ML031250551

ISFSI Cask Storage Pad Concrete Shrinkage & Thermal Stresses, Attachment 2, Appendix SPadNC-TH

ML031250551
Person / Time
Site:	Diablo Canyon
Issue date:	03/03/2003
From:	Tumminelli S Enercon Services
To:	Office of Nuclear Reactor Regulation
References
+sispmjr200505, -RFPFR, DIL-03-003, TAC L23399 PGE-009-CALC-006, Rev 1
Download: ML031250551 (136)

Text

Sheet 1 of 64 ENERCON E

8 SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 Originator:

S. C. Tumminelli Date:

March 3, 2003 Appendix RPadNC-TH This Appendix presents the ANSYS output file documenting the execution of the unconstrained model thermal stress analysis and the output temperatures for checking.

Sheet 2 of 64 ENERCON F

SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 ANSYS Output File:

ANSYS/Mechanical U W E L C O M E T O T H E A N S Y S P R O G R A M ANSYS 6.1 NOTICES

• Copyright 2002 SAS IP, Inc.

All rights reserved.

• Unpublished---rights reserved under the Copyright Laws of

• the United States.

• 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 Rights Reserved.

• CA&SI, 2004 S. Wright Street, Urbana, IL 61821 Ph (217)244-7875 Fax (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.

Sheet 3 of 64 ENERCON SERVICESINC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 Completing ANSYS Load Process.

ANSYS COMMAND LINE ARGUMENTS INITIAL JOBNAME

= PADNC-TH BATCH MODE REQUESTED

= LIST MEMORY REQUESTED (MB)

= 700 DATABASE SIZE REQUESTED (MB) = 75

• • • WARNING ***

CP=

0.210 TIME= 13:35:44 Use of the -M switch is no longer recommended for normal ANSYS use.

ANSYS now dynamically allocates memory as needed.

Only use the -M switch if you are certain that you need to do so.

PARAMETER STATUS-(

1 PARAMETERS DEFINED)

(INCLUDING 1 INTERNAL PARAMETERS) 00245050 VERSION=INTEL NT RELEASE= 6.1 UP20020321 CURRENT JOBNAME=PADNC-TH 13:35:44 JAN 03, 2003 CP=

0.210 1 resume 2

nall 3

eall 4

mpli 5

/com start, change the material properties for each time step, initial 6

/com property is no. 2.

Change back to no. 2 at end and save.

7

/solu 8 /HEADER,ON,OFF,OFF,OFF,ON,OFF 9 elist,530 10 lssolve,1 11 esel,type,2 12 mpchg,3,all 13 eall 14 elist,530 15 lssolve,2 16 esel,type,2 17 mpchg,4,all 18 eall 19 elist,530 20 lssolve,3 21 esel,type,2 22 mpchg,5,all 23 eall 24 elist,530 25 lssolve,4 26 esel,type,2 27 mpchg,6,all 28 eall 29 elist,530 30 lssolve,5 31 esel,type,2 32 mpchg,7,all 33 eall 34 elist,530

NERCO Sheet 4 of 64 F-ENERCON SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 35 lssolve,6 36 esel,type,2 37 mpchg,8,all 38 eall 39 elist,530 40 lssolve,7 41 esel,type,2 42 mpchg,9,all 43 eall 44 elist,530 45 lssolve,8 46 esel,type,2 47 mpchg,10,all 48 eall 49 elist,530 50 lssolve,9 51 esel,type,2 52 mpchg,11,all 53 eall 54 elist,530 55 lssolve,10 56 esel,type,2 57 mpchg,12,all 58 eall 59 elist,530 60 lssolve,11 61 esel,type,2 62 mpchg,2,all 63 eall 64 elist,530 65 finish 66 save 67

/POST1 68

/HEADER,ON,OFF,OFF,OFF,ON,OFF 69

/COM 70

/COM SUM RESULTS, SET TITLES AND WRITE LOAD CASE FILES FOR FURTHER PROCESSING 71

/COM 72 LCSUM,ALL 73 LCDEF,1,1 74 LCDEF,2,2 75 LCDEF,3,3 76 LCDEF,4,4 77 LCDEF,5,5 78 LCDEF,6,6 79 LCDEF,7,7 80 LCDEF,8,8 81 LCDEF,9,9 82 LCDEF,10,10 83 LCDEF,11,11 84 LCASE,1 85

/TITLE,PAD RESPONSE AT END OF 0.25 DAYS -

NO PAD/ROCK CONSTRAINT 86 LCWRITE,1 87 LCOPER,ADD,2 88

/TITLE,PAD RESPONSE AT END OF 0.50 DAYS -

NO PAD/ROCK CONSTRAINT 89 LCWRITE,2 90 LCOPER,ADD,3

Eli Sheet 5 of 64 ENERCON SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 91 92 93 94 95 96 97 98 99 100 101 102 103 104 105 106 107 108 109 110 111 112 113 114 115 116 117 118 119 120 121 122 123 124 125 126 127 128 129 130 131 132 133 134 135 136 137 138 139 140 141 142 143 144 145 146 147

/TITLE,PAD RESPONSE LCWRITE, 3 LCOPER,ADD, 4

/TITLE,PAD RESPONSE LCWRITE, 4 LCOPER,ADD, 5

/TITLE,PAD RESPONSE LCWRITE, 5 LCOPER,ADD, 6

/TITLE,PAD RESPONSE LCWRITE, 6 LCOPER,ADD, 7

/TITLE,PAD RESPONSE LCWRITE, 7 LCOPER,ADD, 8

/TITLE,PAD RESPONSE LCWRITE, 8 LCOPER,ADD,9

/TITLE,PAD RESPONSE LCWRITE,9 LCOPER,ADD,10

/TITLE,PAD RESPONSE LCWRITE,10 LCOPER,ADD,11

/TITLE,PAD RESPONSE LCWRITE,11 FINISH AT END OF 0.625 DAYS -

NO PAD/ROCK CONSTRAINT AT END OF 1.125 DAYS -

NO PAD/ROCK CONSTRAINT AT END OF 1.625 DAYS -

NO PAD/ROCK CONSTRAINT AT END OF 2.125 DAYS -

NO PAD/ROCK CONSTRAINT AT END OF 2.375 DAYS -

NO PAD/ROCK CONSTRAINT AT END OF 3.125 DAYS -

NO PAD/ROCK CONSTRAINT AT END OF 4.125 DAYS -

NO PAD/ROCK CONSTRAINT AT END OF 6.125 DAYS -

NO PAD/ROCK CONSTRAINT AT END OF 7.875 DAYS -

NO PAD/ROCK CONSTRAINT

/com print the temperatures for checking EALL NALL

/POSTl

/HEADER, ON, OFF, OFF, OFF, ON, OFF NSEL,S,LOC,X,0.0 NSEL,R,LOC,Z,0.0 NSEL,R,LOC,Y,0.0,-145.0 NLIS SET,1 NSORT,LOC,Y PRNSOL,BFE SET, 2 NSORT,LOC,Y PRNSOL,BFE SET,3 NSORT,LOC,Y PRNSOL,BFE SET, 4 NSORT,LOC,Y PRNSOL,BFE SET, 5 NSORT,LOC,Y PRNSOL,BFE SET, 6 NSORT,LOC,Y PRNSOL,BFE SET,7 NSORT,LOC,Y PRNSOL,BFE

SERVICESSheet 6 of 64 F-k"10 ENERCON SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 148 SET,8 149 NSORT,LOC,Y 150 PRNSOL,BFE 151 SET,9 152 NSORT,LOC,Y 153 PRNSOL,BFE 154 SET,10 155 NSORT,LOC,Y 156 PRNSOL,BFE 157 SET,11 158 NSORT,LOC,Y 159 PRNSOL,BFE 160 LCASE,1 161 NSORT,LOC,Y 162 PRNSOL,BFE 163 LCASE,2 164 NSORT,LOC,Y 165 PRNSOL,BFE 166 LCASE,3 167 NSORT,LOC,Y 168 PRNSOL,BFE 169 LCASE,4 170 NSORT,LOC,Y 171 PRNSOL,BFE 172 LCASE,5 173 NSORT,LOC,Y 174 PRNSOL,BFE 175 LCASE,6 176 NSORT,LOC,Y 177 PRNSOL,BFE 178 LCASE,7 179 NSORT,LOC,Y 180 PRNSOL,BFE 181 LCASE,8 182 NSORT,LOC,Y 183 PRNSOL,BFE 184 LCASE,9 185 NSORT,LOC,Y 186 PRNSOL,BFE 187 LCASE,10 188 NSORT,LOC,Y 189 PRNSOL,BFE 190 LCASE,11 191 NSORT,LOC,Y 192 PRNSOLBFE 193 NUSORT 194 FINISH 195 eall 196 nall 197

/EXIT,NOSAVE RUN SETUP PROCEDURE FROM FILE= C:\\Program Files\\Ansys Inc\\ANSYS61\\docu\\start61.ans

/INPUT FILE= C:\\Program Files\\Ansys Inc\\ANSYS61\\docu\\start61.ans LINE=

0 RESUME ANSYS DATA FROM FILE NAME=PADNC-TH.db

F; I ENERCON L

z SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006

• • • ANSYS GLOBAL STATUS ***

TITLE = Pad thermal analysis model, no pad/rock constraint Sheet 7 of 64 ANALYSIS TYPE =

STATIC (STEADY-STATE)

NUMBER OF ELEMENT TYPES =

5 8812 ELEMENTS CURRENTLY SELECTED.

10212 NODES CURRENTLY SELECTED.

166 KEYPOINTS CURRENTLY SELECTED.

339 LINES CURRENTLY SELECTED.

2 AREAS CURRENTLY SELECTED.

48 VOLUMES CURRENTLY SELECTED.

22 COMPONENTS CURRENTLY DEFINED MAXIMUM LINEAR PROPERTY NUMBER MAXIMUM REAL CONSTANT SET NUMBER ACTIVE COORDINATE SYSTEM MAX MAX MAX MAX MAX MAX ELEMENT NUMBER =

NODE NUMBER

=

KEYPOINT NUMBER =

LINE NUMBER =

AREA NUMBER

=

VOL.

NUMBER =

9341 10212 166 339 224 48

=

12

=

1 0

(CARTESIAN)

INITIAL JOBNAME = PADNC-TH CURRENT JOBNAME = PADNC-TH 10212 NODES (OF 8812 ELEMENTS (OF 10212 DEFINED) SELECTED BY NALL COMMAND.

8812 DEFINED) SELECTED BY EALL COMMAND.

LIST MATERIALS PROPERTY= ALL 1 TO 12 BY 1

PROPERTY TABLE TEMPERATURE 0.0000 PROPERTY TABLE TEMPERATURE 0.0000 PROPERTY TABLE TEMPERATURE 0.0000 EX MAT=

1 NUM. POINTS=

DATA TEMPERATURE DATA 0.20000E+07 NUXY MAT=

1 NUM. POINTS=

DATA TEMPERATURE DATA 0.24000 ALPX MAT=

1 NUM. POINTS=

DATA TEMPERATURE DATA 0.50000E-05 1

TEMPERATURE 1

TEMPERATURE 1

TEMPERATURE DATA DATA DATA PROPERTY TABLE TEMPERATURE 0.0000 PROPERTY TABLE TEMPERATURE 0.0000 DENS MAT=

1 NUM. POINTS=

DATA TEMPERATURE DATA 0.0000 EX MAT=

2 NUM.

POINTS=

DATA TEMPERATURE DATA 0.92400E+06 TEMPERATURE 1

TEMPERATURE DATA DATA PROPERTY TABLE TEMPERATURE 0.0000 PROPERTY TABLE TEMPERATURE 0.0000 NUXY MAT=

2 NUM. POINTS=

DATA TEMPERATURE DATA 0.15000 ALPX MAT=

2 NUM. POINTS=

DATA TEMPERATURE DATA 0.51800E-05 1

TEMPERATURE 1

TEMPERATURE DATA DATA PROPERTY TABLE DENS MAT=

2 NUM. POINTS=

TEMPERATURE DATA TEMPERATURE DATA 1

TEMPERATURE DATA

F - ;

ENERCON SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 Sheet 8 of 64

0. 0000 0.78100E-01 PROPERTY TABLE TEMPERATURE 0.0000 PROPERTY TABLE TEMPERATURE 0.0000 PROPERTY TABLE TEMPERATURE 0.0000 EX MAT=

3 NUM. POINTS=

DATA TEMPERATURE DATA 0.13060E+07 NUXY MAT=

3 NUM. POINTS=

DATA TEMPERATURE DATA 0.15000 ALPX MAT=

3 NUM.

POINTS=

DATA TEMPERATURE DATA 0.51800E-05 1

TEMPERATURE 1

TEMPERATURE 1

TEMPERATURE DATA DATA DATA PROPERTY TABLE DENS MAT=

3 NUM. POINTS=

TEMPERATURE DATA TEMPERATURE DATA 1

TEMPERATURE DATA 0.0000 0.78100E-01 PROPERTY TABLE TEMPERATURE 0.0000 PROPERTY TABLE TEMPERATURE 0.0000 EX MAT=

4 NUM. POINTS=

DATA TEMPERATURE DATA 0.14600E+07 NUXY MAT=

4 NUM.

POINTS=

DATA TEMPERATURE DATA 0.15000 1

TEMPERATURE 1

TEMPERATURE DATA DATA PROPERTY TABLE TEMPERATURE 0.0000 PROPERTY TABLE TEMPERATURE 0.0000 ALPX MAT=

4 NUM.

POINTS=

DATA TEMPERATURE DATA

0. 518OOE-05 DENS MAT=

4 NUM. POINTS=

DATA TEMPERATURE DATA 0.78100E-01 1

TEMPERATURE 1

TEMPERATURE DATA DATA PROPERTY TABLE TEMPERATURE 0.0000 EX MAT=

5 NUM.

POINTS=

DATA TEMPERATURE DATA 0.19640E+07 1

TEMPERATURE DATA PROPERTY TABLE TEMPERATURE 0.0000 NUXY MAT=

5 NUM.

POINTS=

DATA TEMPERATURE DATA 0.15000 1

TEMPERATURE DATA PROPERTY TABLE TEMPERATURE 0.0000 PROPERTY TABLE TEMPERATURE 0.0000 ALPX MAT=

5 NUM. POINTS=

DATA TEMPERATURE DATA 0.518iOE-05 DENS MAT=

5 NUM.

POINTS=

DATA TEMPERATURE DATA 0.78100E-01 1

TEMPERATURE 1

TEMPERATURE DATA DATA PROPERTY TABLE TEMPERATURE 0.0000 PROPERTY TABLE TEMPERATURE 0.0000 EX MAT=

DATA 0.23580E+07 NUXY MAT=

DATA 0.15000 6

NUM.

POINTS=

TEMPERATURE DATA 6

NUM.

POINTS=

TEMPERATURE DATA 1

TEMPERATURE 1

TEMPERATURE DATA DATA

F I ENERCON c

SRVI]xZTf#T'C!S IfTTNC Sheet 9 of 64 Appendix RPadNC-TH to Calculation PGE-009-CALC-006 PROPERTY TABLE TEMPERATURE 0.0000 PROPERTY TABLE TEMPERATURE 0.0000 ALPX MAT=

6 NUM. POINTS=

DATA TEMPERATURE DATA 0.51800E-05 DENS MAT=

6 NUM.

POINTS=

DATA TEMPERATURE DATA 0.7810GE-01 1

TEMPERATURE 1

TEMPERATURE DATA DATA PROPERTY TABLE TEMPERATURE 0.0000 PROPERTY TABLE TEMPERATURE 0.0000 PROPERTY TABLE TEMPERATURE 0.0000 EX MAT=

7 NUM.

POINTS=

DATA TEMPERATURE DATA 0.26740E+07 NUXY MAT=

7 NUM. POINTS=

DATA TEMPERATURE DATA 0.15000 ALPX MAT=

7 NUM. POINTS=

DATA TEMPERATURE DATA 0.51800E-05 1

TEMPERATURE 1

TEMPERATURE 1

TEMPERATURE DATA DATA DATA PROPERTY TABLE TEMPERATURE 0.0000 PROPERTY TABLE TEMPERATURE 0.0000 DENS MAT=

7 NUM. POINTS=

DATA TEMPERATURE DATA 0.78100E-01 EX MAT=

8 NUM. POINTS=

DATA TEMPERATURE DATA 0.27880E+07 1

TEMPERATURE 1

TEMPERATURE DATA DATA PROPERTY TABLE TEMPERATURE 0.0000 PROPERTY TABLE TEMPERATURE 0.0000 NUXY MAT=

8 NUM. POINTS=

DATA TEMPERATURE DATA 0.15000 ALPX MAT=

8 NUM. POINTS=

DATA TEMPERATURE DATA 0.51800E-05 1

TEMPERATURE 1

TEMPERATURE DATA DATA PROPERTY TABLE TEMPERATURE 0.0000 PROPERTY TABLE TEMPERATURE 0.0000 DENS MAT=

8 NUM. POINTS=

DATA TEMPERATURE DATA 0.78100E-01 EX MAT=

9 NUM. POINTS=

DATA TEMPERATURE DATA 0.30800E+07 1

TEMPERATURE DATA DATA 1

TEMPERATURE PROPERTY TABLE TEMPERATURE 0.0000 NUXY MAT=

9 NUM.

POINTS=

DATA TEMPERATURE DATA 0.15000 I

TEMPERATURE DATA PROPERTY TABLE TEMPERATURE 0.0000 PROPERTY TABLE TEMPERATURE 0.0000 ALPX MAT=

9 NUM. POINTS=

DATA TEMPERATURE DATA 0.51800E-05 DENS MAT=

9 NUM.

POINTS=

DATA TEMPERATURE DATA 0.78100E-01 1

TEMPERATURE 1

TEMPERATURE DATA DATA

FtSheet 10 of 64 j

ENERCON F

SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 PROPERTY TABLE TEMPERATURE 0.0000 PROPERTY TABLE TEMPERATURE 0.0000 EX MAT=

10 NUM.

POINTS=

DATA TEMPERATURE DATA 0.32710E+07 NUXY MAT=

10 NUM. POINTS=

DATA TEMPERATURE DATA 0.15000 1

TEMPERATURE 1

TEMPERATURE DATA DATA PROPERTY TABLE TEMPERATURE 0.0000 PROPERTY TABLE TEMPERATURE 0.0000 ALPX MAT=

10 NUM. POINTS=

DATA TEMPERATURE DATA 0.51800E-05 DENS MAT=

10 NUM.

POINTS=

DATA TEMPERATURE DATA 0.78100E-01 1

TEMPERATURE 1

TEMPERATURE DATA DATA PROPERTY TABLE TEMPERATURE 0.0000 PROPERTY TABLE TEMPERATURE 0.0000 EX MAT=

11 NUM. POINTS=

DATA TEMPERATURE DATA 0.35430E+07 NUXY MAT=

11 NUM. POINTS=

DATA TEMPERATURE DATA 0.15000 1

TEMPERATURE 1

TEMPERATURE DATA DATA PROPERTY TABLE TEMPERATURE 0.0000 PROPERTY TABLE TEMPERATURE 0.0000 ALPX MAT=

11 NUM. POINTS=

DATA TEMPERATURE DATA 0.51800E-05 DENS MAT=

11 NUM. POINTS=

DATA TEMPERATURE DATA 0.78100E-01 1

TEMPERATURE 1

TEMPERATURE DATA DATA PROPERTY TABLE TEMPERATURE 0.0000 EX MAT=

12 NUM.

POINTS=

DATA TEMPERATURE DATA 0.36690E+07 1

TEMPERATURE DATA PROPERTY TABLE NUXY MAT=

12 NUM. POINTS=

TEMPERATURE DATA TEMPERATURE DATA 1

TEMPERATURE DATA 0.0000 0.15000 PROPERTY TABLE TEMPERATURE 0.0000 PROPERTY TABLE TEMPERATURE 0.0000 ALPX MAT=

12 NUM.

POINTS=

DATA TEMPERATURE DATA 0.51800E-05 DENS MAT=

12 NUM. POINTS=

DATA TEMPERATURE DATA 0.78100E-01 1

TEMPERATURE DATA 1

TEMPERATURE DATA start, change the material properties for each time step, initial property is no. 2. Change back to no. 2 at end and save.

ANSYS SOLUTION ROUTINE *****

PRINT HEADER DO NOT PRINT SUBTITLE(S)

DO NOT PRINT LOAD STEP ID DO NOT PRINT NOTE LINE(S)

Sheet 11 of 64 F* i ENERCON ta SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 PRINT COLUMN HEADER LABELS DO NOT PRINT REPORT TOTALS LIST ALL SELECTED ELEMENTS IN RANGE 1

530 TO 530 STEP 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 13:35:44 JAN 03, 2003 CP=

Pad thermal analysis model, no pad/rock constraint 0.421 ELEM MAT TYP REL ESY SEC TSHA 530 2

2 1

0 1

ANSYS RELEASE 6.1 UP20020321 PRINTOUT RESUMED BY /GOP NODES 1

28 29 3

672 1050 1064 13:34:25 01/03/2003 728 Load step file number 1. Begin solution...

ANSYS SOLVE COMMAND *****

NOTE ***

CP=

1.612 TIME= 13:35:45 Real constant 1 has been referenced by element types 4 and 5.

We assume it identifies a contact pair.

1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 13:35:46 JAN 03, 2003 CP=

DELTA T 0.0 TO 0.25 DAYS -

NO PAD/ROCK CONSTRAINT 1.833 S O L U T I O N O P T I O N S PROBLEM DIMENSIONALITY..

......3-D DEGREES OF FREEDOM....

.. UX UY UZ ANALYSIS TYPE.

................STATIC (STEADY-STATE)

EQUATION SOLVER OPTION.............PCG TOLERANCE.................. 1.00000E-06 NEWTON-RAPHSON OPTION.

............ PROGRAM CHOSEN NOTE ***

CP=

1.863 TIME= 13:35:46 Present time 0 is less than or equal to the previous time.

Time will default to 1.

NOTE ***

CP=

1.863 TIME= 13:35:46 Nonlinear analysis, NROPT set to the FULL Newton-Raphson solution procedure for ALL DOFs.

NOTE ***

CP=

1.863 TIME= 13:35:46 The conditions for direct assembly have been met.

No.emat or.erot files will be produced.

Sheet 12 of 64 T

ENERCON FH SERVICES, INC.

Appendix R-PadNC-TH to Calculation PGE-009-CALC-006 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.....

TERMINATE ANALYSIS IF NOT CONVERGED...

CONVERGENCE CONTROLS....

INERTIA LOADS X

ACEL............

0.0000 PRINT OUTPUT CONTROLS...

DATABASE OUTPUT CONTROLS.........

1. 0000 ON 10 10 2

15 NO YES (EXIT)

USE DEFAULTS Y

Z 0.80000 0.0000

...NO PRINTOUT

...ALL DATA WRITTEN FOR THE LAST SUBSTEP NONLINEAR MONITORING INFO IS WRITTEN TO FILE= PADNC-TH.mntr MAXIMUM NUMBER OF EQUILIBRIUM ITERATIONS HAS BEEN MODIFIED TO BE, NEQIT = 26, BY SOLUTION CONTROL LOGIC.

NOTE ***

CP=

2.674 TIME= 13:35:47 Deformable-deformable contact pair identified by real constant set 1 and contact element type 5 has been set up.

Contact algorithm: Augmented Lagrange method Contact detection at: Gauss integration point Default contact stiffness factor FKN 1.0000 The resulting contact stiffness 0.15725E+07 Default penetration tolerance factor FTOLN 0.10000 The resulting penetration tolerance 1.1752 User define tangent contact stiffness FKT 0.1000GE-08 Max. friction stress TAUMAX 0.10000 Average contact surface length 39.172 Average contact pair depth 11.752 Default pinball region factor PINB 1.0000 The resulting pinball region 11.752 User define initial closure ICONT 0.100OOE-05 Initial penetration is excluded.

• • • NOTE ***

CP=

2.674 TIME= 13:35:47 Max.

Initial penetration 1.421085472E-14 was detected between contact element 9172 and target element 9002.

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

CALCULATIONS ASSUME ELEMENT MASS AT ELEMENT CENTROID TOTAL MASS =

0.19272E+07 MOM. OF INERTIA MOM. OF INERTIA

A' -Sheet 13 of 64 F.

J.:

ENERCON Fj INC C

Appendix RPadNC-TH to Calculation PGE-009-CALC-006

"'I-CENTER OF MASS XC =

204.00 YC =

-48.000 ZC =

315.00 ABOUT ORIGIN IXX =

0.2606E+12 IYY =

0.3614E+12 IZZ =

0.1126E+12 IXY =

0.1887E+ll IYZ =

0.2914E+l1 IZX =

-0.1238E+12 ABOUT CENTER OF MASS IXX =

IYY =

IZZ =

IXY =

IYZ =

IZX =

0. 6494E+l1

0. 8995E+l1

0. 2793E+l1

-0.2327E-03

-0.3052E-04 0.2487E-02 MASS

SUMMARY

BY ELEMENT TYPE

• TYPE MASS 2

0.192718E+07 Range of element maximum matrix coefficients in global coordinates Maximum= 549511638 at element 7329.

Minimum= 4772865.79 at element 5330.

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

6602 SOLID45 2.684 0.000407 2

1870 SOLID45 0.951 0.000509 4

170 TARGE170 0.050 0.000295 5

170 CONTA174 0.200 0.001178 Time at end of element matrix formulation CP= 6.91995049.

ALL CURRENT ANSYS DATA WRITTEN TO FILE NAME= PADNC-TH.rdb FOR POSSIBLE RESUME FROM THIS POINT FORCE CONVERGENCE VALUE

0.4318E+06 CRITERION

2203.

PRECONDITIONED SOLVER CP TIME =

5.328 EQUIL ITER 1 COMPLETED.

NEW TRIANG MATRIX.

MAX DOF INC=

0.6684E-02 LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC =

0.6684E-02 FORCE CONVERGENCE VALUE

=

52.11 CRITERION=

70.77

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

ELEMENT RESULT CALCULATION TIMES TYPE NUMBER ENAME TOTAL CP AVE CP 1

6602 2

1870 4

170 5

170 SOLID45 SOLID45 TARGE170 CONTA174 1.552 0.461 0.010 0. 010 0.000235 0.000246 0.000059 0.000059 AVE CP

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

6602 SOLID45 0.050 0.000008 2

1870 SOLID45 0.030 0.000016 4

170 TARGE170 0.000 0.000000 5

170 CONTA174 0.000 0.000000 LOAD STEP 1

SUBSTEP 1

COMPLETED.

• • • TIME =

0.100000 TIME INC =

0.100000

• • • AUTO STEP TIME:

NEXT TIME INC = 0.10000 CUM ITER =

UNCHANGED 1

Sheet 14 of 64 ENERCON F4 SERVICESIC a

NC1s. Appendix RPadNC-TH to Calculation PGE-009-CALC-006 FORCE CONVERGENCE VALUE

=

208.4 CRITERION= 2244.

EQUIL ITER 1 COMPLETED.

NEW TRIANG MATRIX.

MAX DOF INC= -0.2318E-07 LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC = -0.2318E-07 FORCE CONVERGENCE VALUE

= 0.5057E-03 CRITERION= 141.5

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

LOAD STEP 1

SUBSTEP 2

COMPLETED.

CUM ITER =

2 TIME =

0.200000 TIME INC =

0.100000 AUTO TIME STEP:

NEXT TIME INC = 0.15000 INCREASED (FACTOR = 1.5000)

FORCE CONVERGENCE VALUE

=

117.2 CRITERION=

3367.

EQUIL ITER 1 COMPLETED.

NEW TRIANG MATRIX.

MAX DOF INC:

LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC = -

FORCE CONVERGENCE VALUE

0.4110E-03 CRITERION

247.7

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

LOAD STEP 1

SUBSTEP 3

COMPLETED.

CUM ITER =

TIME =

0.350000 TIME INC =

0.150000

• • • AUTO TIME STEP:

NEXT TIME INC = 0.22500 INCREASED (I

= -0.1160E-07

-0.1160E-07

<<< CONVERGED 3

FACTOR = 1.5000)

FORCE CONVERGENCE VALUE

=

439.4 CRITERION=

5052.

EQUIL ITER 1 COMPLETED.

NEW TRIANG MATRIX.

MAX DOF INC:

LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC = -

FORCE CONVERGENCE VALUE

= 0.5355E-03 CRITERION= 406.9

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

LOAD STEP 1

SUBSTEP 4

COMPLETED.

CUM ITER =

• • • TIME =

0.575000 TIME INC =

0.225000

• • • AUTO TIME STEP:

NEXT TIME INC = 0.21250 DECREASED (I

= -0.4661E-07

-0.4661E-07

<<< CONVERGED 4

FACTOR = 0.9444)

FORCE CONVERGENCE VALUE

=

484.0 CRITERION= 4781.

EQUIL ITER 1 COMPLETED.

NEW TRIANG MATRIX.

MAX DOF INC= -0.5138E-07 LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC = -0.5138E-07 FORCE CONVERGENCE VALUE

0.6700E-03 CRITERION

557.3

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

LOAD STEP 1

SUBSTEP 5

COMPLETED.

