 etable, plstr26, 1 etable, plstr27, 1

! Element Forces 30, 35 .eppl, 1 .eppl, 2 .eppl, 3 .eppl, 4 .eppl,. 5 .eppl, 6 .eppl, 7 leppl, 21 .eppl, 22 leppl, 23 leppl, 24 leppl, 25 leppl, 26 leppl, 27

misc, 1

misc, 2

misc, 3

etable, etable,

etable, xfori,

yfori, zfori, s

S S Form 3.1-3 Rev. 1

Automated Engineering Services Corp. NO. B13 OF B16 / D SCCalculation Sheet i Se REVISION NUMBER: 0 CLIENT: Nuclear Management Company DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:

SUBJECT:

EDG Exhaust Evals CHECKED: SAFETY RELATED YES R NO I] CALC. NO.: MN03-P022637-100

etable, etable,

etable, etable,

etable, etable,

etable, etable,

etable,

xmomi, ymomi,

zmomi, xforj,

yforj, zforj,

xmomj, ymomj,

zmomj, smisc, 4

smisc, 5

smisc, 6

smisc, 7

smisc, 8

smisc, 9

smisc, 10 smisc, 11 smisc, 12 ! Element Axial Stresses

etable, etable,

etable, etable,

etable, etable,

etable, etable,

etable, etable,

etable, etable,

etable, etable,

pretab, pretab,

pretab, pretab,

pretab, pretab,

axstrl, axstr2,

axstr3, axstr4,

axstr5, axstr6,

axstr7, axstr21,

axstr22, axstr23,

axstr24, axstr25,

axstr26, axstr27,

pistrl, plstr2l,

xfori, xforj,

axstrl, axstr2l, is, 1

is, 2 is, 3 Is, 4 Is,.5 is, 6 is, 7 is,.21 is, 22 is, 23 is, 24 is, 25 Is, 26 Is, 27

plstr2, plstr3, plstr22, plstr23,

yfori, zfori,

yforj, zforj,

axstr2, axstr3, axstr22, axstr23,

plstr4, plstr24,

xmomi, xmomj,

axstr4, axstr24,

plstrS, plstr25,

ymomi, ymomj,

axstr5, axstr25,

plstr6, pistr7 plstr26, plstr27 zmomi zmomj

axstr6, axstr7 axstr26, axstr27

! Support bGEH W4 x 13 ! Plastic Strains esel, s, elem,,

etable, pistri, '

etable, plstr2, I

etable, plstr3, I

etable, plstr4, 1

etable, plstr5, I

etable, plstr6, I

etable, plstr7, I 40, 45

Leppl, 1

Leppl, 2

Leppl, 3

Leppl, 4

leppl, 5

.eppl, 6 .eppl, 7 Form 3.1-3 Rev. I

Automated Engineering Services Corp. NO. B14 OF B16 A D XC Calculation Sheet E N LJ REVISION NUMBER: 0 CLIENT: Nuclear Management Company DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPAXED:

SUBJECT:

EDG Exhaust Evals CHECKED: Jvv&- SAFETY RELATED YES [53 NO [ CALC. NO.: _N03-P022637-100 etable, plstr21, etable, plstr22, etable, plstr23, etable, plstr24, etable, plstr25, etable, plstr26, etable, plstr27, ! Element Forces

leppl, leppl,

leppl, leppl,

leppl, leppl,

leppl, 21 22 23 24 25 26 27

etable, xfori,

smisc, 1

etable, yfori,

smisc, 2

etable, zfori,

smisc, 3

etable, xmomi,

smisc, 4

etable, ymomi,

smisc, 5

etable, zmomi,

smisc, 6

etable, xforj,

smisc, 7

etable, yforj,

smisc, 8

etable, zforj,

smisc, 9

etable, xmomj, smisc, 10

etable, ymomj, smisc, 11

etable, zmomj, smisc, 12

! Element Axial Stresses

etable, etable,

etable, etable,

etable, etable,

etable, etable,

etable, etable,

etable, etable,

etable, etable,

pretab, pretab,

pretab, pretab,

pretab, pretab,

axstrl, axstr2,

axstr3, axstr4,

axstr5, axstr6,

axstr7, axstr2l,

axstr22, axstr23,

axstr24, axstr25,

axstr26, axstr27,

plstrl, plstr2l,

xfori, xforj,

axstrl, axstr2l, is, 1

is, 2 is, 3 is, 4 is,.5 ls, 6 is, 7 is, 21 is, 22 is, 23 Is, 24 is, 25 is, 26 is, 27

plstr2, plstr3, plstr22, plstr23,

yfori, zfori,

yforj, zforj,

axstr2, axstr3, axstr22, axstr23,

plstr4, plstr24,

-xmomi,

xmomj, axstr4,

axstr24, plstr5,

plstr25, ymomi,

ymomj, axstr5,

axstr25, plstr6,

plstr26, zmomi zmomj axstr6,.

axstr26, plstr7 plstr27 axstr7 axstr27 Form 3.1-3 Rev. I

Automated Engineering Services Corp. NO. B15 OF B16 / D JC -Calculation Sheet REVISION NUMBER: 0 CLIENT: Nuclear Management Company DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:

SUBJECT:

EDG Exhaust Evals CHECKED: %)v"JI-SAFETY RELATED YES F NO II CALC. NO.: MN03-P022637-100 ! Support DGEH C4 x 5.4 ' Plastic Strains esel, s,

etable, etable,

etable, etable,

etable, etable,

etable, etable,

,elem,

plstrl, plstr2,

plstr3, plstr4,

plstr2l, plstr22,

plstr23, plstr24, 50, 61

leppl, 1

leppl, 2

leppl, 3

leppl, 4

leppl, 21 leppl, 22 leppl, 23 leppl, 24 ! Element Forces s

etable, etable,

etable, etable,

etable, etable,

etable, etable,

etable, etable,

etable, etable,

xfori, yfori,

zfori, xmomi,

ymomi, zmomi,

xforj, yforj,

zforj, xmomj,

ymomj, zmomj,

smisc, 1

smisc, 2

smisc, 3

smisc, 4

smisc, 5

smisc, 6

smisc, 7

smisc, 8

smisc, 9

smisc, 10 smisc, 11 smisc, 12 ! Element Axial Stresses

etable, etable,

etable, etable,

etable, etable,

etable, etable,

pretab, pretab,

pretab, pretab,

pretab, axstrl,

axstr2, axstr3,

axstr4, axstr2l,

axstr22, axstr23,

axstr24, plstrl,

plstr2l, xfori,

xforj, axstrl, is, 1

Is, 2 Is, 3 is, 4.. is, 21 is, 22 is, 23 Is, 24

plstr2, plstr3, plstr22, plstr23,

yfori, zfori,

yforj, zforj,

axstr2, axstr3, plstr4 plstr24.

xmomi, xmomj, axstr4

ymomi, zmomi

ymomj, zmomj Form 3.1-3 Rev. I

Automated Engineering Services Corp. NO. OF B16 Calculation Sheet REVISION NUMBER: 0 CLIENT: Nuclear Manazement Companv DATE: 03107/03 PROJECT: Monticello Nuclear Generatine Plant PREPARED:Xte4

SUBJECT:

EDG Exhaust Evals CHECKED: SAFETY RELATED YES Jxj NO CALC. NO.: MN03-P022637-100 pretab, axstr2l, axstr22, axstr23, axstr24 ! Loads on Lugs esel, s, elem,, 224, 227 etable, lugforce, smisc, 1 pretab, lugforce ! Forces in Spring Cans esel, s, elem,, etable, spforce, etable, preload,

etable, elstat, pretab, spforce, esel, all

! Reaction Loads prrsol finish 88, 89 smisc, 1 smisc, 2 nmisc, 1 preload, elstat Form 3.1-3 Rev. 1

Automated Engineering Services Corp. NO. Cl OF C16 / D SCCalculation Sheet REVISION NUMBER: 0 CLIENT: Nuclear Management Company DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:D: ,<0

SUBJECT:

EDG Exhaust Evals CHECKED: JKA-SAFETY RELATED YES RX NO 2 CALC. NO.: MN03-P022637-100 Attachment C ANSYS Input Listing for North Tornado Wind Form 3.1-3 Rev. I

Automated Engineering Services Corp. NO. C2 OF C16 / D D gCalculaffon Sheet REVISION NUMBER: 0 CLIENT: Nuclear Manazement Compan DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:,

SUBJECT:

EDG Exhaust Evals CHECKED: JVU.-' SAFETY RELATED YES R NO CALC. NO.: _MN03-P022637-100 /filnam, north /title, EDG Exhaust Piping North Tornado Wind ! Units are pounds and inches /prep7 tref, 0.0 ! Material Properties ! Material 1 - A-106 GR. B -mp, ex, 1, 27900000. mp, nuxy, 1, 0.3 mp, dens, 1, 490/1728/386.4 ! Material 2 - A-36 mp, ex, 2, 29000000. mp, nuxy, 2, 0.3 mp, dens, 2, 490/1728/386.4 tb, bkin, 2, 1 tbtemp, 0.0 tbdata, 1, 36000.0, 0.0 I Material 3 - rigid mp, ex, 3, 29000000. mp, nuxy, 3, 0.3 mp, dens, 3, 0.0 I element types et, 1, pipel6 et, 2, pipel8 et, 3, beam4 et, .4, mass2l keyopt, 4, 3, 2 et, 5, combin40 ! Gap Element in the x-direction keyopt, 5, 3, 0 et, 6, combin40 ! Gap Element in the z-direction keyopt, 6, 3, 3 et, 7, combinl4 ! Spring Element in the x-direction

keyopt, 7,

2, 1 et, 8, combinl4 ! Spring Element in the y-direction Form 3.1-3 Rev. I

Automated Engineering Services Corp. NO. C3 OF C16 / / DzCCalculation Sheet REVISION NUMBER:. 0 CLIENT: Nuclear Mana ementCompany DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:

SUBJECT:

EDGOExhaust Evals CHECKED: J n SAFETY RELATED YES NO O CALC. NO.: MN03-P022637-100

keyopt, 8,

2, 2 et, 9, combinl4 keyopt, 9, 2, 3 et, 10, combinl4 keyopt, 10, 2, 4 et, 11, combinl4 keyopt, 11, 2, 5 et, 12, combinl4 keyopt, 12, 2, 6 et, 13, beam24 keyopt, 13, 1, 1 et, 14, combin37 keyopt, 14, 2, 2 keyopt, 14, 3, 2 keyopt, 14, 4, 1 et, 15, linklO keyopt, 15, 3, 1 Member Properties ! Spring Element in the z-direction ! Spring Element in the x-rotation ! Spring Element in the y-rotation. ! Spring Element in the z-rotation ! non-linear beam ! Spring Can r, 1, r, 2, r, 3,

rmore, r, 4,

rmore, 22.00, 36.00, 22.00, 0.375 0.350 0.375, 33.0, 4.02, 4.02, 15.588 f

, 15.588 22.00, 0.375 0.007/386.4, 3.0 r, 5,

rmore, r,

6,

rmore, rmore,

rmore, r, 7,

rmore, r, 8, r, 10, r, 11, r, 12,

-r, 13, r, 14, r, 15,

rmore, 22.00, 0.3

, 0.00' -2.03, 1.91 0.0, 1.91 -2.03, -1.9i 2.03, -1.9i 1.127, 1.1 -0.365, -1.I 0.0, 1 155.0/386.4 230.0/386.4 0.0, 1.OE10 10.0. 100. 0, 100( 0.000, 100( 75, 33.0, 7/386.4, 3.0,

075, 075,

075, 075,

852, 852, 0.0, 0.0, 0.0, 0.345, 0.345 0.0, 0.184, 0.0, 4.02, 2.03, 0.0, 0.0,

-0.365, 1.127, 0.125, 4.02,

1. 9075,

-1. 9075, -1. 9075, 1.852, -1.852, 15.588 15.588 0.345 0.280 0.0 0.296 0.296 ! 22" Pipe ! 36" Pipe ! Elbow ! 22" Pipe w/ insul ! Elbow wJ insul ! W4 x 13 ! C4 x 5.4 0.0, 0.0, 0.5, 0.0, 1.OE10 ! Gap Element Flange Weight Flange Weight 0.0, 1.OE1O ! Gap Element I Rigid Stiffness Bellows Stiffness 1.0 ! Rigid Beam Kz Rotational Stiffness Kx Rotational Stiffness 0.0, 1.OE10 ! Gap Element ).O, 1000.0, ).O 1.0, r, 17,. r, 18, r, 19, 6.6E6 5.8E6 0.0, 0..0, 0.0, 0.5, Form 3.1-3 Rev. 1

z) Automated Engineering Services Corp, NO. C4 OF C16 / D /SCalculation Sheet Shee REVISION NUMBER: 0 CLIENT: Nuclear ManagementComyanv DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:

SUBJECT:

EDG Exhaust Evals CHECKED: SAFETY RELATED YES - ] NO [ CALC. NO.: MN03-P022637-100 20, 21, 22, 23, 24, 25, 26, 27, - '10.0 10.0 10.0 10.0 10.0 363.0, 363.0, 1.5 ! Bellows !Bellows ! Bellows !Bellows ! Bellows !DGEH-3 !DGEH-2 .,Stiffness Stiffness Stiffness Stiffness Stiffness 0.0, 0.0, 0.375, 0.0, 0.0, 1.250, -10, 1515.0 -10, 1832.0

csys, 0

! 22" Pipe n, 1, 0.0, n, 2, -37.0, n, 3, -74.0, n, 4, -96.0,

• n, 5,

-100.0, ! 36" Pipe I 0.0, 0.0, 0.0, 0.0, 0.0, 0.0 0.0 0.0 0.0 0.0 n, 6, -135.2! n, 7, -170.5( n, 8, -205.7! n, 9, -241.( ! 22" Pipe n, 10, -245.C n, 11, -266.C n, 12, -305.0 n, 13, -338.0 n, 14, -338.0 n, 15, -338.0 n, 16, -338.0 n, 17, -338.0 n, 18, -338.0 n, 19, -338.0 n, 20, -371.0 n, 21, -394.0 n, 22, -394.0 Support DGEH-3 O, 5, O. O. I, I t 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, -33.0, -66.25, -99. 5, -132.75, -166.0, -190.5, -222.25, -255.25, -255.25, -255.25, 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 ! for bellows stiffnesses n, 30, -74.0, 0.0, 13.125 1*rormn I.I-3 Rev. I

/ Automated Engineering Services Corp. NO. -C5 OF C16 Calculation Sheet E .REVISION NUMBER 0 CLIENT: Nuclear Management Comwany DATE: 03/07/03 PROJECT: Monicello Nuclear Generating Plant PREPARED:

SUBJECT:

EDO Exhaust Evals CHECKED:. SAFETY RELATED YES FRI NO [ CALC. NO.: MN03-P022637-100 I n, 31, n, 32, n, 33, n, 34, n, 35, n, 36, n, 37, n, 38, n, 39, n, 200, -74.0, -30.5, -74.0, -41.0, -74.0, -30.5, -74.0, 0.0, -74.0, -30.5, -74.0, -41.0, -74.0, 0.0, -74.0, 0.0, -74.0, -30.5, -74.0, -41.0, -74.0, -41.0,

13. 125

13. 125 0.0

-13. 125 -13. 125 -13. 125 13.125 -13. 125 0.0

13. 125

-13. 125 ! for ! for !-for ! for ! for lateral gap lateral gap spring can bp stiffnesses bp stiffnesses Sn, 201, ! Support DGEH-2 n, 40, n, 41, n, 42, n, 43, n, 44, n, 45, n, 46, n, 47, n, 48, n, 49, n, 202, n, 203, -266.0, -266.0, -266.0, -266.0, -266.0, -266.0, -266.0, -266.0, -266.0, -266.0, -266.0, -266.0, ! Support DGEH-1 n, 50, n, 51, n, 52, n, 53, n, 54, n, 55, n, 56, n, 57, n, 58, n, 59, n,- 60, n, 61, n, 62, n, 63, n, 64, n, 65, -377.0, -349. 957, -338.0, -326.043, -306.0, -349. 957, -326.043, -377.0, -349.957, -338.0, -326.04 3, -306.0, -338.0, -349. 957, -326.;043, -338.0, 0.0, -30.5, -41.0, -30.5, 0.0, -30.5, -41.0, 0.0, 0.0, -30.5, -41.0, -41.0, -190.5, -190.5, -190.5, -190.5, -190.5, -190.5, -190.5, -190. 5, -190.5, -190.5, -190.5, -190.5, -190. 5, -190.5, -190. 5, -190.5, 13.125 13.125 13.125 0.0 -13.125 -13. 125 -13. 125

13. 125

-13. 125 0.0

13. 125

-13. 125 -11. 957 -11. 957 -11. 957 -11. 957 -11. 957 0.0 0.0

11. 957 11;957

11. 957

11. 957

.11. 957 -11. 957 0.0 0.0 11.957 ! for lateral gap ! for lateral gap ! for spring can ! for bp stiffnesses ! for bp stiffnesses ! for ! for ! for ! for lateral gap lateral gap lateral gap lateral gap V I in£U[n J. 1l Rev. I

Automated Engineering Services Corp. NO. C6 OF C16 / D XCCalculation Sheet JL REVISION NUMBER: 0 CLIENT: Nuclear Management Companm DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED

_, r

SUBJECT:

EDG Exhaust Evals CHEMCED: J Ad-. SAFETY RELATED YES [x1 NO [] CALC. NO.: MN03-P022637-100 n, 72, -338.0, n, 73, -349.957, n, 74, -326.043, rn, 75, -338.0, ! Reference Nodes -186.5, -186.5, -186.5, -186.5, -11.957 0.0 0.0 11.957 ! for vertical support ! for vertical support ! for vertical support ! for vertical support for Elbows n, 100, -305.0, -33.0, 0.0 n, 101, -371.0, -222.25, 0.0 ! Reference Nodes for Beams n, 102, -349.957, -180.5, -11.957 n, 103, -326.043, -180.5, 11.957 ! 22" Pipe mat, 1 type, 1 real, 1 EN, 1, 1, EN, 2, 2, EN, 3, 3, EN, 4, 4, ! 36" Pipe 2 3 4 5 real, 2 EN, 5, 5, 6 EN, 6, 6, 7 EN, 7, 7, 8 EN, 8, 8, 9 22 n Pipe real, 1 EN, 9, 9, 10 EN, 10, 10, 11 EN, 11, 11, 12 type, 2 real, 3 EN, 12, 12, 13, 100 type, 1 real, 1 EN, 13, 13, 14 Form 3.1-3 Rev. 1

Automated Engineering Services Corp. NO. C7 OFF C16 Calculation Sheet REVISION NUMBER: 0 CLIENT: Nuclear Management Companv DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:

SUBJECT:

EDG Exhaust Evals CHECKED: SAFETY RELATED YES FX3 NO F]CALC. NO.: .MN03-P022637-100 EN, 14, 14, 15 EN, 15, 15, 16 EN, 16, 16, 17 real, 4 EN, 17, 17, 18 EN, 18, 18, 19 type, 2 real, 5 EN, 19, 19, 20, 101 type, 1 real, 4 EN, 20, 20, 21 Support DGEH-3 mat, 2 real, 6 type, 13 en, 30, 30, 31, 3 en, 31, 31, 32, 3 en, 32, 31, 33, 3 en, 33, 33, 35, 3 en, 34, 34, 35, 3 en, 35, 35, 36, 3 ! Support DGEH-2 en, 40, 40, 41, 11 en, 41, 41, 42, 11 en, 42, 41, 43, 11 en, 43, 43, 45, 11 en, 44, 44, 45, 11 en, 45, 45, 46, 11 I Support DGEH-1 real, 7 en, 50, 50, 51, 102 en, 51,-51, 52, 102 en, 52, 52, 53, 102 en, 53, 53, 54, 102 en, 54, 55, 51, 102 en, 55, 58, 55, 102-en, 56, 53, 56, 103 en, 57, 56, 60, 103 Fonn 3.1-3 Rev. I

Automated Engineering'Services Corp. NO. C8 OF C16 / D XCCalculation Sheet ak REVISION NUMBER: 0 CLIENT: Nuclear Mana ementCompany DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:

SUBJECT:

EDG Exhaust Evals CHECKED: SAFETY RELATED YES [3 NO L CALC. NO.: MN03-P022637-100 en, 58, 58, 57, 103 en, 59, 59, 58, 103 en, 60, 60, 59, 103 en, 61,. 61, 60, 103 ! Gap Elements mat, 3 type, 3 real, 15 en, 70, 3, 37 en, 71, 3, 38 en, 72, 11, 47 en, 73, 11, 48 type, 6 real, 8 en, 74, 37, 30 en, 75, 34, 38 en, 76, 47, 40 en, 77, 44, 48 type, 3 real, 15 en, 78, 18, 62 en, 79, 18, 63 en, 80, 18, 64 en, 81, 18, 65 type, 6 real, 12 en, 82, 52, 62 en, 85, 65, 59 type, 5 real, 19 en, 83, 63, 55 en, 84, 56, 64 Spring Elements type, 3 real, 15 en, 86, 3, 39 en, 87, 11, 49 type, 14 real, 25 en, 88, 39, 33, 39, 33 real, 26 Form 3.1-3 Rev. I

Automated Engineering Services Corp. NO. C9 OF C16 Calculation Sheet REVISION NUMBER: 0 CLIENT: Nuclear Mana ement Company DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED: A4970

SUBJECT:

EDG Exhaust Evals CHECKED: VAd SAFETY RELATED YES [i] NO [ CALC. NO.: MN03-P022637-100 en, 89, 49, 43, 49, 43 Bellows type, 7 real, 14 en, 94, 21, 22 type, 8 real, 20 en, 95, 21, 22 type, 9 real, 21 en, 96, 21, 22 type, 10 real, 22 en, 97, 21, 22 type, 11 real, 23 en, 98, 21, 22 type, 12 real, 24 en, 99, 21, 22 ! Add Weights type, 4 real, 10 en, 100, 4 en, 101, 10 real, 11 en, 102, 21 Baseplate Stiffnesses type, 10 real, 18 en, 200, 32, 200 en, 203, 36, 201 en, 205, 42, 202 en, 208, 46, 203 type, 12 real, 17 en, 201, 32, 200 en, 204, 36, 201 en, 206, 42, 202 Form 3.1-3 Rev. I

Automated Engineering Services Corp. NO. CIO FOF C16 Calculation Sheet /J/ REVISION NUMBER: 0 CLIENT: Nuclear Mana ement Companv DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:

SUBJECT:

EDG Exhaust Evals CHECKED: SAFETY RELATED YES N NO []1 CALC. NO.: MN03-P022637-100 en, 209, 46, 203 ! Lugs type, 3 real, 15 en, 220, 18, 72 en, 221, 18, 73 en, 222, 18, 74 en, 223, 18, 75

type, 15 real, 27 en; 224, 72, 52 en, 225, 73, 55 en, 226, 74, 56 en, 227, 75, 59 Boundary Conditions d, 22, all, 0.0 d, 32, ux, 0.0,,

,, uy, uz, roty d, 36, ux, 0.0,, ,, uy, uz, roty d, 42, ux, 0.0,, , uy, uz, roty d, 46, ux, 0.0,, , uy, uz, roty d, 50, all, 0.0 d, 54, ux,'00.r. uy, UZ d, 57, all, 0.0 d, 61, ux, 0.0, ,,, uy, uz d, 200, all, 0.0, , 203 nlist, all mplist, all etlist,.all rlist, all elist, all tblist, all, all finish /solu antype, trans, new solcontrol, on timint, off nlgeom, off outres, all, all time, 1.0 nsubst, 1000, 10, 10000 Form 3.1-3 Rev. I

A Automated Engineering Services Corp. No. C1 I OF C16 Calculation Sheet L/ REVISION NUMBER: 0 CLIENT: Nuclear Management Comany DATE: 03/07/03 PROJECT: Monticelio Nuclear Generating Plant PREPARED:

SUBJECT:

EDG Exhaust Evals CHECKED: J SAFETY RELATED YES 3 No ] CALC NO.: MN03-P022637-100 ! Apply Gravity Force acel, 0.0, 386.4, 0. solve time, 2.0 nsubst, 1000, 10, 10000 Apply Gravity Force acel, 0.0, 386.4, 0. Apply Tornado Load wind - 300 pressure - (0.4*0.002558*wind**2)/144 pressw4 - (2.04*0.002558*wind**2)/144 esel, s, elem,, 12, 16 sfe, all, 2, pres,, 22*pressure esel, s, elem,, 30, 33 esel, a, elem,, 40, 43 sfbeam, all, 2, pres, 4*pressw4, 4*pressw4 esel, s, elem,, 34, 35 esel, a, elem,, 44, 45 sfbeam, all, 2, pres, -4*pressw4, -4*pressw4 esel, all solve finish /postl file, north, rst set, 1, last Nodal Displacements prnsol, u Reaction Forces prrsol set, 2, last ! Nodal Displacements prnsol, u Pipe Forces Form 3.1-3 Rev. I Form 3.1-3 Rev. I

Automated Engineering Services Corp. NO C12 l OF C16 Calculation Sheet LJL REVISION NUMBERZ 0 CLIENT: Nuclear Management Comnan-DATE: 03/07/03 PROJECT: Monticello Nuclear Generatin Plant PREPARED:

SUBJECT:

EDG Exhaust Evals CHECKED: Jvi. SAFETY RELATED YES [F NO 2 CALC. NO.: MN03-P022637-100 esel, s, type,, 1, 2 etable, xfori, smisc, 1 etable, yfori, smisc, 2 etable, zfori, smisc, 3 etable, xmomi, smisc, 4 etable, ymomi, smisc, 5 etable, zmomi, smisc, 6 etable, xforj, smisc, 7 etable, yforj, smisc, 8 etable, zforj, smisc, 9 etable, xmomj, smisc, 10 etable, ymomj, smisc, 11 etable, zmomj, smisc, 12 pretab, xfori, yfori, zfori, pretab, xforj, yforj, zforj, Support DGEH W4 x 13 Plastic Strains esel, s, elem,, 30, 35 etable, plstrl, leppl, 1

etable, plstr2, leppl, 2

etable, plstr3, leppl, 3 etable, *plstr4, leppl, 4

etable, plstr5, leppl, 5

etable, plstr6, leppl, 6

etable, plstr7, leppl, 7

etable, plstr2l, leppl, 21 etable, plstr22, leppl, 22 etable, plstr23, leppl, *23 etable, plstr24, leppl, 24 etable, plstr25, leppl, 25 etable, plstr26, leppl, 26 etable, plstr27, leppl, 27 Element Forces

etable, xfori,

smisc, 1

etable, yfori,

smisc, 2

etable, zfori,

smisc, 3

etable, xmomi, smisc, 4

etable, ymomi,

smisc, 5

etable, zmomi,

smisc, 6

xmomi, ymomi, zmomi

xmomj, ymomj, zmomj Form 3.1-3 Rev. 1 Form 3.1-3 ReV. I

a Automated Engineering Seces Corp.NO. C3 Calculation Sheet REVISION NUMBER: 0 CLIENT: Nuclear Management Company DATEM 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:

SUBJECT:

EDI Exhaust Evals CHECKED: J V4-SAFETY RELATED YES NO [ CAMC. NO.: ._M MN03-P022637-100

etable, xforj,

smisc, 7

etable, yforj,

smisc, 8

etable, zforj,

smisc, 9

etable, xmomj, smisc,.10

etable, ymomj, smisc, 11

etable, zmomj, smisc, 12

! Element Axial Stresses I

etable, etable,

etable, etable,

etable, etable,

etable, etable,

etable, etable,

etable, etable,

etable, etable,

pretab, pretab,

pretab, pretab,

pretab, pretab,

axstrI, axstr2,

axstr3, axstr4,

axstrS, axstr6,

axstr7, axstr21,

axstr22, axstr23,

axstr24, axstr25,

axstr26, axstr27,

plstrl, plstr2l,

xfori, xforj,

axstrl, axstr2l, is, 1

Is, 2 is, 3 Is, 4 is, 5 Is, 6 Is, 7 is, 21 is, 22 Is, 23 Is, 24 is, 25 is, 26 is, 27

plstr2, plstr3, plstr22, plstr23,

yfori, zfori,

yforj, zforj,

axstr2, axstr3, axstr22, axstr23,

plstr4, plstr24,

xmomi, xmomj,

axstr4, axstr24,

plstr5, plstr25,

ymomi, ymomj,

axstr5, axstr25,

plstr6, plstr7 plstr26, plstr27 zmomi zmomj

axstr6, axstr7 axstr26, axstr27

! Support DGEH-2-- W4 x 13 ! Plastic Strains I esel, s,

etable, etable,

etable, etable,

etable, etable,

etable, etable,

etable, etable,

,elem,

plstrl, plstr2,

plstr3, plstr4,

plstr5, plstr6,

plstr7, plstr2l,

plstr22, plstr23, 40, 45

leppl, 1

leppl, 2

leppl, 3

leppl, 4

leppl, 5

leppl, 6

leppl, 7

Ieppl, 21 leppl, 22 leppl, 23 Form 3.1-3 Rev. I

Automated Engineering Services Corp. NO. C14 l OF C16 Calculation Sheet REVISION NUMBER: 0 CLIENT: Nuclear Management Company DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED: 7

SUBJECT:

EDG Exhaust Evals CHECKED: J 4 SAFETY RELATED YES [Ii NO CALC. NO.: MN03-P022637-100 etable, plstr24, etable, plstr25, etable, plstr26, etable, plstr27, ! Element Forces

leppl, leppl,

leppl, leppl, 24 25 26 27

etable, etable,

etable, etable,

etable, etable,

etable, etable,

etable, etable,

etable, etable,

!tbe

xfori, yfori,

zfori, xmomi,

ymomi, zmomi,

xforj, yforj,

zforj, xmomj,

ymomj, zmomj,

smisc, 1

smisc, 2

smisc, 3

smisc, 4

smisc, 5

smisc, 6

smisc, 7

smisc, 8

smisc, 9

smisc, 10 smisc, 11 smisc, 12 ! Element Axial Stresses

etable, etable,

etable, etable,

etable, etable,

etable, etable,

etable, etable,

etable, etable,-

etable, -

etable, etable,

axstrl, axstr2,

axstr3, axstr4,

axstr5, axstr6,

axstr7, axstr2l,

axstr22, axstr23,

axstr24, axstr25,

axstr26, axstr27, is, is, is, is, 4

is, is, 0 is, is, 2 is, 2 Is, 2. Is, 24 is, 2! is, 2( is, 27

plstr2, plstr22,

yfori, yforj,

axstr2, axstr22,

pretab, plstrl, pretab, plstr2l,

pretab, xfori,

pretab, xforj,

pretab, axstrl, pretab, axstr2l,

! Support DGEH-1

plstr3, plstr23,

zfori, zforj,

axstr3, axstr23,

plstr4, plstr24,

xnomi, xmomj,

axstr4, axstr24,

plstr5, plstr25,

ymomi, ymomj,

axstr5, axstr.25,

plstr6, plstr26,

- zmomi zmomj

axstr6, axstr26, plstr7 plstr27 axstr7 axstr27 C4 x 5.4 Form 3.1-3 Rev.1 Fonin 3. 1-3 Rev. I

Automated Engineering Services Corp. NO. C15 OF C16 Calculation Sheet REVISION NUMBER: 0 CLIENT: Nuclear Manaaement Company DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:

SUBJECT:

EDG Exhaust Evals CHECKCED: J SAFETY RELATED YES [Rj NO 2 CALC. NO.: MN03-P022637-100 ! Plastic Strains esel, s,

etable, etable,

etable, etable,

etable, etable,

etable, etable,

, elem,,

plstrl, plstr2,

plstr3, plstr4,

plstr2l, plstr22,

plstr23, plstr24, 50, 61

leppl, leppl,

leppl, leppl,

leppl, leppl,

leppl, leppl, 1

2 3 4 21 22 23 24 ! Element Forces . etable,

etable, etable,

etable, etable,

etable, etable,

etable, etable,

etable, etable,

etable, xfori,

yfori, zfori,

xmomi, ymomi,

zmomi, xforj,

yforj, zforj,

xmomjj, ymomj,

zmomj, smisc, 1

smisc, 2

smisc, 3

smisc, 4

smisc, 5

smisc, 6

smisc, 7

smisc, 8

smisc, 9

smisc, 10 smisc, 11 smisc, 12 Element Axial Stresses

etable, axstrl, Is,

etable, axstr2, Is,

etable, axstr3, ls,

etable, axstr4, ls, etable, axstr2l, ls, etable, axstr22, ls, etable, axstr23, ls, etable, axstr24, ls,

pretab, pastr2,

plstr2, pretab, plstr2l, plstr22,

pretab, xfori,

yfori, pretab,

xforj, yforj,

pretab, axstrl,

axstr2, pretab, axstr2l, axstr22, Loads on Lugs 1

2 3 4 21 22 23 24 , plstr3, ,plstr23,

zfori, zforj,

axstr3,

, axstr23, plstr4 plstr24

xmomi, xmomj, axstr4 axstr24

ymomi, zmomi

ymomj, zmom; Form 3.1-3 Rev. I Fonn 3.1-3 Rev. I

a Automated Engineering Services Corp. NO. C16 l OF C16 Calculation Sheet REVISION NUMBER.0 CLIENT: Nuclear Management ComDany DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:,44 '

SUBJECT:

EDO Exhaust Evals CHECKED:.)\\ SAFETY RELATED YES i NO [ CALC. NO.: MN03-P022637-100 esel, s, elem,, 224, 227 etable, lugforce, smisc, 1 pretab, lugforce ! Forces in Spring Cans esel, s, elem,, 88, 89 etable, spforce, smisc, 1 etable, preload, smisc, 2

etable, elstat, nmisc, 1 pretab, spforce, preload, elstat esel, all Reaction Loads prrsol finish r

Form 3.1-3 Rev. I For

3. 1-3 Rev. I

Automated Engineering Services Corp.NO. DI OF D5 Calculation Sheet / REVISION NUMBER: 0 CLIENT: Nuclear Management Company DATE: 03/07/03 PROJECT: MonticelloNuclearGeneratingPlant PREPARED: AMP

SUBJECT:

EDG Exhaust Evals CHECKED: SAFETY RELATED YES [i NO CALC. NO.: MN03-P022637-100 Attachment D ANSYS Input Listing for Support DGEH-1 with South Tornado Wind Form 3.1-3 Rev. 1

Automated Engineering Services Corp. NO. D3 OF D5 Calculation Sheet REVISION NUMBER: 0 CLIENT: Nuclear Management Comnanv DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED: rl

SUBJECT:

EDG Exhaust Evals CHECKED: J 4 SAFETY RELATED YES Ja] NO CALC. NO.: MN03-P022637-100 n, 102, -349.957, -180.5, -11.957 n, 103, -326.043, -180.5, 11.957 ! Support DGEH-1

mat, 2

type, 13 real, 7 en, 50, 50, 51, 102 en, 51, 51,' 52, 102 en, 52, 52, 53, 102 en, 53, 53, 54, 102 en, 54, 55, 51, 102 en, 55, 58, 55, 102 en, 56, 53, 56, 103 en, 57, 56, 60, 103 en, 58, 58, 57, 103 en, 59, 59, 58, 103 en, 60, 60, 59, 103 en, 61, 61, 60, 103 Boundary Conditions d,

50, all, 0.0 d, 54, ux, 0.0, , uy, uz d, 57, all, 0.0 d, 61, ux, 0.0,, , uy, uz nlist, all mplist, all etlist, all rlist, all

elist, all tblist, all, all finish

/solu antype, static, new time, 1.0 f, 55, fx, -2035.0 f, 55, fy, -3602.0 solve finish /postl file, dgehl, rst set, 1 Form 3.1-3 Rev. I

Automated Engineering Services Corp. NO. D2 OF D5 / D D Calculaffon Sheet. / Calulao SREVISION NUMBER: 0 CLEIET: Nuclear Manaetment Comanv DATE: 03/07/03 PROJECT: Monticello Nuclear Generatina Plant PREPARED:

SUBJECT:

EDG Exhaust Evals -CHECKED: I 4 SAFETY RELATED YES E NO L CALC NO.: _MN03-P022637-100 /filnam, dgehl /title, Support DGEH-1 for South Units are pounds and inches /prep7 tref, '0.0 ! Material 2 - A-36 mp, ex, 2, 29000000. mp, nuxy, 2, 0.3 mp, dens, 2, 490/1728/386.4 tb, bkin, 2, 1 tbtemp, 0.0 tbdata, 1, 36000.0, 0.0 ! element types Blowing Wind et, 13, beam24 keyopt, 13, 1, 1 ! non-linear beam ! Member Properties r, 7,

rmore, 1.127, 1.852,

-0.365, -1.852, 0.0, -0.365, 0;184, 1.127, 1.852, 0.296 -1.852, 0.296 ! C4 x 5.4 csys, 0 ! Support DGEH-1 n, 50, -377.0, n, 51, -349.957, n, 52, -338.0, n, 53, -326.043, n, 54, -306.0, n, 55, -349.957, n, 56, -326.043, n, 57, -377.0, n, 58, -349.957, n, 59, -338.0, n, 60, -326.043, n, 61, -306.0, -190.5, -11.957 -190.5, -11.957 -190.5, -11.957 -190.5, -11.957 -190.5, -11.957 -190.5, 0.0 -190.5, . 0.0 -190.5, 11.957 -190.5, 11.957 -190.5, 11.957 -190.5, 11.957 -190.5, 11.957 ! Reference Nodes for Beams Form 3.1-3 Rev. 1 Formn3.1-3 Rev. I

Automated Engineering Services Corp. NQID4 OF D5 / D CCalculation Sheet REVISION NUMBER: 0 CLIENT: Nuclear Management CoMnany DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED:

SUBJECT:

EDG Exhaust Evals CHECKED:. SAFETY RELATED YES x3 NO F CALC. NO.: MN03-P02263 7-1 00 Support DGEH C4 x 5.4 ! Plastic Strains esel, s, elem,, 50, 61 etable, plstrl, leppl, 1

etable, plstr2, leppl, 2

etable, plstr3, leppl, 3

etable, plstr4, leppl, 4

etable, plstr2l, leppl, 21 etable, plstr22, leppl, 22 etable, plstr23, leppl, 23 etable, plstr24, leppl, 24 ! Element Forces

etable, etable,

etable, etable,

etable, etable,

etable, etable,

etable, etable,

etable, etable,

!tbe

xfori, yfori,

zfori, xmomi,

ymomi, zmomi,

xforj, yforj,

zforj, xmomj,

ymomj, zmomj,

smisc, smisc,

smisc, smisc,

smisc, smisc,

smisc, smisc,

smisc, smisc,

smisc, smisc, 10 2

3 4 5 6 7 8 9 10 11 12 ! Element Axial Stresses

etable, etable,

etable, etable,

etable, etable,

etable, etable,

pretab, pretab,

pretab, pretab,

pretab, axstrl,

axstr2, axstr3,

axstr4, axstr2l,

axstr22, axstr23,

axstr24, plstrl,

plstr2l, xfori, xforj,-

axstrl, ls, 1

ls, 2 ls, 3 ls, 4 - ls, 21 ls, 22 ls, 23 ls, 24

plstr2, plstr3, plstr22, plstr23,

yfori, zfori,

yforj, zforj,

axstr2, axstr3, plstr4 plstr24

xmomi, xmomj, axstr4

ymomi, zmomi

ymomj, zmomj Form 3.1-3 Rev. 1

a Automated Engineering Services Corp. D l Calculation Sheet k REVISION NUMBER: 0 CLIENT: Nuclear Management Comanv DATE: 03/07/03 PROJECT: Monticello Nuclear Generating Plant PREPARED: 70

SUBJECT:

EDG Exhaust Evals CHECKED: Jid4-SAFETY RELATED YES FX3 NO [] CALC. NO.: MN03-P022637-100 pretab, axstr2l, axstr22, axstr23, axstr24 esel, all ! Reaction Loads prrsol finish Form 3.1-3 Rev. I Form 3. 1-3 Rev. I

File No. MN03-P022637-100 4h kwe AdA-I I W E L C 0 M E T 0 T K E A N S Y S I P R O G R A M ANSYS 5.7 NOTICES

• Copyright 2000 SAS IP, Inc. All rights reserved.
• Unpublished---rights reserved under the Copyright Laws of
• the United States.

I 1 PrCFW~c At _S ^,\\--'y .1:.' x

• i
• U.S. GOVERNMENT RIGHTS Use, duplication, or disclosure by the U.S.

Government is subject to restrictions set forth in the ANSYS, Inc. license-agreement and as provided in DFARS 227.7202-1(a) and 227.7202-3(a)(1995), DFARS 252.227-7013(c)(1)(ii) (OCT 1988), FAR 12.212(a)(1995), FAR 52.227-19, or FAR52.227-14 (ALT III), as applicable. ANSYS, Inc.

• THIS SOFTWARE CONTAINS CONFIDENTIAL INFORMATION AND TRADE
• SECRETS OF SAS IP, INC.

USE DISCLOSURE, OR REPRODUCTION

• IS PROHIBITED WITHOUT THE PRiOR EXPRESS WRITTEN PERMISSION
• OF SAS IP, INC.
• The Program also contains the following licensed software:
• PCGLSS: Linear Equations Solver
• (C) Copyright 1992-1995 Computational Applications and System Integration Inc.
• All Riahts Reserved.
• CA&SI, Ph Fax 2004 S. Wright Street, Urbana, IL 61821 (217)244-7875 (217)244-7874
• CA&SI DOES NOT GUARANTEE THE CORRECTNESS OR USEFULNESS OF
• THE RESULTS OBTAINED USING PCGLSS. CA&SI IS NOT LIABLE FOR *
• ANY CONCLUSIONS OR ACTIONS BASED ON THE RESULTS. IT IS THE *
• RESPONSIBILITY OF THE USER TO CONFIRM THE ACCURACY AND
• USEFULNESS OF THE RESULTS.

Completing ANSYS Load Process. ANSYS/Mechanical U

• '4**

ANSYS COMMAND LINE ARGUMENTS INITIAL JOBNAME file BATCH MODE REQUESTED LIST 00251976 VERSION-INTEL NT RELEASE-5.7.1 UP20010418 CURRENT JOBNAME-file 21:40:09 MAR 06, 2003 CP-0.150 1 /filnam, exhaust 2 /title, EDG Exhaust Piping Page El

File No. MN03-P022637-100 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19. 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 65 66 67 68 69 70 71 72 73 I Units are pounds and inches /prep7 tref, 0.0 I Material Properties ! Material 1 - A-106 GR. B mp, ex, 1, 27900000. mp, nuxy, 1, 0.3 mp, dens, 1, 490/1728/386.4 I Material 2 - A-36 mp, ex, 2, 29000000. mp, nuxy, 2, 0.3 mp, dens, 2, 490/1728/386.4 tb, bkin, 2, 1 tbtemp, 0.0 tbdata, 1, 36000.0, 0.0 Material 3 - rigid mp, ex, 3, 29000000. mp, nuxy, 3, 0.3 mp, dens, 3, 0.0 ! element types et, 1, pipel6 et, 2, pipel8 et, 3, beam4 et, 4, mass2l keyopt, 4, 3, 2 et, 5, combin40 keyopt, 5, 3, 0 et, 6, combin40 keyopt, 6, 3, 3 et, 7, combinl4 keyopt, 7, 2, 1 et, 8, combinl4 keyopt, 8, 2, 2 et, 9, combinl4

keyopt, 9,

2, 3 et, 10, combinl4 keyopt, 10, 2, 4 et, 11, combinl4 keyopt, 11, 2, 5 et, 12, combinl4 keyopt, 12, 2, 6 et, 13, beam24 keyopt, 13, 1, 1 et, 14, combin37 keyopt, 14, 2, 2 keyopt, 14, 3, 2 keyopt, 14, 4, 1 et, 15, linklO keyopt, 15, 3, 1 I Member Propertie r, 1, 22.00, r, 2, 36.00, r, 3, 22.00,

rmore, f

r, 4, 22.00,

rmore, 0.007/386 r, 5, 22.00, 0

rmore, 0.

! Gap Element in t ! Gap Element in I ! Spring Element i ! Spring Element ! Spring Element ! Spring Element i ! Spring Element i ! Spring Element i I non-linear beam I Spring Can the x-direction the z-direction Ln the x-direction in the y-direction in the z-direction in the x-rotation in the y-rotation in the z-rotation I s 0.375 0.350 0.375, 33.0, 4.02, 0.375. .4, 3.0 .375, 33.0, 4.02, 007/386.4, 3.0, Page E2 4.02, 15.588 , 15.588 4.02, 15.588 , 15.588 I 22" Pipe 1 36" Pipe ! Elbow ! 22" Pipe w/ insul ! Elbow w/ insul

File No. MN03-P022637-100 74 r, 6, -2.0 75 rmore, 0. 76 rmore, -2.0 77

rmore, 2.0 78 r, 7, 1.12' 79

rmore,

-0.36, 80 r, 8, 0.' 81 r, 10, 155.1 82 r, 11, 230.1 83 r, 12, 0.1 84 r, 13, l.OE1l 85 r, 14, 10.t 86 r, 15, 100.4 87

rmore, 0.00O 88 r, 17, 6.6E6 Stiffness 89 r, 18, 5.8E6 Stiffness 90 r, 19, 0.C 91 r, 20, 10.a 92 r, 21, lO.C 93 r, 22, 10.a 94 r, 23, l0.C 95 r, 24, 10.C 96 r, 25, 363.0, 97 r, 26, 363.0, 98 r, 27, 1.5 99 100 csys, 0 101 102

! 22" Pipe 103 104 n, 1, 0 105 n, 2, -37 106 n, 3, -74 107 n, 4, -96 108 n, 5, -100 109 110 ! 36" Pipe 111! 112 n, 6, -135. 113 n, 7, -170. 114 n, 8, -205. 115 n, 9, -241 116 117 ! 22" Pipe 118 119 n, 10, -245 120 n, 11, -266 121 n, 12, -305 122 n, 13, -338 123 n, 14, -338 124 n, 15, -338 125 n, 16, -338 126 n, 17, -338 127 n, 18, -338 128 n, 19, -338 129 n, 20, -371 130 n, 21, -394 131 n, 22, -394 .132 133 ! Support DGEH-134 135 n, 30, -74 136 n, 31, -74, 137 n, 32, -74, 138 n, 33, -74 139 n, 34, -74, 140 n, 35, -74. 141 n, 36, -74. 142 n, 37, -74. 3, 1.9 0, 1.9w 3, -1.9i 3, -1.91 7, 1.1 5, -1.I 0, I 0/386.4 0/386.4

075, 075,

075, 075,

352, 352, 0.0, 0.0,.

0.0, 0.345, 0.345 0.0, 0.184, 0.0, 2.03, 0.0, 0.0, -0.365, 1.127, 0.125,

1. 9075,

-1.9075, -1. 9075, 1.852, -1.852, 0.345 0.280 0.0 ! W4 x 13 0.296 ! C4 x 5.4 0.296 0, 0, 0, 2, 0.0, 0.0, 0.5, 0.0, l.OE10 I Gap Element ! Flange Weight !Flange Weight 0.0, 1.OE10 ! Gap Element ! Rigid Stiffness I Bellows Stiffness 1.0 ! Rigid Beam 1000.0, 1000.0, 1000.0 1.0, 1 Kz Rotational ! Kx Rotational 0.0, 0.0, 0.5, 0.0, 1.OE10 ! Gap Element ! Bellows Stiffness !Bellows Stiffness I Bellows Stiffness ! Bellows Stiffness I Bellows Stiffness 0.0, 0.0, 0.375, -10, 1515.0 ! DGEH-3 0.0, 0.0, 1.250, -10, 1832.0 ! DGEH-2 '.0

.0 5.0 i.0

. 0 25 50 75 .0 .0 .0 .0, .0, .0, .0O, .0O, .04 .0, .0, .01 .00 -3 I I I
FFFII 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, -33.0, -66.25, -99.5, -132.75, -166.0, -190.5, -222.25, -255.25, -255.25, -255.25, 0.0, -30.5, -41.0, -30.5, 0.0, -30.5, -41.0, 0.0, 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 .0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 13.125 13.125 13.125 0.0 -13.125 -13.125 -13.125 13.125 .0O, .0, .0, .0O, .0, .0O, 0, 0, ! for bellows stiffnesses ! for lateral gap Page E3

File No. MN03-P022637-100 143 144 145 146 147 148 149 150 151 152 153 154 155 156 157 158 159 160 161 162 163 164 165 166 167 168 169 170 171 172 173 174 175 176 177 178 179 180 181 182 183 184 185 186 187 188 189 190 191 192 193 194 195 196 197 198 199 200 201 202 203 204 205 206 207 208 209 210 211 212 213 n, n, 38, 39,

200, 201,

-74.0, -74.0, -74.0, -74.0, Support DGEH-2 n, 40, -266.0, n, 41, -266.0, n, 42, -266.0, n, 43, -266.0, n, 44, -266.0, n, 45, -266.0, n, 46, -266.0, n, 47, -266.0, n, 48, -266.0, n, 49, -266.0, n, 202, -266.0, n, 203, -266.0, Support DGEH-1 n, 50, -377.0,- n, 51, -349.957, n, 52, -338.0, n, 53, -326.043, n, 54, -306.0, n, 55, -349.957, n, 56, -326.043, n, 57, -377.0, n, 58, -349.957, n, 59, -338.0, n, 60, -326.043, n, 61, -306.0, n, 62, -338.0, 0.0, -30.5, -41.0, -41.0, 0.0, -30.5, -41.0, -30.5, 0.0, -30.5, -41.0, 0.0, 0.0, -30.5, -41.0, -41.0, -190.5, -190.5, -190.5, -190.5, -190.5, -190.5, -190.5, -190.5, -190.5, -190.5, -190.5, -190.5, -190.5, -13.125 0.0 13.125 -13.125 13.125 13.125

13. 125 0.0

-13.125 -13.125 -13.125 13.125 -13.125 0.0 13.125 -13.125 -11. 957 -11. 957 -11.957 -11.957 -11. 957 0.0 0.0 11.957

11. 957

11. 957

11. 957 11.957

-11.957 0.0 0.0

11. 957

-11. 957 0.0 0.0 11.957 ! for lateral gap ! for spring can ! for bp stiffnesses ! for bp stiffnesses ! for !for I for ! for !for ! for ! for ! for !for !for ! for I for ! for lateral gap lateral gap spring can bp stiffnesses bp stiffnesses lateral gap lateral gap lateral gap lateral gap vertical support vertical support vertical support vertical support n, 63, -349.957, -190.5, n, 64, -326.043, -190.5, n, 65, -338.0, -190.5, n, 72, -338.0, -186.5, n, 73, -349.957, -186.5, n, 74, -326.043, -186.5, n, 75, -338.0, -186.5, Reference Nodes for Elbow, n, 100, -305.0, -33.0, n, 101, -371.0, -222.25, ! Reference Nodes for Beams 0.0 0.0 n, 102, -349.957, n, 103, -326.043, ! 22" Pipe mat, 1 type, 1 real, l EN, 1, 1, 2 EN, 2, 2, 3 EN, 3, 3, 4 EN, 4, 4, 5 3 ! 36" Pipe -180.5, -11.957. -180.5, 11.957

real, EN, EN, EN, EN, 2

5, 5, 6, 6, 7, 7, 8, .8, 6 7 8 9 Page E4

File No. !4N03-P022631-100 214 122" Pipe 215 216 real, 1 217 EN, 9, 9, 10 216 EN, 10, 10, 11 219 EN, 11, 11, 12 220 type, 2 221 real, 3 222 EN, 12, 12, 13, 100 223 type, 1 224 real, I1 225 EN,- 13, 13, 14 226 *EN, 14, 14, 15 227 EN, 15, 15, 16 228 EN, 16, 16, 17 229 real, 4 230 EN, 17, 17, 18 231 EN, 18, 18, 19 232 type, 2 233 real, 5 234 EN, 19, 19,.20, 101 235 type, 1 236 real, 4 237 EN, 20, 20, 21 238 239 ! Support DGEH-3 240 241 mat, 2 242 real, 6 243 type, 13 244 en, 30, 30, 31, 3 245 en, 31, 31, 32, 3 246 en, 32, 31, .33, 3 247 en, 33, 33, 35, 3 248 en, 34, 34, 35, 3 249-en, 35, 35, 36, 3 250 1 251 ! Support DGEH-2 252 253 en, 40, 40, 41, 11 254 en, 41, 41, .42, 11 255 en, 42, 41, 43, 11 256 en, 43, 43, 45, 11 257 en, 44, 44, 45, 11 258 en, 45, 45, 46, 11 259 1 260 ! Support DGEH-l1 .261 262 real, 7 263 en, 50, 56, 61, 102 264 en, 51, 51, 52, 102 265 en, 52, 52, 53, 102 266 en, 53, 53, 54, 102 267 en,. 54, 55, 51, 102 268 en, 55, 56, 55, 102 269 en, 56, 53, 56, 103 270 en, 57, 56, 60, 103 271 en, 58, 58, 57, 103 272 en, 59, 59, 58, 103 273 en, 60, 60, 59, 103 274 en, 61, 61, 60, 103 275 I 276 ! Gap Elements 277 I 278 mat, 3 279 type, 3 280

real, 15 281 en, 70, 3, 37 282-en, 71, 3, 38 283 en, 72, 11, 47 284 en, 73, 11,.48 Page ES

File No. MN03-P022637-100 285 type,,6 286 real, 8 287 en, 74, 37, 30 288 en, 75, 34, 38 289 en, 76, 47, 40 290 en, 77, 44, 48 291 type, 3 292 real, 15 293 en, 78, 18, 62 294 en, 79, 18, 63 295 en, 80, 18, 64 296 en, 81, 18, 65 297 type, 6 298 real, 12 299 en, 82, 52, 62 300 en, 85, 65, 59 301 type, 5 302 real, 19 303 en, 83, 63, 55 304 en, 84, 56, 64 305 306 1 Spring Elements 307 1 308 type, 3 309 real, 15 310 en, 86, 3, 39 311 en, 87, 11, 49 312 type, 14 313 real, 25 314 en, 88, 39, 33, 39, 33 315 real, 26 316 en, 89, 49, 43, 49, 43 317 318 ! Bellows 319 320 type, 7 321 real, 14 322, en, 94, 21, 22 323 type, 8 324 real, 20 325 en, 95, 21, 22 326 type, 9 327 real, 21 328 en, 96, 21, 22 329 type, 10 330 real, 22 331 en, 97, 21, 22 332 type, 11 333 real, 23 334 en, 98, 21, 22 335 type, 12 336 real, 24 337 en, 99, 21, 22 .338 339 ! Add Weights 340 341 type, 4 342 real, 10 343 en, 100, 4 344 en, 101, 10 345 real, 11 346 en, 102, 21 347 348 1 Baseplate Stiffnesses 349 350 type, 10 351 real, 18 352 en, 200, 32, 200 353 en, 203, 36, 201 354 en, 205, 42, 202 355 en, 208, 46, 203 Page E6