CUM ITER =

5 TIME =

0.787500 TIME INC =

0.212500 AUTO STEP TIME:

NEXT TIME INC = 0.21250 UNCHANGED FORCE CONVERGENCE VALUE

=

469.9 CRITERION= 4795.

EQUIL ITER 1 COMPLETED.

NEW TRIANG MATRIX.

MAX DOF INC=

LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC = -0 FORCE CONVERGENCE VALUE

= 0.7436E-03 CRITERION= 707.7

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

LOAD STEP 1

SUBSTEP 6

COMPLETED.

CUM ITER =

• • • TIME =

1.00000 TIME INC =

0.212500

-0.4994E-07

.4994E-07

<<< CONVERGED 6

• • • ANSYS BINARY FILE STATISTICS BUFFER SIZE USED= 16384 45.062 MB WRITTEN ON ELEMENT SAVED DATA FILE: PADNC-TH.esav 19.875 MB WRITTEN ON RESULTS FILE: PADNC-TH.rst ESEL FOR LABEL= TYPE FROM 1870 ELEMENTS (OF 2 TO 2 BY 1

3812 DEFINED) SELECTED BY ESEL COMMAND.

SET MATERIAL OF SELECTED ELEMENTS TO 3

8812 ELEMENTS (OF 8812 DEFINED) SELECTED BY EALL COMMAND.

F-Sheet 15 of 64

-v3 ENERCON byF SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 LIST ALL SELECTED ELEMENTS IN RANGE 1

530 TO 530 STEP 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 13:40:23 JAN 03, 2003 CP=

DELTA T 0.0 TO 0.25 DAYS -

NO PAD/ROCK CONSTRAINT 114. 585 ELEM MAT TYP REL ESY SEC TSHA NODES 530 3

2 1

ANSYS RELEASE 6.1 0

1 UP20020321 1

28 29 3

672 1050 1064 13:34:25 01/03/2003 728 PRINTOUT RESUMED BY /GOP Load step file number 2. Begin solution...

ANSYS SOLVE COMMAND NOTE ***

CP=

115.776 TIME= 13:40:24 Present time 0 is less than or equal to the previous time.

Time will default to 2.

NOTE ***

CP=

115.786 TIME= 13:40:24 Nonlinear analysis, NROPT set to the FULL Newton-Raphson solution procedure for ALL DOFs.

1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 13:40:24 JAN 03, 2003 CP=

115. 927 DELTA T 0.25 TO 0.50 DAYS -

NO PAD/ROCK CONSTRAINT 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.......

TERMINATE ANALYSIS IF NOT CONVERGED.....

CONVERGENCE CONTROLS.............

INERTIA LOADS X

ACEL............

0.0000 0

PRINT OUTPUT CONTROLS............

DATABASE OUTPUT CONTROLS...........

2

.2.0000 ON 10 10 2

15 NO

.YES (EXIT)

.USE DEFAULTS Y

z

.20000 0.0000

.NO PRINTOUT

.ALL DATA WRITTEN FOR THE LAST SUBSTEP

ENERCON

.Sheet 16 of 64 E N ENERC 0N rP SERVICES, INC. Appendix RPadNC-TH to Calculation PGE-009-CALC-006 NONLINEAR MONITORING INFO IS WRITTEN TO FILE= PADNC-TH.mntr MAXIMUM NUMBER OF EQUILIBRIUM ITERATIONS HAS BEEN MODIFIED TO BE, NEQIT = 26, BY SOLUTION CONTROL LOGIC.

FORCE CONVERGENCE VALUE

0.3731E+06 CRITERION

1992.

EQUIL ITER 1 COMPLETED.

NEW TRIANG MATRIX.

MAX DOF INC= -0.8173E-03 LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC = -0.8173E-03 FORCE CONVERGENCE VALUE

=

30.27 CRITERION=

781.6

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

• • • LOAD STEP 2

SUBSTEP 1

COMPLETED.

CUM ITER =

7

• • • TIME =

1.10000 TIME INC =

0.100000

• • • AUTO STEP TIME:

NEXT TIME INC = 0.10000 UNCHANGED FORCE CONVERGENCE VALUE EQUIL ITER 1 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 2 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE

= 0.4804E+05 CRITERION= 1993.

NEW TRIANG MATRIX.

MAX DOF INC=

0.1179E-03 1.000 SCALED MAX DOF INC =

0.1179E-03

=

1296.

CRITERION= 841.4 NEW TRIANG MATRIX.

MAX DOF INC=

0.1132E-04 1.000 SCALED MAX DOF INC =

0.1132E-04

= 0.3743E-01 CRITERION= 858.6

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2

• • • LOAD STEP 2

SUBSTEP 2

COMPLETED.

CUM ITER =

• • • TIME =

1.20000 TIME INC =

0.100000 AUTO TIME STEP:

NEXT TIME INC = 0.15000 INCREASED

(]

9 FACTOR = 1.5000)

FORCE CONVERGENCE VALUE EQUIL ITER 1 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 2 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 3 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 4 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 5 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE

0.1510E+05 CRITERION

2899.

NEW TRIANG MATRIX.

MAX DOF INC=

0.1011E-02 1.000 SCALED MAX DOF INC =

0.1011E-02

= 0.1738E+05 CRITERION= 964.3 NEW TRIANG MATRIX.

MAX DOF INC=

0.2671E-03 1.000 SCALED MAX DOF INC =

0.2671E-03

0.2148E+05 CRITERION

983.9 NEW TRIANG MATRIX.

MAX DOF INC=

0.3632E-03 1.000 SCALED MAX DOF INC =

0.3632E-03

=

8178.

CRITERION=

1004.

NEW TRIANG MATRIX. MAX DOF INC= 0.4921E-04 1.000 SCALED MAX DOF INC =

0.4921E-04

=

3834.

CRITERION=

1024.

NEW TRIANG MATRIX.

MAX DOF INC=

0.6391E-04 0.9998 SCALED MAX DOF INC =

0.6390E-04

78.15 CRITERION

1045.

<<< CONVEIRGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 5

• • • LOAD STEP 2

SUBSTEP 3

COMPLETED.

CUM ITER =

TIME =

1.35000 TIME INC =

0.150000 AUTO STEP TIME:

NEXT TIME INC = 0.15000 UNCHANGED 14 FORCE CONVERGENCE VALUE EQUIL ITER 1 COMPLETED.

LINE SEARCH PARAMETER

=

FORCE CONVERGENCE VALUE EQUIL ITER 2 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 3 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 4 COMPLETED.

0.3409E+05 CRITERION

2937.

NEW TRIANG MATRIX. MAX DOF INC=

0.1317E-02 1.000 SCALED MAX DOF INC =

0.1317E-02

0.4240E+05 CRITERION

1114.

NEW TRIANG MATRIX.

MAX DOF INC=

0.3709E-03 1.000 SCALED MAX DOF INC =

0.3709E-03

0.3237E+05 CRITERION

1137.

NEW TRIANG MATRIX.

MAX DOF INC=

0.3361E-03 1.000 SCALED MAX DOF INC =

0.3361E-03

0.2330E+05 CRITERION

1160.

NEW TRIANG MATRIX. MAX DOF INC=

0.2500E-03

F

'l.0.;

sSheet 17 of 64 r

3 ENERCON i

SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 5 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 6 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE 0.9604 SCALED MAX DOF INC =

0.2401E-03

0.1158E+05 CRITERION

1184.

NEW TRIANG MATRIX.

MAX DOF INC= 0.2217E-04 0.6216 SCALED MAX DOF INC =

0.1378E-04

=

7584.

CRITERION=

1208.

NEW TRIANG MATRIX.

MAX DOF INC= 0.1688E-04 1.000 SCALED MAX DOF INC =

0.1688E-04

0.1078 CRITERION

1233.

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 6

LOAD STEP 2

SUBSTEP 4 COMPLETED.

CUM ITER =

TIME =

1.50000 TIME INC =

0.150000 AUTO TIME STEP:

NEXT TIME INC = 0.22500 INCREASED (I 20 FACTOR = 1.5000)

FORCE CONVERGENCE VALUE EQUIL ITER 1 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 2 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 3 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 4 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 5 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 6 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 7 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 8 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE

0.6908E+05 CRITERION

4331.

NEW TRIANG MATRIX.

MAX DOF INC=

0.1848E-02 1.000 SCALED MAX DOF INC =

0.1848E-02

0.1555E+06 CRITERION

1374.

NEW TRIANG MATRIX.

MAX DOF INC=

0.1838E-02 1.000 SCALED MAX DOF INC =

0.1838E-02

= 0.8063E+05 CRITERION= 1399.

NEW TRIANG MATRIX.

MAX DOF INC=

0.9756E-03 1.000 SCALED MAX DOF INC =

0.9756E-03

= 0.6383E+05 CRITERION= 1427.

NEW TRIANG MATRIX.

MAX DOF INC=

0.7197E-03 1.000 SCALED MAX DOF INC =

0.7197E-03

= 0.4351E+05 CRITERION= 1456.

NEW TRIANG MATRIX.

MAX DOF INC=

0.3812E-03 1.000 SCALED MAX DOF INC =

0.3812E-03

0.2032E+05 CRITERION

1485.

NEW TRIANG MATRIX.

MAX DOF INC=

0.1836E-03 1.000 SCALED MAX DOF INC =

0.1836E-03

0.1218E+05 CRITERION

1516.

NEW TRIANG MATRIX.

MAX DOF INC=

0.1528E-03 1.000 SCALED MAX DOF INC =

0.1528E-03

=

5006.

CRITERION=

1546.

NEW TRIANG MATRIX.

MAX DOF INC=

0.1436E-04 1.000 SCALED MAX DOF INC =

0.1436E-04

=

460.3 CRITERION=

1578.

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 8

• • • LOAD STEP 2

SUBSTEP 5 COMPLETED.

CUM ITER =

• • • TIME =

1.72500 TIME INC =

0.225000 AUTO TIME STEP:

NEXT TIME INC = 0.13750 DECREASED (I 28 FACTOR = 0.6111)

FORCE CONVERGENCE VALUE EQUIL ITER 1 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 2 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 3 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 4 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 5 COMPLETED.

0.4049E+05 CRITERION

2881.

NEW TRIANG MATRIX.

MAX DOF INC=

0.3067E-02 1.000 SCALED MAX DOF INC = 0.3067E-02

= 0.9006E+05 CRITERION= 1537.

NEW TRIANG MATRIX.

MAX DOF INC= 0.9012E-03 1.000 SCALED MAX DOF

0.6440E+05 CRITERION

NEW TRIANG MATRIX.

MAX 1.000 SCALED MAX DOF

0.2276E+05 CRITERION

NEW TRIANG MATRIX.

MAX I INC = 0.9012E-03 1568.

DOF INC=

0.1780E-02

? INC =

0.1780E-02 1598.

DOF INC=

0.4194E-03 1.000 SCALED MAX DOF INC =

0.4194E-03

0.2843E+05 CRITERION

1630.

NEW TRIANG MATRIX.

MAX DOF INC= 0.3437E-03

1 Sheet 18 of 64 F* J:,

ENERCON SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 6 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 7 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE 1.000 SCALED MAX DOF INC =

0.3437E-03

=

8170.

CRITERION=

1663.

NEW TRIANG MATRIX.

MAX DOF INC=

0.8265E-04 1.000 SCALED MAX DOF INC =

0.8265E-04

=

2244.

CRITERION=

1697.

NEW TRIANG MATRIX.

MAX DOF INC=

0.5491E-05 1.000 SCALED MAX DOF INC =

0.5491E-05

0.2719E-01 CRITERION

1731.

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 7

• • • LOAD STEP 2

SUBSTEP 6 COMPLETED.

CUM ITER =

• • • TIME =

1.86250 TIME INC =

0.137500

• • • AUTO STEP TIME:

NEXT TIME INC = 0.13750 UNCHANGED 35 FORCE CONVERGENCE VALUE EQUIL ITER 1 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 2 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 3 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 4 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 5 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 6 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 7 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE

0.5578E+05 CRITERION

2959.

NEW TRIANG MATRIX.

MAX DOF INC=

0.4532E-02 1.000 SCALED MAX DOF INC =

0.4532E-02

= 0.1543E+06 CRITERION= 1698.

NEW TRIANG MATRIX.

MAX DOF INC=

0.2760E-02 1.000 SCALED MAX DOF INC =

0.2760E-02

0.7344E+05 CRITERION

1729.

NEW TRIANG MATRIX.

MAX DOF INC=

0.1086E-02 1.000 SCALED MAX DOF INC =

0.1086E-02

0.9026E+05 CRITERION

1763.

NEW TRIANG MATRIX.

MAX DOF INC=

0.1853E-02 1.000 SCALED MAX DOF INC =

0.1853E-02

0.4200E+05 CRITERION

1794.

NEW TRIANG MATRIX.

MAX DOF INC=

0.4741E-03 1.000 SCALED MAX DOF INC =

0.4741E-03

0.2867E+05 CRITERION

1830.

NEW TRIANG MATRIX.

MAX DOF INC=

0.3608E-03 1.000 SCALED MAX DOF INC =

0.3608E-03

0.1357E+05 CRITERION

1866.

NEW TRIANG MATRIX.

MAX DOF INC=

0.1397E-03 1.000 SCALED MAX DOF INC =

0.1397E-03

821.6 CRITERION

1904.

<<< CONVEFRGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 7

LOAD STEP 2

SUBSTEP 7

COMPLETED.

CUM ITER =

• • • TIME =

2.00000 TIME INC =

0.137500 42 ESEL FOR LABEL= TYPE FROM 2 TO 2 BY 1

1870 ELEMENTS (OF 8812 DEFINED) SELECTED BY ESEL COMMAND.

SET MATERIAL OF SELECTED ELEMENTS TO 4

8812 ELEMENTS (OF 8812 DEFINED) SELECTED BY EALL COMMAND.

LIST ALL SELECTED ELEMENTS IN RANGE 1

530 TO 530 STEP 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 13:56:47 JAN 03, 2003 CP=

634.532 DELTA T 0.25 TO 0.50 DAYS -

NO PAD/ROCK CONSTRAINT

rF^ ENERCON t;1 SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 Sheet 19 of 64 ELEM MAT TYP REL ESY SEC TSHA NODES 530 4

2 1

0 1

ANSYS RELEASE 6.1 UP20020321 1

28 29 3

672 1050 1064 13:34:25 01/03/2003 728 PRINTOUT RESUMED BY /GOP Load step file number 3.

Begin solution...

ANSYS SOLVE COMMAND

• • • NOTE ***

CP=

635.714 TIME= 13:56:48 Present time 0 is less than or equal to the previous time.

Time will default to 3.

• • • NOTE ***

CP=

635.714 TIME= 13:56:48 Nonlinear analysis, NROPT set to the FULL Newton-Raphson solution procedure for ALL DOFs.

1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 13:56:48 JAN 03, 2003 CP=

DELTA T 0.50 TO 0.625 DAYS -

NO PAD/ROCK CONSTRAINT L O A D S T E P O P T I O N S 635.874 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.

TERMINATE ANALYSIS IF NOT CONVERGED..

CONVERGENCE CONTROLS..

INERTIA LOADS X

ACEL.

0.0000 PRINT OUTPUT CONTROLS.

DATABASE OUTPUT CONTROLS...

3 3.0000 ON 10 10 2

15 NO

.YES (EXIT)

. USE DEFAULTS Y

Z 0.10000E-01 0.0000

.NO PRINTOUT

.ALL DATA WRITTEN FOR THE LAST SUBSTEP NONLINEAR MONITORING INFO IS WRITTEN TO FILE= PADNC-TH.mntr MAXIMUM NUMBER OF EQUILIBRIUM ITERATIONS HAS BEEN MODIFIED TO BE, NEQIT = 26, BY SOLUTION CONTROL LOGIC.

FORCE CONVERGENCE VALUE EQUIL ITER 1 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 2 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE

0.4646E+06 CRITERION

2981.

NEW TRIANG MATRIX.

MAX DOF INC= -0.4120E-02 1.000 SCALED MAX DOF INC = -0.4120E-02

0.2043E+05 CRITERION

1700.

NEW TRIANG MATRIX.

MAX DOF INC=

0.2140E-03 1.000 SCALED MAX DOF INC =

0.2140E-03

=

7043.

CRITERION=

1734.

F.>

Sheet 20 of 64 F -i, ENERCON SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 EQUIL ITER 3 COMPLETED.

NEW TRIANG MATRIX.

MAX DOF INC=

0.6592E-04 LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC =

0.6592E-04 FORCE CONVERGENCE VALUE

=

1194.

CRITERION= 1769.

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 3

LOAD STEP 3

SUBSTEP 1 COMPLETED.

CUM ITER =

45 TIME =

2.10000 TIME INC =

0.100000

• • • AUTO STEP TIME:

NEXT TIME INC = 0.10000 UNCHANGED FORCE CONVERGENCE VALUE EQUIL ITER 1 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 2 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE

0.2245E+05 CRITERION

3005.

NEW TRIANG MATRIX.

MAX DOF INC= -0.5312E-02 0.9108 SCALED MAX DOF INC = -0.4839E-02

0.7829E+05 CRITERION

1580.

NEW TRIANG MATRIX.

MAX DOF INC= -0.4441E-03 1.000 SCALED MAX DOF INC = -0.4441E-03

=

342.5 CRITERION= 1613.

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2

• • • LOAD STEP 3

SUBSTEP 2 COMPLETED.

CUM IT]

• • • TIME =

2.20000 TIME INC =

0.100000

• • • AUTO TIME STEP:

NEXT TIME INC = 0.15000 INCREASI

'ER =

47 FD (FACTOR = 1.5000)

FORCE CONVERGENCE VALUE

=

2022.

CRITERION= 4016.

EQUIL ITER 1 COMPLETED.

NEW TRIANG MATRIX.

MAX DOF INC=

0.1150E-04 LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC =

0.1150E-04 FORCE CONVERGENCE VALUE

=

608.9 CRITERION= 1410.

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

• • • LOAD STEP 3

SUBSTEP 3 COMPLETED.

CUM ITER =

48

• • • TIME =

2.35000 TIME INC =

0.150000

• • • AUTO TIME STEP:

NEXT TIME INC = 0.22500 INCREASED (FACTOR = 1.5000)

FORCE CONVERGENCE VALUE

=

3469.

CRITERION= 5672.

EQUIL ITER 1 COMPLETED.

NEW TRIANG MATRIX. MAX DOF INC=

0.2432E-04 LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC =

0.2432E-04 FORCE CONVERGENCE VALUE

=

1008.

CRITERION= 1177.

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

• • • LOAD STEP 3

SUBSTEP 4

COMPLETED.

CUM ITER =

49

• • • TIME =

2.57500 TIME INC =

0.225000

• • • AUTO TIME STEP:

NEXT TIME INC = 0.21250 DECREASED (FACTOR = 0.9444)

FORCE CONVERGENCE VALUE EQUIL ITER 1 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 2 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 3 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE

=

7183.

CRITERION=

5310.

NEW TRIANG MATRIX.

MAX DOF INC=

0.1127E-03 1.000 SCALED MAX DOF INC =

0.1127E-03

=

5362.

CRITERION= 997.7 NEW TRIANG MATRIX.

MAX DOF INC= 0.6234E-04 1.000 SCALED MAX DOF INC =

0.6234E-04

=

3189.

CRITERION=

1018.

NEW TRIANG MATRIX.

MAX DOF INC= 0.2718E-04 1.000 SCALED MAX DOF INC =

0.2718E-04

= 0.2659E-01 CRITERION= 1039.

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 3

• • • LOAD STEP 3

SUBSTEP 5 COMPLETED.

CUM ITER =

• • • TIME =

2.78750 TIME INC =

0.212500 AUTO STEP TIME:

NEXT TIME INC = 0.21250 UNCHANGED 52 FORCE CONVERGENCE VALUE EQUIL ITER 1 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE

=

8875.

CRITERION= 5259.

NEW TRIANG MATRIX. MAX DOF INC-0.2460E-03 1.000 SCALED MAX DOF INC =

0.2460E-03

0.1099E+05 CRITERION

883.7

ENERCON F

SERVICES,INC.

Appendix RPadNC-TH to Caiculation PGE-009-CALC-006 Sheet 21 of 64 EQUIL ITER 2 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 3 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 4 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 5 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 6 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 7 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 8 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE NEW TRIANG MATRIX.

MAX DOF INC= 0.2148E-03 1.000 SCALED MAX DOF INC =

0.2148E-03

0.1279E+05 CRITERION

901.6 NEW TRIANG MATRIX.

MAX DOF INC=

0.2540E-03 0.4813 SCALED MAX DOF

0.2202E+05 CRITERION

NEW TRIANG MATRIX.

MAX 1.000 SCALED MAX DOF

=

5359.

CRITERION=

NEW TRIANG MATRIX.

MAX 1.000 SCALED MAX DOF

=

6626.

CRITERION=

NEW TRIANG MATRIX.

MAX I INC =

0.1222E-03 919.9 DOF INC=

0.2295E-03 I INC =

0.2295E-03 938.5 DOF INC=

0.1636E-03 I INC =

0.1636E-03 957.6 DOF INC=

0.1540E-03 1.000 SCALED MAX DOF INC =

0.1540E-03

=

2895.

CRITERION=

977.1 NEW TRIANG MATRIX.

MAX DOF INC=

0.5269E-04 1.000 SCALED MAX DOF INC =

0.5269E-04

=

2383.

CRITERION=

997.0 NEW TRIANG MATRIX.

MAX DOF INC=

0.6485E-04 1.000 SCALED MAX DOF INC =

0.6485E-04

=

272.5 CRITERION=

1017.

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 8

• • • LOAD STEP 3

SUBSTEP 6 COMPLETED.

CUM ITER =

TIME =

3.00000 TIME INC =

0.212500 60 ESEL FOR LABEL= TYPE FROM 2 TO 2 BY 1

1870 ELEMENTS (OF 8812 DEFINED) SELECTED BY ESEL COMMAND.

SET MATERIAL OF SELECTED ELEMENTS TO 5

8812 ELEMENTS (OF 8812 DEFINED) SELECTED BY EALL COMMAND.

LIST ALL SELECTED ELEMENTS IN RANGE 1

530 TO 530 STEP 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 14:06:18 JAN 03, 2003 CP=

922.727 DELTA T 0.50 TO 0.625 DAYS -

NO PAD/ROCK CONSTRAINT ELEM MAT TYP REL ESY SEC TSHA NODES 530 5

2 1

ANSYS RELEASE 6.1 0

1 UP20020321 1

28 29 3

672 1050 13:34:25 01/03/2003 1064 728 PRINTOUT RESUMED BY /GOP Load step file number 4. Begin solution...

ANSYS SOLVE NOTE ***

COMMAND CP=

923.878 TIME= 14:06:19 Present time 0 is less than or equal to the previous time.

Time will default to 4.

F

~ ENERCON SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 NOTE

• CP=

923.878 TIME= 14:06:19 Nonlinear analysis, NROPT set to the FULL Newton-Raphson solution procedure for ALL DOFs.

1 ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 14:06:19 JAN 03, 2003 CP=

92 Sheet 22 of 64

4. 069 DELTA T 0.625 TO 1.125 DAYS -

NO PAD/ROCK CONSTRAINT 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.

TERMINATE ANALYSIS IF NOT CONVERGED.

CONVERGENCE CONTROLS...

INERTIA LOADS X

ACEL.

0.0000 PRINT OUTPUT CONTROLS..

DATABASE OUTPUT CONTROLS..

4 4.0000 ON 10 10 2

15 NO

.YES (EXIT)

.USE DEFAULTS Y

Z 0.100OOE-01 0.0000

.NO PRINTOUT

.ALL DATA WRITTEN FOR THE LAST SUBSTEP NONLINEAR MONITORING INFO IS WRITTEN TO FILE= PADNC-TH.mntr MAXIMUM NUMBER OF EQUILIBRIUM ITERATIONS HAS BEEN MODIFIED TO BE, NEQIT = 26, BY SOLUTION CONTROL LOGIC.

FORCE CONVERGENCE VALUE EQUIL ITER 1 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 2 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 3 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 4 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 5 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 6 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 7 COMPLETED.

LINE SEARCH PARAMETER =

0.6213E+06 CRITERION

3342.

NEW TRIANG MATRIX.

MAX DOF INC=

0.2765E-01 1.000 SCALED MAX DOF INC =

0.2765E-01

0.3958E+05 CRITERION

1170.

NEW TRIANG MATRIX.

MAX DOF INC=

0.1181E-02 1.000 SCALED MAX DOF INC =

0.1181E-02

0.4961E+05 CRITERION

1193.

NEW TRIANG MATRIX.

MAX DOF INC=

0.1298E-02 1.000 SCALED MAX DOF INC = 0.1298E-02

0.3071E+05 CRITERION

1216.

NEW TRIANG MATRIX.

MAX DOF INC=

0.1402E-02 1.000 SCALED MAX DOF INC =

0.1402E-02

0.3983E+05 CRITERION

1239.

NEW TRIANG MATRIX.

MAX DOF INC=

0.1342E-02 0.7264 SCALED MAX DOF INC =

0.9745E-03

0.5643E+05 CRITERION

1264.

NEW TRIANG MATRIX.

MAX DOF INC=

0.9254E-03 1.000 SCALED MAX DOF INC =

0.9254E-03

0.3241E+05 CRITERION

1288.

NEW TRIANG MATRIX. MAX DOF INC=

0.8728E-03 1.000 SCALED MAX DOF INC =

0.8728E-03

Sheet 23 of 64 V

ENERCON F,

SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 FORCE CONVERGENCE VALUE EQUIL ITER 8 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 9 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 10 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 11 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 12 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE

0.1358E+05 CRITERION

1314.

NEW TRIANG MATRIX.

MAX DOF INC=

0.3576E-03 1.000 SCALED MAX DOF INC =

0.3576E-03

0.2152E+05 CRITERION

1340.

NEW TRIANG MATRIX.

MAX DOF INC=

0.5284E-03 1.000 SCALED MAX DOF INC =

0.5284E-03

=

7742.

CRITERION=

1367.

NEW TRIANG MATRIX.

MAX DOF INC=

0.1498E-03 1.000 SCALED MAX DOF INC =

0.1498E-03

=

9601.

CRITERION=

1394.

NEW TRIANG MATRIX.

MAX DOF INC=

0.1790E-03 0.9929 SCALED MAX DOF INC =

0.1777E-03

=

4456.

CRITERION=

1422.

NEW TRIANG MATRIX.

MAX DOF INC=

0.2672E-04 1.000 SCALED MAX DOF INC =

0.2672E-04

=

18.52 CRITERION=

1451.

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 12 LOAD STEP 4

SUBSTEP 1

COMPLETED.

CUM ITER =

TIME =

3.10000 TIME INC =

0.100000 AUTO STEP TIME:

NEXT TIME INC = 0.10000 UNCHANGED 72 FORCE CONVERGENCE VALUE EQUIL ITER 1 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 2 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE

=

6693.

CRITERION=

3361.

NEW TRIANG MATRIX.

MAX DOF INC= -0.9103E-03 1.000 SCALED MAX DOF INC = -0.9103E-03

=

4650.

CRITERION=

1276.

NEW TRIANG MATRIX.

MAX DOF INC=

0.6610E-04 1.000 SCALED MAX DOF INC =

0.6610E-04

0.1706E-01 CRITERION

1302.

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2

LOAD STEP 4

SUBSTEP 2

COMPLETED.

CUM ITER =

TIME =

3.20000 TIME INC =

0.100000 AUTO TIME STEP:

NEXT TIME INC = 0.15000 INCREASED (I 74 FACTOR = 1.5000)

FORCE CONVERGENCE VALUE EQUIL ITER 1 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 2 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE

=

6926.

CRITERION=

4908.

NEW TRIANG MATRIX.

MAX DOF INC=

1.000 SCALED MAX DOF INC =

(

=

2157.

CRITERION=

1499.

NEW TRIANG MATRIX.

MAX DOF INC=

1.000 SCALED MAX DOF INC =

(

0.4400E-02 CRITERION

1530.

0. 1656E-03

).1656E-03 0.2942E-04

).2942E-04

<<< CONVERGED 76

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2

LOAD STEP 4

SUBSTEP 3

COMPLETED.

CUM ITER =

TIME =

3.35000 TIME INC =

0.150000 AUTO TIME STEP:

NEXT TIME INC = 0.22500 INCREASED (1FACTOR = 1.5000)

FORCE CONVERGENCE VALUE

=

4829.

CRITERION=

7274.

EQUIL ITER 1 COMPLETED.

NEW TRIANG MATRIX.

MAX DOF INC:

LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC =

FORCE CONVERGENCE VALUE

=

421.7 CRITERION=

1905.

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

LOAD STEP 4

SUBSTEP 4

COMPLETED.

CUM ITER =

• • • TIME =

3.57500 TIME INC =

0.225000 AUTO TIME STEP:

NEXT TIME INC = 0.21250 DECREASED (I

=

0.1485E-03

0. 1485E-03

<<< CONVERGED 77 FACTOR = 0.9444)

FORCE CONVERGENCE VALUE EQUIL ITER 1 COMPLETED.

LINE SEARCH PARAMETER =

=

4868.

CRITERION=

6969.

NEW TRIANG MATRIX.

MAX DOF INC=

0.1236E-03 1.000 SCALED MAX DOF INC =

0.1236E-03

Sheet 24 of 64 ENERCON F

i SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 FORCE CONVERGENCE VALUE

= 0.2624E-01 CRITERION= 2331.

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

LOAD STEP 4

SUBSTEP 5

COMPLETED.

CUM ITER =

TIME =

3.78750 TIME INC =

0.212500 AUTO STEP TIME:

NEXT TIME INC = 0.21250 UNCHANGED FORCE CONVERGENCE VALUE

=

419.8 CRITERION= 7082.

EQUIL ITER 1 COMPLETED.

NEW TRIANG MATRIX.

MAX DOF INC=

LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC = -0 FORCE CONVERGENCE VALUE

= 0.3022E-02 CRITERION= 2779.

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

LOAD STEP 4

SUBSTEP 6

COMPLETED.

CUM ITER =

TIME =

4.00000 TIME INC =

0.212500 ESEL FOR LABEL= TYPE FROM 2 TO 2 BY 1

1870 ELEMENTS (OF 8812 DEFINED) SELECTED BY ESEL CO]

SET MATERIAL OF SELECTED ELEMENTS TO 6

8812 ELEMENTS (OF 8812 DEFINED) SELECTED BY EALL CO]

LIST ALL SELECTED ELEMENTS IN RANGE 530 TO 530 STEP

<<< CONVERGED 78

-0.1070E-04

• .1070E-04

<<< CONVERGED 79 DMMAND.

)MMAND.

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 14:16:02 JAN 03, 2003 CP=

1222.067 DELTA T 0.625 TO 1.125 DAYS -

NO PAD/ROCK CONSTRAINT ELEM MAT TYP REL ESY SEC TSHA NODES 530 6

2 1

0 1

1 28 ANSYS RELEASE 6.1 UP20020321 13:34:26 PRINTOUT RESUMED BY /GOP Load step file number 5.

Begin solution...

ANSYS SOLVE COMMAND 29 3

672 1050 1064 728 01/03/2003

• • • NOTE ***

CP=

1223.259 TIME= 14:16:03 Present time 0 is less than or equal to the previous time.

Time will default to 5.

• • • NOTE ***

CP=

1223.259 TIME= 14:16:03 Nonlinear analysis, NROPT set to the FULL Newton-Raphson solution procedure for ALL DOFs.

1 ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 14:16:03 JAN 03, 2003 CP=

1223.459 DELTA T 1.125 TO 1.625 DAYS -

NO PAD/ROCK CONSTRAINT

-fI. V" Sheet 25 of 64 F

ENERCON 3,

SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 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.

TERMINATE ANALYSIS IF NOT CONVERGED..

CONVERGENCE CONTROLS..

INERTIA LOADS X

5 5.0000 ON 10 10 2

15 NO

.YES (EXIT)

. USE DEFAULTS Y

Z 0.10000E-01 0.0000

.NO PRINTOUT

.ALL DATA WRITTEN FOR THE LAST SUBSTEP ACEL.

PRINT OUTPUT CONTROLS.

DATABASE OUTPUT CONTROLS.

0.0000 NONLINEAR MONITORING INFO IS WRITTEN TO FILE= PADNC-TH.mntr MAXIMUM NUMBER OF EQUILIBRIUM ITERATIONS HAS BEEN MODIFIED TO BE, NEQIT = 26, BY SOLUTION CONTROL LOGIC.

FORCE CONVERGENCE VALUE

0.4292E+06 CRITERION

3822.

EQUIL ITER 1 COMPLETED.

NEW TRIANG MATRIX. MAX DOF INC= -0.1462E-01 LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC = -0.1462E-01 FORCE CONVERGENCE VALUE

=

2.580 CRITERION=

3034.

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

• • • LOAD STEP 5

SUBSTEP 1

COMPLETED.

CUM ITER =

80

• • • TIME =

4.10000 TIME INC =

0.100000

• • • AUTO STEP TIME:

NEXT TIME INC = 0.10000 UNCHANGED FORCE CONVERGENCE VALUE =

2120.

CRITERION=

3835.

EQUIL ITER 1 COMPLETED.

NEW TRIANG MATRIX.

MAX DOF INC= -0.1935E-02 LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC = -0.1935E-02 FORCE CONVERGENCE VALUE

0.4969 CRITERION

2874.

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

LOAD STEP 5

SUBSTEP 2

COMPLETED.

CUM ITER =

81 TIME =

4.20000 TIME INC =

0.100000 AUTO TIME STEP:

NEXT TIME INC = 0.15000 INCREASED (FACTOR = 1.5000)

FORCE CONVERGENCE VALUE

=

3.246 CRITERION=

4518.

EQUIL ITER 1 COMPLETED.

NEW TRIANG MATRIX.

MAX DOF INC= -0.1452E-07 LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC = -0.1452E-07 FORCE CONVERGENCE VALUE

0.8580E-05 CRITERION

2638.

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

LOAD STEP 5

SUBSTEP 3

COMPLETED.

CUM ITER =

82 TIME =

4.35000 TIME INC =

0.150000 AUTO TIME STEP:

NEXT TIME INC = 0.22500 INCREASED (FACTOR = 1.5000)

FORCE CONVERGENCE VALUE =

2.172 CRITERION=

5802.

EQUIL ITER 1 COMPLETED.

NEW TRIANG MATRIX.

MAX DOF INC=

0.2709E-08 LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC =

0.2709E-08 FORCE CONVERGENCE VALUE = 0.7065E-05 CRITERION=

2296.

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

u~ M' 4Sheet 26 of 64 F- -- `4 ENERCON F

SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 Vl,;--

• • • LOAD STEP 5

SUBSTEP 4 COMPLETED.

• • • TIME =

4.57500 TIME INC =

0.225000

• • • AUTO TIME STEP:

NEXT TIME INC = 0.21250 CUM ITER =

83 DECREASED (FACTOR - 0.9444)

FORCE CONVERGENCE VALUE

=

1.543 CRITERION=

5381.

EQUIL ITER 1 COMPLETED.

NEW TRIANG MATRIX.

MAX DOF INC=

0.2121E-08 LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC =

0.2121E-08 FORCE CONVERGENCE VALUE = 0.1272E-04 CRITERION=

1992.

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

LOAD STEP 5

SUBSTEP 5

COMPLETED.

CUM ITER =

84 TIME =

4.78750 TIME INC =

0.212500 AUTO STEP TIME:

NEXT TIME INC = 0.21250 UNCHANGED FORCE CONVERGENCE VALUE =

1.499 CRITERION=

5241.

EQUIL ITER 1 COMPLETED.

NEW TRIANG MATRIX.

MAX DOF INC= 0.2060E-08 LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC =

0.2060E-08 FORCE CONVERGENCE VALUE = 0.8331E-05 CRITERION=

1719.

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

LOAD STEP 5

SUBSTEP 6

COMPLETED.

CUM ITER =

85 TIME =

5.00000 TIME INC =

0.212500 ESEL FOR LABEL= TYPE FROM 2 TO 2 BY 1

1870 ELEMENTS (OF 8812 DEFINED) SELECTED BY ESEL COMMAND.

SET MATERIAL OF SELECTED ELEMENTS TO 7

8812 ELEMENTS (OF 8812 DEFINED) SELECTED BY EALL COMMAND.

LIST ALL SELECTED ELEMENTS IN RANGE 530 TO 530 STEP 1

1 ***

ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical t 00245050 VERSION=INTEL NT 14:20:38 JAN 03, 2003 CP=

1342.330 DELTA T 1.125 TO 1.625 DAYS -

NO PAD/ROCK CONSTRAINT ELEM MAT TYP REL ESY SEC TSHA NODES 530 7

2 1

0 1

ANSYS RELEASE 6.1 UP20020321 1

28 29 3

672 1050 1064 728 13:34:26 01/03/2003 PRINTOUT RESUMED BY /GOP Load step file number 6. Begin solution...

ANSYS SOLVE NOTE ***

COMMAND *****

CP=

1343.512 TIME= 14:20:39 Present time 0 is less than or equal to the previous time.

Time will default to 6.

NOTE ***

CP=

1343.512 TIME= 14:20:39 Nonlinear analysis, NROPT set to the FULL Newton-Raphson solution procedure for ALL DOFs.

F ^ ENERCON F1 SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 1

ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 14:20:39 JAN 03, 2003 CP=

134 Sheet 27 of 64 13.742 DELTA T 1.625 TO 2.125 DAYS -

NO PAD/ROCK CONSTRAINT 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.

TERMINATE ANALYSIS IF NOT CONVERGED CONVERGENCE CONTROLS...........

INERTIA LOADS X

ACEL...

0.0000 PRINT OUTPUT CONTROLS..........

DATABASE OUTPUT CONTROLS.........

6 6.0000 ON 10 10 2

15 NO

.YES (EXIT)

...USE DEFAULTS Y

Z 0.10000E-0l 0.0000

...NO PRINTOUT

...ALL DATA WRITTEN FOR THE LAST SUBSTEP NONLINEAR MONITORING INFO IS WRITTEN TO FILE= PADNC-TH.mntr MAXIMUM NUMBER OF EQUILIBRIUM ITERATIONS HAS BEEN MODIFIED TO BE, NEQIT = 26, BY SOLUTION CONTROL LOGIC.

FORCE CONVERGENCE VALUE

0.2461E+06 CRITERION

2202.

EQUIL ITER 1 COMPLETED.

NEW TRIANG MATRIX.

MAX DOF INC= -0.8446E-02 LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC = -0.8446E-02 FORCE CONVERGENCE VALUE

0.6207 CRITERION

1754.

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

• • • LOAD STEP 6

SUBSTEP 1

COMPLETED.

CUM ITER =

86

• • • TIME =

5.10000 TIME INC =

0.100000

• • • AUTO STEP TIME:

NEXT TIME INC = 0.10000 UNCHANGED FORCE CONVERGENCE VALUE

=

1348.

CRITERION=

2187.

EQUIL ITER 1 COMPLETED.

NEW TRIANG MATRIX.

MAX DOF INC= -0.1139E-02 LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC = -0.1139E-02 FORCE CONVERGENCE VALUE

0.1469 CRITERION

1665.

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

• • • LOAD STEP 6

SUBSTEP 2 COMPLETED.

CUM ITER =

87

• • • TIME =

5.20000 TIME INC =

0.100000

• • • AUTO TIME STEP:

NEXT TIME INC = 0.15000 INCREASED (FACTOR = 1.5000)

FORCE CONVERGENCE VALUE

=

7944.

CRITERION=

2570.

EQUIL ITER 1 COMPLETED.

NEW TRIANG MATRIX.

MAX DOF INC= 0.1628E-04 LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC =

0.1628E-04 FORCE CONVERGENCE VALUE

0.7646E-02 CRITERION

1536.

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

• • • LOAD STEP 6

SUBSTEP 3

COMPLETED.

CUM ITER =

88

• • • TIME =

5.35000 TIME INC =

0.150000

F j ENERCON E 2SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 Sheet 28 of 64 AUTO TIME STEP:

NEXT TIME INC = 0.22500 INCREASED (FACTOR = 1.5000)

FORCE CONVERGENCE VALUE

=

2905.

CRITERION=

3296.

EQUIL ITER 1 COMPLETED.

NEW TRIANG MATRIX.

MAX DOF INC=

LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC =

I FORCE CONVERGENCE VALUE

0.2894E-02 CRITERION

1359.

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

LOAD STEP 6

SUBSTEP 4

COMPLETED.

CUM ITER =

TIME =

5.57500 TIME INC =

0.225000 AUTO TIME STEP:

NEXT TIME INC = 0.21250 DECREASED (Fj 0.5952E-05 3.5952E-05

<<< CONVERGED 89

'CTOR = 0.9444)

FORCE CONVERGENCE VALUE = 0.6420 CRITERION=

3065.

EQUIL ITER 1 COMPLETED.

NEW TRIANG MATRIX.

MAX DOF INC=

0.9504E-09 LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC =

0.9504E-09 FORCE CONVERGENCE VALUE

0.1335E-04 CRITERION

1216.

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

• • • LOAD STEP 6

SUBSTEP 5 COMPLETED.

CUM ITER =

90

• • • TIME =

5.78750 TIME INC =

0.212500

• • • AUTO STEP TIME:

NEXT TIME INC = 0.21250 UNCHANGED FORCE CONVERGENCE VALUE = 0.6238 CRITERION= 2994.

EQUIL ITER 1 COMPLETED.

NEW TRIANG MATRIX.

MAX DOF INC=

0.9156E-09 LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC =

0.9156E-09 FORCE CONVERGENCE VALUE = 0.1947E-04 CRITERION=

1104.

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

• • • LOAD STEP 6

SUBSTEP 6 COMPLETED.

CUM ITER =

91 TIME =

6.00000 TIME INC =

0.212500 ESEL FOR LABEL= TYPE FROM 1870 ELEMENTS (OF 2 TO 2 BY 1

3812 DEFINED) SELECTED BY ESEL COMMAND.

SET MATERIAL OF SELECTED ELEMENTS TO 8

8812 ELEMENTS (OF 8812 DE]

LIST ALL SELECTED ELEMENTS IN RANGE 1

FINED) SELECTED BY EALL COMMAND.

530 TO 530 STEP 1

1462.403

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 14:25:13 JAN 03, 2003 CP=

DELTA T 1.625 TO 2.125 DAYS -

NO PAD/ROCK CONSTRAINT ELEM MAT TYP REL ESY SEC TSHA NODES 530 8

2 1

0 1

ANSYS RELEASE 6.1 UP20020321 1

28 29 3

672 1050 1064 13:34:26 01/03/2003 728 PRINTOUT RESUMED BY /GOP Load step file number 7. Begin solution...

ANSYS SOLVE COMMAND

Sheet 29 of 64 F

]

ENERCON m-aSEVCES INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 NOTE ***

CP=

1463.615 TIME= 14:25:15 Present time 0 is less than or equal to the previous time.

Time will default to 7.

• • • NOTE ***

CP=

1463.615 TIME= 14:25:15 Nonlinear analysis, NROPT set to the FULL Newton-Raphson solution procedure for ALL DOFs.

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 14:25:15 JAN 03, 2003 CP=

1463.865 DELTA T 2.125 TO 2.375 DAYS -

NO PAD/ROCK CONSTRAINT 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.....

TERMINATE ANALYSIS IF NOT CONVERGED...

CONVERGENCE CONTROLS...........

INERTIA LOADS X

ACEL............

0.0000 PRINT OUTPUT CONTROLS..........

DATABASE OUTPUT CONTROLS.........

7 7.0000 ON 10 10 2

15 NO

...YES (EXIT)

...USE DEFAULTS Y

Z 0.10000E-01 0.0000

. NO PRINTOUT ALL DATA WRITTEN FOR THE LAST SUBSTEP NONLINEAR MONITORING INFO IS WRITTEN TO FILE= PADNC-TH.mntr MAXIMUM NUMBER OF EQUILIBRIUM ITERATIONS HAS BEEN MODIFIED TO BE, NEQIT = 26, BY SOLUTION CONTROL LOGIC.

FORCE CONVERGENCE VALUE EQUIL ITER 1 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 2 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE

0.1711E+06 CRITERION

1399.

NEW TRIANG MATRIX.

MAX DOF INC= -0.7109E-02 1.000 SCALED MAX DOF INC = -0.7109E-02

=

1389.

CRITERION=

1048.

NEW TRIANG MATRIX.

MAX DOF INC=

0.3765E-05 1.000 SCALED MAX DOF INC =

0.3765E-05

= 0.1351E-02 CRITERION= 1069.

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2

• • • LOAD STEP 7

SUBSTEP 1 COMPLETED.

CUM ITER =

TIME =

6.10000 TIME INC =

0.100000

• • • AUTO STEP TIME:

NEXT TIME INC = 0.10000 UNCHANGED 93 FORCE CONVERGENCE VALUE

=

1667.

CRITERION=

1372.

EQUIL ITER 1 COMPLETED.

NEW TRIANG MATRIX.

MAX DOF INC= -0.3381E-03 LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC = -0.3381E-03 FORCE CONVERGENCE VALUE

0.5729E-01 CRITERION

980.4

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

• • • LOAD STEP 7

SUBSTEP 2 COMPLETED.

CUM ITER =

94

i

.Sheet 30 of 64 ENERCON

>;1 SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006

• • • TIME =

6.20000 TIME INC =

0.100000

• • • AUTO TIME STEP:

NEXT TIME INC = 0.15000 INCREASED (FACTOR = 1.5000)

FORCE CONVERGENCE VALUE

=

5727.

CRITERION=

1656.

EQUIL ITER 1 COMPLETED.

NEW TRIANG MATRIX. MAX DOF INC=

0.8935E-05 LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC = 0.8935E-05 FORCE CONVERGENCE VALUE

0.5787E-02 CRITERION

880.6

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

• • • LOAD STEP 7

SUBSTEP 3

COMPLETED.

CUM ITER =

95

• • • TIME =

6.35000 TIME INC =

0.150000

• • • AUTO TIME STEP:

NEXT TIME INC = 0.22500 INCREASED (FACTOR = 1.5000)

FORCE CONVERGENCE VALUE = 0.1937E+05 CRITERION=

2182.

EQUIL ITER 1 COMPLETED.

NEW TRIANG MATRIX.

MAX DOF INC:

LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC =

FORCE CONVERGENCE VALUE = 709.0 CRITERION=

734.2

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

• • • LOAD STEP 7

SUBSTEP 4

COMPLETED.

CUM ITER =

TIME =

6.57500 TIME INC =

0.225000

• • • AUTO TIME STEP:

NEXT TIME INC = 0.21250 DECREASED (E

= 0.1890E-04

0. 1890E-04

<<< CONVERGED 96 FACTOR = 0.9444)

FORCE CONVERGENCE VALUE EQUIL ITER 1 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 2 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 3 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE

0.5490E+05 CRITERION

2022.

NEW TRIANG MATRIX.

MAX DOF INC= -0.3676E-04 1.000 SCALED MAX DOF

=

7200.

CRITERION=

NEW TRIANG MATRIX.

MAX 1.000 SCALED MAX DOF

=

865.0 CRITERION=

NEW TRIANG MATRIX.

MAX IINC = -0.3676E-04 602.1 DOF INC=

0.5997E-04 I INC =

0.5997E-04 613.8 DOF INC= 0.4426E-05 1.000 SCALED MAX DOF INC =

0.4426E-05

0.9521E-03 CRITERION

626.3

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 3

• • • LOAD STEP 7

SUBSTEP 5

COMPLETED.

CUM ITER =

• • • TIME =

6.78750 TIME INC =

0.212500 AUTO STEP TIME:

NEXT TIME INC = 0.21250 UNCHANGED 99 FORCE CONVERGENCE VALUE EQUIL ITER 1 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 2 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 3 COMPLETED.

LINE SEARCH PARAMETER =

0.1377E+06 CRITERION

1976.

NEW TRIANG MATRIX.

MAX DOF INC= -0.6734E-04 1.000 SCALED MAX DOF INC = -0.6734E-04

0.1313E+05 CRITERION

479.5 NEW TRIANG MATRIX.

MAX DOF INC=

0.1167E-03 0.9923 SCALED MAX DOF INC =

0.1158E-03

=

2959.

CRITERION= 488.4 NEW TRIANG MATRIX.

MAX DOF INC= 0.5754E-05 1.000 SCALED MAX DOF INC =

0.5754E-05 FORCE CONVERGENCE VALUE

0.3291E-02 CRITERION

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION

• • • LOAD STEP 7

SUBSTEP 6

COMPLETED.

CUM TIME =

7.00000 TIME INC =

0.212500 498.3 3

ITER =

1

<<< CONVERGED 102 ESEL FOR LABEL= TYPE FROM 1870 ELEMENTS (OF E

2 TO 2 BY 3812 DEFINED) SELECTED BY ESEL COMMAND.

SET MATERIAL OF SELECTED ELEMENTS TO 9

8812 ELEMENTS (OF 8812 DEFINED) SELECTED BY EALL COMMAND.

Sheet 31 of 64 ENERCON

. J SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 LIST ALL SELECTED ELEMENTS IN RANGE 1

530 TO 530 STEP 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 14:31:37 JAN 03, 2003 CP=

DELTA T 2.125 TO 2.375 DAYS -

NO PAD/ROCK CONSTRAINT 1646.738 ELEM MAT TYP REL ESY SEC TSHA NODES 530 9

2 1

ANSYS RELEASE 6.1 0

1 UP20020321 1

28 29 3

672 1050 1064 13:34:26 01/03/2003 728 PRINTOUT RESUMED BY /GOP Load step file number 8. Begin solution...

ANSYS SOLVE

• • • NOTE ***

COMMAND CP=

1647.910 TIME= 14:31:39 Present time 0 is less than or equal to the previous time.

Time will default to 8.

• • • NOTE ***

CP=

1647.910 TIME= 14:31:39 Nonlinear analysis, NROPT set to the FULL Newton-Raphson solution procedure for ALL DOFs.

1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 14:31:39 JAN 03, 2003 CP=

1648.180 DELTA T 2.375 TO 3.125 DAYS -

NO PAD/ROCK CONSTRAINT 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.....

TERMINATE ANALYSIS IF NOT CONVERGED.

CONVERGENCE CONTROLS...........

INERTIA LOADS X

ACEL............

0.0000 PRINT OUTPUT CONTROLS..........

DATABASE OUTPUT CONTROLS.........

8 8.0000 ON 10 10 2

15 NO YES (EXIT)

...USE DEFAULTS Y

Z 0.10000E-01 0.0000

...NO PRINTOUT

...ALL DATA WRITTEN FOR THE LAST SUBSTEP

F-. Ad Sheet 32 of 64 z3 ENERCON

-a SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 NONLINEAR MONITORING INFO IS WRITTEN TO FILE= PADNC-TH.mntr MAXIMUM NUMBER OF EQUILIBRIUM ITERATIONS HAS BEEN MODIFIED TO BE, NEQIT = 26, BY SOLUTION CONTROL LOGIC.

FORCE CONVERGENCE VALUE EQUIL ITER 1 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 2 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE

0.1434E+06 CRITERION

874.4 NEW TRIANG MATRIX.

MAX DOF INC=

1.000 SCALED MAX DOF INC =

(

=

1432.

CRITERION= 561.7 NEW TRIANG MATRIX.

MAX DOF INC=

1.000 SCALED MAX DOF INC =

C

=

33.40 CRITERION= 573.0 0.3282E-02

).3282E-02

0. 1720E-04 J.1720E-04

<<< CONVERGED 104

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2

• • • LOAD STEP 8

SUBSTEP 1

COMPLETED.

CUM ITER =

TIME =

7.10000 TIME INC =

0.100000 AUTO STEP TIME:

NEXT TIME INC = 0.10000 UNCHANGED FORCE CONVERGENCE VALUE

=

2587.

CRITERION= 905.5 EQUIL ITER 1 COMPLETED.

NEW TRIANG MATRIX.

MAX DOF INC= -0.6956E-03 LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC = -0.6956E-03 FORCE CONVERGENCE VALUE = 0.1320 CRITERION= 639.7

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

LOAD STEP 8

SUBSTEP 2

COMPLETED.

CUM ITER =

105 TIME =

7.20000 TIME INC =

0.100000 AUTO TIME STEP:

NEXT TIME INC = 0.15000 INCREASED (FACTOR = 1.5000)

FORCE CONVERGENCE VALUE =

587.4 CRITERION= 1256.

EQUIL ITER 1 COMPLETED.

NEW TRIANG MATRIX.

MAX DOF INC= 0.1270E-04 LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC =

0.1270E-04 FORCE CONVERGENCE VALUE = 0.2012E-02 CRITERION= 761.3

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

LOAD STEP 8

SUBSTEP 3

COMPLETED.

CUM ITER =

106 TIME =

7.35000 TIME INC =

0.150000 AUTO TIME STEP:

NEXT TIME INC = 0.22500 INCREASED (FACTOR = 1.5000)

FORCE CONVERGENCE VALUE

=

1165.

CRITERION= 1803.

EQUIL ITER 1 COMPLETED.

NEW TRIANG MATRIX.

MAX DOF INC=

LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC =

C FORCE CONVERGENCE VALUE

0.1652E-02 CRITERION

949.6

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

LOAD STEP 8

SUBSTEP 4

COMPLETED.

CUM ITER =

TIME =

7.57500 TIME INC =

0.225000 AUTO TIME STEP:

NEXT TIME INC = 0.21250 DECREASED (F) 0.8370E-05 J.8370E-05

<<< CONVERGED 107

'CTOR = 0.9444)

FORCE CONVERGENCE VALUE =

678.2 CRITERION= 1792.

EQUIL ITER 1 COMPLETED.

NEW TRIANG MATRIX.

MAX DOF INC=

0.5891E-05 LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC =

0.5891E-05 FORCE CONVERGENCE VALUE = 0.6588E-03 CRITERION= 1131.

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

• • • LOAD STEP 8

SUBSTEP 5 COMPLETED.

CUM ITER =

108

• • • TIME =

7.78750 TIME INC =

0.212500 AUTO STEP TIME:

NEXT TIME INC = 0.21250 UNCHANGED FORCE CONVERGENCE VALUE

=

384.3 CRITERION= 1879.

EQUIL ITER 1 COMPLETED.

NEW TRIANG MATRIX.

MAX DOF INC=

0.3927E-05 LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC =

0.3927E-05 FORCE CONVERGENCE VALUE = 0.4297E-03 CRITERION=

1315.

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

4 -.,

Sheet 33 of 64 r-j ENERCON

• 1 SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006

• • • LOAD STEP 8

SUBSTEP 6 COMPLETED.

CU]

TIME =

8.00000 TIME INC =

0.212500 ESEL FOR LABEL= TYPE FROM 2 TO 2 BY 1870 ELEMENTS (OF 8812 DEFINED) SELECTED BY SET MATERIAL OF SELECTED ELEMENTS TO 10 8812 ELEMENTS (OF 8812 DEFINED) SELECTED BY LIST ALL SELECTED ELEMENTS IN RANGE 530 TO 5'

1

.M ITER =

109 1

ESEL COMMAND.

EALL COMMAND.

30 STEP 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 14:36:39 JAN 03, 2003 CP=

1785.247 DELTA T 2.375 TO 3.125 DAYS - NO PAD/ROCK CONSTRAINT ELEM MAT TYP REL ESY SEC TSHA 530 10 2

1 0

1 ANSYS RELEASE 6.1 UP20020321 PRINTOUT RESUMED BY /GOP NODES 1

28 13 :34 : 26 29 3

672 1050 1064 728 01/03/2003 Load step file number 9.

Begin solution...

ANSYS SOLVE COMMAND NOTE ***

CP=

1786.439 TIME= 14:36:40 Present time 0 is less than or equal to the previous time.

Time will default to 9.

• • • NOTE ***

CP=

1786.439 TIME= 14:36:40 Nonlinear analysis, NROPT set to the FULL Newton-Raphson solution procedure for ALL DOFs.

1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 14:36:40 JAN 03, 2003 CP=

DELTA T 3.125 TO 4.125 DAYS -

NO PAD/ROCK CONSTRAINT 1786.729 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...

9 9.0000 ON 10 10 2

15

Y-`;1a.u Sheet 34 of 64 ENERCON F

SERVICESINC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 STEP CHANGE BOUNDARY CONDITIONS....

TERMINATE ANALYSIS IF NOT CONVERGED..

CONVERGENCE CONTROLS...

INERTIA LOADS X

ACEL...

0.0000 PRINT OUTPUT CONTROLS.........

DATABASE OUTPUT CONTROLS........

NO

....YES (EXIT)

....USE DEFAULTS Y

z 0.10000E-01 0.0000

....NO PRINTOUT

....ALL DATA WRITTEN FOR THE LAST SUBSTEP NONLINEAR MONITORING INFO IS WRITTEN TO FILE= PADNC-TH.mntr MAXIMUM NUMBER OF EQUILIBRIUM ITERATIONS HAS BEEN MODIFIED TO BE, NEQIT = 26, BY SOLUTION CONTROL LOGIC.

FORCE CONVERGENCE VALUE EQUIL ITER 1 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 2 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE

0.1579E+06 CRITERION

1544.

NEW TRIANG MATRIX.

MAX DOF INC= -0.4250E-02 1.000 SCALED MAX DOF INC = -0.4250E-02

=

1388.

CRITERION=

1369.

NEW TRIANG MATRIX.

MAX DOF INC=

0.2245E-05 1.000 SCALED MAX DOF INC =

0.2245E-05

0.1330E-02 CRITERION

1397.

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2

• • • LOAD STEP 9

SUBSTEP 1 COMPLETED.

CUM ITER =

• • • TIME =

8.10000 TIME INC =

0.100000

• • • AUTO STEP TIME:

NEXT TIME INC = 0.10000 UNCHANGED 111 FORCE CONVERGENCE VALUE

=

2169.

CRITERION=

1550.

EQUIL ITER 1 COMPLETED.

NEW TRIANG MATRIX.

MAX DOF INC= -0.4096E-03 LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC = -0.4096E-03 FORCE CONVERGENCE VALUE

0.7776E-01 CRITERION

1399.

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

LOAD STEP 9

SUBSTEP 2

COMPLETED.

CUM ITER =

112 TIME =

8.20000 TIME INC =

0.100000 AUTO TIME STEP:

NEXT TIME INC = 0.15000 INCREASED (FACTOR = 1.5000)

FORCE CONVERGENCE VALUE

=

4811.