File No. MN03-P022637-100 356 type, 12 357 real, 17 358 en, 201, 32, 200 359 en, 204, 36, 201 360 en, 206, 42, 202 361 en, 209, 46, 203 362 363 ! Lugs 364 365 type, 3 366 real, 15 367 en, 220, 18, 72 368 en, 221, 18, 73 369 en, 222, 18, 74 370 en, 223, 18, 75 37.1 type, 15 372 real, 27 373 en, 224, 72, 52 374 en, 225, 73, 55 375 en, 226, 74, 56 376 en, 227, 75, 59 377 3 378 ! Boundary Conditions 379 380 d, 22, all, 0.0 381 d, 32, ux, 0.0,... 382 d, 36, ux, 0.0,... 383 d, 42, ux, 0.0,... 384 d, 46, ux, 0.0,... 385. d, 50, all, 0.0 386 d, 54, ux, 0.0,... 387 d, 57, all, 0.0 388 d, 61, ux, 0.0,... 389 d, 200, all, 0.0,, 203 390 nlist, all 391 mplist, all 392 etlist, all 393 rlist, all 394 elist, all 395 tblist, all, all 396 finish 397 /solu 398 antype, trans, new 399 solcontrol, on 400 timint, off 401 nlgeom, off 402 outres, all, all 403 time, 1.0 404 nsubst, 1000, 10, 10000 405 406 1 Apply Gravity Force 407 408 acel, 0.0, 386.4, 0. 409 solve 410 time, 2.0 411 nsubst, 1000, 10, 10000 412 413 ! Apply Gravity Force 414 415 acel, 0.0, 386.4, 0. 416 417 ! Apply Tornado Load 418 4i9 wind - 300 420 pressure - (0.40*0.00255 421 pressw4 - (1.81*0.002558 422 esel, s, elem,, 1, 4 423 esel, a, elem,, 9, 16 424 sfe, all, 4, pres,, 22* 425 esel, a, elem,, 5, 8 426 sfe, all, 4, pres,, 36* uy, uz, roty uy, uz, roty uy, uz, roty uy, uz, roty uy, uz uy, uz 58*wind**2)/144

• wind**2)/144 pressure pressure Page E7

File No. MN03-P022637-100 427 esel, s, elem,, 30, 31 428 esel, a, elem,, 40, 41 429 sfbeam, all, 1, pres, 4*pre 430 esel, s, elem,, 34, 35 431 esel, a, elem,, 44, 45 432 sfbeam, all, 1, pres, -4*pr 433 esel, all 434 solve 435 finish 436 /postl 437 file, exhaust, rst 438 set, 1, last 439 440 1 Nodal Displacements 441 442 prnsol, u 443 1 444 ! Reaction Forces 445 446 prrsol 447 set, 2, last 448 I 449 ! Nodal Displacements 450 451 prnsol, u 452 453 ! Pipe Forces 454 455 esel, s, type,, 1, 2 456 etable, xfori, smisc, 1 457 etable, yfori, smisc; 2 458 etable, zfori, smisc, 3 459 etable, xmomi, smisc, 4 460 etable, ymomi, smisc, 5 461 etable, zmomi, smisc, 6 462 etable, xforj, smisc, 7 463 etable, yforj, smisc, 8 464 etable, zforj, smisc, 9 465 etable, xomaj, smisc, 10 466 etable, ymomj, smisc, 11 467 etable, zmomj, smisc, 12 468 pretab, xfori, yfori, zfori 469 pretab, xforj, yforj, zforj 470 471 ! Support DGEH W4 x 13 472 1 473 ! Plastic Strains 474 475 esel, s, elem,, 30, 35 - 476 etable, plstrl, leppl, 1 477

etable, plstr2, leppl, 2

478

etable, plstr3, leppl, 3

479

etable, plstr4, leppl, 4

480 etable, plstr5, leppl, 5 481

etable, plstr6, leppl, 6

452 etable, plstr7,. leppl, 7 483 etable, pl-str2l, Ieppl, 21 484 etable, plstr22, leppl, 22 485 etable, plstr23, leppl,.23 486 etable, plstr24, leppl, 24 487 etable, plstr25, leppl, 25 488 etable, plstr26, leppl, 26 489 etable, plstr27, 1eppl, 27 490 491 ! Element Forces 492 493 etable,

xfori, smisc, 1

494

etable, yfori,

smisc, 2

495 etable,

zfori, smisc, 3

496 etable,

xmomi, smisc, 4

497

etable, ymomi,

smisc, 5

essw4, 4*pressw4 ressw4, -4*pressw4

, xmomi, ymomi, zmomi , xmomj, ymomj, zmomj Page E8

File No. MN03-P022637-100 498 etable,

zmomi, smisc, 6

499 etable,

xforj, smisc, 7

500 etable, yforj,

smi3c, 8

501 etable,

zforj, smisc, 9

502 etable, xmomj, smisc, 10 503 etable,

ymomj, smisc, 11 504

etable, zmomj, smisc, 12 505 506 ! Element Axial Stresses 507 508 etable,- axstrl, is, 1 509 etable,

axstr2, is, 2 510 etable,

axstr3, ls, 3

511 etable,

axstr4, ls, 4

512 etable,

axstr5, is, 5 513 etable, axstr6,-

is, 6 514

etable, axstr7, ls, 7

515 etable, axstr21, Is, 21 516 etable, axstr22, ls, 22 517 etable, axstr23, ls, 23 518 etable, axstr24, ls, 24 519 etable, axstr25, ls, 25 520 etable, axstr26, is, 26 521 etable, axstr27, is, 27 522 pretab,

plstrl, plstr2,

plstr3, plstr4, plstr5, plstr6, plstr7 523 pretab, plstr2l, plstr22, plstr23, plstr24, plstr25, plstr26, plstr27 524 pretab,

xfori, yfori,

zfori, xmomi,

ymomi, zmomi 525 pretab,

xforj, yforj,

zforj, xmomj,

ymomj, zmomj 526 pretab,

axstrl, axstr2, axstr3, axstr4, axstr5, axstr6, axstr7 527 pretab, axstr2l, axstr22, axstr23, axstr24, axstr25, axstr26, axstr27 528 529 ! Support DGEH W4 x 13 530 !

531 ! Plastic Strains 532 533 esel, s, elem,, 40, 45 534 etable, plstrl, leppl, 1 535 etable, plstr2, leppl, 2 536 etable, plstr3, leppl, 3 537 etable, plstr4, leppl, 4 538 etable, plstr5, leppl, 5 539 etable, plstr6, leppl, 6 540 etable, pIstr7, leppl, 7 541 etable, plstr2l, leppl, 2i1 542 etable, plstr22, leppl, 22 543 etable, plstr23, leppl, 23 544 etable, plstr24, leppl, 24 545 etable, plstr25, leppl, 25 546 etable, plstr26, leppl, 26 547 etable, plstr27, leppl, 27 548 549 ! Element Forces 550 551 etable,

xfori, smisc, 1

552 etable,

yfori, smisc, 2

553 etable,

zfori, smisc, 3

554 etable,

xmomi, smisc, 4

555 etable,

ymomi, smisc, 5

556 etable,

zmomi, smisc, 6.

557 etable',

xforj, smisc, 7

558 etable,

yforj, smisc, 8

559 etable,

zforj, smisc, 9

560 etable,

xmomj, smisc, 10 561 etable,

ymomj, smisc, 11

.562 etable,

zmomj, smisc, 12 563 564

! Element Axial Stresses 565 566 etable,

axstrl, is, 1 567

etable, axstr2, ls, 2

568 etable,

axstr3, ls, 3

Page E9

File No. MN03-PO22637-l00 569 etable,

axstr4, Is, 4 570 etable, axstr5, is, 5 571

etable, axstr6, ls, 6

572 etable,

axstr7, ls, 7

573 etable, axstr2l, ls, 21 574 etable, axstr22, ls, 22 575 etable, axstr23, ls, 23 576 etable, axstr24, ls, 24 577 etable, axstr25, ls, 25 578 etable, axstr26, ls, 26 579 etable, axstr27, ls, 27 580 pretab, plstrl, plstr2,

plstr3, plstr4,

plstr5, plstr6, plstr7 581 pretab, plstr2l, plstr22, plstr23, plstr24, plstr25, plstr26, plstr27 582 pretab,

xfori, yfori,

zfori, xmomi,

ymomi, zmomi 583 pretab,

xforj, yforj,

zforj, xmomj,

ymomj, zmomj 584 pretab, axstrl,

axstr2, axstr3,

axstr4, axstr5,

axstr6, axstr7 585 pretab, axstr2l, axstr22, axstr23, axstr24, axstr25, axstr26, axstr27 586 !

587 ! Support DGEH-l - C4 x 5.4 588 1 589 ! Plastic Strains 590 591 esel, s, elem,, 50, 61 592

etable, pistrl, leppl, 1 593

etable, plstr2, leppl, *2 594

etable, plstr3, leppl, 3 595

etable, plstr4, leppl, 4 596 etable, plstr2l, leppl, 21 597 etable, plstr22, leppl, 22.

598 etable, plstr23, leppl, 23 599 etable, plstr24, leppl, 24 600 ! 601 ! Element Forces 602 ! 603 etable,

xfori, smisc, 1

-604

etable, yfori,

smisc, 2

605

etable, zfori,

smisc, 3

606 etable,

xmomi, smisc, 4

607 etable,

ymomi, smisc, 5

608 etable,

zmomi, smisc, 6

609 etable,

xforj, smisc, 7

610 etable,

yforj, smisc, 8

611 etable,

zforj, smisc, 9

612 etable,

xmomj, smisc, 10 613 etable,

ymomj, smisc, 11 614 etable,

zmomj, smisc, 12 615 616

! Element Axial Stresses 617 618. etable,

axstrl, ls, 1

619 etable,

axstr2, ls, 2

620 etable,

axstr3, ls, 3

621

etable, axstr4, ls, 4

622 etable, axstr2l, ls, 21 623 etable, axstr22, ls, 22 624 etable, axstr23, ls, 23 625 etable, axstr24, ls, 24 626 pretab, plstrl, plstr2, plstr3, plstr4 627 pretab, plstr2l, plstr22, plstr23, plstr24 628

pretab, xfori,

yfori, zfori,

xmomi, ymomi, zmomi 629 pretab,

xforj, yforj,

zforj, xmomj,

ymomj, zmomj 630

pretab, axstrl, axstr2, axstr3,, axstr4 631 pretab, axstr2l, axstr22, axstr23, axstr24 632 633

! Loads on Lugs 634 635 esel, s, elem,, 224, 227

• 636 etable, lugforce, smisc, 1 637 pretab, lugforce 638 I

639 ! Forces in Spring Cans Page E1O

C.~ -v. rl*vUj-rU4zaJ -vUU 640 641 esel, s, elem,, 88, 89 642 etable, spforce, smisc, 1 643 etable, preload, smisc, 2 644

etable, elstat, nmisc, 1 645 pretab, spforce, preload, elstat 646 esel, all 647 648

! Reaction Loads 649 650 prrsol RUN SETUP PROCEDURE FROM FILE-C:\\PROGRAM FILES\\ANSYS INC\\ANSYS57\\docu\\start57.ans /INPUT FILE-C:\\PROGRAM FILES\\ANSYS INC\\ANSYS57\\docu\\start57.ans LINE-0 CURRENT JOBNAME REDEFINED AS exhaust TITLE-EDG Exhaust Piping 1 ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 5.7.1 ANSYS/Mechanical U 00251976 VERSION-INTEL NT 21:40:10 MAR 06, 2003 CP-0.481 EDG Exhaust Piping ANSYS ANALYSIS DEFINITION (PREP7) REFERENCE TEMPERATURE-0.000 (TUNIF-0.000) MATERIAL 1-EX 0.2790000E+08 MATERIAL 1 NUXY - 0.3000000 MATERIAL 1 DENS - 0.7338634E-03 MATERIAL 2 EX 0.2900000E+08 MATERIAL 2 NUXY - 0.3000000 MATERIAL 2 DENS - 0.7338634E-03 DEFINE DATA TABLE BKIN FOR MATERIAL 2 WITH A MAXIMUM OF 1 TEMPERATURE SPECIFICATIONS AND USE THE ALTERNATIVE HARDENING OPTION FOR TEMPERATURE DEPENDENT CURVES (RICE MODEL) TEMPERATURE TO BE USED FOR THE NEXT TBDAT COMMAND- 0.0000 TEMPERATURE SPECIFICATION-1 DATA FOR BKIN TABLE FOR MATERIAL 2 AT TEMPERATURE- 0.0000 LOC-1 36000. 0.0000 .MATERIAL 3 EX. 0.2900000E+08 MATERIAL 3 NUXY 0.3000000 MATERIAL 3 DENS - 0.000000 ELEMENT TYPE 1 IS PIPEI6 ELASTIC STRAIGHT PIPE KEYOPT(1-12)- 0 0 0 0 0 0 0 0 0 0 0 0 CURRENT NODAL DOF SET IS UX UY UZ ROTX ROTY ROTZ THREE-DIMENSIONAL MODEL ELEMENT TYPE 2 IS PIPE18 ELASTIC CURVED PIPE (ELBOW) KEYOPT(1-12)- 0 0 0 0 0 0 0 0 0 0 0 0 Page Ell

t Li-a vov. Pmui-ruzzoai-.vUU CURRENT NODAL DOF SET IS tX UY THREE-DIMENSIONAL MODEL ELEMENT TYPE 3 IS BEAM4 KEYOPT(1-12)- 0 0 0 0 0 0 CURRENT NODAL DOF SET IS UX UY THREE-DIMENSIONAL MODEL ELEMENT TYPE 4 IS MASS21 KEYOPT(1-12)- 0 0 0 0 0 0 CURRENT NODAL DOF SET IS UX UY THREE-DIMENSIONAL MODEL ELEMENT TYPE 4 IS MASS21 STRUC KEYOPT(1-12)m 0 0 2 0 0 0 CURRENT NODAL DOF SET IS UX UY THREE-DIMENSIONAL MODEL ELEMENT TYPE 5 IS COMBIN40 C KEYOPT(1-12)- 0 0 0 0 0 0 CURRENT NODAL DOF SET IS UX UY THREE-DIMENSIONAL MODEL ELEMENT TYPE 5 IS COMBIN40 COMBI KEYOPT(1-12)- 0 0 0 0 0 0 ,CURRENT,NODAL DOF SET IS UX UY THREE-DIMENSIONAL MODEL ELEMENT TYPE 6 IS COMBIN40 CC KEYOPT(1-12)- 0 0 0 0 0 0 CURRENT NODAL DOF SET IS UX UY THREE-DIMENSIONAL MODEL ELEMENT TYPE 6 IS COMBIN40 COMBIb KEYOPT(1-12)- 0 0 3 0 0 0 CURRENT NODAL DOF SET IS UX UY THREE-DIMENSIONAL MODEL ELEMENT TYPE 7 IS COMBIN14 SE KEYOPT(1-12)- 0 0 0 0 0 0 CURRENT NODAL DOF SET IS UX UY THREE-DIMENSIONAL MODEL ELEMENT TYPE 7 IS COMBIN14 SPRING KEYOPT(1-12)- 0 1 0 0 0 0 CURRENT NODAL DOF SET IS UX UY THREE-DIMENSIONAL MODEL ELEMENT TYPE 8 IS COMBIN14 SP] KEYOPT(l-i2)- 0 0 0 0 0 0 CURRENT NODAL DOF SET IS UX UY t THREE-DIMENSIONAL MODEL ELEMENT TYPE 8 IS COMBINli SPRING-KEYOPT(1-12)- 0 2 0 0 0 0 UZ ROTX ROTY ROTZ 3-D ELASTIC BEAM 0 0 0 0 UZ ROTX ROTY STRUCTURAL MASS 0 0 0 O ( UZ ROTX ROTY 0 CTURAL MASS 0 0. 0 UZ ROTXN OMBINATION 0.0 0 UZ ROTX NATION Z OT UZ ROTX OMBINATION Z RO UZ ROTX NATION 0 0 0 UZ ROTX PRING-DAMPEF D OT UZ ROTX 0 ,0 ROT'Y 0 0 ROTY 0 0 ROTY 0 0 ROTY 0 0 ROTY I 0 0 ROTY I 0 0 ROTY f ,0 Q ROTY R 0 0 0 RQTZ 0 ROTZ 0 ROTZ 0 ROTZ 0 ROTZ 0 ROTZ 0 ROTZ 0 ROTZ -DAMPER Z OT UZ ROTX RING-DAMPER .0 0 0 UZ ROTX 0 LOTZ 0 OTZ 0 -DAMPER 0 0 0 CURRENT NODAL DOF SET IS UX UY .UZ THREE-DIMENSIONAL MODEL ELEMENT TYPE 9 IS COMBIN14 SPRD ROTX ROTY ROTZ NG-D)AMPER Page E12

Z.LJ.U Lu. ruvWU-ruSzo jt-vuu KEYOPT(1-12)- 0 0 0 0 0 CURRENT NODAL DOF SET IS UX UY THREE-DIMENSIONAL MODEL ELEMENT TYPE 9 IS COMBIN14 SPRI KEYOPT(1-12)- 0 3 0 0 0 C CURRENT NODAL DOF SET IS UX DY THREE-DIMENSIONAL MODEL ELEMENT TYPE 10 IS COMBIN14 KEYOPT(1-12)- 0 0 0 0 0 C CURRENT NODAL DOF SET IS UX UY THREE-DIMENSIONAL MODEL ELEMENT TYPE 10 IS COMBIN14 SPRI KEYOPT(1-12)- 0 4 0 0 0 0 CURRENT NODAL DOF SET IS UX UY THREE-DIMENSIONAL MODEL ELEMENT TYPE 11 IS COMBIN14 KEYOPT(1-12)- 0 0 0 0 0 0 CURRENT NODAL DOF SET IS UX UY THREE-DIMENSIONAL MODEL ELEMENT TYPE 11 IS COMBIN14 SPRI KEYOPT(1-12)- 0 5 0 0 0 0 CURRENT NODAL DOF SET IS UX UY THREE-DIMENSIONAL MODEL ELEMENT TYPE 12 IS COMBIN14 KEYOPT(1-12)- 0 0 0 0 0 0 CURRENT NODAL DOF SET IS UX UY THREE-DIMENSIONAL MODEL ELEMENT TYPE 12 IS COMBIN14 SPRI KEYOPT(1-12)- 0 6 0 0 0 0 CURRENT NODAL DOF SET IS UX UY THREE-DIMENSIONAL MODEL ELEMENT TYPE 13 IS BEAM24 KEYOPT(1-12)- 0 0 0 0 0 0 CURRENT NODAL DOF SET IS UX UY THREE-DIMENSIONAL MODEL ELEMENT TYPE 13 IS BEAM24 3-D .KEYOPT(1-12)- 1 0 0 0 0 0 CURRENT NODAL DOF SET IS UX UY THREE-DIMENSIONAL MODEL ELEMENT TYPE 14 IS COMBIN37 4 KEYOPT(1-12)- 0 0 0

0. 0 0

CURRENT NODAL DOF SET IS UX UY THREE-DIMENSIONAL MODEL ELEMENT TYPE 14 IS COMBIN37 CONTI KEYOPT(1-12)- 0 2 0 .0 0 0 CURRENT NODAL DOF SET IS UX UY THREE-DIMENSIONAL MODEL o 0 0 0 UZ ROTX 0 0 ROTY 0 0 ROTY 0 ROTZ 0 ROTZ .NG-DAMPER 0 0 0 UZ ROTX SPRING-DAMPER I 0 00 00 0 UZ ROTX ROTY ROTZ

NG-DAMPER 0 0 UZ ROT) 0 0

C ROTY SPRING-DAMPER 0 0 0 UZ ROTX NG-DAMPER 0 0 0 UZ ROTX 0 0

• ROTY 0 0 ROTY 0

0 ROTY 0 ROTZ 0 ROTZ 0 ROTZ 0 ROTZ SPRING-DAMPER D 0 0 UZ ROTX NG-DAMPER UZ ROTX 0 0 0 ROTY ROTZ 3-D THIN-WALLED BEAM 0 00 00 0 UZ ROTX ROTY ROTZ THIN-WALLED BEAM 0 00 0 0 UZ. ROTX ROTY 0 ROTZ CONTROL 0 00 00 0 UZ ROTX ROTY ROTZ ?OL D2 0 00 00 0 Z ROTX ROTY ROTZ Page E13

• ",4W*/

£UveL.jl.LUU ELEMENT TYPE 14 IS COMBIN37 KEYOPT(1-12)- 0 2 2 0 CURRENT NODAL DOF SET IS UX THREE-DIMENSIONAL MODEL ELEMENT TYPE 14 IS COMBIN37 KEYOPT(1-12)- 0 2 2 1 CURRENT NODAL DOF SET IS UX THREE-DIMENSIONAL MODEL ELEMENT TYPE 15 IS LINK10 KEYOPT(1-12)- 0 0 0 0 CONTROL 00 00 0 uY UZ ROTX CONTROL 0 0 ROTY 00 0 0 00 00 UY UZ ROTX ROTY TENSION-ONLY SPAR 0 0 0 0 0 0 0 UY UZ ROTX ROTY COMPRESSION-ONLY SPAR 00 00 00 00 UY UZ ROTX ROTY 0 ROTZ 0 ROTZ 0 ROTZ 0 ROTZ CURRENT NODAL DOF SET IS THREE-DIMENSIONAL MODEL UX ELEMENT TYPE-15 IS LINK10 KEYOPT(1-12)- 0 0 1 CURRENT NODAL DOF SET IS UX THREE-DIMENSIONAL MODEL 0 REAL CONSTANT S 22.000 REAL CONSTANT 36.000 REAL CONSTANT 22.000 REAL CONSTANT 0.0000 REAL CONSTANT 22.000 REAL CONSTANT 0.18116E-04 REAL CONSTANT 22.000 REAL CONSTANT 0.0000 REAL CONSTANT -2.0300 REAL CONSTANT 0.0000 REAL CONSTANT -2.0300 REAL CONSTANT 2.0300 REAL CONSTANT. 1.1270 REAL CONSTANT -0.36500 REAL CONSTANT 0.0000 SI S S .S S S S S S S. 5]

ET 1 ITEMS 1

0.37500 0.0000

ET 2

ITEMS 1 0.35000 0.0000

ET 3 ITEMS 1

0.37500 33.000 3ET 3 ITEMS 7 0.0000 0.0000 3ET 4 TTEMS 1 0.37500 0.0000 ET 4 ITEMS 7 3.0000 0.0000 ET 5 ITEMS 1 0.37500 33.000 ET 5 ITEMS 7 0.18116E-04 3.0000 ET 6 ITEMS 1 1.9075 0.0000 ET 6 ITEMS 7 1.9075 0.0000 ET 6 ITEMS 13 -1.9075 0.34500 ET 6 ITEMS 19 -1.9075 0.34500 ET 7 ITEMS 1 1.8520 0.0000 ET 7 ITEMS 7 -1.8520 0.18400 ET 8 ITEMS 1 0.0000 0.0000 TO TO TO TO TO TO TO TO TO TO TO TO TO TO TO 6 0.0000 6 0.0000 6

4. 0200 12 0.0000 6

0.0000 12

0. 0000

. 6

4. 0200 12 0.0000 6

2. 0300 12

0. 0000 18 0.0000 24

0. 0000 6

-0.36500 12 1.1270 6 0.12500 6 0.0000 0.0000 0.0000 4.0200 0.0000 0.0000 0. 0000 4.0200

0. 0000 1.9075

-1. 9075 -1. 9075 0.0000 1.8520 -1.8520 0.0000 0.0000 0.0000 15.588 15.588 0.0000 0.0000 15.588 15.588 0.34500 0.28000 '0.0000'

0. 0000 0.29600 0.29600 0.10000E+11 REAL CONSTANT SET 10 0.40114 0.0000 ITEMS 1 TO 0.0000 0.0000 0.0000 Page E14

I-1- VL--#AW REAL CONSTANT SET 11 ITEMS 1 0.59524 0.0000 0.0000 REAL CONSTANT SET 12 ITEMS 1 0.0000 0.0000 0.0000 REAL CONSTANT SET 13 ITEMS 1 0.10000E+11 0.0000 0.0000 REAL CONSTANT SET 14 ITEMS 1 10.000 0.0000 0.0000 REAL CONSTANT SET 15 ITEMS' 1 100.00 1000.0 1000.0 REAL CONSTANT SET 15 ITEMS 7 0.0000 1000.0 0.0000 REAL CONSTANT SET 17 ITEMS 1 0.66000E+07 0.0000 0.0000 REAL CONSTANT SET 18 ITEMS 1 0.58000E+07 0.0000 0.0000 REAL CONSTANT SET 19 ITEMS 1 0.0000 0.0000 0.0000 REAL CONSTANT SET . 20 ITEMS 1 10.000 0.0000 0.0000 REAL CONSTANT SET 21 ITEMS 1 10.000 0.0000 0.0000 REAL CONSTANT SET 22 ITEMS 1 10.000 0.0000 0.0000 REAL CONSTANT SET 23 ITEMS .1 10.000 0.0000 0.0000 REAL CONSTANT SET 24 ITEMS 1 10.000 0.0000 0.0000 REAL CONSTANT SET 25 ITEMS 1 363.00 0.0000 0.0000 REAL CONSTANT SET 26 ITEMS 1 363.00 0.0000 0.0000 REAL CONSTANT SET 27 ITEMS 1 1.5000 0.0000 0.0000 ACTIVE COORDINATE SYSTEM SET TO 0 NODE 1 KCS-0 X,Y,Z- 0.0000 NODE. - 2 KCS-0 X,Y,Z- -37.000 NODE 3 KCS-0 X,Y,Z- -74.000 NODE 4 KCS-0.X,Y,Z- -96.000 NODE 5 KCS-0 X,Y,Z- -100.00 NODE 6 KCS-0 X,Y,Z- -135.25 NODE 7 KCS-0 X,Y,Z- -170.50 NODE 8 KCS-0 X,Y,Z- -205.75 NODE 9 KCS-0 X,Y,Z- -241.00 T T T Tt Tt Tt TI T( TC TC TC TC TC r0 6 0.0000 o 6 0.50000 O 6 0.0000 O 6

0. 0000 O

6 1.0000 12

0. 0000 6

0.0000 O 6

0. 0000 O

6 0.50000 O 6 0.0000 O 6 0.0000 O 6

0. 0000 0

6 0.0000 D 6

0. 0000 D

6 0.37500 6 1.2500 6

0. 0000 (CARTESIAN) 0.0000

0. 0000

0. 0000

0. 0000 0.0000 0.0000

0. 0000 0.0000 0.0000 0.0000

0. 0000 0.0000 0.0000 1.0000

0. 0000 0.0000 0.0000 0.0000

0. 0000

0. 0000 0.0000

0. 0000 0.0000

-10.000 -10.000 0.0000 0.0000

0. lOOOOE+11 0.0000

0. 0000 0.0000 0O.