CRITERION=

1812.

EQUIL ITER 1 COMPLETED.

NEW TRIANG MATRIX.

MAX DOF INC=

0.2673E-05 LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC =

0.2673E-05 FORCE CONVERGENCE VALUE

=

337.0 CRITERION=

1448.

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

LOAD STEP 9

SUBSTEP 3

COMPLETED.

CUM ITER =

113 TIME =

8.35000 TIME INC =

0.150000 AUTO TIME STEP:

NEXT TIME INC = 0.22500 INCREASED (FACTOR = 1.5000)

FORCE CONVERGENCE VALUE EQUIL ITER 1 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 2 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 3 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE

>>> SOLUTION CONVERGED AFI LOAD STEP 9

SUBSTEE TIME =

8.57500

0.6516E+05 CRITERION

2291.

NEW TRIANG MATRIX.

MAX DOF INC= 0.3814E-04 1.000 SCALED MAX DOF INC = 0.3814E-04

=

5800.

CRITERION=

1533.

NEW TRIANG MATRIX.

MAX DOF INC=

0.6145E-04 0.7865 SCALED MAX DOF INC =

0.4833E-04

=

3896.

CRITERION=

1565.

NEW TRIANG MATRIX.

MAX DOF INC=

0.1264E-04 1.000 SCALED MAX DOF INC =

0.1264E-04

0.5462E-02 CRITERION

1597.

<<< CONVE

'ER EQUILIBRIUM ITERATION 3

4 COMPLETED.

CUM ITER =

116 TIME INC =

0.225000 RGED

ENERCON 11 SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 Sheet 35 of 64 AUTO STEP TIME:

NEXT TIME INC = 0.22500 UNCHANGED FORCE CONVERGENCE VALUE EQUIL ITER 1 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 2 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 3 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE

0.2643E+06 CRITERION

2333.

NEW TRIANG MATRIX.

MAX DOF INC= -0.5424E-04 1.000 SCALED MAX DOF INC = -0.5424E-04

0.1165E+05 CRITERION

1630.

NEW TRIANG MATRIX.

MAX DOF INC=

0.1006E-03 1.000 SCALED MAX DOF INC =

0.1006E-03

=

2812.

CRITERION=

1662.

NEW TRIANG MATRIX.

MAX DOF INC=

0.9901E-05 1.000 SCALED MAX DOF INC =

0.9901E-05

=

1140.

CRITERION=

1696.

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 3

LOAD STEP 9

SUBSTEP 5

COMPLETED.

CUM ITER =

• • • TIME =

8.80000 TIME INC =

0.225000 AUTO TIME STEP:

NEXT TIME INC = 0.20000 DECREASED (]

119 FACTOR = 0.8889)

FORCE CONVERGENCE VALUE EQUIL ITER 1 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 2 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 3 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 4 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 5 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 6 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE

0.1648E+07 CRITERION

2235.

NEW TRIANG MATRIX.

MAX DOF INC=

0.1566E-03 1.000 SCALED MAX DOF INC =

0.1566E-03

0.1823E+05 CRITERION

1722.

NEW TRIANG MATRIX.

MAX DOF INC=

0.2158E-03 1.000 SCALED MAX DOF INC =

0.2158E-03

=

9137.

CRITERION=

1757.

NEW TRIANG MATRIX.

MAX DOF INC=

0.1434E-03 1.000 SCALED MAX DOF INC =

0.1434E-03

=

8202.

CRITERION=

1792.

NEW TRIANG MATRIX.

MAX DOF INC=

0.9303E-04 1.000 SCALED MAX DOF INC =

0.9303E-04

=

5427.

CRITERION=

1829.

NEW TRIANG MATRIX.

MAX DOF INC=

0.9349E-04 1.000 SCALED MAX DOF INC =

0.9349E-04

=

2773.

CRITERION=

1866.

NEW TRIANG MATRIX.

MAX DOF INC=

0.2899E-04 1.000 SCALED MAX DOF INC =

0.2899E-04

=

1679.

CRITERION=

1904.

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 6

LOAD STEP 9

SUBSTEP 6

COMPLETED.

CUM ITER =

TIME =

9.00000 TIME INC =

0.200000 125 ESEL FOR LABEL= TYPE FROM 2 TO 2 BY 1

1870 ELEMENTS (OF 8812 DEFINED) SELECTED BY ESEL COMMAND.

SET MATERIAL OF SELECTED ELEMENTS TO 11 8812 ELEMENTS (OF 8812 DEFINED) SELECTED BY EALL COMMAND.

LIST ALL SELECTED ELEMENTS IN RANGE 1

530 TO 530 STEP 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 14:45:39 JAN 03, 2003 CP=

2036.839 DELTA T 3.125 TO 4.125 DAYS -

NO PAD/ROCK CONSTRAINT

l..

Sheet 36 of 64 F 3AnCH li ENERCON t 4 SERVICES, INC.

Appendix RPadNC-TH to Calculation PGEC-009-CALC-006 ELEM MAT TYP REL ESY SEC TSHA NODES 530 11 2

ANSYS RELEASE 6.1 1

0 1

UP20020321 1

28 29 3

672 1050 1064 728 13:34:26 01/03/2003 PRINTOUT RESUMED BY /GOP Load step file number 10.

Begin solution...

ANSYS SOLVE COMMAND

• • • NOTE ***

CP=

2038.031 TIME= 14:45:40 Present time 0 is less than or equal to the previous time.

Time will default to 10.

• • • NOTE ***

CP=

2038.031 TIME= 14:45:40 Nonlinear analysis, NROPT set to the FULL Newton-Raphson solution procedure for ALL DOFs.

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 14:45:41 JAN 03, 2003 CP=

2038. 351 DELTA T 4.125 TO 6.125 DAYS -

NO PAD/ROCK CONSTRAINT 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.

TERMINATE ANALYSIS IF NOT CONVERGED..

CONVERGENCE CONTROLS..

INERTIA LOADS X

ACEL.

0.0000 PRINT OUTPUT CONTROLS.

DATABASE OUTPUT CONTROLS..

10 10.000 ON 10 10 2

15 NO

..YES (EXIT)

USE DEFAULTS Y

Z 0.100OOE-01 0.0000

..NO PRINTOUT ALL DATA WRITTEN FOR THE LAST SUBSTEP NONLINEAR MONITORING INFO IS WRITTEN TO FILE= PADNC-TH.mntr MAXIMUM NUMBER OF EQUILIBRIUM ITERATIONS HAS BEEN MODIFIED TO BE, NEQIT = 26, BY SOLUTION CONTROL LOGIC.

FORCE CONVERGENCE VALUE

0.2253E+06 CRITERION

2120.

EQUIL ITER 1 COMPLETED.

NEW TRIANG MATRIX.

MAX DOF INC= -0.5465E-02 LINE SEARCH PARAMETER =

0.4122 SCALED MAX DOF INC = -0.2253E-02 FORCE CONVERGENCE VALUE

0.2073E+06 CRITERION

1943.

EQUIL ITER 2 COMPLETED.

NEW TRIANG MATRIX.

MAX DOF INC= -0.2774E-02 LINE SEARCH PARAMETER =

0.9728 SCALED MAX DOF INC = -0.2699E-02

Sheet 37 of 64 F0 Ia ENERCON Fp SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 FORCE CONVERGENCE VALUE EQUIL ITER 3 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 4 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE

0.5378E+05 CRITERION

1934.

NEW TRIANG MATRIX.

MAX DOF INC= -0.7450E-04 1.000 SCALED MAX DOF INC = -0.7450E-04

=

2300.

CRITERION=

1972.

NEW TRIANG MATRIX.

MAX DOF INC=

0.2536E-04 1.000 SCALED MAX DOF INC =

0.2536E-04

=

787.7 CRITERION=

2012.

<<< CONVEI.RGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 4

• • • LOAD STEP 10 SUBSTEP 1 COMPLETED.

CUM ITER =

TIME =

9.10000 TIME INC =

0.100000

• • • AUTO STEP TIME:

NEXT TIME INC = 0.10000 UNCHANGED 129 FORCE CONVERGENCE VALUE EQUIL ITER 1 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 2 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 3 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 4 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 5 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 6 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE

0.3166E+08 CRITERION

2134.

NEW TRIANG MATRIX.

MAX DOF INC=

0. 1173E-02 1.000 SCALED MAX DOF

0.1385E+06 CRITERION

NEW TRIANG MATRIX.

MAX 0.9298 SCALED MAX DOF 0.2783E+06 CRITERION=

NEW TRIANG MATRIX.

MAX 0.5333 SCALED MAX DOF

0.1771E+06 CRITERION

NEW TRIANG MATRIX. MAX 0.9954 SCALED MAX DOF

0.2250E+05 CRITERION

NEW TRIANG MATRIX.

MAX 1.000 SCALED MAX DOF

=

2999.

CRITERION=

NEW TRIANG MATRIX.

MAX INC =

0.1173E-02 1973.

DOF INC=

0.7425E-03 INC =

0.6903E-03 2013.

DOF INC=

0.6375E-03 INC =

0.3400E-03 2054.

DOF INC=

0.6465E-03 INC =

0.6436E-03 2095.

DOF INC= -0.4733E-04 INC = -0.4733E-04 2138.

DOF INC=

0.2311E-04

1. 000

=

1436.

SCALED MAX DOF INC =

CRITERION=

2182.

0. 2311E-04

<<< CONVERGED 135

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 6

• • • LOAD STEP 10 SUBSTEP 2 COMPLETED.

CUM ITER =

TIME =

9.20000 TIME INC =

0.100000

• • • AUTO STEP TIME:

NEXT TIME INC = 0.10000 UNCHANGED FORCE CONVERGENCE VALUE EQUIL ITER 1 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 2 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 3 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 4 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 5 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 6 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 7 COMPLETED.

LINE SEARCH PARAMETER =

0.3472E+08 CRITERION

2194.

NEW TRIANG MATRIX. MAX DOF INC=

0.1883E-02 1.000 SCALED MAX DOF INC =

0.1883E-02

0.7523E+05 CRITERION

2056.

NEW TRIANG MATRIX.

MAX DOF INC=

0.3608E-03 1.000 SCALED MAX DOF INC =

0.3608E-03

0.1614E+06 CRITERION

2097.

NEW TRIANG MATRIX.

MAX DOF INC=

0.5888E-03 0.9757 SCALED MAX DOF INC =

0.5744E-03

0.7101E+05 CRITERION

2140.

NEW TRIANG MATRIX.

MAX DOF INC=

0.2474E-03 1.000 SCALED MAX DOF INC =

0.2474E-03

0.2848E+05 CRITERION

2183.

NEW TRIANG MATRIX.

MAX DOF INC=

0.2555E-03 1.000 SCALED MAX DOF INC =

0.2555E-03

=

3286.

CRITERION=

2228.

NEW TRIANG MATRIX.

MAX DOF INC=

0.2899E-04 1.000 SCALED MAX DOF INC =

0.2899E-04

=

4628.

CRITERION=

2273.

NEW TRIANG MATRIX.

MAX DOF INC=

0.2636E-04 1.000 SCALED MAX DOF INC =

0.2636E-04

Sheet 38 of 64 ENERCON F SERVICES, IINC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 FORCE CONVERGENCE VALUE =

2624.

CRITERION=

2320.

EQUIL ITER 8 COMPLETED.

NEW TRIANG MATRIX.

MAX DOF INC=

0.4192E-03 LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC =

0.4192E-03 FORCE CONVERGENCE VALUE

=

760.8 CRITERION=

2367.

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 8

LOAD STEP 10 SUBSTEP 3 COMPLETED.

CUM ITER =

143 TIME =

9.30000 TIME INC =

0.100000 AUTO STEP TIME:

NEXT TIME INC = 0.10000 UNCHANGED FORCE CONVERGENCE VALUE EQUIL ITER 1 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 2 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 3 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 4 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 5 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE

0.3647E+05 CRITERION

2261.

NEW TRIANG MATRIX.

MAX DOF INC=

0.9697E-03 0.5317 SCALED MAX DOE

0.5889E+05 CRITERION

NEW TRIANG MATRIX.

MAX 1.000 SCALED MAX DOE

0.1321E+05 CRITERION

NEW TRIANG MATRIX.

MAX I INC =

0.5156E-03 2142.

DOF INC=

0.4404E-03 I INC =

0.4404E-03 2185.

DOF INC=

0.1018E-03 1.000

=

5524.

NEW TRIANC 1.000

=

6326.

NEW TRIANC 1.000

=

775.5 SCALED MAX DOF INC =

0.1018E-03 CRITERION=

2230.

MATRIX.

MAX DOF INC=

0.9431E-SCALED MAX DOF INC =

0.9431E-03 CRITERION=

2275.

MATRIX.

MAX DOF INC=

0.1373E-SCALED MAX DOF INC =

0.1373E-03 CRITERION=

2322.

<<< CON 303 03 VERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 5

LOAD STEP 10 SUBSTEP 4

COMPLETED.

CUM ITER =

TIME =

9.40000 TIME INC =

0.100000

• • • AUTO TIME STEP:

NEXT TIME INC = 0.15000 INCREASED (E 148 FACTOR = 1.5000)

FORCE CONVERGENCE VALUE EQUIL ITER 1 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 2 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 3 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 4 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 5 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE EQUIL ITER 6 COMPLETED.

LINE SEARCH PARAMETER =

FORCE CONVERGENCE VALUE

0.1762E+07 CRITERION

2645.

NEW TRIANG MATRIX.

MAX DOF INC=

0.3878E-03 1.000 SCALED MAX DOF INC =

0.3878E-03

0.4627E+05 CRITERION

NEW TRIANG MATRIX.

MAX 1.000 SCALED MAX DOE

0.1563E+05 CRITERION

NEW TRIANG MATRIX.

MAX 1.000 SCALED MAX DOE

=

9545.

CRITERION=

NEW TRIANG MATRIX.

MAX 1.000 SCALED MAX DOE

=

5850.

CRITERION=

NEW TRIANG MATRIX.

MAX 0.8500 SCALED MAX DOE

0.3980E+05 CRITERION

NEW TRIANG MATRIX.

MAX 1.000 SCALED MAX DOE

0.8449 CRITERION

2276.

DOF INC=

0.2048E-03 INC =

0.2048E-03 2322.

DOF INC=

0.2138E-03 INC =

0.2138E-03 2370.

DOF INC=

0.2450E-03 INC =

0.2450E-03 2418.

DOF INC=

0.4238E-02 INC =

0.3602E-02 2466.

DOF INC=

0.6087E-03 INC =

0.6087E-03 2516.

<<< CONVEi PRGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 6

LOAD STEP 10 SUBSTEP 5

COMPLETED.

CUM ITER =

TIME =

9.55000 TIME INC =

0.150000

• • • AUTO TIME STEP:

NEXT TIME INC = 0.22500 INCREASED (1 154 FACTOR = 1.5000)

FORCE CONVERGENCE VALUE EQUIL ITER 1 COMPLETED.

LINE SEARCH PARAMETER =

0.9352E+06 CRITERION

3335.

NEW TRIANG MATRIX.

MAX DOF INC=

0.8597E-03 1.000 SCALED MAX DOF INC =

0.8597E-03

F<X; Sheet 39 of 64 S.

1 ENERCON Ir SERVICES, INC.

Appendix RPadNC-TH to Calculat:ion PGE-009-CALC-006 FORCE CONVERGENCE VALUE

0.5184E+05 CRITERION

2479.

EQUIL ITER 2 COMPLETED.

NEW TRIANG MATRIX.

MAX DOF INC=

0.2880E-02 LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC =

0.2880E-02 FORCE CONVERGENCE VALUE =

32.89 CRITERION=

2528.

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2

LOAD STEP 10 SUBSTEP 6

COMPLETED.

CUM ITER 156

• • • TIME =

9.77500 TIME INC =

0.225000 AUTO STEP TIME:

NEXT TIME INC = 0.22500 UNCHANGED FORCE CONVERGENCE VALUE

0.1088E+05 CRITERION

3458.

EQUIL ITER 1 COMPLETED.

NEW TRIANG MATRIX.

MAX DOF INC=

0.7359E-03 LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC =

0.7359E-03 FORCE CONVERGENCE VALUE

=

9.771 CRITERION=

2687.

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

LOAD STEP 10 SUBSTEP 7

COMPLETED.

CUM ITER =

157 TIME =

10.0000 TIME INC =

0.225000 ESEL FOR LABEL= TYPE FROM 2 TO 2 BY 1

1870 ELEMENTS (OF 8812 DEFINED) SELECTED BY ESEL COMMAND.

SET MATERIAL OF SELECTED ELEMENTS TO 12 8812 ELEMENTS (OF 8812 DEFINED) SELECTED BY EALL COMMAND.

LIST ALL SELECTED ELEMENTS IN RANGE 1

530 TO 530 STEP 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 15:02:51 JAN 03, 2003 CP=

2522.627 DELTA T 4.125 TO 6.125 DAYS -

NO PAD/ROCK CONSTRAINT ELEM MAT TYP REL ESY SEC TSHA NODES 530 12 2

1 0

1 ANSYS RELEASE 6.1 UP20020321 1

28 29 3

672 1050 1064 728 13:34:26 01/03/2003 PRINTOUT RESUMED BY /GOP Load step file number 11.

Begin solution...

ANSYS SOLVE COMMAND NOTE ***

CP=

2523.809 TIME= 15:02:52 Present time 0 is less than or equal to the previous time.

Time will default to 11.

• • • NOTE ***

CP=

2523.819 TIME= 15:02:52 Nonlinear analysis, NROPT set to the FULL Newton-Raphson solution procedure for ALL DOFs.

1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U

>;-.' ~Sheet 40 of 64 FN 7

ENERCON

)+

SERVICES, INC. Appendix RPaNC-TH toCalculation PGE-009-CALC-006 00245050 VERSION=INTEL NT 15:02:53 JAN 03, 2003 CP=

2524.160 DELTA T 6.125 TO 7.875 DAYS -

NO PAD/ROCK CONSTRAINT 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.....

TERMINATE ANALYSIS IF NOT CONVERGED...

CONVERGENCE CONTROLS...........

INERTIA LOADS X

ACEL............

0.0000 PRINT OUTPUT CONTROLS..........

DATABASE OUTPUT CONTROLS.........

11

11. 000 ON 10 10 2

15 NO

...YES (EXIT)

...USE DEFAULTS Y

Z 0.10000E-01 0.0000

...NO PRINTOUT

...ALL DATA WRITTEN FOR THE LAST SUBSTEP NONLINEAR MONITORING INFO IS WRITTEN TO FILE= PADNC-TH.mntr MAXIMUM NUMBER OF EQUILIBRIUM ITERATIONS HAS BEEN MODIFIED TO BE, NEQIT = 26, BY SOLUTION CONTROL LOGIC.

FORCE CONVERGENCE VALUE

= 0.2269E+06 CRITERION= 2952.

EQUIL ITER 1 COMPLETED.

NEW TRIANG MATRIX.

MAX DOF INC=

0.1480E-02 LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC =

0.1480E-02 FORCE CONVERGENCE VALUE

=

65.01 CRITERION= 2632.

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

LOAD STEP 11 SUBSTEP 1

COMPLETED.

CUM ITER =

158

• • • TIME =

10.1000 TIME INC =

0.100000

• • • AUTO STEP TIME:

NEXT TIME INC = 0.10000 UNCHANGED FORCE CONVERGENCE VALUE =

367.4 CRITERION= 2931.

EQUIL ITER 1 COMPLETED.

NEW TRIANG MATRIX.

MAX DOF INC= -0.3646E-03 LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC = -0.3646E-03 FORCE CONVERGENCE VALUE =

3.477 CRITERION= 2495.

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

LOAD STEP 11 SUBSTEP 2

COMPLETED.

CUM ITER =

159

• • • TIME =

10.2000 TIME INC =

0.100000

• • • AUTO TIME STEP:

NEXT TIME INC = 0.15000 INCREASED (FACTOR = 1.5000)

FORCE CONVERGENCE VALUE

=

76.33 CRITERION=

3146.

EQUIL ITER 1 COMPLETED.

NEW TRIANG MATRIX. MAX DOF INC=

LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC =

(

FORCE CONVERGENCE VALUE

0.7697E-04 CRITERION

2290.

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

• • • LOAD STEP 11 SUBSTEP 3

COMPLETED.

CUM ITER =

TIME =

10.3500 TIME INC =

0.150000 AUTO TIME STEP:

NEXT TIME INC = 0.22500 INCREASED (FM 0.9980E-07 0.9980E-07

<<< CONVERGED 160

'CTOR = 1.5000)

FORCE CONVERGENCE VALUE =

22.86 CRITERION=

3633.

EQUIL ITER 1 COMPLETED.

NEW TRIANG MATRIX.

MAX DOF INC= -0.2672E-07

Sheet 41 of 64 F

~

ENERCON Ft n SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC = -

FORCE CONVERGENCE VALUE

0.8341E-04 CRITERION

1987.

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

• • • LOAD STEP 11 SUBSTEP 4

COMPLETED.

CUM ITER =

TIME =

10.5750 TIME INC =

0.225000

• • • AUTO TIME STEP:

NEXT TIME INC = 0.21250 DECREASED (]

-0.2672E-07

<<< CONVERGED 161 FACTOR = 0.9444)

FORCE CONVERGENCE VALUE

=

30.93 CRITERION=

3316.

EQUIL ITER 1 COMPLETED.

NEW TRIANG MATRIX.

MAX DOF INC= -0.3408E-07 LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF INC = -0.3408E-07 FORCE CONVERGENCE VALUE

0.3075E-04 CRITERION

1706.

<<< CONVERGED

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1

• • • LOAD STEP 11 SUBSTEP 5 COMPLETED.

CUM ITER =

162

• • • TIME =

10.7875 TIME INC =

0.212500

• • • AUTO STEP TIME:

NEXT TIME INC = 0.21250 UNCHANGED FORCE CONVERGENCE VALUE

=

30.05 CRITERION=

EQUIL ITER 1 COMPLETED.

NEW TRIANG MATRIX.

MAX I LINE SEARCH PARAMETER =

1.000 SCALED MAX DOF FORCE CONVERGENCE VALUE

0.2932E-04 CRITERION

>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION LOAD STEP 11 SUBSTEP 6

COMPLETED.

CUM

• • • TIME =

11.0000 TIME INC =

0.212500 3143.

DOF INC= -0.3311E-07 INC = -0.3311E-07 1435.

<<< CONVERGED 1

ITER =

163 ESEL FOR LABEL= TYPE FROM 1870 ELEMENTS (OF 2 TO 2 BY 1

8812 DEFINED) SELECTED BY ESEL COMMAND.

SET MATERIAL OF SELECTED ELEMENTS TO 2

8812 ELEMENTS (OF 8812 DEE LIST ALL SELECTED ELEMENTS IN RANGE

'INED) SELECTED BY EALL COMMAND.

530 TO 530 STEP 1

1

• • • • • ANSYS -

ENGINEER-NG ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=IN7EL NT 15:07:44 JAN 03, 2003 CP=

2642.089 DELTA T 6.125 TO 7.875 DAYS -

NO PAD/ROCK CONSTRAINT ELEM MAT TYP REL ESY SEC TSHA NODES 530 2

2 1

0 1

1 28 29 3

672 1050 1064 728 FINISH SOLUTION PROCESSING

• • • • • ROUTINE COMPLETED *****

CP =

2642.089 ALL CURRENT ANSYS DATA WRITTEN TO FILE NAME= PADNC-TH.db FOR POSSIBLE RESUME FROM THIS POINT 1

Sheet 42 of 64 ENERCON F

SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 15:07:50 JAN 03, 2003 CP=

2642.650 DELTA T 6.125 TO 7.875 DAYS -

NO PAD/ROCK CONSTRAINT

• • • • • ANSYS RESULTS INTERPRETATION (POSTI)

• WARNING ***

CP=

2642.650 TIME= 15:07:50 The current solution may have been produced using different model or boundary condition data than is currently stored.

POSTl results may be erroneous unless you perform a new solution using the stored data.

• • • NOTE ***

CP=

2642.650 TIME= 15:07:51 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).

PRINT HEADER DO NOT PRINT SUBTITLE(S)

DO NOT PRINT LOAD STEP ID DO NOT PRINT NOTE LINE(S)

PRINT COLUMN HEADER LABELS DO NOT PRINT REPORT TOTALS SUM RESULTS, SET TITLES AND WRITE LOAD CASE FILES FOR FURTHER PROCESSING COMBINE ALL RECORDS INCLUDING NON-SUMMABLE LOAD CASE 1 IS LOAD STEP 1

SUBSTEP 6

COMPLEX=

FILE= PADNC-TH.rst DELTA T 0.0 TO 0.25 DAYS -

NO PAD/ROCK CONSTRAINT 0

LOAD CASE 2 IS LOAD STEP 2 SUBSTEP 7 COMPLEX=

FILE= PADNC-TH.rst DELTA T 0.25 TO 0.50 DAYS -

NO PAD/ROCK CONSTRAINT 0

LOAD CASE 3 IS LOAD STEP 3

SUBSTEP 6

COMPLEX=

0 FILE= PADNC-TH.rst DELTA T 0.50 TO 0.625 DAYS -

NO PAD/ROCK CONSTRAINT LOAD CASE 4 IS LOAD STEP 4

SUBSTEP 6

COMPLEX=

FILE= PADNC-TH.rst DELTA T 0.625 TO 1.125 DAYS -

NO PAD/ROCK CONSTRAINT 0

LOAD CASE 5 IS LOAD STEP 5 SUBSTEP 6 COMPLEX=

FILE= PADNC-TH.rst DELTA T 1.125 TO 1.625 DAYS -

NO PAD/ROCK CONSTRAINT 0

Sheet 43 of 64 F.

C eENERCON E< r SERVICES, 'NC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 LOAD CASE 6 IS LOAD STEP FILE= PADNC-TH.rst DELTA T 1.625 TO 2.125 DAYS 6 SUBSTEP 6 COMPLEX=

0 NO PAD/ROCK CONSTRAINT LOAD CASE 7 IS LOAD STEP FILE= PADNC-TH.rst DELTA T 2.125 TO 2.375 DAYS 7 SUBSTEP 6 COMPLEX=

NO PAD/ROCK CONSTRAINT 0

LOAD CASE 8 IS LOAD STEP FILE= PADNC-TH.rst DELTA T 2.375 TO 3.125 DAYS 8 SUBSTEP 6 COMPLEX= 0 NO PAD/ROCK CONSTRAINT LOAD CASE 9 IS LOAD STEP FILE= PADNC-TH.rst DELTA T 3.125 TO 4.125 DAYS 9 SUBSTEP 6 COMPLEX=

0 NO PAD/ROCK CONSTRAINT LOAD CASE 10 IS LOAD STEP FILE= PADNC-TH.rst DELTA T 4.125 TO 6.125 DAYS 10 SUBSTEP 7 COMPLEX=

0 NO PAD/ROCK CONSTRAINT LOAD CASE 11 IS LOAD STEP FILE= PADNC-TH.rst DELTA T 6.125 TO 7.875 DAYS 11 SUBSTEP 6 COMPLEX= 0 NO PAD/ROCK CONSTRAINT COPY LOAD CASE 1 FROM FILE TO DATABASE

• • • WARNING ***

CP=

2642.680 TIME= 15:07:52 Cumulative iteration 6 may have been solved using different model or boundary condition data than currently stored.

POSTI results may be erroneous unless you RESUME from a Jobname.DB file for this substep.

TITLE=

PAD RESPONSE AT END OF 0.25 DAYS -

NO PAD/ROCK CONSTRAINT WRITE LOAD CASE 1 TO FILE PADNC-TH.101 WARNING ***

CP=

2643.621 TIME= 15:08:00 Cumulative iteration 42 may have been solved using different model or boundary condition data than currently stored.

POST1 results may be erroneous unless you RESUME from a Jobname.DB file for this substep.

LCOPER OPERATION ADD USING LOAD CASE=

2 FACTOR=

1.0000 ABS=

0 NOTE ***

CP=

2644.202 TIME= 15:08:05 Load case combination data may not be correct unless viewed in the solution phase coordinate system (RSYS-SOLU).

TITLE=

Sheet 44 of 64 F; -'

ENERCON HI SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 PAD RESPONSE AT END OF 0.50 DAYS -

NO PAD/ROCK CONSTRAINT WRITE LOAD CASE 2 TO FILE PADNC-TH.102

• • • WARNING ***

CP=

2644.513 TIME= 15:08:06 Cumulative iteration 60 may have been solved using different model or boundary condition data than currently stored.

POSTi results may be erroneous unless you RESUME from a Jobname.DB file for this substep.

LCOPER OPERATION ADD USING LOAD CASE=

3 FACTOR=

1.0000 ABS=

0 TITLE=

PAD RESPONSE AT END OF 0.625 DAYS - NO PAD/ROCK CONSTRAINT WRITE LOAD CASE 3 TO FILE PADNC-TH.103

• • • WARNING ***

CP=

2645.364 TIME= 15:08:09 Cumulative iteration 79 may have been solved using different model or boundary condition data than currently stored.

POSTl results may be erroneous unless you RESUME from a Jobname.DB file for this substep.

LCOPER OPERATION ADD USING LOAD CASE=

4 FACTOR=

1.0000 ABS=

0 TITLE=

PAD RESPONSE AT END OF 1.125 DAYS - NO PAD/ROCK CONSTRAINT WRITE LOAD CASE 4 TO FILE PADNC-TH.104

• • • WARNING ***

CP=

2646.285 TIME= 15:08:14 Cumulative iteration 85 may have been solved using different model or boundary condition data than currently stored.

POSTl results may be erroneous unless you RESUME from a Jobname.DB file for this substep.

LCOPER OPERATION ADD USING LOAD CASE=

5 FACTOR= 1.0000 ABS=

0 TITLE=

PAD RESPONSE AT END OF 1.625 DAYS - NO PAD/ROCK CONSTRAINT WRITE LOAD CASE 5 TO FILE PADNC-TH.105

• • • WARNING ***

CP=

2647.227 TIME= 15:08:20 Cumulative iteration 91 may have been solved using different model or boundary condition data than currently stored.

POSTl results may be erroneous unless you RESUME from a Jobname.DB file for this substep.

LCOPER OPERATION ADD USING LOAD CASE=

6 FACTOR=

1.0000 ABS=

0 TITLE=

PAD RESPONSE AT END OF 2.125 DAYS -

NO PAD/ROCK CONSTRAINT WRITE LOAD CASE 6 TO FILE PADNC-TH.106

Sheet 45 of 64 ENERCON F l SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 WARNING ***

CP=

2648.008 TIME= 15:08:22 Cumulative iteration 102 may have been solved using different model or boundary condition data than currently stored.

POSTI results may be erroneous unless you RESUME from a Jobname.DB file for this substep.

LCOPER OPERATION ADD USING LOAD CASE=

7 FACTOR=

1.0000 ABS=

0 TITLE=

PAD RESPONSE AT END OF 2.375 DAYS -

NO PAD/ROCK CONSTRAINT WRITE LOAD CASE 7 TO FILE PADNC-TH.107

• • • WARNING ***

CP=

2648.709 TIME= 15:08:25 Cumulative iteration 109 may have been solved using different model or boundary condition data than currently stored.

POSTI results may be erroneous unless you RESUME from a Jobname.DB file for this substep.

LCOPER OPERATION ADD USING LOAD CASE=

8 FACTOR= 1.0000 ABS=

0 TITLE=

PAD RESPONSE AT END OF 3.125 DAYS -

NO PAD/ROCK CONSTRAINT WRITE LOAD CASE 8 TO FILE PADNC-TH.108

• • • WARNING ***

CP=

2649.470 TIME= 15:08:28 Cumulative iteration 125 may have been solved using different model or boundary condition data than currently stored.

POSTl results may be erroneous unless you RESUME from a Jobname.DB file for this substep.

LCOPER OPERATION ADD USING LOAD CASE=

9 FACTOR= 1.0000 ABS=

0 TITLE=

PAD RESPONSE AT END OF 4.125 DAYS -

NO PAD/ROCK CONSTRAINT WRITE LOAD CASE 9 TO FILE PADNC-TH.109

• • • WARNING ***

CP=

2650.221 TIME= 15:08:31 Cumulative iteration 157 may have been solved using different model or boundary condition data than currently stored.

POSTI results may be erroneous unless you RESUME from a Jobname.DB file for this substep.

LCOPER OPERATION ADD USING LOAD CASE=

10 FACTOR=

1.0000 ABS=

0 TITLE=

PAD RESPONSE AT END OF 6.125 DAYS -

NO PAD/ROCK CONSTRAINT WRITE LOAD CASE 10 TO FILE PADNC-TH.110

• • • WARNING ***

CP=

2650.962 TIME= 15:08:34 Cumulative iteration 163 may have been solved using different model or boundary condition data than currently stored.

POSTl results may be erroneous unless you RESUME from a Jobname.DB file for this substep.

,,;Sheet 46 of 64 F* -

ENERCON SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 LCOPER OPERATION ADD USING LOAD CASE=

11 FACTOR=

1.0000 ABS=

0 TITLE=

PAD RESPONSE AT END OF 7.875 DAYS -

NO PAD/ROCK CONSTRAINT WRITE LOAD CASE 11 TO FILE PADNC-TH.111 EXIT THE ANSYS POSTI DATABASE PROCESSOR

• • • • • ROUTINE COMPLETED *****

CP =

2651.783 print the temperatures for checking 8812 ELEMENTS (OF 8812 DEFINED) SELECTED BY EALL COMMAND.

10212 NODES (OF 10212 DEFINED) SELECTED BY NALL COMMAND.

1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 15:08:37 JAN 03, 2003 CP=

PAD RESPONSE AT END OF 7.875 DAYS - NO PAD/ROCK CONSTRAINT 2651.783

• • • • • ANSYS RESULTS INTERPRETATION (POST1) *****

WARNING ***

CP=

2651.783 TIME= 15:08:38 The current solution may have been produced using different model or boundary condition data than is currently stored.

POSTi results may be erroneous unless you perform a new solution using the stored data.

PRINT HEADER DO NOT PRINT SUBTITLE(S)

DO NOT PRINT LOAD STEP ID DO NOT PRINT NOTE LINE(S)

PRINT COLUMN HEADER LABELS DO NOT PRINT REPORT TOTALS SELECT FOR ITEM=LOC COMPONENT=X KABS=

0.

TOLERANCE= 0.100000E-05 626 NODES (OF 10212 DEFINED)

RESELECT FOR ITEM=LOC COMPONENT=Z KABS=

0. TOLERANCE= 0.100000E-05 26 NODES (OF 10212 DEFINED)

RESELECT FOR ITEM=LOC COMPONENT=Y KABS=

0.

TOLERANCE= 0.145000E-05 18 NODES (OF 10212 DEFINED)

BETWEEN 0.0000 AND 0.0000 SELECTED BY BETWEEN SELECTED BY BETWEEN NSEL COMMAND.

0.0000 AND 0.0000 NSEL COMMAND.

-145.00 AND 0.0000 SELECTED BY NSEL COMMAND.

F.., 2-;-.

Sheet 47 of 64 0:

ENERCON F

JSERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 LIST ALL SELECTED NODES.

1 DSYS=

0

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 15:08:38 JAN 03, 2003 CP=

PAD RESPONSE AT END OF 7.875 DAYS -

NO PAD/ROCK CONSTRAINT 2651.793 NODE 1

16 26 27 28 61 71 72 73 74 113 123 133 146 156 169 179 180 X

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 0.0000 0.0000 0.0000

0. 0000 0.0000 Y

0.0000

-24.000

-18.000

-12. 000

-6. 0000

-84.000

-72.000

-60.000

-48.000

-36.000

-96. 000

-90.000

-96.000

-108.00

-102.00

-144. 00

-132.00

-120.00 z

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 0.0000 0.0000 0.0000 0.0000

0. 0000 THXY 0. 0 0 0.00 0.00 0.00 0.00 0. 0 0 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 THYZ 0.00 0.00 0. 00 0. 00 0.00 0. 0 0 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 THZX 0.00 0.00 0.00 0.00 0.00 0. 00 0.00 0.00 0.00 0.00 0.00 0. 0 0 0.00 0. 0 0 0. 0 0 0.00

0. 0 0 0.00 USE LOAD STEP 1

SUBSTEP 0

FOR LOAD CASE 0

• • • WARNING ***

Cumulative iteration CP=

2651.793 TIME= 15:08:39 6 may have been solved using different model or boundary condition data than currently stored.

POST1 results may be erroneous unless you RESUME from a Jobname.DB file for this substep.

SET COMMAND GOT LOAD STEP=

1 SUBSTEP=

6 CUMULATIVE ITERATION=

TIME/FREQUENCY= 1.0000 TITLE= DELTA T 0.0 TO 0.25 DAYS -

NO PAD/ROCK CONSTRAINT 6

SORT ON ITEM=LOC COMPONENT=Y ORDER= 0 KABS= 0 NMAX=

10212 SORT COMPLETED FOR 18 VALUES.

PRINT BFE NODAL SOLUTION PER NODE 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 15:08:40 JAN 03, 2003 CP=

2652.394 DELTA T 0.0 TO 0.25 DAYS -

NO PAD/ROCK CONSTRAINT

Sheet 48 of 64 ENERCON F,

SERVICES,INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 NODE BFETEMP 1

15.000 28 18.000 27 19.670 26 21.330 16 21.330 74 21.330 73 21.330 72 21.330 71 21.330 61 20.500 123 19.660 113 10.670 133 10.670 156 1.6700 146 0.84000 180 0.0000 179 0.0000 169 0.0000 USE LOAD STEP 2

SUBSTEP 0

FOR LOAD CASE 0

• • • WARNING ***

CP=

2652.404 TIME= 15:08:40 Cumulative iteration 42 may have been solved using different model or boundary condition data than currently stored.

POSTl results may be erroneous unless you RESUME from a Jobname.DB file for this substep.

SET COMMAND GOT LOAD STEP=

2 SUBSTEP=

7 CUMULATIVE ITERATION=

42 TIME/FREQUENCY= 2.0000 TITLE= DELTA T 0.25 TO 0.50 DAYS -

NO PAD/ROCK CONSTRAINT SORT ON ITEM=LOC COMPONENT=Y ORDER= 0 KABS= 0 NMAX=

10212 SORT COMPLETED FOR 18 VALUES.

PRINT BFE NODAL SOLUTION PER NODE 1

ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 15:08:41 JAN 03, 2003 CP=

2652.935 DELTA T 0.25 TO 0.50 DAYS -

NO PAD/ROCK CONSTRAINT NODE BFETEMP 1

-2.5000 28 10.500 27 9.2500 26 8.0000 16 16.670 74 25.330 73 25.330 72 25.330 71 25.120 61 21.410

iF!:!-'I A-v:?f Sheet 49 of 64 ENERCON SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 123 17.920 113 12.660 133 12.660 156 7.4100 146 3.9100 180 0.21000 179 0.0000 169 0.0000 USE LOAD STEP 3

SUBSTEP 0

FOR LOAD CASE 0

• • • WARNING ***

CP=

2652.935 TIME= 15:08:41 Cumulative iteration 60 may have been solved using different model or boundary condition data than currently stored.

POSTI results may be erroneous unless you RESUME from a Jobname.DB file for this substep.

SET COMMAND GOT LOAD STEP=

3 SUBSTEP=

6 CUMULATIVE ITERATION=

TIME/FREQUENCY=

3.0000 TITLE= DELTA T 0.50 TO 0.625 DAYS -

NO PAD/ROCK CONSTRAINT 60 SORT ON ITEM=LOC COMPONENT=Y ORDER= 0 KABS= 0 NMAX=

10212 SORT COMPLETED FOR 18 VALUES.

PRINT BFE NODAL SOLUTION PER NODE I

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 15:08:42 JAN 03, 2003 CP=

2653.526 DELTA T 0.50 TO 0.625 DAYS -

NO PAD/ROCK CONSTRAINT NODE BFETEMP 1

-3.0000 28

-1.3500 27 9.3200 26 13.460 16 9.3300 74 9.3300 73 9.3300 72 9.3300 71 9.3300 61 9.3300 123 2.0400 113 4.6700 133 4.6700 156 7.3000 146 0.0000 180 0.0000 179 0.0000 169 0.0000 USE LOAD STEP 4

SUBSTEP 0

FOR LOAD CASE 0

Sheet 50 of 64 FI ]

ENERCON SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 WARNING ***

CP=

2653.526 TIME= 15:08:42 Cumulative iteration 79 may have been solved using different model or boundary condition data than currently stored.

POSTI results may be erroneous unless you RESUME from a Jobname.DB file for this substep.

SET COMMAND GOT LOAD STEP=

4 SUBSTEP=

6 CUMULATIVE ITERATION=

79 TIME/FREQUENCY=

4.0000 TITLE= DELTA T 0.625 TO 1.125 DAYS -

NO PAD/ROCK CONSTRAINT SORT ON ITEM=LOC COMPONENT=Y ORDER= 0 KABS= 0 NMAX=

10212 SORT COMPLETED FOR 18 VALUES.

PRINT BFE NODAL SOLUTION PER NODE 1

ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 15:08:42 JAN 03, 2003 CP=

2654.056 DELTA T 0.625 TO 1.125 DAYS -

NO PAD/ROCK CONSTRAINT NODE BFETEMP 1

-5.4000 28

-7.4400 27

-8.8100 26

-3.1000 16 2.6200 74 15.000 73 20.110 72 20.320 71 17.860 61 11.880 123 11.110 113 10.330 133 10.330 156 9.5500 146 8.7800 180 2.8100 179 0.35000 169 0.100OOE-01 USE LOAD STEP 5

SUBSTEP 0

FOR LOAD CASE 0 WARNING ***

CP=

2654.056 TIME= 15:08:42 Cumulative iteration 85 may have been solved using different model or boundary condition data than currently stored.

POSTI results may be erroneous unless you RESUME from a Jobname.DB file for this substep.

SET COMMAND GOT LOAD STEP=

5 SUBSTEP=

6 CUMULATIVE ITERATION=

85 TIME/FREQUENCY'=

5.0000 TITLE= DELTA T 1.125 TO 1.625 DAYS -

NO PAD/ROCK CONSTRAINT SORT ON ITEM=LOC COMPONENT=Y ORDER= 0 KABS= 0 NMAX=

10212

Sheet 51 of 64 F

'~ENERCON lJ SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 SORT COMPLETED FOR 18 VALUES.

PRINT BFE NODAL SOLUTION PER NODE 1

ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 15:08:43 JAN 03, 2003 CP=

2654.587 DELTA T 1.125 TO 1.625 DAYS -

NO PAD/ROCK CONSTRAINT NODE BFETEMP 1 -2.1000 28

-5.5000 27

-6.4600 26

-4.7300 16

-3.0000 74 2.2500 73 7.3200 72 8.4500 71 6.3200 61 3.7400 123 4.4500 113 5.1600 133 5.1600 156 5.8800 146 6.6000 180 3.9800 179 1.3800 169 0.25000 USE LOAD STEP 6

SUBSTEP 0

FOR LOAD CASE 0

• • • WARNING ***

CP=

2654.597 TIME= 15:08:43 Cumulative iteration 91 may have been solved using different model or boundary condition data than currently stored.

POSTi results may be erroneous unless you RESUME from a Jobname.DB file for this substep.

SET COMMAND GOT LOAD STEP=

6 SUBSTEP=

6 CUMULATIVE ITERATION=

91 TIME/FREQUENCY=

6.0000 TITLE= DELTA T 1.625 TO 2.125 DAYS -

NO PAD/ROCK CONSTRAINT SORT ON ITEM=LOC COMPONENT=Y ORDER= 0 KABS= 0 NMAX=

10212 SORT COMPLETED FOR 18 VALUES.

PRINT BFE NODAL SOLUTION PER NODE 1

ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 15:08:43 JAN 03, 2003 CP=

2655.138 DELTA T 1.625 TO 2.125 DAYS -

NO PAD/ROCK CONSTRAINT

Sheet 52 of 64 ENERCON F 3 SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 NODE 1

28 27 26 16 74 73 72 71 61 123 113 133 156 146 180 179 169 BFETEMP

-0.80000

-3.0600

-4.0600

-3.9600

-3.8700

-2.2200 0.96000 2.2900 1.5300 0.91000 1.8700 2.8300 2.8300 3.7800 4.7200 3.8200 1.9800 0.53000 USE LOAD STEP 7

SUBSTEP 0

FOR LOAD CASE 0

• • • WARNING ***

Cumulative iteration 102 may boundary condition data than erroneous unless you RESUME CP=

2655.138 TIME= 15:08:43 have been solved using different model or currently stored.

POSTI results may be from a Jobname.DB file for this substep.

SET COMMAND GOT LOAD STEP=

TIME/FREQUENCY=

7.0000 7

SUBSTEP=

6 CUMULATIVE ITERATION=

102 TITLE= DELTA T 2.125 TO 2.375 DAYS -

NO PAD/ROCK CONSTRAINT SORT ON ITEM=LOC COMPONENT=Y ORDER= 0 KABS= 0 NMAX=

10212 SORT COMPLETED FOR 18 VALUES.

PRINT BFE NODAL SOLUTION PER NODE 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 15:08:44 JAN 03, 2003 CP=

2655.658 DELTA T 2.125 TO 2.375 DAYS -

NO PAD/ROCK CONSTRAINT NODE BFETEMP 1 -0.20000 28 -0.94000 27

-1.2800 26

-1.4700 16

-1.6500 74

-1.5100 73 -0.54000 72 0.80000E-01

, i '..' /-.

ISheet 53 of 64 F-Do ENERCON SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 71 61 123 113 133 156 146 180 179 169 0.90000E-01 0.20000 0.63000 1.0600 1.0600 1.4600 1.8600 1.7300

1. 0500 0.33000 USE LOAD STEP 8 SUBSTEP 0 FOR LOAD CASE 0 WARNING ***

Cumulative iteration 109 may boundary condition data than erroneous unless you RESUME CP=

2655.668 TIME= 15:08:44 have been solved using different model or currently stored. POSTl results may be from a Jobname.DB file for this substep.

SET COMMAND GOT LOAD STEP=

TIME/FREQUENCY=

8.0000 8 SUBSTEP=

6 CUMULATIVE ITERATION=

109 TITLE= DELTA T 2.375 TO 3.125 DAYS -

NO PAD/ROCK CONSTRAINT SORT ON ITEM=LOC COMPONENT=Y ORDER= 0 KABS= 0 NMAX=

10212 SORT COMPLETED FOR 18 VALUES.

PRINT BFE NODAL SOLUTION PER NODE I

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 15:08:45 JAN 03, 2003 CP=

2656.209 DELTA T 2.375 TO 3.125 DAYS -

NO PAD/ROCK CONSTRAINT NODE 1

28 27 26 16 74 73 72 71 61 123 113 133 156 146 180 179 169 BFETEMP

-0.50000

-2.1300

-3.0700

-3.9000

-4.7400

-5.6000

-4.2000

-2.7200

-1.8500

-0.66000 0.64000 1.9400 1.9400 3.1000 4.2600 4.3900 3.0000 1.0300

';-s Ad Sheet 54 of 64 ENERCON F

SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 USE LOAD STEP 9 SUBSTEP 0 FOR LOAD CASE 0 WARNING ***

CP=

2656.209 TIME= 15:08:45 Cumulative iteration 125 may have been solved using different model or boundary condition data than currently stored.

POSTi results may be erroneous unless you RESUME from a Jobname.DB file for this substep.

SET COMMAND GOT LOAD STEP=

9 SUBSTEP=

6 CUMULATIVE ITERATION=

TIME/FREQUENCY= 9.0000 TITLE= DELTA T 3.125 TO 4.125 DAYS - NO PAD/ROCK CONSTRAINT 125 SORT ON ITEM=LOC COMPONENT=Y ORDER= 0 KABS= 0 NMAX=

10212 SORT COMPLETED FOR 18 VALUES.

PRINT BFE NODAL SOLUTION PER NODE 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 15:08:45 JAN 03, 2003 CP=

2656.750 DELTA T 3.125 TO 4.125 DAYS -

NO PAD/ROCK CONSTRAINT NODE 1

28 27 26 16 74 73 72 71 61 123 113 133 156 146 180 179 169 BFETEMP

-0.30000

-2.0300

-3.1400

-4.4900

-5.8400

-8.3400

-8.3500

-7.1100

-5.3300

-2.9100

-1.1900 0.54000 0.54000 1.9800 3.4300 4.1800 3.1900 1.1800 USE LOAD STEP 10 SUBSTEP 0 FOR LOAD CASE 0

• • • WARNING ***

Cumulative iteration 157 may boundary condition data than erroneous unless you RESUME CP=

2656.750 TIME= 15:08:45 have been solved using different model or currently stored.

POSTl results may be from a Jobname.DB file for this substep.

SET COMMAND GOT LOAD STEP=

TIME/FREQUENCY=

10.000 10 SUBSTEP=

7 CUMULATIVE ITERATION=

157 TITLE= DELTA T 4.125 TO 6.125 DAYS - NO PAD/ROCK CONSTRAINT

F~

ENERCON SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 Sheet 55 of 64 SORT ON ITEM=LOC COMPONENT=Y SORT COMPLETED FOR 18 VALUES.

PRINT BFE NODAL SOLUTION PER NODE 1

ORDER= 0 KABS= 0 NMAX=

10212

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 15:08:46 JAN 03, 2003 CP=

DELTA T 4.125 TO 6.125 DAYS -

NO PAD/ROCK CONSTRAINT 2657.281 NODE 1

28 27 26 16 74 73 72 71 61 123 113 133 156 146 180 179 169 BFETEMP 0.0000

-1.3800

-2.6100

-4.7600

-6.9100

-11.780

-13.650

-12.770

-9.8200

-5.6000

-3.3600

-1.1200

-1.1200 0.66000 2.4300 4.0600 3.5200 1.3700 USE LOAD STEP 11 SUBSTEP 0 FOR LOAD CASE 0

• • • WARNING ***

CP=

2657.291 TIME= 15:08:46 Cumulative iteration 163 may have been solved using different model or boundary condition data than currently stored.

POSTl results may be erroneous unless you RESUME from a Jobname.DB file for this substep.

SET COMMAND GOT LOAD STEP=

11 SUBSTEP=

6 CUMULATIVE ITERATION=

163 TIME/FREQUENCY= 11.000 TITLE= DELTA T 6.125 TO 7.875 DAYS -

NO PAD/ROCK CONSTRAINT SORT ON ITEM=LOC COMPONENT=Y ORDER= 0 KABS= 0 NMAX=

10212 SORT COMPLETED FOR 18 VALUES.

PRINT BFE NODAL SOLUTION PER NODE 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 15:08:47 JAN 03, 2003 CP=

2657.822

F 3..

aI ENERCON SERVICES, INC.

Sheet 56 of 64 Appendix RPadNC-TH to Calculation PGE-009-CALC-006 DELTA T 6.125 TO 7.875 DAYS -

NO PAD/ROCK CONSTRAINT NODE 1

28 27 26 16 74 73 72 71 61 123 113 133 156 146 180 179 169 BFETEMP 0.0000

-0.69000

-1.3300

-2.5100

-3.6900

-6.5800

-8.1200

-8.1000

-6.7500

-4.5600

-3.3800

-2.2000

-2.2000

-1.2300

-0.25000 0.85000 1.0100 0.43000 COPY LOAD CASE 1 FROM FILE TO DATABASE SORT ON ITEM=LOC COMPONENT=Y ORDER= 0 KABS= 0 NMAX=

10212 SORT COMPLETED FOR 18 VALUES.

PRINT BFE NODAL SOLUTION PER NODE I

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 15:08:47 JAN 03, 2003 CP=

2658.473 PAD RESPONSE AT END OF 0.25 DAYS -

NO PAD/ROCK CONSTRAINT NODE BFETEMP 1

15.000 28 18.000 27 19.670 26 21.330 16 21.330 74 21.330 73 21.330 72 21.330 71 21.330 61 20.500 123 19.660 113 10.670 133 10.670 156 1.6700 146 0.84000 180 0.0000

1 Sheet 57 of 64 F

'~ENERCON

JSERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 179 0.0000 169 0.0000 COPY LOAD CASE 2 FROM FILE TO DATABASE SORT ON ITEM=LOC COMPONENT=Y ORDER= 0 KABS= 0 NMAX=

10212 SORT COMPLETED FOR 18 VALUES.

PRINT BFE NODAL SOLUTION PER NODE 1

ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 15:08:48 JAN 03, 2003 CP=

2659.144 PAD RESPONSE AT END OF 0.50 DAYS -

NO PAD/ROCK CONSTRAINT NODE BFETEMP 1

12.500 28 28.500 27 28.920 26 29.330 16 38.000 74 46.660 73 46.660 72 46.660 71 46.450 61 41.910 123 37.580 113 23.330 133 23.330 156 9.0800 146 4.7500 180 0.21000 179 0.0000 169 0.0000 COPY LOAD CASE 3 FROM FILE TO DATABASE SORT ON ITEM=LOC COMPONENT=Y ORDER= 0 KABS= 0 NMAX=

10212 SORT COMPLETED FOR 18 VALUES.

PRINT BFE NODAL SOLUTION PER NODE 1

ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 15:08:49 JAN 03, 2003 CP=

2659.794 PAD RESPONSE AT END OF 0.625 DAYS -

NO PAD/ROCK CONSTRAINT NODE BFETEMP 1

9.5000

F.3 28 27 26 16 74 73 72 71 61 123 113 133 156 146 180 179 169 Sheet 58 of 64 ENERCON SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 27.150 38.240 42.790 47.330 55.990 55.990 55.990 55.780 51.240 39.620 28.000 28.000 16.380 4.7500 0.21000 0.0000 0.0000 COPY LOAD CASE 4 FROM FILE TO DATABASE SORT ON ITEM=LOC COMPONENT=Y ORDER=

0 KABS= 0 NMAX=

10212 SORT COMPLETED FOR 18 VALUES.

PRINT BFE NODAL SOLUTION PER NODE 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 15:08:49 JAN 03, 2003 CP=

2660.456 PAD RESPONSE AT END OF 1.125 DAYS -

NO PAD/ROCK CONSTRAINT NODE BFETEMP 1

4.1000 28 19.710 27 29.430 26 39.690 16 49.950 74 70.990 73 76.100 72 76.310 71 73.640 61 63.120 123 50.730 113 38.330 133 38.330 156 25.930 146 13.530 180 3.0200 179 0.35000 169 0.100OOE-01 COPY LOAD CASE 5 FROM FILE TO DATABASE SORT ON ITEM=LOC COMPONENT=Y ORDER=

0 KABS= 0 NMAX=

10212

Sheet 59 of 64 F - TENERCON SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 SORT COMPLETED FOR 18 VALUES.

PRINT BFE NODAL SOLUTION PER NODE 1

ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 15:08:50 JAN 03, 2003 CP=

2661.107 PAD RESPONSE AT END OF 1.625 DAYS -

NO PAD/ROCK CONSTRAINT NODE BFETEMP 1

2.0000 28 14.210 27 22.970 26 34.960 16 46.950 74 73.240 73 83.420 72 84.760 71 79.960 61 66.860 123 55.180 113 43.490 133 43.490 156 31.810 146 20.130 180 7.0000 179 1.7300 169 0.26000 COPY LOAD CASE 6 FROM FILE TO DATABASE SORT ON ITEM=LOC COMPONENT=Y ORDER= 0 KABS= 0 NMAX=

10212 SORT COMPLETED FOR 18 VALUES.

PRINT BFE NODAL SOLUTION PER NODE 1

ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 15:08:51 JAN 03, 2003 CP=

2661.758 PAD RESPONSE AT END OF 2.125 DAYS -

NO PAD/ROCK CONSTRAINT NODE BFETEMP 1

1.2000 28 11.150 27 18.910 26 31.000 16 43.080 74 71.020 73 84.380

Sheet 6 F00-ENERCON S

E I

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 72 87.050 71 81.490 61 67.770 123 57.050 113 46.320 133 46.320 156 35.590 146 24.850 180 10.820 179 3.7100 169 0.79000 COPY LOAD CASE 7 FROM FILE TO DATABASE SORT ON ITEM=LOC COMPONENT=Y ORDER= 0 KABS= 0 NMAX=

10212 SORT COMPLETED FOR 18 VALUES.

PRINT BFE NODAL SOLUTION PER NODE 1

ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 15:08:51 JAN 03, 2003 CP=

2662.408 PAD RESPONSE AT END OF 2.375 DAYS -

NO PAD/ROCK CONSTRAINT NODE BFETEMP 1

1.0000 28 10.210 27 17.630 26 29.530 16 41.430 74 69.510 73 83.840 72 87.130 71 81.580 61 67.970 123 57.680 113 47.380 133 47.380 156 37.050 146 26.710 180 12.550 179 4.7600 169 1.1200 COPY LOAD CASE 8 FROM FILE TO DATABASE SORT ON ITEM=LOC COMPONENT=Y ORDER= 0 KABS= 0 NMAX=

10212 SORT COMPLETED FOR 18 VALUES.

PRINT BFE NODAL SOLUTION PER NODE 1

60 of 64

Sheet 61 of 64 F- -

ENERCON SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 15:08:52 JAN 03, 2003 CP=

2663.059 PAD RESPONSE AT END OF 3.125 DAYS -

NO PAD/ROCK CONSTRAINT NODE BFETEMP 1

0.50000 28 8.0800 27 14.560 26 25.630 16 36.690 74 63.910 73 79.640 72 84.410 71 79.730 61 67.310 123 58.320 113 49.320 133 49.320 156 40.150 146 30.970 180 16.940 179 7.7600 169 2.1500 COPY LOAD CASE 9 FROM FILE TO DATABASE SORT ON ITEM=LOC COMPONENT=Y ORDER= 0 KABS= 0 NMAX=

10212 SORT COMPLETED FOR 18 VALUES.

PRINT BFE NODAL SOLUTION PER NODE 1

ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 15:08:53 JAN 03, 2003 CP=

2663.720 PAD RESPONSE AT END OF 4.125 DAYS -

NO PAD/ROCK CONSTRAINT NODE BFETEMP 1

0.20000 28 6.0500 27 11.420 26 21.140 16 30.850 74 55.570 73 71.290 72 77.300 71 74.400 61 64.400 123 57.130 113 49.860 133 49.860

Sheet 62 of 64 ENERCON F

SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 156 42.130 146 34.400 180 21.120 179 10.950 169 3.3300 COPY LOAD CASE 10 FROM FILE TO DATABASE SORT ON ITEM=LOC COMPONENT=Y ORDER= 0 KABS= 0 NMAX=

10212 SORT COMPLETED FOR 18 VALUES.

PRINT BFE NODAL SOLUTION PER NODE 1

• • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U

00245050 VERSION=INTEL NT 15:08:53 JAN 03, 2003 CP=

2664.371 PAD RESPONSE AT END OF 6.125 DAYS -

NO PAD/ROCK CONSTRAINT NODE BFETEMP 1

0.20000 28 4.6700 27 8.8100 26 16.380 16 23.940 74 43.790 73 57.640 72 64.530 71 64.580 61 58.800 123 53.770 113 48.740 133 48.740 156 42.790 146 36.830 180 25.180 179 14.470 169 4.7000 COPY LOAD CASE 11 FROM FILE TO DATABASE SORT ON ITEM=LOC COMPONENT=Y ORDER= 0 KABS= 0 NMAX=

10212 SORT COMPLETED FOR 18 VALUES.

PRINT BFE NODAL SOLUTION PER NODE 1

ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 15:08:54 JAN 03, 2003 CP=

2665.022 PAD RESPONSE AT END OF 7.875 DAYS -

NO PAD/ROCK CONSTRAINT

FI F.,I Sheet 63 of 64 ENERCON SERVICES, INC.