0000

0. 0000 0.0000 0.10000E+ll 0.0000 0.0000 0.0000

0.0000 0.0000 1515.0 1832.0 0.0000 0.0000

0. 0000

0. 0000

0. 0000 0.0000

0. 0000 0.0000

0. 0000 0.0000 Page E15

c &%V nL. r.LMUJ-rufuj-jUV NODE 10 KCS-0 X,Y,Z- -245.00 0.0000 0.0000 NODE 11 KCS-0 X,Y,Z- -266.00 0.0000 0.0000 NODE 12 KCS-0 XY,Z- -305.00 0.0000 0.0000 NODE 13 KCS-0 X,YZ- -338.00 -33.000 0.0000 NODE 14 KCS-0 X,Y,Z- -338.00 -66.250 0.0000 NODE 15 KCS-0 X,Y,Z- -338.00 -99.500 0.0000 NODE 16 KCS= 0 X,Y,Z- -338.00 -132.75 0.0000 NODE 17 KCS-0 X,Y,Z- -338.00 -166.00 0.0000. NODE 18 KCS-0 XY, Z- -338.00 -190.50 0.0000 NODE 19 KCS-0 X,Y,Z- -338.00 -222.25 0.0000 NODE 20 KCS-0 X,Y,Z- -371.00 -255.25 0.0000 NODE 21 KCS-0 X,Y,Z- -394.00 -255.25 0.0000 NODE 22 KCS-0 X,Y,Z- -394.00 -255.25 0.0000 NODE 30 KCS-0 XY,Z- -74.000 0.0000 13.125 NODE 31 KCS-0 XY,Z- -74.000 -30.500 13.125 NODE 32 KCS-0 X,Y,Z- -74.000 -41.000 13.125 NODE 33 KCS-0 XY,Z- -74.000 -30.500 0.0000 NODE 34 KCS-0 X,Y,Z- -74.000 0.0000 -13.125 NODE 35 KCS-0 X,Y,Z- -74.000 -30.500 -13.125 NODE 36 KCS-0 X,Y,Z- -74.000 -41.000 -13.125 NODE 37 KCS-0 X,Y,Z- -74.000 0.0000 13.125 NODE 38 KCS= 0 X,Y,Z- -74.000 0.0000 -13.125 NODE

39. KCS-0 X,Y,Z- -74.000

-30.500 0.0000 NODE 200 KCS-0 X,Y,Z- -74.000 -41.000 13.125 NODE 201 KCS-0 X,Y,Z- -74.000 -41.000 -13.125 NODE

40. KCS-0 X,Y,Z- -266.00 0.0000 13.125 NODE 41 KCS-0 X,Y,Z- -266.00

-30.500 13.125 NODE 42 KCS-0 X,YZ- -266.00 -41.000 13.125 NODE 43 KCS-0 XY,Z- -266.00 -30.500 0.0000 NODE 44 KCS-0 XYZ -266.00 0.0000 -13.125 NODE 45 KCS-0 X,Y,Z- -266.00 -30.500 -13.125 NODE 46 KCS-0 X,Y,Z- -266.00 -41.000 -13.125 NODE 47 KCS-0 X,Y,Z- -266.00 0.0000 13.125 NODE 48 KCS-0 XY,Z- -266.00 0.0000 -13.125 NODE 49 XCS-0 X,Y,Z- -266.00 -30.500 0.0000 Page E16

z£ j awU rlmvJ-ru<zuj /-uVU NODE NODE NODE NODE NODE NODE NODE NODE NODE NODE NODE NODE NODE NODE NODE NODE NODE NODE NODE NODE NODE NODE NODE NODE NODE NODE 202 KCS-203 KCS= 50 KCS-51 KCS-52 KCS-53 KCS-54 KCS-55 KCS-56 KCS-57 KCS-58 KCS-59 KCS-60 KCS-61 KCS-62 KCS-63 KCS-64 KCS-65 KCS-72 KCS-73 KCS-74 KCS-75 KCS-100 KCS-101 KCS-102 KCS-103 KCS-0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 X,Y,Z- -266.00 X,YZ- -266.00 X,Y,Z- -377.00 X,Y,Z- -349.96 X,Y,Z- -338.00 X,YZ- -326.04 X,Y,Z- -306.00 X,Y,Z- -349.96 X,Y,Z- -326.04 X,Y,Z- -377.00 X,Y,Z- -349.96 X,Y,Z- -338.00 X,Y,Z- -326.04 X,Y,Z- -306.00 X,Y,Z- -338.00 X,YZ- -349.96 X,Y,Z- -326.04. X,Y,Z- -338.00 X,Y,Z- -338.00 X,Y,Z- -349.96 X,Y,Z- -326.04 X,Y,Z- -338.00 X,Y,Z- -305.00 X,Y,Z- -371.00 X,Y,Z- -349.96 X,Y,Z- -326.04 -41.000 -41. 000 -190.50 -190.50 -190.50 -190.50 -190.50 -190.50 -190.50 -190.50 -190.50 -190.50 -190.50 -190.50 -190.50 -190.50 -190.50 -190.50 -186.50 -186.50 -186.50 -186.50 -33. 000 -222.25 -180.50 -180.50 13.125 -13.125 -11.957 -11. 957 -11.957 -11. 957 -1l. 957

0. 0000

0. 0000 11.957

11. 957 11.957

11. 957 11.957

-11.957 0.0000

0. 0000

11. 957

-11.957

0. 0000 O.0000 11.957-O. 0000

0. 0000

-11.957 11.957 MATERIAL NUMBER SET T( ELEMENT TYPE SET TO REAL CONSTANT NUMBER-ELEMENT 1 1 ELEMFNT 2 ELEMENT 3 3 ELEMENT 4 4 REAL CONSTANT NUMBER-ELEMENT

• 5 5

ELEMENT 6 6 ) 1 1 1 L I 2 0 3 0 4 0 5 0 2 5 6 0 6 7 0 Page E17

ELEMENT 7 7 8 0 ELEMENT 8 8 9 0 REAL CONSTANT NUMBER-1 ELEMENT 9 9 10 0 ELEMENT 10 10 11 0 ELEMENT 11 11 12 0 ELEMENT TYPE SET TO 2 REAL CONSTANT NUMBER-3 ELEMENT 12 12 13 100 ELEMENT TYPE SET TO 1 REAL CONSTANT NUMBER-1 ELEMENT 13 13 14 0 ELEMENT 14 14 15 0 ELEMENT 15 15 16 0 ELEMENT 16 16 17 0 REAL CONSTANT NUMBER-4 ELEMENT 17 17 18 0 ELEMENT 18 18 19 0 ELEMENT TYPE SET TO 2 REAL CONSTANT NUMBER-5 ELEMENT 19 19 20 101 ELEMENT TYPE SET TO 1 REAL CONSTANT NUMBER-4 ELEMENT 20 20 21 0 MATERIAL NUMBER SET TO 2 REAL CONSTANT NUMBER-6 ELEMENT TYPE SET TO 13 ELEMENT 30 30 31 3 ELEMENT 31 31 32 3 ELEMENT 32 31 33 3 ELEMENT 33 33 35 3 ELEMENT 34 34 35 3 ELEMENT 35 35 36 3 ELEMENT 40 40 41 11 ELEMENT 41 41 42 11 Page E18

ELEMENT 42 41 ELEMENT 43 43 ELEMENT 44 44 ELEMENT 45 45 REAL.CONSTANT NUMBER-ELEMENT 50 50 ELEMENT 51 51 ELEMENT 52 52 ELEMENT 53 53 ELEMENT 54 55 ELEMENT 55 58 ELEMENT 56 53 ELEMENT 57 56 ELEMENT 58 58 ELEMENT 59 59 ELEMENT 60 60 ELEMENT 61 61 MATERIAL NUMBER SET TO ELEMENT TYPE SET TO REAL CONSTANT NUMBER-ELEMENT 70 3 ELEMENT 71 3 ELEMENT 72 11 ELEMENT 73 11 ELEMENT TYPE SET TO REAL CONSTANT NUMBER-ELEMENT 74 37 ELEMENT 75 34 ELEMENT 76 47 43 11 45 11 45 11 46 11 7 51 102 52 102 53 102 54 102 51 102 55 102 56 103 60 103 57 103 58 103 59 103' 60 103 3 3 15. 37 38 47 48 6 0 0 0 0 8 30 38 40 ELEMENT 77 44 48 ELEMENT TYPE SET TO 3 REAL CONSTANT NUMBER= 15 ELEMENT 78 18 62 ELEMENT 79 18 63 ELEMENT 80 18 64 ELEMENT 81 18 65 0 0 0 0 ' Page E19

ELEMENT TYPE SET TO REAL CONSTANT NUMBER-ELEMENT 82 52 ELEMENT 85 65 ELEMENT TYPE SET TO REAL CONSTANT NUMBER-ELEMENT 83 63 ELEMENT 84 56 ELEMENT TYPE SET TO REAL CONSTANT NUMBER-ELEMENT 86 3 ELEMENT 87 11 ELEMENT TYPE SET TO REAL CONSTANT NUMBER-ELEMENT 88 39 REAL CONSTANT NUMBER-ELEMENT 89 49 ELEMENT TYPE SET TO REAL CONSTANT NUMBER-ELEMENT 94 21 ELEMENT TYPE SET TO REAL CONSTANT NUMBER-ELEMENT 95 21 ELEMENT TYPE SET TO REAL CONSTANT NUMBER-ELEMENT 96 21 ELEMENT TYPE -SET TO REAL CONSTANT NUMBER-ELEMENT 97 21 ELEMENT TYPE SET TO REAL CONSTANT NUMBER-ELEMENT 98 21 ELEMENT TYPE SET TO REAL CONSTANT NUMBER-ELEMENT 99 21 6 12 62 59 5 19 55 64 3 15 39

49 14 25 33 26 43

.7 14 22 8 20 22 9 21 22 10 22 22 11 23 22 12' 24 22 0 0 39 33 49 43 Page E20

ELEMENT TYPE SET TO REAL CONSTANT NUMBER-ELEMENT 100 4 ELEMENT 101 10 REAL CONSTANT NUMBER-ELEMENT 102 21 ELEMENT TYPE SET TO REAL CONSTANT NUMBER-ELEMENT 200 32 ELEMENT 203 36 ELEMENT 205 42 ELEMENT 208 46 ELEMENT TYPE SET TO REAL CONSTANT NUMBER-ELEMENT 201 32 ELEMENT 204 36 ELEMENT 206 42 ELEMENT 209 46 ELEMENT TYPE SET TO REAL CONSTANT NUMBER-ELEMENT 220 10 ELEMENT 221 18 ELEMENT 222 18 ELEMENT 223 18 ELEMENT TYPE SET TO REAL CONSTANT NUMBER-ELEMENT 224 72 ELEMENT 225 73 ELEMENT 226 74 ELEMENT 227 75 SPECIFIED CONSTRAINT UX REAL-0.00000000 ADDITIONAL DOFS-UY SPECIFIED CONSTRAINT UX REAL-0.00000000 ADDITIONAL DOFS-UY SPECIFIED CONSTRAINT UX REAL-0.00000000 ADDITIONAL DOFS-UY 4 10 11 10 18 200 201 202 203 12 17 200 201 202 203 3 15 72 73 74 75 15 27 52 55 56 59 FOR SE IMAG-C UZ RC FOR SE IMAG-C UZ RC FOR SE IMAG-C UZ RC I 0 0 0 0 ELECTED NODES [.00000000 )TX ROTY ROTZ

LECTED NODES 1.00000000

)TY ELECTED NODES I.00000000 CTY 22 TO 32 TO 36 TO 22 BY 1 32 BY 1 36 BY 1 Page E21

SPECIFIED CONSTRAINT REAL- 0.00000000 ADDITIONAL DOFS-UY SPECIFIED CONSTRAINT REAL-0.00000000 ADDITIONAL DOFS-UY SPECIFIED CONSTRAINT REAL- 0.00000000 ADDITIONAL DOFS-UY SPECIFIED CONSTRAINT REAL-0.00000000 ADDITIONAL DOFS-UY SPECIFIED CONSTRAINT REAL- 0.00000000 ADDITIONAL DOFS-UY SPECIFIED CONSTRAINT REAL- 0.00000000 ADDITIONAL DOFS-UY UX FOR SELECTED NODES IMAG- 0.00000000 UZ ROTY UX FOR IMAG- -UZ UX FOR IMAG-UZ SELECTED NODES 0.00000000 ROTY SELECTED NODES 0.00000000 ROTX ROTY ROTZ 42 TO -46 TO 50 TO 54 TO 57 TO 61 TO 42 BY 1 46 BY 1 50 BY 1 UX FOR SELECTED NODES IMAG-0.00000000 UZ 54 BY 1 UX FOR IMAG-UZ SELECTED NODES 0.00000000 ROTX ROTY ROTZ 57 BY 1 UX FOR SELECTED NODES IMAG-0.00000000 UZ 61 BY 1 SPECIFIED CONSTRAINT REAL-0.00000000 ADDITIONAL DOFS-UY UX FOR SELECTED NODES IMAG-0.00000000 UZ ROTX ROTY ROTZ 200 TO 203 BY 1 LIST ALL SELECTED NODES. DSYS-0 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 5.7.1 ANSYS/Mechanical U 00251976 VERSION-INTEL NT 21:40:21 MAR 06, 2003 CP-

0. 901 EDG Exhaust Piping NODE 1

2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 30 31 32 33 34 35 36 37 38 X 0.0000 -37.000 -74.000 -96. 000 -100.00 -135.25 -170.50 -205.75 -241.00 -245.00 -266.00 -305.00 -338.00 -338.00 -338.00 -338.00 -338.00 -338.00 -338.00 -371.00 -394.00 -394.00 -74.000 -74.000 -74.000 -74.000 -74.000 -74.000 -74.000 -74.000 -74.000 Y 0.0000

0. 0000 0.0000

0. 0000 0.0000 0.0000 0.0000 0.0000

0. 0000 0.0000 0.0000

0. 0000-

-33.000 -66.250 -99.500 -132.75 -166.00 -190.50 -222.25 -255.25 -255.25 -255.25 0.0000 -30.500 -41.000 -30.500 0.0000 -30.500 -41.000 0.0000 0.0000 z 0.0000 0.0000 0.0000 0.0060 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 'O.0000

0. 0000

0. 0000 0.0000 0.0000 0.0000 0.00 00 0.0000 13.125 13.125 13.125 0.0000

-13.125 -13.125 -13.125 13.125 -13.125 THXY 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 THYZ 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 THZX 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 Page E22

39 -74.000 40 -266.00 41 -266.00 42 -266.00 43 -266.00 44 -266.00 45 -266.00 46 -266.00 47 -266.00 4B -266.00 49 -266.00 50 -377.00 51 -349.96 52 -338.00 53 -326.04 54 -306.00 55 -349.96 56 -326.04 57 -377.00 -30.500 0.0000 -30.500 -41.000 -30.500 0.0000 -30.500 -41.000 0.0000 0.0000 -30.500 -190.50 -190.50 -190.50 -190.50 -190.50 -190.50 -190.50 -190.50 0.0000 13.125 13.125 13.125 0.0000 -13.125 -13.125 -13.125 13.125 -13.125 0.0000 -11. 957 -11.957 -11.957 -11.957 -11.957

0. 0000 0.0000 11.957 0.0.0 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 a.00 0.00 0.00 0.'00

.0.00 0.00 0.00 0.00 0.00 0.00 0.00 .0.00 1

• • • • • ANSYS - ENGINEERING ANALYSIS SYSTI ANSYS/Mechanical C 00251976 EM RELEASE 5.7.1 21:40:21 MAR 06, 2003 CP-VERSION-INTEL NT 0.921 EDG Exhaust Piping NODE 58 59 60 61 62 63 64 65 72 73 74 75 100 101 102 103 200 201 202 203 X

-349.96 -338.00 -326.04 -306.00 -338.00 -349.96 -326.04 -338.00 -338.00 -349.96 -326.04 -338.00 -305.00 -371.00 -349.96 -326.04 -74.000 -74.000 -266.00 -266.00 Y ' -190.50 -190.50 -190.50 -190.50 -190.50 -190.50 -190.50 -190.50 -186.50 -186.50 -186.50 -186.50 -33.000 -222.25 -180.50 -180.50 -41.000 -41.D000 -41.000 -41.000 z

11. 957

11. 957

.11. 957

11. 957

-11. 957 0.0000

0. 0000

11. 957

-11. 957 0.0000

0. 0000

11. 957 0.0000

0. 0000

-11. 957

11. 957

13. 125

-13. 125

13. 125

-13. 125 THXY 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 THYZ 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 .0.00 0.00 0.00 0.00 0.00 0.00 0.00 THZX 0.00 0.00 . 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 LIST MATERIALS PROPERTY-ALL 1 TO 3 BY 1 PROPERTY TABLE EX TEMPERATURE MAT-1 NU] DATA TEMPERATURE

2. POINTS-DATA 1

U.UU0U 0.27900E+08 TEMPERATURE TEMPERATURE DATA DATA PROPERTY TABLE TEMPERATURE 0.0000 NUXY MAT-1 NUM. POINTS-1 DATA TEMPERATURE DATA I

0. 30000 PROPERTY TABLE DENS MAT-1 NUM.

POINTS-TEMPERATURE DATA TEMPERATURE DATA 0.0000 0.73386E-03 1 TEMPERATURE+ DATA PROPERTY TABLE TEMPERATURE 0.0000 EX MAT-2 NUN. POINTS-DATA TEMPERATURE DATA 0.29000E+08 1 TEMPERATURE DATA PROPERTY TABLE NUXY MAT-2 NUM. POINTS-1 TEMPERATURE DATA TEMPERATURE DATA TEMPERATURE DATA Page E23

0.0000 0.30000 PROPERTY TABLE DENS MAT-2 NUN. TEMPERATURE DATA TEMPERATURE 0.0000 0.73386E-03 PROPERTY TABLE EX MAT-3 NUN. TEMPERATURE DATA TEMPERATURE 0.0000 0.29000E+08 PROPERTY TABLE NUXY MAT-3 NUN. TEMPERATURE DATA TEMPERATURE 0.0000 0.30000 PROPERTY TABLE DENS MAT-3 NUM. TEMPERATURE DATA TEMPERATURE 0.0000 0.0000 POINTS-DATA POINTS-DATA POINTS-DATA POINTS-DATA 1 TEMPERATURE 1 TEMPERATURE 1 TEMPERATURE 1 TEMPERATURE DATA DATA DATA DATA LIST ELEMENT TYPES FROM 1 TO 15 BY 1 1

• • • • • ANSYS -

ENGINEERING ANALYSIS ANSYS/Mechanical U 00251976 VERSION-INTEL NT SYSTEM RELEASE 5.7.1 21:40:21 MAR 06, 2003 CP-0.941 EDG Exhaust Piping ELEMENT TYPE KEYOPT( 1-12) - ELEMENT TYPE KEYOPT(1-12)- ELEMENT TYPE KEYOPT(1-12)- ELEMENT TYPE KEYOPT(1-12)- ELEMENT TYPE KEYOPT(1-12)- ELEMENT TYPE CEYOPT(1-12)- ELEMENT TYPE KEYOPT(1-12)- ELEMENT TYPE KEYOPT(1-12)- ELEMENT TYPE KEYOPT(1-12)- ELEMENT TYPE KEYOPT(1-12)- ELEMENT TYPE KEYOPT(1-12)- ELEMENT TYPE KEYOPT(1-12)- ELEMENT TYPE KEYOPT( 1-12) - ELEMENT TYPE KEYOPT(1-12)- ELEMENT TYPE 1 IS PIPE16 0 00 00 2 IS PIPE18 0 00 00 3 IS BEAM4 0 00 0 4 IS MASS21 0 0 2 0 0 5 IS COMBIN40 0 00 00 6 IS COMBIN40 0 0 3 0 0 7 IS COMBIN14 0 1 0 0 0 -8 IS COMBIN14 0 2 0 0 0 9 IS COMBIN14 0 3 0 0 0 10 IS COMBIN14 0 4 0 .0 0 11 IS COMBIN14 0 5 0 0 0 12 IS COMBIN14 0 6 0 0 0 13 IS BEAM24 1 0 0 0 0 14 IS COMBIN37 0 2 2 1 0 15 IS LINK10 ELASTIC STRAIGHT PIPE 0 0 0 0 0 0 0 ELASTIC CURVED PIPE (ELBOW) 0 00 0 00 0 3-D ELASTIC BEAM 0 00 0 00 0 STRUCTURAL MASS 0 00 00 00 0 COMBINATION 0 0 0 0 0 0 0 COMBINATION 0 00 00 00 0 SPRING-DAMPER 0 00 0 0 0 0 SPRING-DAMPER 0 00 00 00 0 SPRING-DAMPER 0 000 00 0 SPRING-DAMPER 0 00 0 0 0 0 SPRING-DAMPE9 0 0 00 0 0 0 SPRING-DAMPER 0 00 0 00 0 3-D THIN-WALLED BEAM 0 00 0 00 0 CONTROL 0 00 0 00 0 COMPRESSION-ONLY SPAR Page E24 INOPR 0 INOPR INOPR INOPR INOPR INOPR INOPR INOPR INOPR INOPR INOPR INOPR INOPR INOPR 0 INOPR

KEYOPT(1-12)- 0 0 1 CURRENT NODAL DOF SET IS UX THREE-DIMENSIONAL MODEL 1 00 UY 0 000 00 r0 0 UZ ROTX ROTY ROTZ SYSTEM RELEASE 5.7.1 21:40:21 MAR 06, 2003 CP-

• • • • • ANSYS - ENGINEERING ANALYSIS ANSYS/Mechanical U 00251976 VERSION-INTEL NT EDG Exhaust Piping 0.971 LIST REAL SET REAL CONSTANT 22.000 S

SET 0.3750( REAL CONSTANT SET 36.000 0.3500( REAL CONSTANT SET 22.000 0.3750( REAL CONSTANT SET 0.0000 0.000c REAL CONSTANT SET 22.000 0.3750C REAL CONSTANT SET 0.18116E-04 3.OOOC REAL CONSTANT SET 22.000 0.3750C REAL CONSTANT SET 0.0000 0.18116 REAL CONSTANT SET -2.0300 1.9075 REAL CONSTANT SET 0.0000 1.9075 REAL CONSTANT SET -2.0300 -1.9075 REAL CONSTANT SET 2.0300 -1.9075 REAL CONSTANT SET 1.1270 1.8520 REAL CONSTANT SET -0.36500 -1.8520 REAL CONSTANT SET 0.0000 0.0000 REAL CONSTANT SET 0.40114 0.0000 REAL CONSTANT SET 0.59524 0.0000 REAL CONSTANT SET 0.0000 0.0000 REAL CONSTANT SET 0.10000E+11 0.0000 I TO 1 2 3 3 4 4 5 5 iE-04 6 6 6 6 7 .7 8 10 11 12 13 27 BY 1 ITEMS 1 TO 6 0.0000 0.0000 ITEMS 1TO 6 0.0000 0.0000 ITEMS 1TO 6 33.000 4.0200 ITEMS 7 TO 12 0.0000 0.0000 ITEMS-1 TO 6 0.0000 0.0000 ITEMS 7 TO 12 .*0.0000, 0.0000 ITEMS 1 TO 6 33.000 4.0200 ITEMS 7 TO 12 3.0000 0.0000 ITEMS 1TO 6 0.0000 2.0300 ITEMS 7 TO 12 0.0000 0.0000 ITEMS 13 TO 18 0.34500 0.0000 ITEMS 19 TO 24 0.34500 0.0000 ITEMS ITO 6 0.0000 -0.36500 ITEMS 7TO 12 0.18400 1.1270 ITEMS 1 TO 6 0.0000 0.12500 ITEMS 1 TO 6 .0.0000 0.0000 ITEMS 1 TO 6 0.0000' 0.0000 ITEMS ITO 6 0.0000 0.50000 ITEMS 1 TO 6 0.0000 0.0000 0.0000 0.0000 4.0200 0.0000 0.0000 0.0000 4.0200 0.0000

1. 9075

-1. 907 5 -1. 9075 . 0.0000 1.8520 -1.8520 0.0000 0.0000 0.0000 0.0000 . 0.0000 0.0000 0.0000 15.588 15.588 0.0000 0.0000 15.588 15.588 0.34500 0.28000

0. 0000 0.0000 0.29600 0.29600 0.10000E+11

0. 0000 0.0000 0.10000E+11

0. 0000 Page E25

-4.- .D REAL CONSTANT SET 14 ITEMS 1 TO 6 10.000 0.0000 0.0000 0.0000 0.0000 REAL CONSTANT SET 15 ITEMS 1 TO 6 100.00 1000.0 1000.0 1.0000 1.0000 REAL CONSTANT SET 15 ITEMS 7 TO 12 0.0000 1000.0 0.0000 0.0000 0.0000 REAL CONSTANT SET 17 ITEMS 1 TO 6 0.66000E+07 0.0000 0.0000 0.0000 0.0000 REAL CONSTANT SET 18 ITEMS 1 TO 6 0.58000E+07 0.0000 0.0000 0.0000 0.0000 REAL CONSTANT SET 19 ITEMS 1 TO 6 0.0000 0.0000 0.0000 0.50000 0.0000 '1 ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 5.7.1 ANSYS/Mechanical U 00251976 VERSION-INTEL NT 21:40:21 MAR 06, 2003 CP-EDG Exhaust Piping REAL CONSTANT SET 20 ITEMS 1 TO 6 10.000 0.0000 0.0000 0.0000 0.0000 REAL CONSTANT SET 21 ITEMS 1 TO 6 10.000 0.0000 0.0000 -0.0000 0.0000 REAL CONSTANT SET 22 ITEMS 1 TO 6 - 10.000 0.0000 0.0000 0.0000 0.0000 REAL CONSTANT SET 23 ITEMS 1 TO 6 10.000 0.0000 0.0000 0.0000 0.0000 REAL CONSTANT SET 24 ITEMS 1 TO 6 10.000 0.0000 0.0000 0.0000 0.0000 REAL CONSTANT SET 25 ITEMS 1 TO 6 363.00 0.0000 0.0000 0.37500 -10.000 REAL CONSTANT SET 26 ITEMS 1 TO 6 363.00 0.0000 0.0000 1.2500 -10.000 REAL CONSTANT SET 27 ITEMS 1 TO 6 1.5000 0.0000 0.0000 0.0000 0.0000 0.0000

• 0.0000 0.0000 0.0000 0.0000 0.10000E+ll 0.991 0.0000 0.0000 0.0000 0.0000 0.0000 1515.0 1832.0 0.0000 LIST ALL SELECTED ELEMENTS.

1 (LIST NODES) ANSYS - ENGINEERING ANALYSIS ANSYS/Mechanical U 00251976 VERSION-INTEL NT EDW Exhaust Piping ELEM MAT TYP REL ESY SEC 1 1 1 1 0 1 1 2 1 1 1 0 1 2 3 1 1 i 0 1 3 4 1 1 1 0 1 4 5 1 1 2 0 1 5 6 1 1 2 0 1 6 7 1 1 2 0 1 7 8 1 1 2 0-1 8 SYSTEM RELEASE 5.7.1 21:40:21 MAR.06, 2003'CP-1.021 NODES 2 3 4 5 6 7 8 9 Page 0 0 0 0 0 0 0 0 E26

1-v - - ~vv vv 9 1 1 10 1 1 11 1 1 12 1 2 13 1 1 14 1 1 15 1 1 16 1 1 17 1 1 18 1 1 19 1 2 20 1 1 30 2 13 31 2 13 32 2 13 33 2 13 34 2 13 35 2 13 40 2 13 41 2 13 42 2 13 43 2 13 44 2 13 45 2 13 50 2 13 51 2 13 52 2 13 53 2 13 54 2 13 55 2 13 56 2 13 57 2 13 58 2 13 59 2 13 60 2 13 .61 2 13 70 3 3 71 3 3 72 3 3 73 3 3 74 3 6 75 3 6 1 0 1 1 0 1 1 0 1 3 0 1 1 0 1 1 0 1 1 0 1 1 0 1 4 0 1 4 0 1 5 0 1 4 0 1 6 0 1 6 0 1 6 0 1 6 0 1 6 0 1 6 0 1 6 0 1 6 0 1 6 0 1 6 '0 1 6 0 1 6 0 1 7 0 1 7 0 1 7 0 1 7 0 1 7 0 1 7 0 1 7 0 1 7 0 1 7 0 1 7 0 1 7 0 1 7 0 1 15 0 1 15 0 1 15 0 1 15 0 1 8.0 1 8 0 9 10 11 12 13 14 15 16 17 18 19 20 30 31 31 33 34 35 40 41 41 43 44 45 50 '51 52 53 55 58 53 56 58 59 60 ,61 .3 3 11 11 37 34 10 0 -11 0 12 0 13 100 14 0 15 0 16 0 17 0 18 0 19 0 20 101 21 0 31 3 32 3 33 3 35 3 35 3 36 3 41 11 42 11 43 11 45 11 45 11 46 11 51 102 52 102 53 102 54 102 51 102 55 102 56 103 60 103 57 103 58 103 59 103 60 103 37 0 38 0 47 0 48 0-30 38 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 5.7.1 ANSYS/Mechanical U. 00251976 VERSION-INTEL NT 21:40:21 MAR 06, 2003 CP-EDG Exhaust Piping 1.041 ELEM MAT TYP REL ESY SEC NODES 76 3 6 8 0 77 3 6 8 0 78 3 3 15 0 79 3 3 15 0 80 3 3 15 0 81 3 3 15 0 82 3 6 12 0 83 3 5 19 0 84 3 5 19 0 85 3 6 12 0 86 3 3 15 0 87 3 3 15 0 88 3 14 25 0 89 3 14 26 0 94 3 7 14 0 95 3 8 20 0 96 3 9 21 0 97 3 10 22 0 1 47 40 1 44 48 1 18 62 1 18 63 1 18 64 1 18 65 1 52 62 1 63 55 1 56 64 1 65 59 1 3 39' 1 -11 49 1 .39 33 1 49 43 1 21 - 22 1 21 22 1 -21 22 1 21 22 0 0 0 0 0 0 39 49 33 43 Page E27

v dA. i v v 98 3 11 23 0 1 21 22 99 3 12 24 0 1 21 22 100 3 4 10 0 1 4 101 3 4 10 0 1 10 102 3 4 11 0 1 21 200 3 10 18 0 1 32 200 201 3 12 17 0 1 32 200 203 3 10 18 0 1 36 201 204 3 12 17 0 1 36 201 205 3 10 18 0 1 42 202 206 3 12 17 0 1 42 202 208 3 10 18 0 1 46 203 209 3 12 17 0 1 46 203 220 3 3 15 0 1 18 72 0 221 3 3 15 0 1 18 73 0 222 3 3 15 0 1 18 74 0 223 3 3 15 0 1 18 75 0 224 3 15 27 0 1 72 52 225 3 i5 27 0 1 73 55 226 3 15 27 0 1 74 56 227 3 15 27

0. 1 75 59 LIST DATA TABLE ALL FOR ALL MATERIALS 1

ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 5.7.1 ANSYS/Mechanical U 00251976 VERSION-INTEL NT 21:40:21 MAR 06, 2003 CP-1.052 EDG Exhaust Piping BiKin P1 (BKIN) Table For Material 2 1 Temps 0.0000 Yld Strs 36000. Tang Mod 0.0000 ROUTINE COMPLETED

• CP -

1.052 ANSYS SOLUTION ROUTINE PERFORM A TRANSIENT ANALYSIS THIS WILL BE A NEW ANALYSIS NEW SOLUTION CONTROL OPTION IS ACTIVATED, THE-FOLLOWING COMMANDS ARE RESET TO NEW DEFAULTS: AUTOTS, DELTIM, NSUB, CNVTOL, LNSRCH, PRED, NROPT, TINTP, CUTCONTROL, OPNCONTROL, MONITOR, NEQIT, SSTIF, KBC. NO CONTACT, LOSS OF CONTACT OR STICK/SLIDE TIME PREDICTIONS ARE PERFORMED DO NOT INCLUDE TRANSIENT EFFECTS FOR ALL DOFS THIS LOAD STEP SMALL DEFORMATION ANALYSIS WRITE ALL ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL FOR ALL APPLICABLE ENTITIES TIME-1.0000 WARNING

• CP-1.072 TIME-21:40:22 The maximum number of substeps (NSBMX -

10) must be greater than the initial value for the number of substeps (NSBSTP -

.1000). The NSUBST command is ignored. Page E28

ACEL-0.0000 386.40 0.0000 COMMAND ***** ANSYS SOLVE 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 5.7.1 ANSYS/Mechanical U 00251976 VERSION-INTEL NT 21:40:22 MAR 06, 2003 CP-EDG Exhaust Piping 1.082 S O L U T I O N 0 P T I O N S PROBLEM DIMENSIONALITY... DEGREES OF FREEDOM..... ANALYSIS TYPE....... SOLUTION METHOD..... PLASTIC MATERIAL PROPERTIES NEWTON-RAPHSON OPTION... UX UY . 3-D UZ ROTX ROTY ROTZ . TRANSIENT . FULL . YES . PROGRAM CHOSEN INCLUDED..

• • • NOTE ***

CP-1.082 This load step will be a static (steady-state) step. TIME-21:40:22 NOTE *** CP-1.082 TIME-21:40:22 Nonlinear analysis, NROPT set to the FULL Newton-Raphson solution procedure for ALL DOFs. SOLCONTROL,ON uses sparse matrix direct solver WARNING *** CP-1.082 TIME-21:40:22 The program chosen initial timestep/load-factor is arbitrary. It is necessary for the user to supply a suitable initial timestep/load-factor through the NSUB or DELTIM command for convergence and overall efficiency. L O A D S T E P O P T I O N S LOAD STEP NUMBER................ 1 TIME AT END OF THE LOAD STEP.......... 1.0000 AUTOMATIC TIME STEPPING .ON INITIAL NUMBER OF SUBSTEPS.. 1 MAXIMUM NUMBER OF SUBSTEPS......... 1000 MINIMUM NUMBER OF SUBSTEPS.......... 1 START WITH TIME STEP FROM PREVIOUS SUBSTEP YES MAXIMUM NUMBER OF EQUILIBRIUM ITERATIONS.. 15 STEP CHANGE BOUNDARY CONDITIONS........ NO TRANSIENT (INERTIA) EFFECTS.......... OFF TERMINATE ANALYSIS IF NOT CONVERGED......YES (EXIT) CONVERGENCE CONTROLS..............USE DEFAULTS INERTIA LOADS X Y Z ACEL. ... i 0.0000 386.40 0.0000 COPY INTEGRATION POINT VALUES TO NODE.....YES, FOR ELEMENTS WITH PRINT OUTPUT CONTROLS............ DATABASE OUTPUT CONTROLS ITEM FREQUENCY COMPONENT ALL ALL ACTIVE MAT. NONLINEARITIES NO PRINTOUT NONLINEAR MONITORING INFO IS WRITTEN TO FILE-exhaust.mntr MAXIMUM NUMBER OF EQUILIBRIUM ITERATIONS HAS BEEN MODIFIED TO BE, NEQIT - 22, BY SOLUTION CONTROL LOGIC. ALL CURRENT ANSYS DATA WRITTEN TO FILE NAME-exhaust.rdb FOR POSSIBLE RESUME FROM THIS POINT Estimated number of active DOF-332. Maximum wavefront-49. Page E29

• -1~.

-ie. U Uww CROSS SECTION PARAMETERS, ELEMENT PT Y-COORD Z-COORD 1 1.127 1.852 2 -0.3650 1.852 3 -0.3650 -1.852 4 1.127 -1.852 CENTROID - ( 0.5609E-01, 0.000 6840E-15) AREA - 1.565 IY - 3.809 IZ - 0.3779 01 IW - 0.9069 PRINCIPAL M OF I: IYP - 3.809 1079E-16 CROSS SECTION PARAMETERS, ELEMENT PT Y-COORD Z-COORD 1 1.127 1.852 2 -0.3650 1.852 3 -0.3650 -1.852 4 1.127 -1.852 CENTROID - ( 0.5609E-01, 0.000 6840E-15) AREA - 1.565 IY - 3.809 IZ - 0.3779 01 IW - 0.9069 PRINCIPAL M OF I: IYP - 3.809 1079E-16 CROSS SECTION PARAMETERS, ELEMENT PT Y-COORD Z-COORD 1 1.127 1.852 2 -0.3650 1.852 3 -0.3650 -1.852 4 1.127 -1.852 CENTROID - l 0.5609E-01, 0.000 6840E-15) AREA

• 1.565 IY -

3.809 IZ - 0.3779 01 IW.- 0.9069 PRINCIPAL M OF I: IYP - 3.809 1079E-16 CROSS SECTION PARAMETERS, ELEMENT PT Y-COORD Z-COORD 1 1.127 1.852 2 -0.3650 1.852 3 -0.3650 -l1852 4 1.127 -1.852 CENTROID - ( 0.5609E-01, 0.000 6840E-15) AREA 1.565 ly - 3.809 IZ - 0.3779 01 IW - 0.9069 PRINCIPAL M OF I: IYP - 3.809 1079E-16 - CROSS SECTION PARAMETERS, ELEMENT. PT Y-COORD Z-COORD 1 1.127 1.852 2 -0.3650 1.852 - 3 -0.3650 -1.852 4 1.127 .-1.852 CENTROID - ( 0.5609E-01, 0.000 6840E-15) AREA - 1.565 IY - 3.809 IZ - 0.3779 01 IW - 0.9069 PRINCIPAL M OF I: IYP - 3.809 1079E-16 50 THICK 0.000 0.2960

0. 1840 0.2960 58 THICK

- 0.000 0.2960

0. 1840 0.2960 54 THICK 0.000

0. 2 960 0.1840 0.2960 SHEAR CENTER -

C -0.9584 IYZ - -0.3701E IZP 0.3779 SHEAR CENTER -0.9584 IYZ - -0.3701E-16 IZP - 0.3779 SHEAR CENTER - ( -0.9584 IYZ -0.3701E-16 J IZP - 0.3779 I, -0. J - 0.3349E-THETAP - 0. f -0. T - 0.3349E-THETAP - 0. I -0. J - 0.3349E-THETAP - 0. 55 THICK 0.000 0.2960

0. 1840

0. 2 960 SHEAR CENTER -

( -0.9584 -0. IYZ - -0.3701E-16 J - 0.3349E-IZP - 0.3779 THETAP - 0. 5 THICK 0.000 0.2960 0.1840 0.2960 1 SHEAR CENTER - ( -0.9584 -0. IYZ - -0.3701E-16 J - 0.3349E-IZP - 0.3779 THETAP - 0. Page E30

.*af#.1

• vLvv CROSS SECTION PARAMETERS, ELEMENT PT Y-COORD Z-COORD 1

1.127 1.852 2 -0.3650 1.852 3 -0.3650 -1.852 4 1.127 -1.852 CENTROID - ( 0.5609E-01, 0.000 6840E-15) AREA - 1.565 IY - 3.809 IZ - 0.3779 01 IW - 0.9069 PRINCIPAL M OF I: IYP.- 3.809 1079E-16 CROSS SECTION PARAMETERS, ELEMENT PT Y-COORD Z-COORD 1 1.127 1.852 2 -0.3650 1.852 3 -0.3650 -1.852 4 1.127 -1.852 CENTROID - ( 0.56609E-01, 0.000 6840E-15) AREA - 1.565 ly - 3.809 IZ - 0.3779 01 IW - 0.9069 PRINCIPAL M OF I; IYP - 3.809 1079E-16 CROSS SECTION PARAMETERS, ELEMENT PT Y-COORD Z-COORD 1 1.127 1.852 2 -0.3650 1.852 3 -0.3650 -1.852 4 1.127 -1.852 CENTROID - 0 0.5609E-01, 0.000 6840E-15) AREA - 1.565 ly - 3.809 IZ 0.3779 01 IW - 0.9069 PRINCIPAL M OF I: IYP - 3.809 1079E-16 CROSS SECTION PARAMETERS, ELEMENT PT Y-COORD Z-COORD 1 1.127 1.852 2 -0.3650 1.852 t 3 -0.3650 -1.852 4 1.127 -1.852 CENTROID - ( 0.5609E-01, 0.000 6840E-15) AREA - 1.565 ly - 3.809 IZ = 0.3779 01 IW - 0.9069 PRINCIPAL M OF I: -IYP - 3.809 1079E-16 CROSS SECTION PARAMETERS, ELEMENT PT Y-COORD Z-COORD 1 1.127 1.852 2- -0.3650 1.852 C -3 -0.3650 -1.852 a 4 1.127 -1.852 a CENTROID - ( 0.5609E-01, 0.000 6840E-15) AREA - 1.565 IY - 3.809 -IZ - 0.3779 01 IW - 0.9069 PRINCIPAL M OF I: IYP - 3.809 1079E-16 CROSS SECTION PARAMETERS, ELEMENT 59 THICK 0.000 0.2 960-

0. 1840 9.2960 52 THICK 0.000

0. 2960

0. 1840 0.2960 60 THICK 0.000

0. 2 960 0.1840 0.2960 SHEAR CENTER -

( -0.9584 IYZ - -0.3701E-16 IZP - 0.3779 SHEAR CENTER - ( -0.9584 IYZ - -0.3701E-16 IZP - 0.3779 SHEAR CENTER - C -0.9584 IYZ - 0.3701E-16 J IZP - 0.3779 -0. J - 0.3349E-THETAP - 0. F -0. J - 0.3349E-THETAP - 0. J - 0.3349E-THETAP - 0. 56 THICK 0.000 0.2960 0.1840 0.2960 SHEAR CENTER - ( -0.9584 -0. IYZ - -0.3701E-16 J - 0.3349E-IZP - 0.3779 THETAP - 0. 57. THICK 0.000 0.2960 ).1840 0.2960 ) SHEAR CENTER - ( -0.9584 IYZ - -0.3701E-16 J - IZP - 0.3779 THE -0.

0. 3349E-ETAP -

0. 53 Page E31

1 - &A'. L J&4U.Ji.J.UU PT Y-COORD 1 1.127 2 -0.3650 3 -0.3650 4 1.127 Z-COORD 1.852 1.852 -1.852 -1.852 CENTROID - ( 0.5609E-01, 0.000 6840E-15) AREA - 1.565 IY - 3.809 IZ - 0.3779 01 IW - 0.9069 PRINCIPAL M OF I: IYP - 3.809 1079E-16 6 THICK 0.000 0.2960 0.1840 0.2960 ) SHEAR CENTER - ( -0.9584 -0. IYZ - -0.3701E-16 J - 0.3349E-IZP - 0.3779 THETAP - 0. PT 1 2 34 CROSS SECTION PARAMETERS, ELEMENT Y-COORD Z-COORD 1.127 1.852 -0.3650 1.852 -0.3650 -1.852 1.127 -1.852 61 THICK 0.000 0.2960

0. 1840

0. 2 960 CENTROID -

( 0.5609E-01, 0.000 6840E-15) AREA - 1.565 IY - 3.809 IZ - 0.3779 01 IW - 0.9069 PRINCIPAL M OF I: IYP - 3.809 1079E-16 SHEAR CENTER - C -0.9584 -0. IYZ - -0.3701E-16 J - 0.3349E-IZP - 0.3779 THETAP - 0. PT 1 2 3 4 5 6 7 CROSS SECTION Y-COORD -2.030 -2.030 0.000 0.000 -2.030 0.000 2.030 PARAMETERS, ELEMENT Z-COORD 1.907 1.907 1.907 -1.907 -1.907 -1.907 -1.907 45 THICK 0.000 0.3450 0.000 0.2800 0.3450 0.000 0.3450 CENTROID - ( 0.000 7694E-16) AREA - IY - 11.49 IW - 14.00 PRINCIPAL M OF I: 000 f I 0.000 3.870 IZ 3.848 IYP - 11.49 SHEAR CENTER - ( IYZ - 0.000 IZP - 3.848 O. 000 0 0. J - 0.1391 ' THETAP - 0. PT 1 2 3 4 5 6 7 CROSS SECTION Y-COORD -2.030 2.030 0.000 0.000 -2.030 0.000 2.030 PARAMETERS, ELEMENT Z-COORD 1.907 1.907 1.907 -1.907 -1.907 -1.907 -1.907 41 THICK 0.000 0.3450 0.000 0.2800 0.3450 0.000 0.3450 SHEAR CENTER - ( 0.000 CENTROID-C 0.000 7694E-16) AREA - IY - 11.49 IW - 14.00 PRINCIPAL M OF I: 000 f 0.000 3.870 IZ - 3.841 I I 0. I - 0.1391 3 IYP - 11.49 IYZ - 0.000 IZP - 3.848 THETAP - 0. PT 1 2 3 4 5 6 7 CROSS SECTION Y-COORD -2.030

• 2.030 0.000 0.000

-2.030 0.000 2.030 PARAMETERS, ELEMENT 43 Z-COORD THICK 1.907 0.000 1.907 0.3450 1.907 0.000 -1.907 0.2800 -1.907 0.3450 -1.907 0.000 -1.907 0.3450 Page E32

V. L.VU) -r U* u Ul CENTROID - ( 0.000 7694E-16) AREA = ly - 11.49 IW - 14.00 PRINCIPAL M OF I: 000 0.000 ) SHEAR CENTER - ( 0.000 3.870 IZ - I0 0. 3.848 IYZ - 0.000 IZP - 3.848 J - 0.1391 THETAP - 0. IYP - 11.49

• PT 1

2 3 4 5 6 7 CROSS SECTION Y-COORD -2.030 2.030 0.000 0.000 -2.030 0.000 2.030 PARAMETERS, ELEMENT Z-COORD 1.907 1.907 1.907 -1.907 -1.907 -1.907 -1.907 42 THICK 0.000 0.3450 0.000 0.2800 0.3450 0.000 0.3450 CENTROID - ( 0.000 7694E-16) AREA - IY - 11.49 IW - 14.00 PRINCIPAL M OF I: 000 3.870 IZ - 0.000 ) SHEAR CENTER - ( 0.000 0. 3.848 IYZ - 0.000 IZP - 3.848 J - 0.1391 THETAP - 0. IYP - 11.49 PT 1 2 3 4 5 6 7 CROSS SECTION Y-COORD -2.030 2.030 0.000 0.000 -2.030 0.000 2.030 PARAMETERS, ELEMENT Z-COORD 1.907 1.907 1.907 -1.907 -1.907 -1.907 -1.907 4 4 THICK 0.000 0.3450 0.000 0.2800 0.3450

0. 000

0. 3450 CENTROID -

( 0.000 7694E-16) AREA - IY - 11.49 IW - 14.00 PRINCIPAL M OF I: 000 0.000 ) SHEAR CENTER - I 3.870 IZ - 0.000 0. 3.848 IYZ - 0.000 IZP - 3.848 J - 0.1391 THETAP - IYP - 11.49 0. PT 1 2 3 4 5 6 7 CROSS SECTION Y-COORD -2.030 2.030 0.000 0.000 -2.030 0.000 2.030 PARAMETERS, ELEMENT Z-COORD 1.907 1.907 1.907 -1.907 -1.907 -1.907 -1.907 40 THICK 0.000 0.3450

0. 000 0.2800

0. 3450 0.000 0.3450 CENTROID -

C 0.000 7694E-16) AREA - IY - 11.49 IW - 14.00 PRINCIPAL M OF I: 000 3.870 IZ - 0.000 ) SHEAR CENTER - ( 0.000 0. 3.848 IYZ - 0.000 IZP - 3.848 J - 0.1391 THETAP - IYP - 11.49 0. CROSS SECTION PT. Y-COORD 1 -2.030-2 2.030 3 0.000 4 0.000 5 -2.030 I6 0.000 7 2.030 PARAMETERS, ELEMENT Z-COORD 1.907 1.907 1.907 -1.907 -1.907 -1.907 -1.907 35 THICX 0.000 0.3450 0.000 0.2800 0.3450 0.000

0. 3450 CENTROID -

( 0.000 7694E-16) AREA - IY - 11.49 0.000 ) SHEAR CENTER - ( 0.000 3.870 IZ - 0.

3. 848 IYZ -

0.000 J - 0.1391 Page E33

-fi r-W'.D

• WLu&

tvvI IW 14.00 PRINCIPAL M OF I: 000 IYP - 11.49 IZP - 3.848 THETAP - 0. CROSS SECTION PARAMETERS, ELEMENT PT Y-COORD Z-COORD 1 -2.030 1.907 2 2.030 1.907 3 0.000 1.907 4 0.000 -1.907 5 -2.030 -1.907 6 0.000 -1.907 7 2.030 -1.907 31 THICK -0.000 0.3450

0. 000 0.2800 0.3450 0.000 0.3450 CENTROID -

( 0.000 7694E-16) AREA - IY - 11.49 IW - 14.00 PRINCIPAL M OF I: 000 r 0.000 3.870 IZ - 3.848 IYP - 11.49 SHEAR CENTER - ( 0.000 0. IYZ - 0.000 IZP - 3.848 J - 0.1391 THETAP - 0. PT 1 2 3 4 5 6 7 CROSS SECTION PARAMETERS, ELEMENT Y-COORD Z-COORD -2.030 1.907 2.030 1.907 0.000 1.907 0.000 -1.907 -2.030 -1.907 0.000 -1.907 2.030 -1.907 33 THICK 0.000 0.3450 0.000 0.2800 0.3450 0.000

0. 3450 CENTROID -

( 0.000 7694E-16) AREA - IY - 11.49 IW - 14.00 PRINCIPAL M OF I: 000 3.870 IZ 0.000 ) SHEAR CENTER - ( 0.000 0. 3.848 IYZ - 0.000 IZP - 3.848 J - 0.1391 THETAP - IYP - 11.49 O.. PT 1 2 3 4 5 6 7 CROSS SECTION Y-COORD -2.030 2.030 0.000 0..000 -2.030 0.000 2.030 PARAMETERS, ELEMENT Z-COORD 1.907 1.907 1.907 -1.907 -1.907 -1.907 -1.907 3: THICK 0.000

0. 3450 0.000

0. 2800 0.3450 0.000 0.3450 2

CENTROID - I 0.000 7694E-16) AREA - IY - 11.49 IW - 14.00 PRINCIPAL M OF I: 000 I 0.000 3.870 IZ-3.848 IYP - 11.49 ) SHEAR CENTER - ( IYZ - 0.000 IZP - 3.848 0.000 0. J - 0.1391 THETAP 0. PT 1 2 3 4 5 6 7 CROSS SECTION Y-COORD -2.030 2.030 0.000 0.000 -2.030 0.000 2.030 PARAMETERS, ELEMENT 34 Z-COORD THICK 1.907 0.000 1.907 0.3450 1.907 0.000 -1.907 0.2800 -1.907 0.3450 -1.907 0.000 -1.907 0.3450 CENTROID - I 0.000 7694E-16) AREA - IY - 11.49 IW - 14.00 PRINCIPAL N OF I: 000 0.000 ) SHEAR CENTER - ( I

0. 000 0.

3.870 IZ - 3.848 IYZ - 0.000 IYP - J - 0.1391 THETAP - 11.49 IZP - 3.848 0. Page E34

V PT 1 2 3 4 5 6 7 CROSS SECTION Y-COORD -2.030 2.030 0.000 0.000 -2.030 0.000 2.030 PARAMETERS, ELEMENT Z-COORD 1.907 1.907 1.907 -1.907 -1.907 -1.907 -1.907 30 THICK

0. 000 0.3450 0.000 0.2800 0.3450 0.000

0. 3450 CENTROID -

( 0.000 7694E-16) AREA - IY - 11.49 IW - 14.00 PRINCIPAL M OF I: 000 0.000 ) SHEAR CENTER - ( O.000 3.870 IZ - O. 3.848 IYZ - 0.000 IZP - 3.848 J - 0.1391 THETAP - 0. IYP - 11.49

• • • • • CENTROID, MASS, AND MASS MOMENTS OF INERTIA *****

CALCULATIONS ASSUME ELEMENT MASS AT ELEMENT CENTROID TOTAL MASS - 15.819 MOM. OF INERTIA ABOUT ORIGIN MOM. OF INERTIA ABOUT CENTROID CENTROID XC - YC - ZC - -244.93 -72.114

0. 0000 IXX -

IYY - IZZ - IXY - IYZ - IZX - 0.2267E+06 0.1148E+07 0.1374E+07 -0.4022E+06 0.000 0.000 IXX - IYY - IZZ - IXY - IYZ - IZX - 0.1444E+06

0. 1986E+06 0.3428E+06

-0.1228E+06 0.000 0.000 MASS

SUMMARY

BY ELEMENT TYPE *** TYPE MASS 1 11.4288 2 2.15954 4 1.39752 13 0.832796 Range of element maximum matrix coefficients in global coordinates Maximum-1.052654208E+10 at element 4. Minimum-10 at element 95.

• • • WARNING ***

CP-2.183 TIME-21:40:26 Coefficient ratio exceeds l.0e8 - Check results.