Appendix RPadNC-TH to Calculation PGE-009-CALC-006 NODE BFETEMP 1

0.20000 28 3.9800 27 7.4800 26 13.870 16 20.250 74 37.210 73 49.520 72 56.430 71 57.830 61 54.240 123 50.390 113 46.540 133 46.540 156 41.560 146 36.580 180 26.030 179 15.480 169 5.1300 NODE SORT REMOVED EXIT THE ANSYS POSTi DATABASE PROCESSOR

• • • • • ROUTINE COMPLETED *****

CP =

2665.022 8812 ELEMENTS (OF 8812 DEFINED) SELECTED BY EALL COMMAND.

10212 NODES (OF 10212 DEFINED) SELECTED BY NALL COMMAND.

EXIT ANSYS WITHOUT SAVING DATABASE NUMBER OF WARNING MESSAGES ENCOUNTERED=

NUMBER OF ERROR MESSAGES ENCOUNTERED=

25 0

ANSYS RUN COMPLETED Release 6.1 UP20020321 INTEL NT ll Maximum Scratch Memory Used

=

5713800 Words 21.796 MB If CP Time (sec) =

2665.022 Time

=

15:08:54 l

Elapsed Time (sec) =

5591.000 Date = 01/03/2003

,: Ve 'Sheet 64 of 64 Fn n ENERCON t

SERVICES, INC.

Appendix R-PadNC-TH to Calculation PGE-009-CALC-006 I

Sheet 1 of 18 ENERCON SERVICES, INC.

Appendix EPadNC-TH to Calculation PGE-009-CALC-006 Originator:

S. C. u2n0inelli Date:

March 3, 2003 Appendix EPadNC-TH This Appendix presents the ANSYS output file documenting the equilibrium check for the unconstrained thermal stress analysis. Contains the ANSYS Input file, followed by manual calculations for expected forces, followed by the ANSYS Output File.

Sheet 2 of 18 F;

t ENERCON SERVICES, INC.

Appendix EPadNC-TH to Calcuiation PGE-009-CALC-006 ANSYS Input File:

/com,

/com, This routine processes load results data for the

/com, evaluation of equilibrium.

/com

/com, Load Case Results

/com

/com

/corm

/corm

/com

/com ****** Reactions *

/com

/filePadNC-Th resume

/header,on,on,on

/postl spoint,,0,0,0

/com

/corm

/com *****

LOAD CASE 1 *****

lcfile,1 lcase,1 eall cmsel,s,bot cmsel,a,symxy cmsel,a,symyz cmsel,a,xedge cmsel,a,zedge fsum

/com

/corm

/com *****

LOAD CASE 2 *****

lcfile,2 lcase,2 eall cmsel,s,bot cmsel,a,symxy cmsel,a,symyz cmsel,a,xedge cmsel,a,zedge fsum

/com

/corm

/com *****

LOAD CASE 3

• lcfile,3 lcase,3 eall cmsel,s,bot cmsel,a,symxy cmsel,a,symyz cmsel,a,xedge cmsel,a,zedge fsum

/com

/corm

ENERCON SERVICES, INC.

Appendix EPadNC-TH to Calculation PGE-009-CALC-006

/com *****

LOAD CASE 4 *****

lcfile,4 lcase,4 eall cmsel,s,bot cmsel,a,symxy cmsel,a,symyz cmsel,a,xedge cmsel,a,zedge fsum

/com

/com *

/com *****

LOAD CASE 5 *****

lcfile,5 lcase, 5 eall cmsel,s,bot cmsel,a,symxy cmsel,a,symyz cmsel,a,xedge cmsel,a,zedge fsum

/com

/comr

/com *****

LOAD CASE 6

• lcfile, 6 lcase, 6 eall cmsel,s,bot cmsel,a,symxy cmsel,a,symyz cmsel,a,xedge cmsel,a,zedge fsum

/com

/com ************************

/com *****

LOAD CASE 7 *****

lcfile,7 lcase,7 eall cmsel,s,bot cmsel,a,symxy cmsel,a,symyz cmsel,a,xedge cmsel,a,zedge fsum

/com

/comr

/com *****

LOAD CASE 8

• lcfile,8 lcase,8 eall cmsel,s,bot cmsel,a,synxy cmsel,a,symyz cmsel,a,xedge cmsel,a,zedge Sheet 3 of 18

Sheet 4 of 18 ENERCON F JSERVICES, IC SINC.

Appendix EPadNC-TH to Calculation PGE-009-CALC-006 f sum

/corn

/comr

/com *****

LOAD CASE 9 *****

lcfile,9 lcase,9 eall cmsel,s,bot cmsel,a,synxy cmsel,a,symyz cmsel,a,xedge cmsel,a,zedge fsum

/com

/com *

/com *****

LOAD CASE 10

• lcfile,10 1case,10 eall cmsel,s,bot cmsel,a,symxy cmsel,a,symyz cmsel,a,xedge cmsel,a,zedge fsum

/com

/comr

/com *****

LOAD CASE 11

• lcfile,11 1case,11 eall cmsel,s,bot cmsel,a,symxy cmsel,a,symyz cmsel,a,xedge cmsel,a,zedge fsum

/com

/comr

/comr

/com fini

/output

/exit,nosave

Sheet 5 of 18 F

~ ENERCON SERVICES, INC.

Appendix EPadNC-TH to Calculation PGE-009-CALC-006 Manual Calculation for Dead Weight:

Pad weight model for load step 1 is 72% (0.8*0.9) of 1/4 of the pad weight at 150 pcf:

W model (LS1)= 0.72 x 0.25 x 105 x 68 x 8 x 150 = 1,542,240 lbs W model (LS2)= 0.90 x 0.25 x 105 x 68 x 8 x 150 = 1,927,800 lbs And the incremental weight for each subsequent load step is 19,278 lbs.

Thus for LS 1 W And for LS 2 W And for LS 3 W And for LS 4 W And for LS 5 W And for LS 6 W And for LS 7 W And for LS 8 W And for LS 9 W And for LS 10 W And for LS 11 W

= 1,542,240

= 1,927,800

= 1,927,800

= 1,947,078

= 1,966,356

= 1,985,634

= 2,004,912

= 2,024,190

= 2,043,468

= 2,062,746

= 2,082,024 Target ANSYS

= 1,542,240 Vs 1,541,759

= 1,927,800 Vs 1,927,201

+ 19278

+ 19278

+ 19278

+ 19278

+ 19278

+ 19278

+ 19278

+ 19278

+ 19278

= 1,947,078

= 1,966,356

= 1,985,634

= 2,004,912

= 2,024,190

= 2,043,468

= 2,062,746

= 2,082,024

= 2,101,302 Vs 1,946,473 Vs 1,965,745 Vs 1,985,017 Vs 2,004,289 Vs 2,023,561 Vs 2,042,833 Vs 2,062,104 Vs 2,081,376 Vs 2,100,648

Sheet 6 of 18 F

a ENERCON SERVICES, INC.

Appendix EPadNC-TH to Calculation PGE-009-CALC-006 ANSYS Output File:

ANSYS/Mechanical U W E L C O M E T O T H E A N S Y S P R O G R A M ANSYS 6.1 NOTICES

• Copyright 2002 SAS IP, Inc.

All rights reserved.

• Unpublished---rights reserved under the Copyright Laws of

• the United States.

• 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 Rights Reserved.

• CA&SI, 2004 S. Wright Street, Urbana, IL 61821 Ph (217)244-7875 Fax (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

F

~ ENERCON

.SERVICES, INC.

Appendix EPadNC-TH to Calculation PGE-009-CALC-006

• USEFULNESS OF THE RESULTS.

Completing ANSYS Load Process.

ANSYS COMMAND LINE ARGUMENTS INITIAL JOBNAME

= PADNC-TH BATCH MODE REQUESTED

= LIST MEMORY REQUESTED (MB)

= 700 DATABASE SIZE REQUESTED (MB) = 75

• • • WARNING ***

CP=

0.200 TIME= 10:19:03 Use of the -M switch is no longer recommended for normal ANSYS use.

ANSYS now dynamically allocates memory as needed.

Only use the -M switch if you are certain that you need to do so.

Sheet 7 of 18 PARAMETER STATUS-1 PARAMETERS DEFINED) 1 INTERNAL PARAMETERS)

(INCLUDING 00245050 VERSION=INTEL NT CURRENT JOBNAME=PADNC-TH 10:19:03 RELEASE= 6.1 FEB 11, 2003 CP=

UP20020321 0.210 1

/com, 2

/com, This routine processes load results data for the 3

/com, evaluation of equilibrium.

4 /com 5

/com, Load Case Results 6

/com 7 /com 8

/com 9 /com

• 10

/com 11

/com ****** Reactions ******

12

/com 13

/file,PadNC-Th 14 resume 15

/header,on,on,on 16

/postl 17 spoint,,0,0,0 18

/com 19

/com 20

/com *****

LOAD CASE 1

• 21 lcfile,l 22 lcasel 23 eall 24 cmsel,s,bot 25 cmsel,a,symxy 26 cmsel,a,symyz 27 cmsel,a,xedge 28 cmsel,a,zedge 29 fsum 30

/com 31

/com 32

/com *****

LOAD CASE 2

• 33 lcfile,2

ENERCON F 3 SERVICES, INC.

Appendix EPadNC-TH to Calculation PGE-009-CALC-006 34 lcase,2 35 eall 36 cmsel,s,bot 37 cmsel,a,symxy 38 cmsel,a,symyz 39 cmsel,a,xedge 40 cmsel,a,zedge 41 fsum 42

/com 43

/com ************

44

/com *****

LOAD CASE 3

• 45 lcfile,3 46 lcase,3 47 eall 48 cmsel,s,bot 49 cmsel,a,symxy 50 cmsel,a,symyz 51 cmsel,a,xedge 52 cmsel,a,zedge 53 fsum 54

/com 55

/com ************

56

/com *****

LOAD CASE 4

• 57 lcfile,4 58 lcase,4 59 eall 60 cmsel,s,bot 61 cmsel,a,symxy 62 cmsel,a,symyz 63 cmsel,a,xedge 64 cmsela,zedge 65 fsum 66

/com 67

/com 68

/com *****

LOAD CASE 5

• 69 lcfile,5 70 lcase,5 71 eall 72 cmsel,s,bot 73 cmsel,a,symxy 74 cmsel,a,symyz 75 cmsel,a,xedge 76 cmsel,a,zedge 77 fsum 78

/com 79

/com ***********************

80

/com *****

LOAD CASE 6

• 81 lcfile,6 82 lcase,6 83 eall 84 cmsel,s,bot 85 cmsel,a,symxy 86 cmsel,a,symyz 87 cmsel,a,xedge 88 cmsel,a,zedge 89 fsum 90

/com Sheet 8 of 18

F>

ENERCON F

SERVICES INC.

Appendix EPadNC-TH to Calculation PGE-009-CALC-006 91

/com ************************

92

/com *****

LOAD CASE 7 *****

93 lcfile,7 94 lcase,7 95 eall 96 cmsel,s,bot 97 cmsel,a,symxy 98 cmsel,a,symyz 99 cmsel,a,xedge 100 cmsel,a,zedge 101 fsum 102

/com 103

/com

• 104

/com *****

LOAD CASE 8 *****

105 lcfile,8 106 lcase,8 107 eall 108 cmsel,s,bot 109 cmsel,a,symxy 110 cmsel,a,symyz 111 cmsel,a,xedge 112 cmsel,a,zedge 113 fsum 114

/com 115

/com ************

116

/com *****

LOAD CASE 9

• 117 lcfile,9 118 lcase,9 119 eall 120 cmsel,s,bot 121 cmsel,a,symxy 122 cmsel,a,symyz 123 cmsel,a,xedge 124 cmsel,a,zedge 125 fsum 126

/com 127

/com ************************

128

/com *****

LOAD CASE 10

• 129 lcfile,10 130 lcase,10 131 eall 132 cmsel,s,bot 133 cmsel,a,synxy 134 cmsel,a,symyz 135 cmsel,a,xedge 136 cmsel,a,zedge 137 fsum 138

/com 139

/com *************************

140

/com *****

LOAD CASE 11

• 141 lcfile,11 142 1case,11 143 eall 144 cmsel,s,bot 145 cmsel,a,symxy 146 cmsel,asymyz 147 cmsel,a,xedge Sheet 9 of 18

F-iENERCON F

~SERVICES, INC. Appendix EPadNC-TH to Calculation PGE-009-CALC-006 148 cmsel,a,zedge 149 fsum 150

/com 151

/com *************************

152

/com *************************

153

/com 154 fini 155

/output 156

/exit,nosave 157 158 159 160 RUN SETUP PROCEDURE FROM FILE= C:\\Program Files\\Ansys Inc\\ANSYS61\\docu\\start6l.ans

/INPUT FILE= C:\\Program Files\\Ansys Inc\\ANSYS61\\docu\\start6l.ans LINE=

This routine processes load results data for the evaluation of equilibrium.

Load Case Results Sheet 10 of 18 0

• • • • • • Reactions ******

CURRENT JOBNAME REDEFINED AS PadNC-Th RESUME ANSYS DATA FROM FILE NAME=PadNC-Th.db

• • • ANSYS GLOBAL STATUS ***

TITLE = END OF 2.375 DAYS SZ ON Z SIDE ANALYSIS TYPE =

STATIC (STEADY-STATE)

NUMBER OF ELEMENT TYPES =

5 1870 ELEMENTS CURRENTLY SELECTED. r 10212 NODES CURRENTLY SELECTED.

1 166 KEYPOINTS CURRENTLY SELECTED. I 339 LINES CURRENTLY SELECTED.

r 2 AREAS CURRENTLY SELECTED.

r 48 VOLUMES CURRENTLY SELECTED.

r 22 COMPONENTS CURRENTLY DEFINED MAXIMUM LINEAR PROPERTY NUMBER MAXIMUM REAL CONSTANT SET NUMBER ACTIVE COORDINATE SYSTEM AAX 4AX MAX M1AX rAAX MAX ELEMENT NUMBER =

NODE NUMBER =

KEYPOINT NUMBER =

LINE NUMBER =

AREA NUMBER =

VOL. NUMBER =

9341 10212 166 339 224 48

=

12

=

1

=

0 (CARTESIAN)

INITIAL JOBNAME = PADNC-TH CURRENT JOBNAME = PadNC-Th PRINT HEADER PRINT SUBTITLE(S)

Sheet 11 of 18 ENERCON SERVICES, INC.

Appendix EPadNC-TH to Calculation PGE-009-CALC-006 PRINT LOAD STEP ID DO NOT PRINT NOTE LINE(S)

PRINT COLUMN HEADER LABELS DO NOT PRINT REPORT TOTALS 1

ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 10:19:05 FEB 11, 2003 CP=

0.551 END OF 2.375 DAYS SZ ON Z SIDE

• • • • • ANSYS RESULTS INTERPRETATION (POSTI)

• WARNING ***

CP=

0.551 TIME= 10:19:05 The current solution may have been produced using different model or boundary condition data than is currently stored.

POSTI results may be erroneous unless you perform a new solution using the stored data.

• • • NOTE ***

CP=

0.551 TIME= 10:19:05 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).

NOTE ***

CP=

0.551 TIME= 10:19:05 The force summations will be in global Cartesian when the summation point is at the origin.

NODE FOR MOMENT SUMMATION=

0 MOMENT SUMMATION LOCATION=

0.00000 0.00000 0.00000 LOAD CASE 1 I

LOAD CASE 1 IS LOAD STEP 1 SUBSTEP 1 COMPLEX=

0 FILE= PadNC-Th.101 PAD RESPONSE AT END OF 0.25 DAYS -

NO PAD/ROCK CONSTRAINT COPY LOAD CASE 1 FROM FILE TO DATABASE 8812 ELEMENTS (OF 8812 DEFINED) SELECTED BY EALL COMMAND.

SELECT COMPONENT BOT ALSO SELECT COMPONENT SYMXY ALSO SELECT COMPONENT SYMYZ ALSO SELECT COMPONENT XEDGE ALSO SELECT COMPONENT ZEDGE

• • • • • SUMMATION OF TOTAL FORCES AND MOMENTS IN GLOBAL COORDINATES *****

NERCON FSERVICES, IC EINC.

Appendix EPadNC-TH to Calculation PGE-009-CALC-006 FX

= -0.1051892E-04 FY = -1541759.

FZ

-0.7701914E-04 MX

0.4857015E+09 MY

=

0.4467307E-01 MZ

= -0.3145495E+09 SUMMATION POINT= 0.0000 0.0000 0.0000 LOAD CASE 2

• LOAD CASE 2 IS LOAD STEP 2 SUBSTEP 1 COMPLEX= 0 FILE= PadNC-Th.102 PAD RESPONSE AT END OF 0.50 DAYS -

NO PAD/ROCK CONSTRAINT Sheet 12 of 18 COPY LOAD CASE 2 FROM FILE TO DATABASE 8812 ELEMENTS (OF 8812 DEFINED) SELECTED BY EALL COMMAND.

SELECT COMPONENT BOT ALSO SELECT COMPONENT SYMXY ALSO SELECT COMPONENT SYMYZ ALSO SELECT COMPONENT XEDGE ALSO SELECT COMPONENT ZEDGE

• • • • • SUMMATION OF TOTAL FORCES AND MOMENTS IN GLOBAL COORDINATES *****

FX

= -0.1711750E-02 FY

=

-1927201.

FZ

= -0.4494740E-03 MX

=

0.6071229E+09 MY = -1.379594 MZ

= -0.3931819E+09 SUMMATION POINT= 0.0000 0.0000 0.0000 LOAD CASE 3

• LOAD CASE 3 IS LOAD STEP 3 SUBSTEP 1 COMPLEX= 0 FILE= PadNC-Th.103 PAD RESPONSE AT END OF 0.625 DAYS -

NO PAD/ROCK CONSTRAINT COPY LOAD CASE 3 FROM FILE TO DATABASE 8812 ELEMENTS (OF 8812 DEFINED) SELECTED BY EALL COMMAND.

SELECT COMPONENT BOT ALSO SELECT COMPONENT SYMXY

F X

ENERCON r-j1 SERVICES, INC.

Appendix EPadNC-TH to Calculation PGE-009-CALC-006 Sheet 13 of 18 ALSO SELECT COMPONENT SYMYZ ALSO SELECT COMPONENT XEDGE ALSO SELECT COMPONENT ZEDGE

• • • • • SUMMATION OF TOTAL FX

= -0.1662139E-02 FY

=

-1946473.

FZ

= -0.6303782E-03 MX

=

0.6131936E+09 MY

=

-1.413520 MZ

-0.3971134E+09 SUMMATION POINT

0.0000 LOAD CASE 4

• LOAD CASE 4 IS LOAD STEP FILE= PadNC-Th.104 PAD RESPONSE AT END OF 1.125 FORCES AND MOMENTS IN GLOBAL COORDINATES *****

0. 0000 0.0000 4 SUBSTEP 1 COMPLEX=

0 DAYS -

NO PAD/ROCK CONSTRAINT COPY LOAD CASE 4 FROM FILE TO DATABASE 8812 ELEMENTS (OF 8812 DEFINED) SELECTED BY EALL COMMAND.

SELECT COMPONENT BOT ALSO SELECT COMPONENT SYMXY ALSO SELECT COMPONENT SYMYZ ALSO SELECT COMPONENT XEDGE ALSO SELECT COMPONENT ZEDGE

• • • • • SUMMATION OF TOTAL FORCES AND MOMENTS IN GLOBAL COORDINATES *****

FX = -0.1628839E-02 FY

=

-1965745.

FZ

= -0.6716764E-03 MX

=

0.6192643E+09 MY

=

-1.404136 MZ

= -0.4010449E+09 SUMMATION POINT= 0.0000 0.0000 0.0000 LOAD CASE 5

• LOAD CASE 5 IS LOAD STEP 5 SUBSTEP 1 COMPLEX= 0 FILE= PadNC-Th.105 PAD RESPONSE AT END OF 1.625 DAYS -

NO PAD/ROCK CONSTRAINT COPY LOAD CASE 5 FROM FILE TO DATABASE

Sheet 14 of 18 F:

f ENERCON

>\\\\9SERVICES, INC.

Appendix EPadNC-TH to Calculation PGE-009-CALC-006 8812 ELEMENTS (OF 8

SELECT COMPONENT BOT ALSO SELECT COMPONENT SYMXY ALSO SELECT COMPONENT SYMYZ ALSO SELECT COMPONENT XEDGE ALSO SELECT COMPONENT ZEDGE

• • • • • SUMMATION OF TOTAL FX

= -0.1628884E-02 FY

=

-1985017.

FZ

= -0.6719177E-03 MX

= 0.6253349E+09 MY

=

-1.404028 MZ

-0.4049763E+09 SUMMATION POINT

0.0000 LOAD CASE 6

• LOAD CASE 6 IS LOAD STEP FILE= PadNC-Th.106 PAD RESPONSE AT END OF 2.125 812 DEFINED) SELECTED BY EALL COMMAND.

FORCES AND MOMENTS IN GLOBAL COORDINATES *****

0.0000 0.0000 6 SUBSTEP 1 COMPLEX=

0 DAYS -

NO PAD/ROCK CONSTRAINT COPY LOAD CASE 6 FROM FILE TO DATABASE 8812 ELEMENTS (OF 8812 DEFINED) SELECTED BY SELECT COMPONENT BOT ALSO SELECT COMPONENT SYMXY ALSO SELECT COMPONENT SYMYZ ALSO SELECT COMPONENT XEDGE ALSO SELECT COMPONENT ZEDGE

• • • • • SUMMATION OF TOTAL FORCES AND MOMENTS IN GLOI FX

= -0.1628904E-02 FY

=

-2004289.

FZ

= -0.6718816E-03 MX

=

0.6314055E+09 MY

=

-1.404046 MZ

-0.4089078E+09 SUMMATION POINT

0.0000 0.0000 0.0000 LOAD CASE 7

• EALL COMMAND.

3AL COORDINATES *****

4I!.,

Sheet 15 of 18 F

NERCON l

SERVICES, INC.

Appendix EPadNC-TH to Calculation PGE-009-CALC-006 LOAD CASE 7 IS LOAD STEP 7 SUBSTEP 1 COMPLEX=

0 FILE= PadNC-Th.107 PAD RESPONSE AT END OF 2.375 DAYS -

NO PAD/ROCK CONSTRAINT COPY LOAD CASE 7 FROM FILE TO DATABASE 8812 ELEMENTS (OF 8812 DEFINED) SELECTED BY EALL COMMAND.

SELECT COMPONENT BOT ALSO SELECT COMPONENT SYMXY ALSO SELECT COMPONENT SYMYZ ALSO SELECT COMPONENT XEDGE ALSO SELECT COMPONENT ZEDGE

• • • • • SUMMATION OF TOTAL FORCES AND MOMENTS IN GLOBAL COORDINATES *****

FX

= -0.1707448E-02 FY

=

-2023561.

FZ

= -0.6852017E-03 MX

=

0.6374762E+09 MY = -1.324389 MZ

-0.4128392E+09 SUMMATION POINT

0.0000 0.0000 0.0000 LOAD CASE 8

• LOAD CASE 8 IS LOAD STEP 8 SUBSTEP 1 COMPLEX= 0 FILE= PadNC-Th.108 PAD RESPONSE AT END OF 3.125 DAYS -

NO PAD/ROCK CONSTRAINT COPY LOAD CASE 8 FROM FILE TO DATABASE 8812 ELEMENTS (OF 8812 DEFINED) SELECTED BY EALL COMMAND.

SELECT COMPONENT BOT ALSO SELECT COMPONENT SYMXY ALSO SELECT COMPONENT SYMYZ ALSO SELECT COMPONENT XEDGE ALSO SELECT COMPONENT ZEDGE

• • • • • SUMMATION OF TOTAL FORCES AND MOMENTS IN GLOBAL COORDINATES

• FX = -0.1697010E-02 FY

=

-2042833.

FZ

= -0.7519997E-03 MX

=

0.6435468E+09

ENERCON SERVICES, INC.

Appendix EPadNC-TH to Calculation PGE-009-CALC-006 MY = -1.294351 MZ

= -0.4167707E+09 SUMMATION POINT= 0.0000 0.0000 0.0000 LOAD CASE 9 *****

LOAD CASE 9 IS LOAD STEP 9 SUBSTEP 1 COMPLEX=

0 FILE= PadNC-Th.109 PAD RESPONSE AT END OF 4.125 DAYS -

NO PAD/ROCK CONSTRAINT Sheet 16 of 18 COPY LOAD CASE 9 FROM FILE TO DATABASE 8812 ELEMENTS (OF 8812 DEFINED) SELECTED BY EALL COMMAND.

SELECT COMPONENT BOT ALSO SELECT COMPONENT SYMXY ALSO SELECT COMPONENT SYMYZ ALSO SELECT COMPONENT XEDGE ALSO SELECT COMPONENT ZEDGE

• • • • • SUMMATION OF TOTAL FORCES AND MOMENTS IN GLOBAL COORDINATES *****

FX

= -0.1657006E-02 FY = -2062104.

FZ

= -0.6929606E-03 MX

=

0.6496174E+09 MY

=

-1.181507 MZ

-0.4207021E+09 SUMMATION POINT

0.0000 0.0000 0.0000 LOAD CASE 10

• LOAD CASE 10 IS LOAD STEP 10 SUBSTEP 1 COMPLEX=

0 FILE= PadNC-Th.110 PAD RESPONSE AT END OF 6.125 DAYS -

NO PAD/ROCK CONSTRAINT COPY LOAD CASE 10 FROM FILE TO DATABASE 8812 ELEMENTS (OF 8812 DEFINED) SELECTED BY EALL COMMAND.

SELECT COMPONENT BOT ALSO SELECT COMPONENT SYMXY ALSO SELECT COMPONENT SYMYZ ALSO SELECT COMPONENT XEDGE

Tfs-.0, F.. bI ENERCON F

SERVICES, INC.

Appendix EPadNC-TH to Calculation PGE-009-CALC-006 Sheet 17 of 18 ALSO SELECT COMPONENT ZEDGE

• • • • • SUMMATION OF TOTAL FORCES AND MOMENTS IN GLOBAL COORDINATES *****

FX

= -0.2281821E-02 FY

=

-2081376.

FZ

= -0.5014647E-03 MX

=

0.6556874E+09 MY

=

-2.134902 MZ

-0.4246332E+09 SUMMATION POINT

0.0000 0.0000 0.0000 LOAD CASE 11

• LOAD CASE 11 IS LOAD STEP 11 SUBSTEP 1 COMPLEX=

0 FILE= PadNC-Th.111 PAD RESPONSE AT END OF 7.875 DAYS -

NO PAD/ROCK CONSTRAINT COPY LOAD CASE 11 FROM FILE TO DATABASE 8812 ELEMENTS (OF 8812 DEFINED) SELECTED BY SELECT COMPONENT BOT ALSO SELECT COMPONENT SYMXY ALSO SELECT COMPONENT SYMYZ ALSO SELECT COMPONENT XEDGE ALSO SELECT COMPONENT ZEDGE

• • • • • SUMMATION OF TOTAL FORCES AND MOMENTS IN GLOI FX

= -0.2280719E-02 FY

=

-2100648.

FZ

= -0.5055810E-03 MX

=

0.6617577E+09 MY

= -2.132106 MZ

-0.4285644E+09 SUMMATION POINT

0.0000 0.0000 0.0000 EALL COMMAND.

BAL COORDINATES *****

EXIT THE ANSYS POST1 DATABASE PROCESSOR

• • • • • ROUTINE COMPLETED *****

CP =

8.222 EXIT ANSYS WITHOUT SAVING DATABASE

Sheet 18 of 18 F; -

ENERCON INC.

Appendix EPadNC-TH to Calculation PGE-009-CALC-006 NUMBER OF WARNING MESSAGES ENCOUNTERED=

2 NUMBER OF ERROR MESSAGES ENCOUNTERED=

0 ll ANSYS RUN COMPLETED ll Release 6.1 UP20020321 INTEL NT Maximum Scratch Memory Used 1025420 Words 3.912 MB l

CP Time (sec) =

8.222 Time

=

10:19:25 Elapsed Time (sec) =

23.000 Date

=

02/11/2003

Sheet 1 of 47 F

'~ENERCON SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006 Originator:

S. C. Tumminelli Date:

March 3, 2003 Appendix SPadNC-TH This Appendix presents the ANSYS output file documenting the pad stress response for the unconstrained thermal stress analysis.

Sheet 2 of 47 F

by ENERCON SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006 ANSYS/Mechanical U W E L C O M E T O T H E A N S Y S P R O G R A M ANSYS 6.1 NOTICES

• Copyright 2002 SAS IP, Inc.

All rights reserved.

• Unpublished---rights reserved under the Copyright Laws of

• the United States.

• 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 Rights Reserved.

• CA&SI, 2004 S. Wright Street, Urbana, IL 61821 Ph (217)244-7875 Fax (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.

Sheet 3 of 47 ENERCON

-l SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006 Completing ANSYS Load Process.

ANSYS COMMAND LINE ARGUMENTS INITIAL JOBNAME

= PADNC-TH BATCH MODE REQUESTED

= LIST MEMORY REQUESTED (MB)

= 700 DATABASE SIZE REQUESTED (MB) = 75

• • • WARNING ***

CP=

0.260 TIME= 20:02:45 Use of the -M switch is no longer recommended for normal ANSYS use.

ANSYS now dynamically allocates memory as needed.

Only use the -M switch if you are certain that you need to do so.

PARAMETER STATUS-(

1 PARAMETERS DEFINED)

(INCLUDING 1 INTERNAL PARAMETERS) 00245050 VERSION=INTEL NT RELEASE= 6.1 UP20020321 CURRENT JOBNAME=PADNC-TH 20:02:45 FEB 10, 2003 CP=

0.260 1

/COM 2

/COM 3

/COM STRESS DATA SORTED AND PRINTED BY LOAD CASE 4

/COM 5

/COM 6

/COM 7

/COM THIS ROUTINE SORTS AND PRINTS STRESS DATA BY LOAD CASE 8

/COM FIRST SX, SZ, SI (MAX) AND S3 (MIN) 9

/COM 10

/COM 11

/file,PadNC-Th 12 resume 13

/header,on,off,off,off,on,off 14

/postl 15

/COM 16 EALL 17 NALL 18

/COM 19

/COM=

20

/COMN 21

/COMN 22

/COM LCASE 1 23

/COM 24 LCFILE,1 25 LCASE,1 26 ESEL,TYPE,2 27 NELEM 28

/COM 29

/COMN 30

/COM MAXIMUM VALUES OF SX 31

/COM 32 NSORT,S,X,0,0,2,SEL 33 PRNSOL,S 34 NUSORT 35

/COM

Sheet 4 of 47 ENERCON F

J SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006 36

/COM=

37

/COM MINIMUM VALUES OF SX 38

/COM 39 NSORT,S,X,1,0,2,SEL 40 PRNSOL,S 41 NUSORT 42

/COM 43

/COM 44

/COM MAXIMUM VALUES OF SZ 45

/COM 46 NSORT,S,Z,0,0,2,SEL 47 PRNSOL,S 48 NUSORT 49

/COM 50

/COMN 51

/COM MINIMUM VALUES OF SZ 52

/COM 53 NSORT,S,Z,1,0,2,SEL 54 PRNSOL,S 55

/COM 56

/COM 57

/COMN 58

/COM MAXIMUM VALUES OF SI 59

/COM 60 NSORT,S,1,0,0,2,SEL 61 PRNSOL,S,PRIN 62 NUSORT 63

/COM 64

/COMN 65

/COM MINIMUM VALUES OF S3 66

/COM 67 NSORT,S,3,1,0,2,SEL 68 PRNSOL,S,PRIN 69 NUSORT 70

/COM 71

/COMN 72

/COMN 73

/COMN 74

/COM LCASE 2 75 ICOM 76 LCFILE,2 77 LCASE,2 78 ESEL,TYPE,2 79 NELEM 80

/COM 81

/COMN 82

/COM MAXIMUM VALUES OF SX 83

/COM 84 NSORT,S,X,0,0,2,SEL 85 PRNSOL,S 86 NUSORT 87 ICOM 88

/COMN 89

/COM MINIMUM VALUES OF SX 90

/COM 91 NSORT,S,X,1,0,2,SEL 92 PRNSOL,S

Sheet 5 of 47 ENERCON SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006 93 NUSORT 94

/COM 95

/COM=

96 ICOM MAXIMUM VALUES OF SZ 97

/COM 98 NSORT,S,Z,0,0,2,SEL 99 PRNSOL,S 100 NUSORT 101

/COM 102

/COM=

103

/COM MINIMUM VALUES OF SZ 104

/COM 105 NSORT,S,Z,1,0,2,SEL 106 PRNSOL,S 107 ICOM 108

/COM 109

/COMN 110

/COM MAXIMUM VALUES OF SI 111

/COM 112 NSORT,S,1,0,0,2,SEL 113 PRNSOL,S,PRIN 114 NUSORT 115

/COM 116

/COMN 117

/COM MINIMUM VALUES OF S3 118

/COM 119 NSORT,S,3,1,0,2,SEL 120 PPNSOL,SPRIN 121 NUSORT 122

/COM 123

/COMN 124 ICOMN 125

/COMN 126

/COM LCASE 3 127

/COM 128 LCFILE,3 129 LCASE,3 130 ESEL,TYPE,2 131 NELEM 132

/COM 133

/COMN 134

/COM MAXIMUM VALUES OF SX 135

/COM 136 NSORT,S,X,0,0,2,SEL 137 PRNSOL,S 138 NUSORT 139

/COM 140

/COMN 141

/COM MINIMUM VALUES OF SX 142

/COM 143 NSORT,S,X,1,0,2,SEL 144 PRNSOL,S 145 NUSORT 146

/COM 147

/COMN 148

/COM MAXIMUM VALUES OF SZ 149

/COM

Sheet 6 of 47 F = qENERCON SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006 150 NSORT,S,Z,0,0,2,SEL 151 PRNSOL,S 152 NUSORT 153

/COM 154

/COM=

155

/COM MINIMUM VALUES OF SZ 156

/COM 157 NSORT,S,Z,1,0,2,SEL 158 PRNSOL,S 159

/COM 160

/COM 161

/COMN 162

/COM MAXIMUM VALUES OF SI 163

/COM 164 NSORT,S,1,0,0,2,SEL 165 PRNSOL,S,PRIN 166 NUSORT 167

/COM 168

/COMN 169

/COM MINIMUM VALUES OF S3 170

/COM 171 NSORT,S,3,1,0,2,SEL 172 PRNSOL,S,PRIN 173 NUSORT 174

/COM 175

/COMN 176

/COMN 177

/COMN 178

/COM LCASE 4 179

/COM 180 LCFILE,4 181 LCASE,4 182 ESEL,TYPE,2 183 NELEM 184

/COM 185

/COMN 186

/COM MAXIMUM VALUES OF SX 187

/COM 188 NSORT,S,X,0,0,2,SEL 189 PRNSOL,S 190 NUSORT 191

/COM 192

/COMN 193

/COM MINIMUM VALUES OF SX 194

/COM 195 NSORT,S,X,1,0,2,SEL 196 PRNSOL,S 197 NUSORT 198

/COM 199

/COMN-200

/COM MAXIMUM VALUES OF SZ 201

/COM 202 NSORT,S,Z,0,0,2,SEL 203 PRNSOL,S 204 NUSORT 205

/COM 206

/COMN-

Sheet 7 of 47 F

k ENERCON F

SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006 207

/COM MINIMUM VALUES OF SZ 208

/COM 209 NSORT,S,Z,1,0,2,SEL 210 PRNSOL,S 211

/COM 212

/COM 213

/COM 214

/COM MAXIMUM VALUES OF SI 215

/COM 216 NSORT,S,1,0,0,2,SEL 217 PRNSOL,S,PRIN 218 NUSORT 219

/COM 220

/COMN 221

/COM MINIMUM VALUES OF S3 222

/COM 223 NSORT,S,3,1,0,2,SEL 224 PRNSOL,S,PRIN 225 NUSORT 226

/COM 227

/COMN 228

/COMN 229

/COMN 230

/COM LCASE 5 231

/COM 232 LCFILE,5 233 LCASE,5 234 ESEL,TYPE,2 235 NELEM 236

/COM 237

/COMN 238

/COM MAXIMUM VALUES OF SX 239

/COM 240 NSORT,S,X,0,0,2,SEL 241 PRNSOL,S 242 NUSORT 243

/COM 244

/COMN 245

/COM MINIMUM VALUES OF SX 246

/COM 247 NSORT,S,X,1,0,2,SEL 248 PRNSOL,S 249 NUSORT 250

/COM 251

/COMN 252

/COM MAXIMUM VALUES OF SZ 253

/COM 254 NSORT,S,Z,0,0,2,SEL 255 PRNSOL,S 256 NUSORT 257

/COM 258

/COMN 259

/COM MINIMUM VALUES OF SZ 260

/COM 261 NSORT,S,Z,1,0,2,SEL 262 PRNSOL,S 263

/COM

Sheet 8 of 47

~

'j ENERCON

• r

=

SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006 264

/COM 265

/COMN 266

/COM MAXIMUM VALUES OF S1 267

/COM 268 NSORT,S,1,0,0,2,SEL 269 PRNSOL,S,PRIN 270 NUSORT 271

/COM 272 ICOMN 273

/COM MINIMUM VALUES OF S3 274

/COM 275 NSORT,S,3,1,0,2,SEL 276 PRNSOL,S,PRIN 277 NUSORT 278

/COM 279

/COMN 280

/COMN 281

/COMN 282

/COM LCASE 6 283

/COM 284 LCFILE,6 285 LCASE,6 286 ESEL,TYPE,2 287 NELEM 288

/COM 289

/COMN 290

/COM MAXIMUM VALUES OF SX 291

/COM 292 NSORT,S,X,0,0,2,SEL 293 PRNSOL,S 294 NUSORT 295 /COM 296

/COMN 297

/COM MINIMUM VALUES OF SX 298

/COM 299 NSORT,S,X,1,0,2,SEL 300 PRNSOL,S 301 NUSORT 302

/COM 303

/COMN 304

/COM MAXIMUM VALUES OF SZ 305

/COM 306 NSORT,S,Z,0,0,2,SEL 307 PRNSOL,S 308 NUSORT 309

/COM 310

/COMN 311

/COM MINIMUM VALUES OF SZ 312

/COM 313 NSORT,S,Z,1,0,2,SEL 314 PRNSOL,S 315

/COM 316

/COM 317

/COMN 318

/COM MAXIMUM VALUES OF S1 319 NSORT,S,1,0,0,2,SEL 320 PRNSOL,S,PRIN

Sheet 9 of 47 F

-ENERCON F1 ~ SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006 321 NUSORT 322

/COM 323

/COMN 324

/COM MINIMUM VALUES OF S3 325

/COM 326 NSORT,S,3,1,0,2,SEL 327 PRNSOL,S,PRIN 328 NUSORT 329

/COM 330

/COMN 331

/COMN 332

/COMN 333

/COM LCASE 7 334

/COM 335 LCFILE,7 336 LCASE,7 337 ESEL,TYPE,2 338 NELEM 339

/COM 340

/COMN 341

/COM MAXIMUM VALUES OF SX 342

/COM 343 NSORT,S,X,0,0,2,SEL 344 PRNSOL,S 345 NUSORT 346

/COM 347

/COMN 348

/COM MINIMUM VALUES OF SX 349

/COM 350 NSORT,S,X,1,0,2,SEL 351 PRNSOL,S 352 NUSORT 353

/COM 354

/COMN 355

/COM MAXIMUM VALUES OF SZ 356

/COM 357 NSORT,S,Z,0,0,2,SEL 358 PRNSOL,S 359 NUSORT 360

/COM 361

/COMN 362

/COM MINIMUM VALUES OF SZ 363

/COM 364 NSORT,S,Z,1,0,2,SEL 365 PRNSOL,S 366

/COM 367

/COM 368

/COMN 369

/COM MAXIMUM VALUES OF S1 370

/COM 371 NSORT,S,1,0,0,2,SEL 372 PRNSOL,S,PRIN 373 NUSORT 374

/COM 375

/COM 376

/COM MINIMUM VALUES OF S3 377

/COM

Sheet 10 of 47 e ]

ENERCON F

1 SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006 378 NSORT,S,3,1,0,2,SEL 379 PRNSOL,S,PRIN 380 NUSORT 381

/COM 382

/COM===

383

/COMN 384

/COMN 385 ICOM LCASE 8 386

/COM 387 LCFILE,8 388 LCASE,8 389 ESEL,TYPE,2 390 NELEM 391

/COM 392

/COMN 393

/COM MAXIMUM VALUES OF SX 394

/COM 395 NSORT,S,X,0,0,2,SEL 396 PRNSOL,S 397 NUSORT 398

/COM 399

/COMN 400

/COM MINIMUM VALUES OF SX 401

/COM 402 NSORT,S,X,1,0,2,SEL 403 PRNSOL,S 404 NUSORT 405

/COM 406

/COMN 407

/COM MAXIMUM VALUES OF SZ 408

/COM 409 NSORT,S,Z,0,0,2,SEL 410 PRNSOL,S 411 NUSORT 412

/COM 413

/COMN 414

/COM MINIMUM VALUES OF SZ 415

/COM 416 NSORT,S,Z,1,0,2,SEL 417 PRNSOL,S 418

/COM 419

/COM 420

/COMN 421

/COM MAXIMUM VALUES OF S1 422

/COM 423 NSORT,S,1,0,0,2,SEL 424 PRNSOL,S,PRIN 425 NUSORT 426

/COM 427

/COMN 428

/COM MINIMUM VALUES OF S3 429

/COM 430 NSORT,S,3,1,0,2,SEL 431 PRNSOL,S,PRIN 432 NUSORT 433

/COM 434

/COMN

Sheet 11 of 47 F

ENERCON SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006 435

/COM=

436

/COMN 437

/COM LCASE 9 438

/COM 439 LCFILE,9 440 LCASE,9 441 ESEL,TYPE,2 442 NELEM 443

/COM 444

/COMN 445

/COM MAXIMUM VALUES OF SX 446

/COM 447 NSORT,S,X,0,0,2,SEL 448 PRNSOL,S 449 NUSORT 450

/COM 451

/COMN 452

/COM MINIMUM VALUES OF SX 453

/COM 454 NSORT,S,X,1,0,2,SEL 455 PRNSOL,S 456 NUSORT 457

/COM 458

/COMN 459

/COM MAXIMUM VALUES OF SZ 460

/COM 461 NSORT,S,Z,0,0,2,SEL 462 PRNSOL,S 463 NUSORT 464

/COM 465

/COMN 466

/COM MINIMUM VALUES OF SZ 467

/COM 468 NSORTS,Z,1,0,2,SEL 469 PRNSOL,S 470

/COM 471

/COM 472

/COMN 473

/COM MAXIMUM VALUES OF S1 474

/COM 475 NSORT,S,1,0,0,2,SEL 476 PRNSOL,S,PRIN 477 NUSORT 478

/COM 479

/COMN 480

/COM MINIMUM VALUES OF S3 481

/COM 482 NSORT,S,3,1,0,2,SEL 483 PRNSOL,S,PRIN 484 NUSORT 485

/COM 486

/COMN 487

/COMN 488

/COMN 489

/COM LCASE 10 490

/COM 491 LCFILE,10

Sheet 12 of 47 ENERCON F SERVICES, IC SINC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006 492 LCASE,10 493 ESEL,TYPE,2 494 NELEM 495

/COM 496

/COMN 497

/COM MAXIMUM VALUES OF SX 498

/COM 499 NSORT,S,X,0,0,2,SEL 500 PRNSOL,S 501 NUSORT 502

/COM 503

/COMN 504

/COM MINIMUM VALUES OF SX 505

/COM 506 NSORT,S,X,1,0,2,SEL 507 PRNSOL,S 508 NUSORT 509

/COM 510

/COMN 511

/COM MAXIMUM VALUES OF SZ 512

/COM 513 NSORT,SZ,0,0,2,SEL 514 PRNSOL,S 515 NUSORT 516

/COM 517

/COMN 518

/COM MINIMUM VALUES OF SZ 519

/COM 520 NSORT,S,Z,1,0,2,SEL 521 PRNSOL,S 522

/COM 523

/COM 524

/COMN 525

/COM MAXIMUM VALUES OF Si 526

/COM 527 NSORT,S,1,0,0,2,SEL 528 PRNSOL,S,PRIN 529 NUSORT 530

/COM 531

/COMN 532 ICOM MINIMUM VALUES OF S3 533

/COM 534 NSORT,S,3,1,0,2,SEL 535 PRNSOL,S,PRIN 536 NUSORT 537 ICOM 538

/COMN 539

/COMN 540

/COMN 541

/COM LCASE 11 542

/COM 543 LCFILE,11 544 LCASE,11 545 ESEL,TYPE,2 546 NELEM 547

/COM 548

/COMN

Sheet 13 of 47 F2 t ENERCON SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006 549

/COM MAXIMUM VALUES OF SX 550

/COM 551 NSORT,S,X,0,0,2,SEL 552 PRNSOL,S 553 NUSORT 554

/COM 555

/COMN 556

/COM MINIMUM VALUES OF SX 557

/COM 558 NSORT,S,X,1,0,2,SEL 559 PRNSOL,S 560 NUSORT 561

/COM 562

/COMN 563

/COM MAXIMUM VALUES OF SZ 564

/COM 565 NSORT,S,Z,0,0,2,SEL 566 PRNSOL,S 567 NUSORT 568

/COM 569

/COMN 570

/COM MINIMUM VALUES OF SZ 571

/COM 572 NSORT,S,Z,1,0,2,SEL 573 PRNSOL,S 574

/COM 575

/COM 576

/COMN 577

/COM MAXIMUM VALUES OF S1 578

/COM 579 NSORT,S,1,0,0,2,SEL 580 PRNSOL,S,PRIN 581 NUSORT 582

/COM 583

/COMN 584

/COM MINIMUM VALUES OF S3 585

/COM 586 NSORT,S,3,1,0,2,SEL 587 PRNSOL,S,PRIN 588 NUSORT 589

/COM 590

/COMN 591

/COMN 592

/COMN 593

/COMN 594

/COM 595 EALL 596 NALL 597 FINI 598

/OUTPUT 599

/EXIT,NOSAVE RUN SETUP PROCEDURE FROM FILE= C:\\Program Files\\Ansys Inc\\ANSYS61\\docu\\start61.ans

/INPUT FILE= C:\\Program Files\\Ansys Inc\\ANSYS61\\docu\\start61.ans LINE=

0

F I-NERCON E'~ SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006 STRESS DATA SORTED AND PRINTED BY LOAD CASE Sheet 14 of 47 THIS ROUTINE SORTS AND PRINTS STRESS DATA BY FIRST SX, SZ, Si (MAX) AND S3 (MIN)

LOAD CASE CURRENT JOBNAME REDEFINED AS PadNC-Th RESUME ANSYS DATA FROM FILE NAME=PadNC-Th.db

• • • ANSYS GLOBAL STATUS ***

TITLE = END OF 2.375 DAYS SZ ON Z SIDE ANALYSIS TYPE =

STATIC (STEADY-STATE)

NUMBER OF ELEMENT TYPES =

5 1870 ELEMENTS CURRENTLY SELECTED.

MAX 10212 NODES CURRENTLY SELECTED.

MAX 166 KEYPOINTS CURRENTLY SELECTED. MAX 339 LINES CURRENTLY SELECTED.

MAX 2 AREAS CURRENTLY SELECTED.

MAX 48 VOLUMES CURRENTLY SELECTED.

MAX 22 COMPONENTS CURRENTLY DEFINED MAXIMUM LINEAR PROPERTY NUMBER

=

MAXIMUM REAL CONSTANT SET NUMBER ACTIVE COORDINATE SYSTEM ELEMENT NUMBER =

NODE NUMBER =

KEYPOINT NUMBER =

LINE NUMBER =

AREA NUMBER =

VOL. NUMBER =

9341 10212 166 339 224 48 12 1

0 (CARTESIAN)

INITIAL JOBNAME = PADNC-TH CURRENT JOBNAME = PadNC-Th PRINT HEADER DO NOT PRINT DO NOT PRINT DO NOT PRINT PRINT COLUMN DO NOT PRINT 1

SUBTITLE(S)

LOAD STEP ID NOTE LINE(S)

HEADER LABELS REPORT TOTALS

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:46 FEB 10, 2003 CP=

0. 611 END OF 2.375 DAYS SZ ON Z SIDE

• • • • • ANSYS RESULTS INTERPRETATION (POST1) *****

WARNING ***

CP=

0.611 TIME= 20:02:46 The current solution may have been produced using different model or boundary condition data than is currently stored.

POST1 results may be erroneous unless you perform a new solution using the stored data.

• • • NOTE ***

CP=

0.611 TIME= 20:02:46

F. 4 ENERCON SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006 Sheet 15 of 47 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).

8812 ELEMENTS (OF 10212 NODES (OF 8812 DEFINED) SELECTED BY EALL COMMAND.

10212 DEFINED) SELECTED BY NALL COMMAND.

LCASE 1

=

LOAD CASE 1 IS LOAD STEP 1

SUBSTEP 1

COMPLEX=

0 FILE= PadNC-Th.101 PAD RESPONSE AT END OF 0.25 DAYS -

NO PAD/ROCK CONSTRAINT COPY LOAD CASE 1 FROM FILE TO DATABASE ESEL FOR LABEL= TYPE FROM 2 TO 2 BY 1

1870 ELEMENTS (OF 8812 DEFINED) SELECTED BY ESEL COMMAND.

SELECT ALL NODES HAVING ANY ELEMENT IN ELEMENT SET.

2376 NODES (OF 10212 DEFINED) SELECTED FROM 1870 SELECTED ELEMENTS BY NELE COMMAND.

MAXIMUM VALUES OF SX SORT ON ITEM=S COMPONENT=X ORDER= 0 KABS= 0 NMAX=

2 SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U

00245050 VERSION=INTEL NT 20:02:47 FEB 10, 2003 CP=

1.262 PAD RESPONSE AT END OF 0.25 DAYS -

NO PAD/ROCK CONSTRAINT NODE 2357 2355 SX 55.557 55.524 SY

-6.5627

-6.4748 SZ 54.667 54.239 SXY

-0.21157

-0.21328 SYZ SXZ

-0.14933

-0.11882

-0.47766E-01-0.75912E-01 NODE SORT REMOVED

F

~

ENERCON SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006

MINIMUM VALUES OF SX Sheet 16 of 47 SORT ON ITEM=S COMPONENT=X SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

ORDER= 1 KABS= 0 NMAX=

2

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:47 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 0.25 DAYS -

NO PAD/ROCK CONSTRAINT 1.282 NODE SX 2703

-6.9609 52

-6.6497 NODE SORT REMOVED SY

-2.9178

-0.76182 Sz

-6.2015

-5.6077 SXY

-0.60510

-0.64664 SYZ SXZ

-1.4155 0.91587E-01

-0.41871E-03 0.10156E-02 MAXIMUM VALUES OF SZ SORT ON ITEM=S COMPONENT=Z SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

ORDER= 0 KABS= 0 NMAX=

2

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:47 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 0.25 DAYS - NO PAD/ROCK CONSTRAINT 1.302 NODE SX 2273 54.546 2275 54.162 NODE SORT REMOVED SY

-6.9690

-6.8950 SZ 55.042 55.028 SXY SYZ SXZ

-0.95016E-01-0.18425E-01-0.12883

-0.34288E-01-0.20324E-01-0.71414E-01 MINIMUM VALUES OF SZ

==-

SORT ON ITEM=S COMPONENT=Z SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE ORDER= 1 KABS= 0 NMAX=

2

F^

ENERCON FSERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006 1

ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:47 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 0.25 DAYS -

NO PAD/ROCK CONSTRAINT Sheet 17 of 47 1.322 NODE 2706 671 SX

-6.3930

-6.0346 SY

-5.7859

-2. 8234 Sz

-6.5363

-6.4821 SXY

-1.9099

-2.0368 SYZ SXZ

-1.3308 0.44730E-01

-0.17288E-01 0.89020E-01 MAXIMUM VALUES OF S1

==

SORT ON ITEM=S COMPONENT=1 SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE ORDER= 0 KABS= 0 NMAX=

2

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:47 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 0.25 DAYS -

NO PAD/ROCK CONSTRAINT 1.342 NODE Si 2357 55.573 2355 55.530 NODE SORT REMOVED S2 54. 652 54.235 S3

-6.5638

-6.4756 SINT 62.137

62. 005 SEQV 61.681 61.368 MINIMUM VALUES OF S3

==-

SORT ON ITEM=S COMPONENT=3 SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

ORDER= 1 KABS= 0 NMAX=

2

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:47 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 0.25 DAYS - NO PAD/ROCK CONSTRAINT 1.372 NODE Si S2 S3 SINT SEQV

E

~I ENERCON SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006 Sheet 18 of 47 2268 2.9838 2267 51.694

-1.1806 37.450

-10.869

-10.706 13.853 62.400 12. 311

56. 638 NODE SORT REMOVED LCASE 2

=-

LOAD CASE 2 IS LOAD STEP 2

SUBSTEP 1

COMPLEX=

0 FILE= PadNC-Th.102 PAD RESPONSE AT END OF 0.50 DAYS -

NO PAD/ROCK CONSTRAINT COPY LOAD CASE 2 FROM FILE TO DATABASE ESEL FOR LABEL= TYPE FROM 1870 ELEMENTS (OF 2 TO 2 BY 1

3812 DEFINED)

SELECTED BY ESEL COMMAND.

SELECT ALL NODES HAVING ANY ELEMENT IN ELEMENT SET.

2376 NODES (OF 10212 DEFINED)

SELECTED FROM 1870 SELECTED ELEMENTS BY NELE COMMAND.

MAXIMUM VALUES OF SX

==-

SORT ON ITEM=S COMPONENT=X ORDER= 0 KABS= 0 NMAX=

2 SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:48 FEB 10, 2003 CP=

2.003 PAD RESPONSE AT END OF 0.50 DAYS -

NO PAD/ROCK CONSTRAINT NODE 675 674 SX 203.89 203.89 SY

-0.23631

-0.21134 Sz 204.77 204.77 SXY 0.10852 0.11000 SYZ SXZ

-0.51902E-02-0.50266E-02 0.65581E-02 0.51627E-02 NODE SORT REMOVED MINIMUM VALUES OF SX

==

SORT ON ITEM=S COMPONENT=X ORDER= 1 KABS= 0 NMAX=

2

FWj ENERCON F

SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006 Sheet 19 of 47 SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:48 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 0.50 DAYS -

NO PAD/ROCK CONSTRAINT 2.023 SXz

-0.76031

-1.2980 NODE SX 2805

-66.820 2108

-66.216 NODE SORT REMOVED SY

-20.730

-1.8499 SZ

-53.285

-59.501 SXY

-1.4875

-2.8964 SYZ

-6.6828

-2.5938 MAXIMUM VALUES OF SZ SORT ON ITEM=S COMPONENT=Z SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

ORDER=

0 KABS= 0 NMAX=

2

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:48 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 0.50 DAYS -

NO PAD/ROCK CONSTRAINT 2.043 NODE SX SY SZ SXY SYZ SXZ 675 203.89

-0.23631 204.77 0.10852

-0.51902E-02-0.50266E-02 674 203.89

-0.21134 204.77 0.11000 0.65581E-02 0.51627E-02 NODE SORT REMOVED MINIMUM VALUES OF SZ

==

SORT ON ITEM=S COMPONENT=Z SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

ORDER= 1 KABS=

0 NMAX=

2

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:48 FEB 10, 2003 CP=

2. 053

F-I, ENERCON F

SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006 Sheet 20 of 47 PAD RESPONSE AT END OF 0.50 DAYS -

NO PAD/ROCK CONSTRAINT NODE 1460 1461 SX

-58.101

-58.358 SY 1.7662 1.7189 Sz

-67.465

-67.453 SXY

-0.49279

-0.84714 SYZ

-4. 0126

-3.9042 SXz

-0.26920

-0. 51787 MAXIMUM VALUES OF S1

==-

SORT ON ITEM=S COMPONENT=1 SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

ORDER=

0 KABS= 0 NMAX=

2

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:48 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 0.50 DAYS -

NO PAD/ROCK CONSTRAINT 2.073 NODE S1 S2 S3 SINT SEQa 675 204.77 203.89

-0.23637 205.00 204.

674 204.77 203.89

-0.21140 204.98 204.