• • • ELEMENT MATRIX FORMULATION TIMES TYPE NUMBER ENAME TOTAL CP AVE CP 1

2 3 4 5 6 .7 8 9 10 11 12 13 14 15 Time at 18 2 14 3 2 6 1 1 S.5 1 5 24 2 4 end of PIPE16. 0.000. 0.000000 PIPE18 0.000 0.000000 BEAM4 0.000 0.000000 MASS21 0.000 0.000000 COMBIN40 0.000 0.000000 COMBIN40 0.000 0.000000 COMBIN14 0.000 0.000000 COMBIN14 0.000 0.000000 COMBIN14 0.000 0.000000 COMBIN14 0.000 0.000000 COMBIN14 0.000 0.000000 COMBIN14 0.000 0.000000 BEAM24 0.050 0.002086 COMBIN37 0.000 0.000000 LINK10 0.000 0.000000 element matrix formulation CP-2.19315362. Page E35

-= .
. 1-A"Uj.-rV44QJ1/-jVV FORCE CONVERGENCE VALUE MOMENT CONVERGENCE VALUE - Time at end of matrix assembly 3620. CRITERION-2Z99. CRITERION-CP-2.19315362. 18.47 11.73 SPARSE MATRIX DIRECT SOLVER. Number of equations -

332, Maximum wavefront Memory available for solver -

0.76 MB Memory required for in-core - 0.06 MB Optimal memory required for out-of-core - 0.04 MB Least memory required for out-of-core - 0.04 MB EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX FORCE CONVERGENCE VALUE - 0.1719E-07 CRITERION-MOMENT CONVERGENCE VALUE - 0.4649E-07 CRITERION- >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION ELEMENT RESULT CALCULATION TIMES TYPE NUMBER ENAME TOTAL CP AVE CP 49 DOF INC-

22. 63 124.8 1

-0.9276E-01 <<< CONVERGED <<< CONVERGED 1 18 PIPE16 2 2 PIPE18 3 14 BEAM4 4 3 MASS21 5 2 COMBIN40 6 6 COMBIN40 7 1 COMBIN14 8 1 COMBIN14 9 1 COMBIN14 10 5 COMBIN14 11 1 COMBIN14 12 5-COMBIN14 13 24 BEAM24 14 2 COMBIN37 15 4 LINK10 0.010 0.000

0. 000

0. 000 0.000 0.000 0.000 0.000

0. 000 0.000 0.000 0.000

'0.010 0.000I 0.000 0.000556 0.000000

0. 000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000417 0.000000 0.000000 AVE CP

• • • NODAL LOAD CALCULATION TIMES TYPE NUMBER ENAME TOTAL CP 1

18 PIPE16 0.000 0.000000 2 2 PIPE18 0.000 0.000000 3 14 BEAM4 0.000 0.000000 4 3 MASS21 0.000 0.000000 5 2 COMBIN40 0.000 0.000000 6 6 COMBIN40 0.000 0.000000 7 1 COMBIN14 0.000 0.000000 8 1 COMBIN14 0.000 0.000000 9 1 COMBIN14 0.000 0.000000 10 5 COMBIN14 0.000 0.000000 11 1 COMBIN14 0.000 0.000000 12 5 COMBIN14 0.000 0.000000 13 24 BEAM24 0.000 0.000000 14 2 COMBIN37 0.000 0.000000 15 4 LINK10 0.000 0.000000 LOAD STEP 1 SUBSTEP 1 COMPLETED. TIME - 1.00000 TIME INC - 1.0000 CUM ITER - 1

• • • PROBLEM STATISTICS ACTUAL NO. OF ACTIVE DEGREES OF FREEDOM -

R.M.S. WAVEFRONT SIZE - 0.0 332

• • • ANSYS BINARY FILE STATISTICS BUFFER SIZE USED-16384 0.125 MB WRITTEN ON ELEMENT MATRIX FILE: exhaust.emat 0.188 MB WRITTEN ON ELEMENT SAVED DATA FILE: exhaust.esav 0.063 MB WRITTEN ON ASSEMBLED MATRIX FILE: exhaust.full 0.188 MB WRITTEN ON RESULTS FILE: exhaust.rst TIME-2.0000
    • WARNING ***

CP-2.584 TIME-21:40:27 Page E36

I--- -W
,
W
The maximum number of substeps (NSBMX -

10) must be greater than the initial value for the number of substeps (NSBSTP -

1000). The NSUBST command is ignored. ACEL-0.0000 386.40 0.0000 PARAMETER WIND 300.0000 PARAMETER PRESSURE - 0.6395000 PARAMETER PRESSW4 - 2.893738 SELECT FOR ITEM-ELEM COMPONENT-IN RANGE 1 TO 4 STEP 1 4 ELEMENTS (OF 89 DEFINED) SELECTED BY ESEL COMMAND. ALSO SELECT FOR ITEM-ELEM COMPONENT-IN RANGE 9 TO 16 STEP 1 12 ELEMENTS (OF 89 DEFINED) SELECTED BY ESEL COMMAND. SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS LKEY - 4 KVAL 1 VALUES - 14.069 14.069 14.069 14.069 SELECT FOR ITEM-ELEM COMPONENT-IN RANGE 5 TO 8 STEP 1 4 ELEMENTS (OF 89 DEFINED) SELECTED BY* ESEL COMMAND. SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS LKEY - 4 KVAL - 1 VALUES - 23.022 23.022 23.022 23.022 SELECT FOR ITEM-ELEM COMPONENT-IN RANGE 30 TO 31 STEP 1 2 ELEMENTS (OF 89 DEFINED) SELECTED BY ESEL COMMAND. ALSO SELECT FOR ITEM-ELEM COMPONENT-IN RANGE 40 TO 41 STEP -1 4 ELEMENTS (OF 89 DEFINED) SELECTED BY ESEL COMMAND. SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED BEAM ELEMENTS LKEY - 1 VALIVALJ 11.575 11.575 SELECT FOR ITEM=ELEM COMPONENT-IN RANGE 34 TO 35 STEP 1 2 ELEMENTS (OF 89 DEFINED) SELECTED BY ESEL COMMAND. ALSO SELECT FOR ITEM-ELEM COMPONENT-IN RANGE 44 TO 45 STEP 1 4 ELEMENTS (OF 89 DEFINED) SELECTED BY ESEL COMMAND. SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED BEAM ELEMENTS LKEY - 1 VALIVALJ -11.575 -11.575 ALL SELECT FOR ITEM-ELEM COMPONENT-IN RANGE 1 TO 227 STEP 1 89 ELEMENTS (OF 89 DEFINED) SELECTED BY ESEL COMMAND.

• • • • f ANSYS SOLVE COMMAND
• WARNING ***

CP-2.604 TIME-21:40:28 This load step will be a static (steady-state) step. NOTE **t CP-2.604 TIME-21:40:28 The step data was checked and warning messages were found. Page E37

X-C "
. r'"V4-rV'fX.Vj$_ Luv Please review output or errors file ( file.err ) for these warning messages.

• • • • NOTE ***

Nonlinear analysis, NROPT procedure for ALL DOFs. CP-2.604 TIME-21:40:28 set to the FULL Newton-Raphson solution SOLCONTROL,ON uses sparse matrix direct solver 1

• • • • • ANSYS -

ENGINEERING ANSYS/Mechanical U 00251976 VERSION-ANALYSIS SYSTEM RELEASE 5.7.1 -INTEL NT 21:40:28 MAR 06, 2003 CP-2.614 EDG Exhaust Piping L O A D S T E P O P T I O N S LOAD STEP NUMBER. TIME AT END OF THE LOAD STEP. AUTOMATIC TIME STEPPING......... INITIAL NUMBER OF SUBSTEPS......... MAXIMUM NUMBER OF SUBSTEPS......... MINIMUM NUMBER OF SUBSTEPS......... MAXIMUM NUMBER OF EQUILIBRIUM ITERATIONS. STEP CHANGE BOUNDARY CONDITIONS........ TRANSIENT (INERTIA) EFFECTS. TERMINATE ANALYSIS IF NOT CONVERGED...... CONVERGENCE CONTROLS. INERTIA LOADS X ACEL............. 0.0000 38 COPY INTEGRATION POINT VALUES TO NODE...... PRINT OUTPUT CONTROLS DATABASE OUTPUT CONTROLS ITEM FREQUENCY COMPONENT ALL ALL 2 2.0000 ON 1 100 1 15 NO OFF YES (EXIT) USE DEFAULTS Y Z 6.40 0.0000

YES, FOR ELEMENTS WITH ACTIVE MAT. NONLINEARITIES NO PRINTOUT NONLINEAR MONITORING INFO IS WRITTEN TO FILE-exhaust.mntr MAXIMUM NUMBER OF EQUILIBRIUM ITERATIONS HAS BEEN MODIFIED TO BE, NEQIT -

22, BY SOLUTION CONTROL LOGIC. FORCE CONVERGENCE VALUE 2221. MOMENT CONVERGENCE VALUE - 5680. CRITERION= 24.90 CRITERION-125.7 ERROR *** CP-2.714 TIME-21:40:28 DOF (e.g. Displacement) limit exceeded at time 2 (load step 2 substep 1 equilibrium iteration 1)' Max.absolute value-58021552.2 (limit-1000000) at UZ of node 1 May be due to an unrestrained or unstable model. >>> DOF LIMIT EXCEEDED. MAX VALUE- 0.5802155E+08 LIMIT- 0.000000 LOAD STEP 2 SUBSTEP 1 NOT COMPLETED. CUM ITER - 2 BEGIN BISECTION NUMBER 1 NEW TIME INCREMENT-0.50000 FORCE CONVERGENCE VALUE - 1111. MOMENT CONVERGENCE VALUE - 2840. CRITERION-22.89 CRITERION-123.2

• • • ERROR ***

CP-2.784 TIME-21:40:29 DOF (e.g. Displacement) limit exceeded at time 1.5 (load step 2 substep 1 equilibrium iteration 1) Max.absolute value-29010776.1 (limit-1000000) at UZ of node 1 May be due to an unrestrained or unstable model. >>> DOF LIMIT EXCEEDED. MAX VALUE- 0.2901078E+08 LIMIT- 0.000000

• • • LOAD STEP 2

SUBSTEP 1 NOT COMPLETED. CUM ITER - 3 BEGIN BISECTION NUMBER 2 NEW TIME INCREMENT- 0.25000 FORCE CONVERGENCE VALUE 555.3 MOMENT CONVERGENCE VALUE - 1420. CRITERION= 22.36 CRITERION-122.5 Page E38

• • • ERROR ***

CP-2.864 TIME-21:40:29 DOF (e.g. Displacement) limit exceeded at time 1.25 (load step 2 substep 1 equilibrium iteration 1) Max.absolute value-14505388 (limit-1000000) at UZ of node 1'. May be due to an unrestrained or unstable model. >>> DOF LIMIT EXCEEDED. MAX VALUE- 0.1450539E+08 LIMIT-0.000000

• • • LOAD STEP 2

SUBSTEP 1 NOT COMPLETED. CUM ITER - 4

• • • BEGIN BISECTION NUMBER 3

NEW TIME INCREMENT-0.12500 FORCE CONVERGENCE VALUE - 277.6 MOMENT CONVERGENCE VALUE - 710.0 CRITERION-22.22 CRITERION-122.4 ERROR

• CP-2.954 TIME-21:40:29 DOF (e.g.

Displacement) limit exceeded at time 1.125 (load step 2 substep 1 equilibrium iteration 1) Max.absolute value-7252694.02 (limit-1000000) at UZ of node 1 May be due to an unrestrained or unstable model. >>> DOF LIMIT EXCEEDED. MAX VALUE-7252694. LIMIT- 0.000000 LOAD STEP 2 SUBSTEP 1 NOT COMPLETED. CUM ITER - 5 BEGIN BISECTION NUMBER 4 NEW TIME INCREMENT- 0.62500E-01 FORCE CONVERGENCE VALUE MOMENT CONVERGENCE VALUE - 138.8 355.0 CRITERION-22.19 CRITERION-122.3

• • • ERROR CP-3.024 TIME-21:40:30 DOF (e.g.

Displacement) limit exceeded at time 1.0625 (load step 2 substep 1 equilibrium iteration 1) Max.absolute value-3626347.01 (limit-1000000) at UZ of node 1 May be due to an unrestrained or unstable model. >>> DOF LIMIT EXCEEDED. MAX VALUE-3626347. LIMIT- 0.000000

• • LOAD STEP 2

SUBSTEP 1 NOT COMPLETED. CUM ITER - 6 BEGIN BISECTION NUMBER 5 NEW TIME INCREMENT-0.31250E-0l FORCE CONVERGENCE VALUE 69.41 MOMENT CONVERGENCE VALUE - 177.5 CRITERION-22.18 CRITERION-122.3

• • • ERROR ***

CP-3.084 TIME-21:40:30 DOF (e.g. Displacement) limit exceeded at time 1.03125 (load step 2 substep 1 equilibrium iteration 1) Max.absolute value-1813173.51 (limit-1000000) at UZ of node 1. May be due to an unrestrained or unstable model. >>> DOF LIMIT EXCEEDED. MAX VALUE-1813174. LIMIT- 0.000000

• • • LOAD STEP 2

SUBSTEP 1 NOT COMPLETED. CUM ITER - 7

• • • BEGIN BISECTION NUMBER 6

NEW TIME INCREMENT- 0.15625E-01 FORCE CONVERGENCE VALUE - 34.70 CRITERION-22.18 MOMENT CONVERGENCE VALUE - 88.74 CRITERION-122.3 EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOE INC-FORCE CONVERGENCE VALUE - 0.1136E+17 CRITERION-23.71 MOMENT CONVERGENCE VALUE - 0.7798E-01 CRITERION-216.8

• RESIDUAL INCREASED. PREV SOLN REMOVED. DESCENT PARAM SET FORCE CONVERGENCE VALUE -

34.71 CRITERION-22.63 MOMENT CONVERGENCE VALUE - 88.74 CRITERION-124.8 EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC-FORCE CONVERGENCE VALUE - 0.1136E+17 CRITERION-24.19 MOMENT CONVERGENCE VALUE - 0.7887E-01 CRITERION-221.2 EQUIL ITER 3 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC-FORCE CONVERGENCE VALUE - 0.5751E+06 CRITERION-23.45 MOMENT CONVERGENCE VALUE - 0.4750E-01 CRITERION-125.0 EQUIL ITER 4 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC-FORCE CONVERGENCE VALUE 0.3575E+06* CRITERION-23.94 MOMENT-CONVERGENCE VALUE - 0.2180E-06 CRITERION-130.0 EQUIL ITER 5 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC-FORCE CONVERGENCE VALUE - 0.1887E-06 CRITERION-24.43 MOMENT CONVERGENCE VALUE - 0.110SE-06 CRITERION-135.8 RESIDUAL DECREASED. DESCENT PARAMETER SET TO.0.2500 >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 5 LOAD STEP 2 SUBSTEP 1 COMPLETED. CUM ITER - TIME - 1.01563 TIME INC - 0.156250E-01

• • • AUTO STEP TIME:

NEXT TIME INC - 0.15625E-Oi UNCHANGED 0.9066E+06 <<< CONVERGED TO 1.000 - 0.9066E+06 <<< CONVERGED -0.9066E+06 "< CONVERGED -0.5956 '<< CONVERGED 0.2196 '<< CONVERGED <<< CONVERGED 12 Page E39

Lfll%. LtUJ.U FORCE CONVERGENCE VALUE - 34.70 CRITERION-22.08 MOMENT CONVERGENCE VALUE - 88.74 CRITERION-122.8 EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOE INC-0.1414 FORCE CONVERGENCE VALUE - 0.5451E-07 CRITERION-22.55 <<< CONVERGED MOMENT CONVERGENCE VALUE - 0.1129E-06 CRITERION-126.8 <<<< CONVERGED >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1 LOAD STEP 2 SUBSTEP 2 COMPLETED. CUM ITER - 13 TIME - 1.03125 TIME INC - 0.156250E-01 AUTO TIME.STEP:. NEXT TIME INC - 0.23438E-01 INCREASED (FACTOR - 1.5000) FORCE CONVERGENCE VALUE - 52.06 CRITERION-22.10 MOMENT CONVERGENCE VALUE - 133.1 CRITERION-124.3 EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC-FORCE CONVERGENCE VALUE - 0.4375E-07 CRITERION-22.78 MOMENT CONVERGENCE VALUE - 0.1715E-06 CRITERION-131.3 >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

• • • LOAD STEP 2

SUBSTEP 3 COMPLETED. CUM ITER -

• • • TIME -

1.05469 TIME INC - 0.234375E-01 0.2120 <<< CONVERGED <<< CONVERGED 14

• • • AUTO TIME STEP:

NEXT TIME INC - 0.35156E-01 INCREASED (FACTOR - 1.5000) FORCE CONVERGENCE VALUE MOMENT CONVERGENCE VALUE - EQUIL ITER 1 COMPLETED. I FORCE CONVERGENCE VALUE MOMENT CONVERGENCE VALUE -

• RESIDUAL INCREASED.

PREV 78.09 CRITERION-22.34 199.7 CRITERION-128.7 NEW TRIANG MATRIX. MAX DOT INC-0.3175E+10 CRITERION-23.58 0.1834E-06 CRITERION-142.0 SOLN REMOVED. DESCENT PARAM SET 0.3181 <<< CONVERGED TO 1.000 FORCE CONVERGENCE VALUE - 78.09 CRITERION-. 22.79 MOMENT CONVERGENCE VALUE - 193.7 CRITERION-131.3 EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INO FORCE CONVERGENCE VALUE - 0.3175E+10 CRITERION-24.06 MOMENT CONVERGENCE VALUE - 0.1559E-06 CRITERION-144.9 EQUIL ITER 3 COMPLETED. NEW TRIANG MATRIX. MAX DOT INC FORCE CONVERGENCE VALUE 0.4739E+05 CRITERION-24.27 MOMENT CONVERGENCE VALUE - 0.2416E-06 CRITERION-137.7 EQUIL ITER 4 COMPLETED. NEW TRIANG MATRIX. MAX DOT INC' FORCE CONVERGENCE VALUE - 0.5477E-07 CRITERION-24.74 MOMENT CONVERGENCE VALUE - 0.2111E-06 CRITERION-139.9 RESIDUAL DECREASED. DESCENT PARAMETER SET TO 0.2500 >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION.- 4 LOAD STEP 2 SUBSTEP 4 COMPLETED. CUM ITER - TIME - 1.08984 TIME INC - 0.351563E-01

• t*

AUTO STEP TIME: NEXT TIME INC - 0.35156E-01 UNCHANGED 0.3181 <<< CONVERGED -0.2964 <<< CONVERGED -0.2431E-02 <<< CONVERGED <<< CONVERGED 18 FORCE CONVERGENCE VALUE - 78.09 CRITERION-22.84 MOMENT CONVERGENCE VALUE - 199.7 CRITERION-129.1 EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOT INC- 0.8008E-02 FORCE CONVERGENCE VALUE - 0.2345E-07 CRITERION-24.10 <<< CONVERGED MOMENT CONVERGENCE VALUE - 0.2452E-06 CRITERION-131.7 <<< CONVERGED >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1 LOAD STEP 2 SUBSTEP 5 COMPLETED. CUM ITER - 19 TIME - 1.12500 TIME INC - 0.351563E-D1 AUTO TIME STEP: NEXT TIME INC - 0.52734E-01 INCREASED (FACTOR - 1.5000) FORCE CONVERGENCE VALUE - 117.1 CRITERION-23.66 MOMENT CONVERGENCE VALUE - 299.5 CRITERION-129.1 EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOT INC- 0.1201E-01 FORCE CONVERGENCE VALUE - 0.4952E-07 CRITERION-25.85 <<< CONVERGED MOMENT CONVERGENCE VALUE - 0.2508E-06 CRITERION-131.8 <<< CONVERGED >>> SOLUTION CONVERGED AFTER EQUILIBRIUM.ITERATION 1 LOAD STEP 2 SUBSTEP 6 COMPLETED. CUM ITER - 20. TIME - 1.17773 TIME INC - 0;527344E-01 AUTO TIME STEP: NEXT TIME INC - 0.79102E-01 INCREASED (FACTOR - 1.5000) FORCE CONVERGENCE VALUE - 175.7 CRITERION-25.42 MOMENT CONVERGENCE VALUE - 449.3 CRITERION-129.3 EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC-FORCE CONVERGENCE VALUE - 0.6305E-07 CRITERION-29.42 MOMENT CONVERGENCE VALUE - 0.3125E-06 CRITERION-132.3 >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

• • • LOAD STEP 2

SUBSTEP 7 COMPLETED. CUM ITER -

• • • TIME -

1.25684 TIME INC - 0.791016E-01 0.1802E-01 <<< CONVERGED <<< CONVERGED 21 Page E40

r"1V.J-zVt.4U.J#_ Ljv

• • • AUTO TIME STEP:

NEXT TIME INC - 0.11865 INCREASED (FACTOR'- 1.5000) FORCE CONVERGENCE VALUE - 263.5 CRITERION-29.00 MOMENT CONVERGENCE VALUE - 673.9 CRITERION-129.9 EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC-FORCE CONVERGENCE VALUE - 0.5392E-07 CRITERION-36.21 MOMENT CONVERGENCE VALUE - 0.4333E-06. CRITERION-133.7 >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

• • • LOAD STEP 2

SUBSTEP 8 COMPLETED. CUM ITER -

• • • TIME -

1.37549 TIME INC - 0.118652

• • • AUTO TIME STEP:

NEXT TIME INC - 0.17798 INCREASED (F; 0.2703E-01 <<< CONVERGED <<< CONVERGED 22 LCTOR - 1.5000) FORCE CONVERGENCE VALUE - 395.3 CRITERION-35.78 MOMENT CONVERGENCE VALUE - 1011. CRITERION-131.6 EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC-FORCE CONVERGENCE VALUE - 0.6853E-07 CRITERION-48.12 MOMENT CONVERGENCE VALUE - 0.3843E-06 CRITERION-137.4 i>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1 LOAD STEP 2 SUBSTEP 9 COMPLETED. CUM ITER - TIME - 1.55347 TIME INC - 0.177979 A AUTO TIME STEP: NEXT TIME INC - 0.26697 INCREASED (E

0. 4054E-01 c<< CONVERGED C<< CONVERGED 23 FACTOR -

1.5000) FORCE CONVERGENCE VALUE - 593.0 CRITERION-47.66 MOMENT CONVERGENCE VALUE - 1516. CRITERION-135.8 EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC-FORCE CONVERGENCE VALUE - 0.1159E-06 CRITERION-67.67 MOMENT CONVERGENCE VALUE - 0.2315E-06 CRITERION-146.1 >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1 LOAD STEP 2 SUBSTEP 10 COMPLETED. CUM ITER - TIME - 1.82043 TIME INC - 0.266968 AUTO TIME STEP: NEXT TIME INC - 0.17957 DECREASED (FA FORCE CONVERGENCE VALUE - 398.8 CRITERION-66.64 MOMENT CONVERGENCE VALUE - 1020. CRITERION-144.1 EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC-FORCE CONVERGENCE VALUE - 0.6402E-07 CRITERION-81.32 MOMENT CONVERGENCE VALUE - 0.2748E-06 CRITERION-153.8 >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

• • • LOAD STEP 2

SUBSTEP 11 COMPLETED. CUM ITER - TIME - 2.00000 TIME INC - 0.179565. FINISH SOLUTION PROCESSING

0. 6081E-01

<<< CONVERGED <<< CONVERGED - 24 LCTOR - 0.6726)

0. 4090E-01

<<< CONVERGED <<c CONVERGED 25

• • • • • ROUTINE COMPLETED *****

CP - 5.077 1

• • • • • ANSYS - ENGINEERING ANALYSIS SYSTEM, RELEASE 5;7.1

,ANSYS/Mechanical U 00251976 VERSION-INTEL NT 21:40:39 MAR 06, 2003 CP-EDG Exhaust Piping 5.077 ANSYS RESULTS INTERPRETATION (POST1) *

• • • NOTE **

CP-5.077 TIME-21:40:39 The model contains an element type ( COMBIN37 ) that operates entirely in the nodal coordinate system. Viewing nodal displacements or forces in other than the nodal coordinate system may be. invalid. See the elements manual description for more information. NOTE

• CP-5.077 TIME-21:40:39 Reading results into the database (SET command) will update the current displacement and force boundary conditions in the database with the values from the results file for that load set.

Note that any subsequent solutions will use these values unless action is taken to either SAVE the current values or not overwrite them (/EXIT,NOSAVE). Page E41

.,-c 41v.

• L

-r= -~ DATA FILE CHANGED TO FILE-exhaust.rst USE LOAD STEP 1 SUBSTEP 0 'FOR LOAD CASE 0 SET COMMAND GOT LOAD STEP-TIME/FREQUENCY-1.0000 TITLE-EDG Exhau'st Piping 1 SUBSTEP-1 CUMULATIVE ITERATION-1 PRINT U I NODAL SOLUTION PER NODE

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 5.7.1

• • • 1*

ANSYS/Mechanical U 00251976 VERSION-INTEL NT 21:40:40 MAR 06, 2003 CP EDG Exhaust Piping POST1 NODAL DEGREE OF FREEDOM LISTING **** LOAD STEP-1 SUBSTEP-1 TIME-1.0000 LOAD CASE-0 THE FOLLOWING DEGREE OF FREEDOM RESULTS ARE IN GLOBAL COORDINATES 5.107 NODE UX UY UZ 1 -0.80678E-01-0.92760E-01 0.27256E-06 2 -0.80678E-01-0.B6537E-01 0.24697E-06 3 -0.80678E-01-0.80431E-01 0.22137E-06 4 -0.80678E-01-0.77225E-01 0.20615E-06 5 -0.80678E-01-0.76641E-01 0.20338E-06 6 -0.80678E-01-0.71356E-01 0.17900E-06 7 -0.80678E-01-0.65B70E-01 0.15461E-06 8 -0.80678E-01-0.60165E-01 0.13023E-06 .9 -0.80678E-01-0.54318E-01 0.10584E-06 10 -0.80678E-01-0.53645E-01 0.10307E-06 11 -0.80678E-01-0.50223E-01 0.88547E-07 12 -0.80678E-01-0.45279E-01 0.61568E-07 13 -0.76220E-01-0.46327E-01 0.38739E-07 14 -0.67148E-01-0.46320E-01 0.38739E-07 15 -0.57598E-01-0.46301E-01 0.38739E-07 16 -0.47571E-01-0.46271E-01 0.38739E-07 17 -0.37066E-01-0.46229E-01 0.38740E-07 18 -0.29019E-01-0.46191E-01 0.38740E-07 19 -0.18066E-01-0.46237E-01 0.38740E-07 20 0.17259E-08-0.6827$E-01 0.15911E-07 21 0.17259E-08-0.86191E-01-0.13299E-14 22 0.0000 0.0000 0.0000 30 0.0000 -0.81795E-04-0.14350E-02 31 0.0000 -0.77247E-04-0.45255E-04 32 0.0000 0.0000 0.0000 33 0.0000 -0.81689E-03 0.25411E-18 34 0.0000 -0.81795E-04 0.14350E-02 35 0.0000 -0.77247E-04 0.45255E-04 36 0.0000 0.0000 0.0000 37 -0.80678E-01-0.80431E-01 0.22137E-06 38 -0.80678E-01-0.80431E-01 0.22137E-06 39 -0.85431E-01-0.80414E-01 0.22137E-06 40 0.0000 -0.96110E-04-0.17159E-02 41 0.0000 -0.91562E-04-0.54114E-04 42 0.0000 0.0000 0.0000 43 0.0000 -0.97625E-03 0.32865E-18 44 0.0000 -0.96110E-04 0.17159E-02 1 USUM

0. 12294 0.11831

0. 11392

0. 11168

0. 11126 0.10771 0.10415 0.10064 0.97259E-01 0.968B5E-01 0.95033E-01 0.92515E-01 0.89195E-01 0.81574E-01 0.73901E-01 0.66362E-01 0.59254E-01 0.54550E-01 0.49641E-01 0.68275E-01 0.86191E-01 0.0000 0.14373E-02 0.89528E-04

0. 0000 0.81689E-03 0.14373E-02 0.89528E-04

0. 0000 0.11392 0.11392 0.11732 0.17185E-02 0.10636E-03 0.0000 0.97625E 0.17185E-02

'.e I

• • • • • ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 5.7.1 ANSYS/Mechanical U 00251976 VERSION-INTEL NT 21:40:40 MAR 06, 2003 CP-5.117 EDG Exhaust Piping Page E42

StV 4 4 J4 D I V

• • • • • POST1 NODAL DEGREE OF FREEDOM LISTING *****

LOAD STEP-1 SUBSTEP= 1 TIME-1.0000 LOAD CASE-0 THE FOLLOWING DEGREE OF FREEDOM RESULTS ARE IN GLOBAL COORDINATES NODE UX UY UZ 45 0.0000 -0.91562E-04 0.54114E-04 46 0.0000 0.0000 0.0000 47 -0.80678E-01-0.50223E-01 0.88547E-07 48 -0.80678E-01-0.50223E-01 0.88547E-07 49 -0.85137E-01-0.50203E-01-0.88548E-07 50 0.0000 0.0000 0.0000 51 -0.94826E-39-0.29422E-01 0.35218E-38 52 0.81256E-40-0.46139E-01 0.10356E-36 53 0.16061E-38-0.37712E-01 0.16203E-38 54 0.0000 0.0000 0.0000 55 -0.53825E-37-0.50043E-01-0.70457E-52 56 0.90636E-37-0.42172E-01-0.94291E-52 57 0.0000 .0.0000 0.0000 58 -0.94826E-39-0.29422E-01-0.35218E-38 59 0.81256E-40-0.46139E-01-0.10356E-36 60 0.16061E-38-0.37712E-01-0.16203E-38 61 0.0000 0.0000 0.0000 62 -0.29019E-01-0.46191E-01 0.38740E-07 63 -0.29019E-01-0.50181E-01 0.30468E-07 64 -0.29019E-01-0.42201E-01 0.47011E-07 65 -0.29019E-01-0.46191E-01 0.38740E-07 .72 -0.30354E-01-0.46181E-01 0.26368E-05 73 -0.30347E-01-0.50155E-01 0.30468E-07 74 -0.30356E-01-0.42196E-01 0.47011E-07 75 -0.30354E-01-0.46181E-01-0o.25593E-05 200 0.0000 0.0000 0.0000 201 0.0000 0.0000 0.0000 202 0.0000 0.0000 0.0000 203 0.0000 0;0000 0.0000 USUM 0.10636E-03 0.0000 0.95033E-01 0.95033E-01 0.98837E-01 0.0000 0.29422E-01 0.46139E-,01 0.37712E-01 0.0000 0.50043E-01 0.42172E-01 0.0000 0.29422E-01 0.46139E-01 0.37712E-01

0. 0000 0.54550E-01 0.57968E-01 0.51216E-01 0.54550E-01 0.55264E-01 0.58622E-01 0.51980E-01 0.55264E-01 0.0000 0.0000

.0.0000 0.0000 MAXIMUM ABSOLUTE VALUES NODE 39 1 44 1 VALUE -0.85431E-01-0.92760E-olo.17159E-02 0.12294 PRINT REACTION SOLUTIONS PER-NODE 1 ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 5.7.1 ANSYS/Mechanical U 00251976 VERSION-INTEL NT 21:40:40 MAR 06, 2003 CP= EDG Exhaust Piping POST1 TOTAL REACTION SOLUTION LISTING ***** LOAD STEP-1 SUBSTEP-1 TIME-1.0000 LOAD CASE-0 THE FOLLOWING X,YZ SOLUTIONS ARE IN GLOBAL COORDINATES 5.137 NODE 22 32 36 42 46 50 54 57 61 FX FY -0.17259E-07 0.86191 0.0000 831.34 0.0000 831.34 1 0.0000 984.33 0.0000 984.33 0.0000 879.49 0.28422E-13 360.59 0.0000 879.49 0.28422E-13 360.59 FZ MX MY MZ 0.13299E-13 0.39737E-13 0.69178E-08-0.77711E-02 -386.93 0.0000 386.93 0.0000 -462.67 0.0000 462.67 0.0000 0.94223E-14 -841.38 -0.18176E-12 16877. -0.19756E-1-2 -0.94223E-14 841.38 0.18176E-12 16877. 0.19633E-12 Page E43

• f-

-w 200 201 202 203 0.0000 0.0000

0. 0000

0. 0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 O..0000

-90.503 90.503 -108.22 108.22 0.0000 0.0000 0.0000 0.0000

0. 0000 0.0000

0. 0000 0.0000 TOTAL VALUES VALUE

-0.17259E-07 6112.3 -0.58071E-13-0.10341E-08 0.69178E-08 33754. USE LOAD STEP 2 SUBSTEP 0 FOR LOAD CASE 0 2 SUBSTEP-11 CUMULATIVE ITERATION-SET COMMAND GOT LOAD STEP-TIME/FREQUENCY-2.0000 TITLE-EDG Exhaust Piping 25 PRINT U NODAL SOLUTION PER NODE 1 ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 5.7.1 l ANSYS/Mechanical U 00251976 VERSION-INTEL NT 21:40:40 MAR 06, 2003 CP-EDG Exhaust Piping POST1 NODAL DEGREE OF FREEDOM LISTING ***** 5.137 LOAD STEP-2 TIME-2.0000 SUBSTEP-11 LOAD CASE-0 THE FOLLOWING DEGREE OF FREEDOM RESULTS ARE IN GLOBAL COORDINATES NODE UX UY 1 -0.82550E-01-0.89702E-01 2,-0.82550E-01-0.83810E-01 3 -0.82550E-01-0.78036E-01 4 -0.82550E-01-0.75027E-01 5 -0.82550E-01-0.74479E-01 6 -0.82550E-01-0.69510E-01 7 -0.82550E-01-0.64340E-01 8 -0.82550E-01-0.58950E-01 9 -0.82550E-01-0.53419E-01 10 -0.8'2550E-01-0.52782E-01 11 -0.82550E-01-0.49548E-01 12 -0.82550E-01-0.44954E-01 0.77827E-01-0.46282E-01 14 -0.68508E-01-0.46274E-01 15 -0.58714E-01-0.46256E-01 16 -0.48445E-01-0.46226E-01 17 -0.37700E-01-0.46184E-01 18 -0.29479E-01-0.46146E-01 19 -0.18301E-01-0.46192E-01 20 0.94502E-11-0.68465E-01 21 0.94501E-11-0.86544E-01 UZ 0.21619 0.23132 0.24667 0.25658 0.25840 0.274 19 0.28968 0.30487 0.31997 0.32168 0.33117 0.35262

0. 41996

0. 45824

0. 4 94 86 0.52969 0.56297

0. 58690 0.61801 0.67382 0.69018 0.0000 0.12166 0.99049E-02 0.0000 0.94506E-02 0.27172E-01 0.89962E-02 0.0000 0.24666 0.24667 0.28715 0.20615 0.16100E-01 0.0000 0.15283E-01

0. 39873E-01 USUM 0.24819 0.25951 0.27157 0.27978 0.28130 0.29466 0.30800 0.32130 0.33474 0.33627 0.34488 0.36493 0.42961 0.46564 0.50048 0.53390 0.56611 0.58945 0.62001

0. 67729

0. 69558 0.0000 0.12166 0.99170E-02

0. 0000 0.95816E-02 0.,27174E-01 0.90025E-02 0.0000 0.26537 0.27882 0.31003 0.20615 0.16118E-01 0.0000 0.15614E-01 0.39878E-01 22 0.0000 30 0.0000 31 0.0000 32 0.0000 33 '0.0000 34 0.0000 35 0.0000 36 0.0000 0.0000

-0.49481E-03 -0.49027E-03 0 O.0000 0.15790E-02 0.33122E-03 0.33577E-03 0.0000 37 -0.76870E-01-0.60616E-01 38 -0.88231E-01-0.95455E-01 39 -0.87030E-01-0.78019E-01 40 0.0000 -0.76958E-03 41 0.0000 -0.76503E-03 42 0.0000 0.0000 43 0.0000 0.31996E-02 44 0.0000 0.57724E-03 1 Page E44

I.-*

• AL-t wVLLlUJ U
  • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 5.7.1 ANSYS/Mechanical U 00251976 VERSION-INTEL NT 21:40:40 MAR 06, 2003 CP-EDG Exhaust Piping 5.157

• • • POST1 NODAL LOAD STEP-2 TIME-2.0000 DEGREE OF FREEDOM LISTING *****

SUBSTEP-11 LOAD CASE-0 THE FOLLOWING DEGREE OF FREEDOM RESULTS ARE IN GLOBAL COORDINATES NODE UX 'UY UZ 45 0.0000 0.58179E-03 0.144661 46 0.0000 0.0000 0.0000 47 -0.76072E-01-0.32129E-01 0.33115 48 -0.89029E-01-0.66967E-01 0.33117 49 -0.86736E-01-0.49528E-01 0.37165 50 0.0000 0.0000 0.0000 51 -0.88479E-04-0.35657E-01 0.65243E 52 -0.15786E-03-0.57790E-01 0.750991 53 -0.18968E-03-0.45982E-01 0.734041 54 0.0000 0.0000 0.0000 55 0.26148E-02-0.50083E-01 0.65214E 56 -0.26169E-02-0.42043E-01 0.73396E 57 0.0000 0.0000 0.0000 58 0.12826E-03-0.23150E-01 0.654421 59 0.14495E-03-0.34398E-01 0.868951 60 0.12441E-03-0.29327E-01 0.736011 61 0.0000 0.0000 0.0000 62 -0.38029E-01-0.57866E-01 0.58690 63 -0.29479E-01-0.50221E-01 0.59545 64 -0.29479E-01-0.42071E-01 0.57835 65 -0.20930E-01-0.34426E-01 0.58690 72 -0.39392E-01-0.57852E-01 0.58298 73 -t0.30836E-01-0.50195E-01 0.59153 74 -0.30844E-01-0.42066E-01 0.57443 75 -0.22293E-01-0.34421E-01 0.58298 200 0.0000 0.0000 0.0000 201 0.0000 0.0000 0.0000 202 0.0000 0.0000 0.0000 203 0.0000 0.0000 0.0000 MAXIMUM ABSOLUTE VALUES NODE 48 38 21 VALUE -0.89029E-01-0.95455E-01 0.69018 E-01 E-01 E-01 E-01 E-01 i-01 iE-01 E-01 USUM 0.14478E-01

0. 0000

0. 34 129

0. 34 940 0.38483 0.0000 0.74351E-01 0.94761E-01 0.86617E-01

0. 0000 0.82268E-01 0.84625E-01 0.0000 0.69417E-01 0.93456E-01 0.79229E-01 0.0000

0. 59097 0.59829 0.58063 0-.58828 0.58717 0.59445 0.57679'

0. 58442 0.0000 0.0000

0. 0000 0.0000 21

0. 69558

.SELECT FOR ITEM-TYPE COMPONENT-IN RANGE 1 TO 2 STEP 1 20 ELEMENTS (OF 89 DEFINED) SELECTED BY ESEL COMMAND. STORE XFORI FROM ITEM-SMIS COMP-1 FOR ALL SELECTED ELEMENTS STORE YFORI FROM ITEM-SMIS COMP-2 FOR ALL SELECTED ELEMENTS STORE ZFORI FROM ITEM-SMIS COMP-3 FOR ALL SELECTED ELEMENTS STORE XMOMI FROM ITEM-SMIS COMP-4 FOR ALL SELECTED ELEMENTS STORE YMOMI FROM ITEM-SMIS COMP-5 FOR ALL SELECTED ELEMENTS STORE ZMOMI FROM ITEM=SMIS COMP-6 FOR ALL SELECTED ELEMENTS STORE XFORJ FROM ITEM-SMIS COMP-7 FOR ALL SELECTED ELEMENTS STORE YFORJ FROM ITEM-SMIS COMP-8 FOR ALL SELECTED ELEMENTS Page E45

-
r4Llv.J-rve_4-v.30-.LvU STORE ZFORJ STORE XMOMJ STORE YMOMJ STORE ZMOMJ PRINT ELEMENT I. FROM ITEM-SMIS COMP-9 FROM ITEM-SMIS COMP-10 FROM ITEM-SMIS COMP-11 FROM ITEM-SMIS COMP-12 TABLE ITEMS PER ELEMENT FOR ALL SELECTED ELEMENTS FOR ALL SELECTED ELEMENTS FOR ALL SELECTED ELEMENTS FOR ALL SELECTED ELEMENTS

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 5.7.1 ANSYS/Mechanical U 00251976 VERSION-INTEL NT 21:40:40 MAR 06, 2003 CP-EDG Exhaust Piping

• • • • • POST1 ELEMENT TABLE LISTING *****

5.207 STAT ELEM 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 CURRENT CURRENT CURREI XFORI YFORI ZFORI 0.0000 -0.59401E-11 0.473511 0.0000 -267.30 -520.55 0.0000 1009.3 1568.8 0.0000 695.37 1259.3. 0.0000 666.47 1203.0 0.0000 274.65 391.45 0.0000 -117.17 -420.08 0.0000 -508.99 -1231.6 0.0000 -900.81 -2043.1 0.0000 -1084.7 -2099.4 0.23283E-09 614.72 2154.6 0.44639E-10 -1605.9 332.98 -41.498 -0.10004E-09 876.63 -281.70 -0.11460E-09 408.84 -521.91 -0.10914E-09 -58.955 -762.11 -0.11642E-09 -526.75 -1002.3 -0.94587E-10 -994.54 1174.9 -0.83674E-10 -6.9018 893.20 -6.9018 0.67303E 0.94501E-10 433.23 -6.9018 ,T E-1i CURRENT CURRENT CURRENT XMOMI YMOMI ZMOMI 0.0000 0.15095E-08-0.39086E-09 0.0000- -9630.2 4945.0 0.93132E-09 -38521. 19780. 0.0000 -7412.7 -676.57 0.18626E-08 -2488.3 -3400.3 0.93132E-09 25613. -19988. 0.0000 25109. -22763. 0.18626E-08 -4002.0 -11727. 0.18626E-08 -61719. 13121. 0.69849E-09 -70004.. 16782. -0.14203E-07-0.11719E+06 41154. -0.14451E-07 -22673. -43864. 386.51 37674. 17864. 386.51 59045. 17864. 386.51 64862. 17864. 386.51 55125. 17864. 386.51 29833. 17864. 386.51 446.90 29503. 386.51 29503. -227.77 -0.97684E-02 158.75 7617.1 E-1c MINIMUM VALUES ELEM 17 12 -10 VALUE -1002.3 -1605.9 -2099.4 MAXIMUM VALUES ELEM 18 3 11 VALUE 1174.9 1009.3 2154.6 PRINT ELEMENT TABLE ITEMS PER ELEMENT 1 20 11 12 -0.97684E-02-0.11719E+06 -43864. 19' 386.51 15 11 64862. - 41154.

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 5.7.1 ANSYS/Mechanical U 00251976 VERSION-INTEL NT 21:40:41 MAR 06, 2003 CP-EDG Exhaust Piping 5.218

• • • • • POST1 ELEMENT STAT CURRENT ELEM XFORJ 1

0.0000 2 0.0000 3 0.0000 4 0.0000 5 0.0000 6 0.0000 TABLE LISTING ***** CURRENT CURRENT CURRENT YFORJ ZFORJ XMOMJ -267.30 -520.55 0.0000 -534.59 -1041.1 0.0000 850.37 1259.3 0.93132E-09 666.47 1203.0 0.0000 274.65 391.45 0.18626E-08 -117.17 -420.08 0.93132E-09 Page E46 CURRENT YMOMJ -9630.2 -38521. -7412.7 -2488.3 25613. 25109. CURRENT ZMOMJ 4945.0 19780. -676.57 -3400.3 -19988. -22763.

vw MINIMt ELEM VALUE MAXIMtU ELEM VALUE SELECT IN RI 7 0.0000 -508.99 -1231.6 8 0.0000' -900.81 -2043.1 9 0.0000 -929.71 -2099.4 LO 0.0000 -1236.4 -2394.9 L 0.23283E-09 332.98 1605.9 L2 -41.498 -876.63 -0.74579E-L3 -281.70 -0.10004E-09 408.84 L4 -521.91 -0.11460E-09 -58.955 L5 -762.11 -0.10914E-09 -526.75 L6 -1002.3 -0.11642E-09 -994.54 17 -1219.7 -0.94587E-10 -994.54 .8 893.20 -0.83674E-10 -6.9018 .9 0.983770E-10 -6.9018 -433.23 20 0.94501E-i0 229.13 -6.9018 FM VALUES 17 10 10. -1219.7 -1236.4 -2394.9 TM VALUES 18 3 11 893.20 850.37 1605.9 FOR ITEM=ELEM COMPONENT- ,NGE 30 TO 35 STEP 6 ELEMENTS (OF 89 DEFINED) 0.0000 -4002.0 -11727. 0.18626E-08 -61719. 13121. 0.18626E-08 -70004. 16782. 0.69849E-09-0.11719E+06 41154. -0.14203E-07 -43864. 22673. -10 386.51 -17864. 37674. 386.51 59045. 17864. 386.51 64862. 17864. 386.51 55125. 17864. 386.51 29833. 17864. 386.51 5466.8 17864. 386.51 227.77 29503. -0.97684E-02 7617.1 -158.75 -0.97684E-02 0.71137E-02-0.78421E-02 20 10 6 -0.97684E-02-0.11719E+06 -22763. 18 386.51 14 64862. 10 41154. I SELECTED BY ESEL COMMAND. STORE STORE STORE STORE STORE STORE STORE STORE STORE STORE STORE STORE STORE STORE STORE STORE STORE STORE STORE STORE STORE PLSTR1 PLSTR2 PLSTR3 PLSTR4 PLSTR5 PLSTR6 PLSTR7 PLSTR21 PLSTR22 PLSTR23 PLSTR24 PLSTR25 PLSTR26 PLSTR27 XFORI YFORI ZFORI XMOMI YMOMI ZMOMI XFORJ FROM FROM FROM FROM FROM FROM FROM FROM FROM FROM FROM FROM FROM FROM FROM FROM FROM FROM FROM FROM FROM ITEM-LEPP ITEM-LEPP ITEM-LEPP ITEM-LEPP ITEM-LEPP ITEM=LEPP ITEM-LEPP ITEM-LEPP ITEM-LEPP ITEM=LEPP ITEM-LEPP ITEM-LEPP ITEM-LEPP ITEM-LEPP ITEM-SMIS ITEM=SMIS ITEM-SMIS ITEM-SMIS ITEM-SMIS ITEM-SMIS ITEM-SMIS COMP-COMP-COMP-COMP-COMP-COMP-COMP-COMP-COllP-COMP-COMP-COMP-COMP-COMP-COMP-COMP-COMP-COMP-COMP-COMP-COMP-1 2 3 4 5 6 7 21 22 23 24 25 26 27 1 2 3 4 5 6 7 8 FOR ALL FOR ALL FOR ALL FOR ALL FOR ALL FOR ALL FOR ALL FOR ALL FOR ALL FOR ALL FOR ALL FOR ALL FOR ALL FOR ALL FOR ALL FOR ALL EOR ALL FOR ALL FOR ALL SELECTED SELECTED SELECTED SELECTED SELECTED SELECTED SELECTED SELECTED SELECTED SELECTED SELECTED SELECTED SELECTED SELECTED SELECTED SELECTED SELECTED SELECTED SELECTED ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS FOR ALL SELECTED ELEMENTS FOR ALL SELECTED ELEMENTS FOR ALL SELECTED ELEMENTS STORE YFORJ FROM ITEM=SMIS COMP-Page E47

11
W
STORE ZFORJ STORE XMOMJ STORE YMOMJ STORE ZMOMJ STORE AXSTR1 STORE AXSTR2 STORE AXSTR3 STORE AXSTR4 STORE AXSTR5 STORE AXSTR6 STORE AXSTR7 STORE AXSTR21 STORE AXSTR22 STORE AXSTR23 STORE AXSTR24 STORE AXSTR25 STORE AXSTR26 STORE AXSTR27 PRINT ELEMENT 1; FROM ITEM=SMIS FROM ITEM-SMIS FROM ITEM-SMIS FROM ITEM-SMIS FROM ITEM-LS FROM ITEM-LS FROM ITEM-LS FROM ITEM-LS FROM ITEM-LS FROM ITEM-LS FROM ITEM-LS FROM ITEM-LS FROM ITEM=LS FROM ITEM-LS FROM ITEM-LS FROM ITEM=LS FROM ITEM-LS FROM ITEM-LS TABLE ITEMS PER COMP-COMP-COMP-COMP-COMP-COMP-COMP-COMP-COMP-COMP-COMP-COMP-COMP-COMP-COMP-COMP-COMP-COMP-ELEMENT 9 FOR ALL 10 FOR ALL 11 FOR ALL 12 FOR ALL 1 FOR ALL 2 FOR ALL 3 FOR ALL 4 FOR ALL S FOR ALL 6 FOR'ALL 7 FOR ALL 21 FOR ALL 22 FOR ALL 23 FOR ALL 24 FOR ALL 25 FOR ALL 26 FOR ALL 27 FOR ALL SELECTED SELECTED SELECTED SELECTED SELECTED SELECTED SELECTED SELECTED SELEQTED SELECTED SELECTED SELECTED SELECTED SELECTED SELECTED SELECTED SELECTED SELECTED ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 5.7.1 ANSYS/Mechanical U 00251976 VERSION-INTEL NT 21:40:42 MAR 06, 2003 CP-EDG Exhaust Piping 5.358

• • • • • POSTi ELEMENT STAT CURRENT CURRENT ELEM PLSTR1 PLSTR7 30 0.0000 0000 31 0.0000 0000 32 0.0000 0000 33 0.0000 0000 34 0.0000 0000 35 0.0000 0000 MINIMUM VALUES ELEM 30 30 VALUE 0.0000 0000 TABLE LISTING *****

CURRENT CURRENT PLSTR2 PLSTR3 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 CURRENT PLSTR4 0.0000 0.0000

0. 0000 0.0000 0.0000

• 0.0000 30

0. 0000 CURRENT PLSTR5 0.0000 0.0000

- 0.0000 0.0000 0.0000 0.0000 30 0.0000 CURRENT PLSTR6 0.0000

0. 0000

0. 0000 0. 0000

0. 0000

0. 0000 30

0. 0000 0.

0. 0. 0. 0. 0. 0. 30 0.0000 30 0.0000 Page E48

MAXIMUM VALUES ELEM 30 30 30 30 VALUE 0.0000 0.0000 0.0000 0000 PRINT ELEMENT TABLE ITEMS PER ELEMENT 1 30

0. 0000 30 0.0000 30 0.0000 0.

ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 5.7.1 ANSYS/Mechanical U 00251976 VERSION-INTEL NT 21:40:42 MAR 06, 2003 CP-EDG Exhaust Piping

• t
  • POST1 ELEMENT TABLE LISTING
• 5.368 STAT CURRENT ELEM PLSTR27

' 30 0000 31 0000 32 0000 33 0000 34 000-0 35 0000 CURRENT PLSTR21 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 CURRENT PLSTR22 0.0000

0. 0000

0. 0000

0. 0000

0. 0000

0. 0000 30 0.0000 CURRENT PLSTR23 0.0000

0. 0000

0. 0000 0.0000 0.0000 0.0000 30 0.0000 CURRENT PLSTR24 0.0000 0.0000 0.0000 0.0000

0. 0000 0.0000 30 0.0000 CURRENT PLSTR25

0. 0000' 0.0000 O..0000

0. 0000*

0.0000 0.0000 30 0.0000 CURRENT PLSTR26 0.0000 0.0000

0. 0000 0.0000 0.0000 0.0000 30 0.0000 0.

0. 0. 0. 0. 0. 0. MINIMUM VALUES ELEM r 30 30 VALUE 0.0000 0000 MAXIMUM VALUES ELEM 30 30-VALUE 0.0000 ,0000 30

0. 0000 30

0. 0000 30 0.0000 30 0.0000 30

0. 0000 0.

PRINT ELEMENT TABLE ITEMS PER ELEMENT 1

• • • • t ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 5.7.1 ANSYS/Mechanical U 00251976 VERSION-INTEL NT 21:40:42 MAR 06, 2003 CP-EDG ExhaustPiping 5.368

• • • • • POST1 ELEMENT STAT MIXED ELEM XFORI 30 -0.71054E-13

31. -5233.9 32 3884.6 33 3884.6 34 0.99476E-13 35 3594.3 MINIMUM VALUES ELEM 31 TABLE LISTING *****

MIXED MIXED YFORI ZFORI 0.0000 2609.9 0.0000 -921.72 0.0000 -5200.5 0.0000 -3642.2 0.0000 -0.34106E-12 0.0000 -4237.7 MIXED XMOMI 0.0000' 0.0000 0.0000 0.0000 0.0000 0.0000 MIXED YMOMI -0.34902E-10 13810. 71175. 3013.7 0.89813E-11

• 39312.

MIXED ZMOMI 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 30 30 32 .Page E49 30 30

VALUE -5233.9 0.0000 -5200.5 0.0000 -0.34902E-10 MAXIMUM VALUES ELEM 32 30 30 30 32 VALUE 3884.6 0.0000 2609.9 0.0000 71175. PRINT ELEMENT TABLE ITEMS PER ELEMENT 1 ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 5.7.1 ANSYS/Mechanical U 00251976 VERSION-INTEL NT 21:40:42 MAP 06, 2003 CP-EDG Exhaust Piping 0.0000 30

0. 0000 5.368 POST1 ELEMENT TABLE LISTING *****

STAT MIXED MIXED MIXED ELEM XFORJ YFORJ ZFORJ 30 -33.467 0.0000 2962.9' 31 -5245.5 0.0000 -800.18 32 3884.6 0.0000 -5186.1 33 3884.6 0.0000 -3627.8 34 -33.467 0.0000 -353.04 35 3582.8 0.0000 -4359.2 MINIMUM VALUES ELEM 31 30 32 VALUE -5245.5 0.0000 -5186.1 MAXIMUM VALUES ELEM 32 30 30 VALUE 3884.6 0.0000 2962.9 PRINT ELEMENT TABLE ITEMS PER ELEMENT 1 MIXED XMOMJ 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 30

0. 0000 30

0. 0000 MIXED YMOMJ 84985.

4769.7 3013.7 -44695. -5383.8 -5821.9 33 -44695. 30 84 985. MIXED ZMOMJ 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 30

0. 0000 30 0.0000

• • • • • ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 5.7.1 ANSYS/Mechanical U 00251976 VERSION-INTEL NT 21:40:42 MAR 06, 2003 CP-EDG Exhaust Piping 5.378 POST1 ELEMENT STAT CURRENT CURRENT ELEM AXSTR1 AXSTR7 30 -0.77974E 82273E-11 31 940.29 3645.4 32 12821.

10814. 33 1504.3 503.51 34 0.89947E-12 88105E-12 35 7455.9 5598.2 MINIMUM VALUES ELEM 30 32 VALUE -0.77974E-11-C 10814. MAXIMUM VALUES TABLE LISTING ***** CURRENT CURRENT CURRENT CURRENT CURRENT

• AXSTR2 AXSTR3 AXSTR4 AXSTR5 AXSTR6

-0.77974E-11-0.77974E-11 0.82273E-11 0.82273E-11 0.82273E-11 0. 940.29 940.29 -3645.4 -3645.4 -3645.4 12821. 12821. -10814. -10814. -10814. 1504.3 1504.3 503.51 503.51 503.51 0.89947E-12 0.89947E-12-0.88105E-12-0.88105E-12-0.88105E-12-0. 7455.9 7455.9 -5598.2 -5598.2 -5598.2 30 30 32 ).77974E-11-0.77974E-11 -10814. 32 -10814. 32 -10814. Page E50

v.- 1 ~W v ELEM 32 33 VALUE 12821. 51 32 12821. 32 12821. 33 503.51 33 503.51 33 503.51 503. PRINT ELEMENT TABLE ITEMS PER ELEMENT 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 5.7.1 ANSYS/Mechanical U 00251976 VERSION-INTEL NT 21:40:42 MAR 06, 2003 CP-EDG Exhaust Piping - 5.388

• • • • • POSTi ELEMENT STAT CURRENT CURRENT ELEM AXSTR21 AXSTR27 TABLE LISTING *****

CURRENT CURRENT AXSTR22 AXSTR23 30 1410; 14119. 31 -563. 2147.5 32 1504. 503.51 33 -6417, 8424.8 - 34 -902.' 885.24 35 -40.71 1892_5 MINIMUM VALUES ELEM 3: 30 VALUE -6417.J 14119. MAXIMUM VALUES ELEM 3( 33 VALUE 14102. 8424.8 2. 53 .3 .1 50 1 14102. -563.63 1504.3 - -6417.1 -902.54 -40.760 33 -6417.1 30

• 14102.

14102. -563.63 1504.3 -6417.1 -902.54 -40.760 33 -6417.1 30 14102. CURRENT AXSTR24 -14119. -2147.5 503.51 8424.8 885.24 1892.5 30 -14119. 33 8424.8 CURRENT AXSTR25 -14119. -2147.5 503.51 8424.8 885.24 1892.5 30 -14119. 33 8424.8 CURRENT AXSTR26 -14119. -2147.5 503.51 8424.8 885.24 1892.5 30 -14119. 33

• 8424.8 L

so SELECT FOR ITEM-ELEM COMPONENT-IN RANGE 40 TO 45 STEP 1 6 ELEMENTS (OF 89 DEFINED) SELECTED BY ESEL COMMAND. STORE PLSTR1 FROM ITEM-LEPP COMP-' 1 FOR ALL SELECTED ELEMENTS STORE PLSTR2 FROM ITEM-LEPP COMP-2 FOR ALL SELECTED ELEMENTS STORE PLSTR3 FROM ITEM-LEPP COMP-3 FOR ALL SELECTED ELEMENTS STORE PLSTR4 FROM ITEM-LEPP COMP-4 FOR ALL SELECTED ELEMENTS STORE PLSTR5 FROM ITEM-LEPP COMP-5 FOR ALL SELECTED ELEMENTS STORE PLSTR6 FROM ITEM-LEPP COMP-6 FOR ALL SELECTED ELEMENTS STORE PLSTR7 FROM ITEM-LEPP COMP-7 FOR ALL SELECTED ELEMENTS STORE PLSTR21 FROM ITEM-LEPP COMP-21 FOR ALL SELECTED ELEMENTS STORE PLSTR22 FROM ITEM-LEPP COMP-22 FOR ALL SELECTED ELEMENTS STORE PLSTR23 FROM ITEM=LEPP COMP-23 FOR ALL SELECTED ELEMENTS Page E51

STORE PLSTR24 -STORE PLSTR2! STORE PLSTR2( STORE PLSTR21 STORE XFORI STORE YFORI STORE ZFORI STORE XMOMI. STORE YMOMI STORE ZMOMI STORE XFORJ STORE YFORJ STORE ZFORJ STORE XMOMJ STORE YMOMJ STORE ZMOMJ STORE AXSTR1 STORE AXSTR2 STORE AXSTR3 STORE AXSTR4 STORE AXSTR5 STORE AXSTR6 STORE AXSTR7 STORE AXSTR21 STORE AXSTR22 STORE AXSTR23 STORE AXSTR24 STORE AXSTR25 STORE AXSTR26 STORE AXSTR27 I FROM ITEM=LZPP 5 FROM ITEM-LEPP 6 FROM ITEM-LEPP FROM ITEM-LEPP FROM ITEM-SMIS FROM ITEM-SMIS FROM ITEM-SMIS FROM ITEM-SMIS FROM ITEM-SMIS FROM ITEM-SMIS FROM ITEM-SMIS FROM ITEM-SMIS FROM ITEM-SMIS FROM ITEM-SMIS FROM ITEM-SMIS FROM ITEM-SMIS FROM ITEM=LS FROM ITEM=LS FROM ITEM-LS. FROM ITEM-LS FROM ITEM-LS FROM ITEM-LS FROM ITEM-LS FROM ITEM-LS FROM ITEM-LS FROM ITEM-LS FROM ITEM-LS FROM ITEM-LS FROM ITEM-LS FROM ITEM-LS COMP-COMP-COMP-COMP-COMP-COMP-COMP-COMP-COMP-COMP-COMP-COMP-COMP-COMP-COMP-COMP-COMP-COmP-COMP-COMP-COMP-COMp-COMP-COMP-COMP-COMP-COMP-COMp-COMP-COMP-24 25 26 27 1 2 3 4 5 6 7 8 9 10 11 12 1 2 3 4 5 6 7 21 22 23 24 25 26 27 FOR FOR FOR FOR FOR FOR FOR FOR FOR FOR FOR FOR FOR FOR FOR FOR FOR FOR FOR FOR FOR 'FORi FOR ; FORi FOR ; FOR. FOR. FOR, FOR FOR ] ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL ALL

• SELECTED ELEMENTS

,SELECTED ELEMENTS SELECTED ELEMENTS SELECTED ELEMENTS SELECTED ELEMENTS SELECTED ELEMENTS SELECTED ELEMENTS SELECTED ELEMENTS SELECTED ELEMENTS SELECTED ELEMENTS SELECTED ELEMENTS SELECTED ELEMENTS SELECTED ELEMENTS SELECTED ELEMENTS SELECTED ELEMENTS SELECTED ELEMENTS SELECTED ELEMENTS SELECTED ELEMENTS SELECTED ELEMENTS SELECTED ELEMENTS SELECTED ELEMENTS SELECTED ELEMENTS SELECTED ELEMENTS SELECTED ELEMENTS SELECTED ELEMENTS SELECTED ELEMENTS SELECTED ELEMENTS SELECTED ELEMENTS SELECTED ELEMENTS SELECTED ELEMENTS PRINT ELEMENT TABLE ITEMS PER ELEMENT ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 5.7.1 ANSYS/Mechanical U 00251976 VERSION-INTEL NT 21:40:44 MAR 06, 2003 CP-EDG Exhaust Piping POSTI ELEMENT TABLE LISTING ***** 5.498 Page E52

--u &
.v.J-rv4&1jPj-.Lvv STAT MIXED ELEM PLSTR7 40 0000 41 0000 42 0000 43 0000 44 0000 45 0000 MIXED PLSTR1 0.0000

0. 0000 0.0000 0.0000 0.0000 0.0000 MIXED PLSTR2 0.0000 0.0000 0.0000 0.0000

0. 0000 0.0000 40 0.0000 40 0.0000 MIXED PLSTR3 0.0000

0. 0000

0. 0000 0.0000 0.0000 0.0000 40 0.0000 40 0.0000 MIXED PLSTR4 0.0000 0.0000 0.0000

0. 0000 0.0000

0. 0000 40

'O.0000 40 0.0000 MIXED PLSTR5

0. 0000 0.0000 0.0000 0.0000 0.0000 0.0000 40 0.0000 40 0.0000 MIXED PLSTR6 0. 0000 0.0000 0.0000 0.0000 0.0000 0.0000 40 0.0000 40 0.0000 0.

0. 0.* ' 0. 0. 0. 0. 0. MINIMUM VALUES ELEM 40 40 VALUE 0.0000 0000 MAXIMUM VALUES ELEM 40 40 VALUE 0.0000 0000 PRINT ELEMENT TABLE 1 ITEMS PER ELEMENT

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 5.7.1 ANSYS/Mechanical U 00251976 VERSION-INTEL NT 21:40:44 MAR 06, 2003 CP-EDG Exhaust Piping '5.508

• • • • • POST1 ELEMENT STAT MIXED MIXED ELEM PLSTR21 PLSTR27 40 0.0000 0000 41 0.0000 0000 42 0.0000 0000 43 0.0000 0000 44 0.0000 0000 45 0.0000 0000 MINIMUM VALUES ELEM 40 40 VALUE.

0.0000 0000 MAXIMUM VALUES ELEM 40 40 VALUE 0.0000 0000 TABLE LISTING ***** MIXED MIXED PLSTR22 PLSTR23 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 MIXED PLSTR24 0.0000

0. 0000

0. 0000 0.0000 0.0000 0.0000 40 0.0000 40 0.0000 MIXED PLSTR25

0. 0000 0.0000

0. 0000 0.0000 0.0000 0.0000 40 0.0000 40 0.0000 MIXED PLSTR26 0.0000

0. 0000 0.0000 0.0000 0.0000 0.0000 40 0.0000 0.

0. 0. 0. 0. 0. 0. 40 0.0000 40 0.60000 40, 0.0000 40 0.0000 I 40 0.0000 0. Page E53

nan, S UL v r-.LUV PRINT ELEMENT TABLE ITEMS PER ELEMENT ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 5.7.1 ANSYS/Mechanical U 00251976 VERSION-INTEL NT 21:40:44 MAR 06, 2003 CP= EDG Exhaust Piping 5.508

• • • • • POSTl ELEMENT STAT MIXED ELEM XFORI 40 0.12932E-11 41 -8170.5 42 6983.1 43 6983.1 44 0.99476E-13 45 6223.6 MINIMUM VALUES ELEM 41 VALUE

-8170.5 MAXIMUM VALUES ELEM 42 VALUE 6983.1 TABLE LISTING ***** MIXED MIXED YFORI ZFORI 0.0000 4549.5 0.0000 -2080.6 0.0000 -8137.0 0.0000 -6271.4 0.0000 -0.45475E-12 0.0000 -7336.1 MIXED XMOMI 0.0000 0.0000 0.0000

0. 0000 0.0000 0.0000 MIXED YMOMI

-0.10766E-09 28773. 0.11537E+06 8665.7 0.64801E-ll 68169. MIXED ZMOMI

0. 0000 0.0000

0. 0000 0.0000 0.0000 0.0000 40 0.0000 40 0.0000 42

-8137.0 40 4549.5 40 40 40 0.0000 -0.10766E-09 0.0000 40 42 40' 0.0000 0.11537E+06 0.0000 PRINT ELEMENT TABLE ITEMS PER ELEMENT ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 5.7.1 ANSYS/Mechanical U 00251976 VERSION-INTEL NT 21:40:44 MAR 06, 2003 CP-EDG Exhaust Piping 5.518 POST1 ELEMENT STAT MIXED ELEM XFORJ 40 -33.467 41 -8182.0 42 6983.1 43 6983.1 44 -33.467 45 6212.1 MINIMUM VALUES ELEM 41 VALUE -8182.0 - MAXIMUM VALUES ELEM 42 VALUE 6983.1 PRINT ELEMENT TABLE 3 1 TABLE LISTING ***** MIXED MIXED YFORJ ZFORJ 0.0000 4902.5 0.0000 -1959.0 0.0000 -8122.6 0.0000 -6257.0 0.0000 -353.04 0.0000 -7457.6 MIXED XMOMJ 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 40 .0.0000 MIXED YMOMJ 0.14414E+06 7565.3 8665.7 -73553. -5383.8 -9498.5 43 -73553. MIXED ZMOMJ

0. 0000.

0.0000 0.0000

0. 0000 0.0000 0.0000 40 0.0000 40

0. 0000 40 0.0000 40 0.0000 ITEMS PER 42

-8122.6 40 4902.5 ELEMENT 40 40 0.0000 0.14414E+06

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 5.7.1 ANSYS/Mechanical U 00251976 VERSION-INTEL NT 21:40:44 MAR 06, 2003 CP-EDG Exhaust Piping 5.528 MIXED

• • • • • POSTI ELEMENT TABLE LISTING *****

STAT MIXED MIXED MIXED MIXED MIXED Page E54

I. -fl

• .fl~w.

A.U.&IJ 4vj MIXED ELEM AXSTR1 AXSTR2 AXSTR3 AXSTR4 AXSTR5 AXSTR6 AXSTR7 40 -0.10693E-10-0.10693E-10-0.10693E-10 0.11330E-10 0.11330E-10 0.11330E-10 0. 11330E-10 41 2665.9 2665.9 2665.9. -6888.8 -6888.8 -6888.8 6888.8 42 20960. 20960. 20960. -17351. -17351. -17351. 17351. 43 3243.4 3243.4 3243.4 365.80 365.80 365.80 365.80 44 0.52462E-12 0.52462E-12 0.52462E-12-0.50620E-12-0.50620E-12-0.50620E-12-0. 50620E-12 45 12927. 12927. 12927. -9710.0 -9710.0 -9710.0 9710.0 MINIMUM VALUES ELEM 40 40 40 42 42 42 42 VALUE -0.10693E-10-0.10693E-10-0.10693E-10 -17351. -17351. -17351. 17351. MAXIMUM VALUES ELEM 42 42 42 43 43 43 43 VALUE 20960. 20960. 20960. 365.80 365.80 365.80 365. 80 PRINT ELEMENT TABLE ITEMS PER ELEMENT 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 5.7.1 ANSYS/Mechanical U 00251976 VERSION-INTEL NT 21:40:44 MAR 06, 2003 CP-EDG Exhaust Piping 5.548

• • • • • POST1 ELEMENT STAT MIXED MIXED ELEM-AXSTR21 AXSTR27 40 23924.-

23941. 41 -858.34 3370.5 42 3243.4 365.80 43 -10408. 14017. 44 -902.54 885.24 45 28.276 3182.4 MINIMUM VALUES ELEM 43 .40 VALUE -10408. 23941. MAXIMUM VALUES ELEM 40 43 VALUE 23924. 14017. SELECT FOR ITED IN RANGE 50 TO TABLE LISTING ***** MIXED MIXED AXSTR22 AXSTR23 23924. - -23924. -858.34 -858.34 3243.4 3243.4 -10408. -10408. -902.54 -902.54 28.276 28.276 MIXED AXSTR24 -23941. -3370.5 365.80 14017. 885.24 3182.4 40 -23941. 43 14017. MIXED AXSTR25 -23941. -3370.5 365.80 14017. 885.24 3182.4 40 -23941. 43 i4017. MIXED AXSTR26 -23941. -3370.5 365.80 14017. 885.24 3182.4 40 -23941. 43 14017. 43 -10408. 40 23924. 43 -10408. 40 23924. I-ELEM COMPONENT-61 STEP 1 Page E55,

a-VU rvj C ULC.UJl-AV 12 ELEMENTS (OF 89 DEFINED) SELECTED BY ESEL COMMAND. STORE PLSTR1 FROM ITEM-LEPP COMP STORE PLSTR2 FROM ITEM-LEPP COMP STORE PLSTR3 FROM ITEM-LEPP COMP STORE PLSTR4 FROM ITEM-LEPP COMP STORE PLSTR21 FROM ITEM-LEPP COMP STORE PLSTR22 FROM ITEM-LEPP COMP STORE PLSTR23 FROM ITEM-LEPP COMP STORE PLSTR24 FROM ITEM-LEPP COMPE STORE XFORI FROM ITEM-SMIS COMPN STORE YFORI FROM ITEM-SMIS COMPN STORE ZFORI FROM ITEM-SMIS COMP STORE XMOMI FROM ITEM-SMIS COMP STORE YMOMI FROM ITEM-SMIS COMP STORE ZMOMI FROM ITEM-SMIS COMP STORE XFORJ FROM ITEM-SMIS COMP STORE YFORJ FROM ITEM-SMIS COMPE STORE ZFORJ FROM ITEM-SMIS COME' STORE XMOMJ FROM ITEM-SMIS COMPE STORE YMOMJ FROM ITEM-SMIS COMP, STORE ZMOMJ FROM ITEM-SMIS COMPN STORE AXSTR1 FROM ITEM-LS COMPE STORE AXSTR2 FROM ITEM-LS COMPE STORE AXSTR3 FROM ITEM-LS COM? STORE AXSTR3 FROM ITEM-LS COMP STORE AXSTR21 FROM ITEM-LS COMP? STORE AXSTR22 FROM ITEM-LS COMPN STORE AXSTR23 FROM ITEM-LS COMPN STORE AXSTR24 FROM ITEM-LS COMPE PRINT ELEMENT TABLE ITEMS PER ELEM 1 ANSYS - ENGINEERING ANALYSIS ANSYS/Mechanical U 00251976 VERSION-INTEL NT EDG Exhaust Piping 1 FOR ALL SELECTED 2 FOR ALL SELECTED 3 FOR ALL SELECTED 4 FOR ALL SELECTED 21 FOR ALL SELECTED 22 FOR ALL SELECTED 23 FOR ALL SELECTED 24 FOR ALL SELECTED 1 FOR ALL SELECTED 2 FOR ALL SELECTED 3 FOR ALL SELECTED 4 FOR ALL SELECTED 5 FOR ALL SELECTED 6 FOR ALL SELECTED 7 FOR ALL SELECTED 8 FOR ALL SELECTED 9 FOR ALL SELECTED 10 FOR ALL SELECTED 11 FOR ALL SELECTED 12 FOR ALL SELECTED 1 FOR ALL SELECTED 2 FOR ALL SELECTED 3 FOR ALL SELECTED 4 FOR ALL SELECTED 21 FOR ALL SELECTED 22 FOR ALL SELECTED 23 FOR ALL SELECTED 24 FOR ALL SELECTED ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ELEMENTS ENT

SYSTEM RELEASE 5.7.1 21

40:45 MAR 06, 2003 CP-5.678

• • • • • POST1 ELEMENT TABLE LISTING *****

Page E56

STAT ELEM 50 51 52 53 54 55 56 57 58 59 60 61 MINIMUM ELEM VALUE MIXED PLSTR1 0.0000

0. 0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 VALUES 50 0.0000 MIXED PLSTR2 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000

0. 0000

0. 0000 0.0000 0.0000 50 0.0000 MIXED PLSTR3

0. 0000

0. 0000 0.0000 0.0000 0.0000

0. 0000

.0.0000 0.0000 0.0000 0.0000 0.0000

0. 0000 50

0. 0000 MIXED PLSTR4 0.0000

0. 0000 0.0000 0.0000

0. 0000

0. 0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 50

0. 0000 50 0.0000 MAXIMUM VALUES ELEM 50 VALUE 0.0000 50 50 0.0000 0.0000 PRINT ELEMENT TABLE ITEMS PER ELEMENT, 3.

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM ANSYS/Mechanical U 00251976 VERSION-INTEL NT 21 EDG Exhaust Piping RELEASE 5.7.1 1:40:45 MAR 06, 2003 CP-5.678

• • • • • POST1 ELEMENT TABLE LISTING *****

STAT ELEM 50 51 52 53 54 55 56 57 58 59 60 61 MIXED PLSTR21 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000

0. 0000 0.0000 0.0000 0.0000 0.0000 0.0000 MIXED PLSTR22 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 MIXED PLSTR23 0.0000 0.0000 0.0000 0.0000

0. 0000

0. 0000 0.0000 0.0000 0.0000 0.0000

• 0.0000 0.0000 MIXED PLSTR24 0.0000 0.0000 0.0000 0.0000

0. 0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 MINIMUM VALUES ELEM 50 VALUE 0.0000 50 50 0.0000 '

0.0000 'MAXIMUM ELEM VALUE VALUES 50 0.0000 50 0.0000 50 O. 0000 50 0.0000 50

0. 0000 PRINT ELEMENT TABLE ITEMS PER ELEMENT 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 5.7.1 ANSYS/Mechanical U 00251976 VERSION-INTEL NT 21:40:45 MAR 06, 2003 CP-EDG Exhaust Piping POST1 ELEMENT TABLE LISTING ***** 5.688 STAT MIXED MIXED MIXED MIXED MIXED MIXED Page E57

vv ELEM XFORI 50 -46.442 51 -397.68 52 -397.68 53 -106.25 54 285.07 55 285.07 56 282.13 57 282.13 58 31.489 59 382.72 60 382.72 61 91.298 MINIMUM VALUES ELEM 52 VALUE -397.68 YFORI -336.40 -51.336 -51.336 230.80 351.23 351.23 -291.43 -291.43 -259.67 -544.73 442.91 160.78 59 -544.73 60 - 442.91 ZFORI -1022.9 -385.79 291.20 428.39 619.81 -607.75 -131.88 122.27 724.71 111.65 -145.51 -281.98 50 -1022.9 58 724.71 XMOMI -9.0666 -332.98 315.83 410.56 593.99 -582.48 -128.40 115.17 -17.572 121.72 -124.73 -270.24 55 -582.48 54 593.99 YMOMI ZMOMI 19895. -4988.0 -7605.6 271.72 -12187. 885.54 -8675.3 4619.9 -6508.3 397.86 726.84 4597.6 36.757 -3088.4 -1508.4 396.22 -5906.0 -2719.9 -7272.7 -4631.9 -5564.6 663.96 -0.46789E-11 5.1205 52 50 -12187. -4988.0 50 53 19895. 4619.9 MAXIMUM VALUES ELEM 59 VALUE 382.72 PRINT ELEMENT TABLE ITEMS PER ELEMENT 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM ANSYS/Mechanical U 00251976 VERSION-INTEL NT 21 EDG Exhaust Piping

• • • • • POST1 ELEMENT TABLE LISTING ****

RELEASE 5.7.1 L:40:45 MAR 06, 2003 CP-5.698 STAT ELEM 50 51 52 53 54 55 56 57 58 59 60 61 MIXED XFORJ -46. 442 -397.68 -397.68 -106.25 285.07 285.07 282.13 282.13 31.4 89 382.72 382.72 91.298 MIXED YFORJ -336.40 -51.336 -51.336 230.80 351.23 351.23 -291.43 -291.43 -259.67 -544.73 442.91 160.78 MIXED ZFORJ -1010.9 -380.49 296.50 437.28 625.12 -602.45 -126.58 . 127.58 - 736.71 116. 96 -140.20 -273.09 MIXED XMOMJ 2.4335 -327.90 320.92 ,419.08 599.08 -577.40 -123.32 120.26 -6.0715 126.81 -119.65 -261.72 MIXED YMOMJ -7605.6 -12187. -8673.2 0.44160E-11 934.52 -6508.3 -1508.4 -14.719 13855. -5906.0 -7272.7 -5562.6 MIXED ZMOMJ 4109.3 885.54 1499.4 -5. 9592 -3801.9 397.86 396.22 3880.8 4302.3 1881.4 -4631.9 -3217.4 MINIMUM ELEM VALUE MAXIMUM ELEM VALUE VALUES 52 -397.68 VALUES 59 382.72 59 -544.73 50 -1010. 9 55 -577.40 51 -12187. 58 13855. 60 -4631.9 58 4302.3 60 58 54 442.91 736.71 599.08 PRINT ELEMENT TABLE ITEMS PER ELEMENT 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 5.7.1 ANSYS/Mechanical U 00251976 VERSION-INTEL NT 21:40:45 MAR-06, 2003 CP-EDG Exhaust Piping

• • • • • POST1 ELEMENT TABLE LISTING *****

5.708 STAT MIXED ELEM AXSTR1 MIXED AXSTR2 MIXED AXSTR3 MIXED AXSTR4-Page E58

50 23778. 51 -4722.3 52 -8685.2 53 -17377. 54 -4109.9 55 -12492. 56 8949.2 57 -1675.9 58 4855.2 59 9833.0 60 -4342.6 61 43.836 MINIMUM VALUES ELEM 53 VALUE -17377. MAXIMUM VALUES ELEM 50 VALUE 23778. PRINT ELEMENT TABLE 3.1 4086.8 -3649.6 -5193.4 861.01 -2539.3 5658.0 -3242.7 -111.73 -5882.1 -8452.5 -1721.5

64. 050 59

-8452.5 55 5658.0 ITEMS PER -15261. 3746.8 6658.4 - 9297.8 3790.1 4951.2 -3278.5 1355.2 -138.41 -1379.7 3690.1 64.050 50 -15261. 53 9297.8 ELEMENT 4430.2 2674.2 3162.5 -8940.2 2219.5 -13199. 8913.4 -208.94 10599. 16906. 1069.0

43. 836 55

-13199. 59 16906.

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM ANSYS/Mechanical U 00251976 VERSION-INTEL NT 21 EDG Exhaust Piping RELEASE 5.7.1

40:45 MAR 06, 2003 CP=

5.728

• • • • • POST1 ELEMENT TABLE LISTING *****

STAT MIXED ELEM AXSTR21 50 -15372. 51 -8689.2 52 -8720.1 53 -51.015 54 11409. 55 -4109.9 56 -1675.9 57 -10823. 58 -5433.8 59 -7958.3 60 9833.0 61 6470.1 MINIMUM VALUES ELEM 50 VALUE -15372. MAXIMUM VALUES ELEM 54 VALUE 11409. MIXED AXSTR22 850.46 -5193.4 -2801.0 -74.540 -3599.3 -2539.3 -111.73 4497.0 11550. -531.04 -8452.5 -6231.1 60 -8452.5 58 11550. MIXED AXSTR23 8246.9 6658.4 5633.8 -74.540 -4508.1 3790.1 1355.2 4511.3 -1923.3 5212.6 -1379.7 -821.48 54 -4508.1 50 8246.9 MIXED AXSTR24 -7975.2 3162.5 -285.27 -51.015 10501. 2219.5 -208.94 -10809. -18907. -2214.7 16906. 11880. 58 -18907. 60 16906. SELECT FOR ITEM-ELEM COMPONENT-IN RANGE 224 TO 227 STEP 1 4 ELEMENTS (OF 89 DEFINED) SELECTED BY ESEL COMMAND. STORE LUGFORCE FROM ITEM-SMIS COMP-1 FOR ALL SELECTED ELEMENTS PRINT ELEMENT TABLE ITEMS PER ELEMENT

• ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 5.7.1 ANSYS/Mechanical U 00251976 VERSION-INTEL NT 21:40:45 MAR 06, 2003 CP-EDG Exhaust Piping 5.738 Page E59

POSTi ELEMENT TABLE LISTING ***** STAT CURRENT ELEM LUGFORCE 224 -671.69 225 -1222.3 226 -248.85 227 -251.85 MINIMUM VALUES ELEM 225 VALUE -1222.3 MAXIMUM VALUES ELEM 226 VALUE -248.85 SELECT FOR ITEM-ELEM COMPONENT-IN RANGE 88 TO 89 STEP 1 2 ELEMENTS (OF 89 DEFINED) SELECTED BY ESEL COMMAND. STORE SPFORCE FROM ITEM-SMIS COMP-1 FOR ALL SELECTED ELEMENTS STORE PRELOAD FROM ITEM-SMIS COMP-2 FOR ALL SELECTED ELEMENTS STORE ELSTAT FROM ITEM-NMIS COMP-1 FOR ALL SELECTED ELEMENTS PRINT ELEMENT TABLE ITEMS PER ELEMENT 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 5.7.1 ANSYS/Mechanical U 00251976 VERSION-INTEL NT 21:40:46 MAR 06, EDG Exhaust Piping 2003 CP-5.748 POSTi ELEMENT TABLE LISTING ***** STAT CURRENT CURRENT CURRENT ELEM SPFORCE PRELOAD ELSTAT 88 28.894 1515.0 1.0000 89 19.140 1832.0 1.0000 MINIMUM VALUES ELEM 89 88 88 VALUE 19.140 1515.0 1.0000 MAXIMUM VALUES ELEM 88 89 88 VALUE 28.894 1832.0 1.0000 ALL SELECT FOR ITEM-ELEM COMPONENT-IN RANGE 1 TO 227 STEP 1 89 ELEMENTS (OF 89 DEFINED) SELECTED BY PRINT REACTION SOLUTIONS PER NODE 1 ESEL COMMAND.

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 5.7.1 ANSYS/Mechanical U 00251976 VERSION-INTEL NT 21:40:46 MAR 06, 2003 CP-EDG Exhaust Piping 5.758

• • • • • POSTi TOTAL REACTION SOLUTION LISTING *****

Page E60

X-. 11-.

• fWVj ZU&LU w.

LOAD STEP-2 TIME-2.0000 SUBSTEP-11 LOAD CASE-0 THE FOLLOWING X,Y,Z NODE FX 22 -0.94501E-10 32 0.0000 36 0.0000 42 0.0000 46 0.0000 50 46.442 54 -106.25 57 -31.489 61 91.298 200 .0.0000 201 0.0000 202 0.0000 203 0.0000 TOTAL VALUES VALUE -0.94673E-10 SOLUTIONS ARE IN GLOBAL COORDINATES FY 0.86544 5245.5 -3582.8 8182.0 -6212.1 1022.9 437.28 736.71 281.98 0.0000 0.0000 0.0000 0.0000 6112.3 FZ -6.9018 800.18 -4359:2 1959.0 -7457.6 -336.40 -230.80 -259.67 -160.78

0. 0000 0.0000

0. 0000

0. 0000

-10052. MX MY MZ 0.97684E-02-0.71137E-02-0.78421E-02

0. 0000 0.0000 0.0000 0.0000

-971.27 4985.4 19895. 712.12 4300.5 13855. -4769.7 0.0000 0.0000 -5821.9 0.0000 0.0000 -7565.3 0.0000 0.0000 -9498.5 0.0000 0.0000 -27915. 9285.9 33749.

• • • • • END OF INPUT ENCOUNTERED NUMBER OF WARNING MESSAGES ENCOUNTERED-NUMBER OF ERROR MESSAGES ENCOUNTERED-5 6
        • PROBLEM TERMINATED BY INDICATED ERROR(S)

OR BY END OF INPUT DATA ***** ANSYS RUN COMPLETED Release.5.7.1 UP20010418 INTEL NT Maximum Scratch Memory Used 2156624 Words 8.227 MB CP Time (sec) - 5.788 Time - 21:40:46 Elapsed Time (sec) - 40.000 Date - 03/06/2003 I-Page E61}}