NODE SORT REMOVED MINIMUM VALUES OF S3 V

57 54 SORT ON ITEM=S COMPONENT=3 SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

ORDER= 1 KABS= 0 NMAX=

2

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:48 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 0.50 DAYS -

NO PAD/ROCK CONSTRAINT 2.093 NODE S1 1485 2.3224 1481 2.2139 NODE SORT REMOVED S2

-65.038

-63. 832 S3

-67. 827

-67.763 SINT 70.149 69.977 SEQV 68.797 68.097

ENERCON F 3 SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006 Sheet 21 of 47 LCASE 3

=-

LOAD CASE 3 IS LOAD STEP 3 SUBSTEP 1 COMPLEX=

0 FILE= PadNC-Th.103 PAD RESPONSE AT END OF 0.625 DAYS -

NO PAD/ROCK CONSTRAINT COPY LOAD CASE 3 FROM FILE TO DATABASE ESEL FOR LABEL= TYPE FROM 2 TO 2 BY 1

1870 ELEMENTS (OF 8812 DEFINED) SELECTED BY ESEL COMMAND.

SELECT ALL NODES HAVING ANY ELEMENT IN ELEMENT SET.

2376 NODES (OF 10212 DEFINED) SELECTED FROM 1870 SELECTED ELEMENTS BY NELE COMMAND.

MAXIMUM VALUES OF SX

==-

SORT ON ITEM=S COMPONENT=X ORDER= 0 KABS= 0 NMAX=

2 SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:49 FEB 10, 2003 CP=

2. 674 PAD RESPONSE AT END OF 0.625 DAYS -

NO PAD/ROCK CONSTRAINT NODE SX 1

299.76 672 299.76 SY

-0.30122

-0.29726 Sz 301.75 301.75 SXY SYZ SXZ

-0.30600E-01-0.49331E-02-0.36448E-02

-0.30989E-01-0.22666E-02-0.84480E-02 NODE SORT REMOVED MINIMUM VALUES OF SX SORT ON ITEM=S COMPONENT=X ORDER= 1 KABS= 0 NMAX=

2 SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1

ENERCON SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:49 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 0.625 DAYS -

NO PAD/ROCK CONSTRAINT Sheet 22 of 47 2.694 NODE SX 2805

-82.092 2108

-80.850 NODE SORT REMOVED SY

-29.545

-1.2557 Sz

-62.260

-73.077 SXY

-1.4638

-2.9251 SYZ

-7.7521

-2.8302 SXz

-0.80283

-1.4399 MAXIMUM VALUES OF SZ SORT ON ITEM=S COMPONENT=Z SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

ORDER= 0 KABS= 0 NMAX=

2

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:49 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 0.625 DAYS -

NO PAD/ROCK CONSTRAINT 2.714 NODE SX 1

299.76 672 299.76 NODE SORT REMOVED SY

-0.30122

-0.29726 SZ 301.75 301.75 SXY SYZ SXZ

-0.30600E-01-0.49331E-02-0.36448E-02

-0.30989E-01-0.22666E-02-0.84480E-02 MINIMUM VALUES OF SZ

==-

SORT ON ITEM=S COMPONENT=Z SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

ORDER= 1 KABS= 0 NMAX=

2

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:49 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 0.625 DAYS -

NO PAD/ROCK CONSTRAINT 2.724 SXz

-0.28288

-0. 54443 NODE 1460 1461 SX

-71. 615

-71. 862 SY 3.9185 3.8995 SZ

-82.074

-82.053 SXY

-0.49898

-0.87152 SYZ

-4. 5789

-4. 4690

F -t ENERCON SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006 MAXIMUM VALUES OF Si Sheet 23 of 47 SORT ON ITEM=S COMPONENT=1 ORDER= 0 KABS= 0 NMAX=

2 SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:49 FEB 10, 2003 CP=

2.744 PAD RESPONSE AT END OF 0.625 DAYS -

NO PAD/ROCK CONSTRAINT NODE Si 1

301.75 672 301.75 S2 299.76 299.76 S3

-0.30123

-0.29726 SINT 302.05 302.05 SEQV 301.06 301.06 NODE SORT REMOVED MINIMUM VALUES OF S3 SORT ON ITEM=S COMPONENT=3 ORDER= 1 KABS= 0 NMAX=

2 SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:49 FEB 10, 2003 CP=

2.764 PAD RESPONSE AT END OF 0.625 DAYS -

NO PAD/ROCK CONSTRAINT NODE 1485 1460 S1 5.0822 4.1647 S2

-79.403

-71.609 S3

-82.404

-82. 326 SINT 87.486

86. 490 SEQV 86.025

81. 661 NODE SORT REMOVED LCASE 4

=-

LOAD CASE 4 IS LOAD STEP 4

SUBSTEP 1

COMPLEX=

0

Sheet 24 of 47 F

~

ENERCON rD

, SERVICES, INC. Appendix SPadNC-TH to Calculation PGE-009-CALC-006 FILE= PadNC-Th.104 PAD RESPONSE AT END OF 1.125 DAYS - NO PAD/ROCK CONSTRAINT COPY LOAD CASE 4 FROM FILE TO DATABASE ESEL FOR LABEL= TYPE FROM 2 TO 2 BY 1

1870 ELEMENTS (OF 8812 DEFINED) SELECTED BY ESEL COMMAND.

SELECT ALL NODES HAVING ANY ELEMENT IN ELEMENT SET.

2376 NODES (OF 10212 DEFINED) SELECTED FROM 1870 SELECTED ELEMENTS BY NELE COMMAND.

MAXIMUM VALUES OF SX SORT ON ITEM=S COMPONENT=X ORDER= 0 KABS= 0 NMAX=

2 SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:49 FEB 10, 2003 CP=

3.355 PAD RESPONSE AT END OF 1.125 DAYS -

NO PAD/ROCK CONSTRAINT NODE SX SY SZ SXY SYZ SXZ 1

353.61

-0.60843 359.69

-0.41014

-0.31084

-0.23498 672 352.93

-0.50990 358.32

-0.32125

-0.26291

-0.42168 NODE SORT REMOVED MINIMUM VALUES OF SX SORT ON ITEM=S COMPONENT=X ORDER= 1 KABS= 0 NMAX=

2 SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:49 FEB 10, 2003 CP=

3.375 PAD RESPONSE AT END OF 1.125 DAYS -

NO PAD/ROCK CONSTRAINT

F.I NODE 2806 2120 Sheet 25 of 47 ENERCON SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006 SX

-189.76

-187.80 SY

-63.241

-0.31959 Sz

-135.53

-184. 55 SXY

-1.7794

-3.8514 SYZ

-1. 5128

-2. 8126 SXz 0.98109E-02

-0.48908E-01 NODE SORT REMOVED MAXIMUM VALUES OF SZ

==

SORT ON ITEM=S COMPONENT=Z ORDER= 0 KABS= 0 NMAX=

2 SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:49 FEB 10, 2003 CP=

3.385 PAD RESPONSE AT END OF 1.125 DAYS -

NO PAD/ROCK CONSTRAINT NODE SX 1

353.61 3

350.40 SY

-0.60843

-0.49481 SZ 359.69 358.49 SXY

-0.41014

-0.47728 SYZ

-0.31084

-0.19144 SXZ

-0.23498

-0.39094 NODE SORT REMOVED MINIMUM VALUES OF SZ

==

SORT ON ITEM=S COMPONENT=Z ORDER= 1 KABS= 0 NMAX=

2 SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:49 FEB 10, 2003 CP=

3.405 PAD RESPONSE AT END OF 1.125 DAYS -

NO PAD/ROCK CONSTRAINT NODE 1459 1462 SX

-183.40

-183.42 SY 8.8250 8.8236 Sz

-189. 58

-189.57 SXY

-0.53611

-0.94638 SYZ

-4. 5059

-4.3920 SXZ

-0.23094E-01

-0.44428E-01 MAXIMUM VALUES OF S1

==-

ENERCON F

SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006 Sheet 26 of 47 SORT ON ITEM=S COMPONENT=1 ORDER= 0 KABS= 0 NMAX=

2 SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE I

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:49 FEB 10, 2003 CP=

3.415 PAD RESPONSE AT END OF 1.125 DAYS -

NO PAD/ROCK CONSTRAINT NODE S1 1

359.70 3

358.51 S2 353.60 350.39 S3

-0. 60917

-0.49556 SINT 360.31 359.01 SEQV 357.30 355.01 NODE SORT REMOVED MINIMUM VALUES OF S3 SORT ON ITEM=S COMPONENT=3 ORDER= 1 KABS= 0 NMAX=

2 SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

• • • • • ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:49 FEB 10, 2003 CP=

3.435 PAD RESPONSE AT END OF 1.125 DAYS -

NO PAD/ROCK CONSTRAINT NODE 2806 1459 S1

-63.184 8.9288 S2

-135.56

-183.40 S3

-189.78

-189.68 SINT 126.60 198.61 SEQV 110.01 195. 54 NODE SORT REMOVED LCASE 5

=

LOAD CASE 5 IS LOAD STEP 5

SUBSTEP 1

COMPLEX=

0 FILE= PadNC-Th.105 PAD RESPONSE AT END OF 1.625 DAYS -

NO PAD/ROCK CONSTRAINT COPY LOAD CASE 5 FROM FILE TO DATABASE

r

~ ENERCON A'

SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006 Sheet 27 of 47 ESEL FOR LABEL= TYPE FROM 2 TO 2 BY 1

1870 ELEMENTS (OF 8812 DEFINED) SELECTED BY ESEL COMMAND.

SELECT ALL NODES HAVING ANY ELEMENT IN ELEMENT SET.

2376 NODES (OF 10212 DEFINED) SELECTED FROM 1870 SELECTED ELEMENTS BY NELE COMMAND.

MAXIMUM VALUES OF SX SORT ON ITEM=S COMPONENT=X SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

ORDER= 0 KABS= 0 NMAX=

2

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U

00245050 VERSION=INTEL NT 20:02:50 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 1.625 DAYS -

NO PAD/ROCK CONSTRAINT 4.026 SXz 5.4365 6.3827 NODE SX SY SZ SXY SYZ 2272 398.88

-11.335 404.90

-0.91894

-0.96606 2372 398.72

-3.4558 389.53

-1.0083

-1.1788 NODE SORT REMOVED MINIMUM VALUES OF SX SORT ON ITEM=S COMPONENT=X SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

ORDER= 1 KABS= 0 NMAX=

2

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:50 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 1.625 DAYS -

NO PAD/ROCK CONSTRAINT 4. 036 NODE SX 2806

-260.59 2120

-258.42 NODE SORT REMOVED SY SZ

-78.386

-191.61 0.10735E-01 -254.67 SXY

-1.7137

-3.8520 SYZ

-3.5846

-3.1475 SXz 0.17264E-01

-0.54963E-01

F 4 EENERCON

=3SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006 Sheet 28 of 47 MAXIMUM VALUES OF SZ

==-

SORT ON ITEM=S COMPONENT=Z SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

ORDER= 0 KABS= 0 NMAX=

2

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:50 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 1.625 DAYS -

NO PAD/ROCK CONSTRAINT 4.056 NODE SX 2269 359.81 2278 360.94 NODE SORT REMOVED SY

-11.708

-11.620 Sz 406.00 405.93 SXY SYZ

-0.69325E-01 -1.2247

-0.12123

-1.2066 SXz 1.1593 2.3232 MINIMUM VALUES OF SZ SORT ON ITEM=S COMPONENT=Z SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

ORDER= 1 KABS= 0 NMAX=

2

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:50 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 1.625 DAYS -

NO PAD/ROCK CONSTRAINT 4.076 SXz

-0.23474E-01

-0.45191E-01 NODE 1459 1462 SX

-253.25

-253.26 SY 12.212 12.219 Sz

-261.46

-261.44 SXY

-0. 54561

-0.96296 SYZ

-4.1101

-3.9958 MAXIMUM VALUES OF S1 SORT ON ITEM=S COMPONENT=1 SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

ORDER= 0 KABS= 0 NMAX=

2

F ENERCON SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006

• A ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:50 FEB 10, 2003 CP=

Sheet 29 of 47 4.076 PAD RESPONSE AT END OF 1.625 DAYS - NO PAD/ROCK CONSTRAINT NODE 2272 2276 S1 408.11 406.19 S2 395.68 367.84 S3

-11.340

-11. 702 SINT 419.45 417.89 SEQV 413.37 400.10 NODE SORT REMOVED MINIMUM VALUES OF S3

==

SORT ON ITEM=S COMPONENT=3 ORDER= 1 KABS= 0 NMAX=

2 SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:50 FEB 10, 2003 CP=

4.096 PAD RESPONSE AT END OF 1.625 DAYS -

NO PAD/ROCK CONSTRAINT NODE 1459 1462 S1 12.275 12.281 S2

-253.25

-253.26 S3

-261.52

-261. 50 SINT 273.79 273.78 SEQV 269.75 269.76 NODE SORT REMOVED LCASE 6 LOAD CASE 6 IS LOAD STEP 6 SUBSTEP 1 COMPLEX=

0 FILE= PadNC-Th.106 PAD RESPONSE AT END OF 2.125 DAYS -

NO PAD/ROCK CONSTRAINT COPY LOAD CASE 6 FROM FILE TO DATABASE ESEL FOR LABEL= TYPE FROM 2 TO 2 BY 1

1870 ELEMENTS (OF 8812 DEFINED) SELECTED BY ESEL COMMAND.

SELECT ALL NODES HAVING ANY ELEMENT IN ELEMENT SET.

F; -`X ENERCON Fr SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006 Sheet 30 of 47 2376 NODES (OF 10212 DEFINED) SELECTED FROM 1870 SELECTED ELEMENTS BY NELE COMMAND.

MAXIMUM VALUES OF SX SORT ON ITEM=S COMPONENT=X ORDER= 0 KABS= 0 NMAX=

2 SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:51 FEB 10, 2003 CP=

4.677 PAD RESPONSE AT END OF 2.125 DAYS -

NO PAD/ROCK CONSTRAINT NODE 2272 2372 SX 403.47 403.36 SY

-11.610

-3.1764 Sz 409.62 393.90 SXY

-1.0490

-1.1438 SYZ

-1.0118

-1.4198 SXZ 5.7236 6.7425 NODE SORT REMOVED MINIMUM VALUES OF SX SORT ON ITEM=S COMPONENT=X ORDER= 1 KABS= 0 NMAX=

2 SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:51 FEB 10, 2003 CP=

4. 687 PAD RESPONSE AT END OF 2.125 DAYS -

NO PAD/ROCK CONSTRAINT NODE 2806 2120 SX

-283.75

-281.67 SY

-80.992

-0.10820 Sz

-211.73

-277.97 SXY

-1.6811

-3.8867 SYZ

-5.4488

-3.4825 SXz 0.17635E-01

-0.60352E-01 NODE SORT REMOVED MAXIMUM VALUES OF SZ SORT ON ITRM=S COMPONENT=Z ORDER= 0 KABS= 0 NMAX=

2

-ENERCON SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006 SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:51 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 2.125 DAYS -

NO PAD/ROCK CONSTRAINT Sheet 31 of 47 NODE SX SY SZ SXY SYZ 2269 362.89

-12.071 410.85

-0.67207E-01 -1.2718 2278 364.05

-11.979 410.78

-0.12373

-1.2536 NODE SORT REMOVED MINIMUM VALUES OF SZ 1

2 4.707 sXz

.2012

..4079 SORT ON ITEM=S COMPONENT=Z SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE ORDER= 1 KABS= 0 NMAX=

2 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:51 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 2.125 DAYS -

NO PAD/ROCK CONSTRAINT 4.727 NODE 1459 1462 SX

-276.51

-276.52 SY 13.008 13. 020 SZ

-285.33

-285.31 SXY

-0.55512

-0. 97942 SYZ

-3.7740

-3. 6593 SXZ

-0.23697E-01

-0.45631E-01 MAXIMUM VALUES OF S1 SORT ON ITEM=S COMPONENT=1 ORDER=

0 KABS= 0 NMAX=

SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

2

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:51 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 2.125 DAYS -

NO PAD/ROCK CONSTRAINT 4.737

F f

ENERCON r

SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006 Sheet 32 of 47 NODE 2272 2276 Si 413.05 411.02 S2 400.05 371.10 S3

-11. 615

-12. 061 SINT 424.67 423.08 SEQV 418.32 404.60 NODE SORT REMOVED MINIMUM VALUES OF S3 SORT ON ITEM=S COMPONENT=3 ORDER= 1 KABS= 0 NMAX=

2 SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE I

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:51 FEB 10, 2003 CP=

4. 757 PAD RESPONSE AT END OF 2.125 DAYS -

NO PAD/ROCK CONSTRAINT NODE 1459 1462 S1 13.057 13. 068 S2

-276.51

-276.52 S3

-285.38

-285.36 SINT 298.43 298.43 SEQV 294.10 294.11 NODE SORT REMOVED LCASE 7

==

LOAD CASE 7 IS LOAD STEP 7 SUBSTEP 1

COMPLEX=

0 FILE= PadNC-Th.107 PAD RESPONSE AT END OF 2.375 DAYS -

NO PAD/ROCK CONSTRAINT COPY LOAD CASE 7 FROM FILE TO DATABASE ESEL FOR LABEL= TYPE FROM 2 TO 2 BY 1

1870 ELEMENTS (OF 8812 DEFINED) SELECTED BY ESEL COMMAND.

SELECT ALL NODES HAVING ANY ELEMENT IN ELEMENT SET.

2376 NODES (OF 10212 DEFINED) SELECTED FROM 1870 SELECTED ELEMENTS BY NELE COMMAND.

MAXIMUM VALUES OF SX

F -2 ENERCON

.El SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006 Sheet 33 of 47 SORT ON ITEM=S COMPONENT=X SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE ORDER= 0 KABS= 0 NMAX=

2 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:51 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 2.375 DAYS -

NO PAD/ROCK CONSTRAINT 5.348 NODE SX SY SZ SXY SYZ 2272 395.37

-11.579 401.43

-1.0775

-1.0327 2372 395.26

-3.1176 385.54

-1.1730

-1.4790 NODE SORT REMOVED MINIMUM VALUES OF SX SXZ 6.0139 7.1015 SORT ON ITEM=S COMPONENT=X SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

ORDER= 1 KABS= 0 NMAX=

2

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:51 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 2.375 DAYS - NO PAD/ROCK CONSTRAINT 5.358 NODE SX 2806

-283.45 2120

-281.48 NODE SORT REMOVED SY

-79.648

-0.23265 Sz

-212.47

-277.89 SXY

-1.7071

-3. 9865 SYZ

-6.1725

-3. 8116 SXz 0.16274E-01

-0.65530E-01 MAXIMUM VALUES OF SZ

=

SORT ON ITEM=S COMPONENT=Z SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE ORDER= 0 KABS= 0 NMAX=

2 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U

ENERCON SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006 00245050 VERSION=INTEL NT 20:02:51 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 2.375 DAYS -

NO PAD/ROCK CONSTRAINT Sheet 34 of 47 5.378 NODE SX 2269 353.94 2278 355.13 NODE SORT REMOVED SY

-12.068

-11.976 Sz 402.91 402. 83 SXY SYZ

-0.69059E-01 -1.2941

-0.12581

-1.2759 SXz 1.2434 2.4932 MINIMUM VALUES OF SZ

=

SORT ON ITEM=S COMPONENT=Z SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

ORDER= 1 KABS= 0 NMAX=

2

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:51 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 2.375 DAYS -

NO PAD/ROCK CONSTRAINT 5.398 SXz

-0.23887E-01

-0.46000E-01 NODE 1459 1462 SX

-276.45

-276.46 SY 12.822 12.835 Sz

-285.24

-285.22 SXY

-0.56491

-0.99619 SYZ

-3.7470

-3. 6319 MAXIMUM VALUES OF S1 SORT ON ITEM=S COMPONENT=1 SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

ORDER= 0 KABS= 0 NMAX=

2

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:51 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 2.375 DAYS - NO PAD/ROCK CONSTRAINT 5.398 NODE S1 2272 405.14 2276 403.07 NODE SORT REMOVED S2 391.67 362.31 S3

-11.584

-12.058 SINT 416.73 415.13 SEQV 410.16 396.32

F-I tENERCON F1 SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006 Sheet 35 of 47 MINIMUM VALUES OF S3 SORT ON ITEM=S COMPONENT=3 SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

ORDER= 1 KABS= 0 NMAX=

2

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:51 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 2.375 DAYS -

NO PAD/ROCK CONSTRAINT 5.418 NODE Si 1459 12.870 1462 12.883 NODE SORT REMOVED S2

-276.45

-276.47 S3

-285.29

-285. 27 SINT 298.16 298.15 SEQV 293. 84 293.85 LCASE 8

==-

LOAD CASE 8 IS LOAD STEP 8

SUBSTEP 1

COMPLEX=

0 FILE= PadNC-Th.108 PAD RESPONSE AT END OF 3.125 DAYS -

NO PAD/ROCK CONSTRAINT COPY LOAD CASE 8 FROM FILE TO DATABASE ESEL FOR LABEL= TYPE FROM 2 TO 2 BY 1

1870 ELEMENTS (OF 8812 DEFINED) SELECTED BY ESEL CC SELECT ALL NODES HAVING ANY ELEMENT IN ELEMENT SET.

2376 NODES (OF 10212 DEFINED) SELECTED FROM 1870 SELECTED ELEMENTS BY NELE COMMAND.

MAXIMUM VALUES OF SX

)MMAND.

2 JMAX=

SORT ON ITEM=S COMPONENT=X SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

ORDER= 0 KABS= 0 IN

E I ENERCON M.

SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:52 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 3.125 DAYS -

NO PAD/ROCK CONSTRAINT Sheet 36 of 47 NODE SX 2272 342.19 2372 342.11 NODE SORT REMOVED SY

-11.076

-3.1392 SZ 347.67 332.46 SXY

-1.0610

-1.1518 SYZ

-1. 0171

-1.4763 6

7

6. 009

Xz

.3125

.4643 MINIMUM VALUES OF SX SORT ON ITEM=S COMPONENT=X SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

ORDER= 1 KABS= 0 NMAX=

2

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:52 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 3.125 DAYS -

NO PAD/ROCK CONSTRAINT 6.029 NODE SX 2806 -255.91 2120 -254.35 NODE SORT REMOVED SY

-69.317

-0.77977 SZ

-193.96

-251.34 SXY

-1.7156

-4.0655 SYZ

-7.4772

-4.1444 SXz 0.94392E-02

-0.70234E-01 MAXIMUM VALUES OF SZ

==

SORT ON ITEM=S COMPONENT=Z SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

ORDER= 0 KABS= 0 NMAX=

2

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:52 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 3.125 DAYS -

NO PAD/ROCK CONSTRAINT 6.039 NODE SX SY SZ SXY SYZ SXZ

F-s ENERCON F

- M SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006 Sheet 37 of 47 2269 300.75 2278 301.97

-11. 614

-11. 522 349.54

-0.72289E-01 -1.2803 349.45

-0.12781

-1.2621 1.2856

2. 5786 NODE SORT REMOVED MINIMUM VALUES OF SZ

==

SORT ON ITEM=S COMPONENT=Z ORDER= 1 KABS= 0 NMAX=

2 SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:52 FEB 10, 2003 CP=

6. 059 PAD RESPONSE AT END OF 3.125 DAYS NO PAD/ROCK CONSTRAINT NODE 1459 1462 SX

-250.10

-250.11 SY

10. 891

10. 906 Sz

-258.01

-257.99 SXY

-0.57442

-1.0128 SYZ

-3. 5651

-3.4495 SXZ

-0. 23954E-01

-0.46122E-01 MAXIMUM VALUES OF S1 SORT ON ITEM=S COMPONENT=1 ORDER= 0 KABS= 0 NMAX=

2 SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:52 FEB 10, 2003 CP=

6.069 PAD RESPONSE AT END OF 3.125 DAYS -

NO PAD/ROCK CONSTRAINT NODE 2272 2276 S1 351.82 349.71 S2 338.05 309.24 S3

-11. 082

-11.605 SINT 362.90 361.32 SEQV 356.22 342.88 NODE SORT REMOVED MINIMUM VALUES OF S3 SORT ON ITEM=S COMPONENT=3 ORDER= 1 KABS= 0 NMAX=

2

F-3 I

p S

C t

ENERCON F

I SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006 Sheet 38 of 47 SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:52 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 3.125 DAYS -

NO PAD/ROCK CONSTRAINT 6.089 NODE S1 1721

-32.225 1459 10.940 NODE SORT REMOVED S2

-250.67

-250.10 S3

-258.72

-258.05 SINT 226.49 268.99 SEQV 222.58 265.11 LCASE 9 LOAD CASE 9 IS LOAD STEP 9

SUBSTEP 1

COMPLEX=

0 FILE= PadNC-Th.109 PAD RESPONSE AT END OF 4.125 DAYS -

NO PAD/ROCK CONSTRAINT COPY LOAD ESEL FOR 1870 SELECT 2376 1870

) CASE 9 FROM FILE TO DATABASE t LABEL= TYPE FROM 2 TO 2 BY ELEMENTS (OF 8812 DEFINED) SELECTED BY E

ALL NODES HAVING ANY ELEMENT IN ELEMENT SET.

NODES (OF 10212 DEFINED) SELECTED FROM SELECTED ELEMENTS BY NELE COMMAND.

1 ISEL COMMAND.

MAXIMUM VALUES OF SX SORT ON ITEM=S COMPONENT=X SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE ORDER= 0 KABS= 0 NMAX=

2 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:53 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 4.125 DAYS - NO PAD/ROCK CONSTRAINT 6.670

Sheet 39 of 47 E

']

ENERCON E

SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006 NODE SX SY SZ SXY SYZ SXZ 2372 235.81

-3.4244 226.65

-1.0100

-1.3203 7.8295 2272 235.81

-9.9488 239.91

-0.93263

-0.91506 6.6227 NODE SORT REMOVED MINIMUM VALUES OF SX

==-

SORT ON ITEM=S COMPONENT=X ORDER= 1 KABS= 0 NMAX=

2 SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:53 FEB 10, 2003 CP=

6.690 PAD RESPONSE AT END OF 4.125 DAYS -

NO PAD/ROCK CONSTRAINT NODE SX SY SZ SXY SYZ SXZ 72

-211.18

-49.944

-217.91

-10.719

-8.1540

-0.54385 77

-211.00

-26.764

-216.44

-13.892

-5.4226

-0.56553 NODE SORT REMOVED MAXIMUM VALUES OF SZ

==-

SORT ON ITEM=S COMPONENT=Z ORDER= 0 KABS= 0 NMAX=

2 SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U

00245050 VERSION=INTEL NT 20:02:53 FEB 10, 2003 CP=

6.710 PAD RESPONSE AT END OF 4.125 DAYS -

NO PAD/ROCK CONSTRAINT NODE SX SY SZ SXY SYZ SXZ 27 229.27

-4.4456 247.54

-3.4903

-2.6630

-0.65711 30 223.53

-2.9182 245.09

-5.1647

-2.0503

-1.0563 NODE SORT REMOVED

W`i~ '-li ;-

ENERCON F

I SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006

=== MINIMUM VALUES OF SZ Sheet 40 of 47 SORT ON ITEM=S COMPONENT=Z SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE I

ORDER= 1 KABS= 0 NMAX=

2

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:53 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 4.125 DAYS -

NO PAD/ROCK CONSTRAINT 6.720 SXZ

-0.70701

-0. 54385 NODE SX 1721

-210.24 72

-211.18 SY

-34. 037

-4 9. 944 Sz

-218.37

-217. 91 SXY

-8.4071

-10.719 SYZ

-11.644

-8.1540 MAXIMUM VALUES OF S1

==

SORT ON ITEM=S COMPONENT=I SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE ORDER= 0 KABS= 0 NMAX=

2 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:53 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 4.125 DAYS -

NO PAD/ROCK CONSTRAINT 6.740 NODE S1 S2 S3 SINT SEQV 27 247.59 229.30

-4.5260 252.11 243.48 30 245.16 223.61

-3.0532 248.21 238.17 NODE SORT REMOVED MINIMUM VALUES OF S3

=-

SORT ON ITEM=S COMPONENT=3 SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

ORDER= 1 KABS= 0 NMAX=

2

F

^ EENERCON SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006 ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:53 FEB 10, 2003 CP=

Sheet 41 of 47 6.750 PAD RESPONSE AT END OF 4.125 DAYS -

NO PAD/ROCK CONSTRAINT NODE 1721 72 S1

-32.912

-48.846 S2

-210.46

-211.72 S3

-219.28

-218.48 SINT 186.36 169. 63 SEQV 182.12 166.35 NODE SORT REMOVED LCASE 10 LOAD CASE 10 IS LOAD STEP 10 SUBSTEP 1

COMPLEX=

0 FILE= PadNC-Th.110 PAD RESPONSE AT END OF 6.125 DAYS -

NO PAD/ROCK CONSTRAINT COPY LOAD CASE 10 FROM FILE TO DATABASE ESEL FOR LABEL= TYPE FROM 2 TO 2 BY 1

1870 ELEMENTS (OF 8812 DEFINED) SELECTED BY ESEL COMMAND.

SELECT ALL NODES HAVING ANY ELEMENT IN ELEMENT SET.

2376 NODES (OF 10212 DEFINED) SELECTED FROM 1870 SELECTED ELEMENTS BY NELE COMMAND.

I MAXIMUM VALUES OF SX

==-

SORT ON ITEM=S COMPONENT=X ORDER= 0 KABS= 0 NMAX=

2 SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U

00245050 VERSION=INTEL NT 20:02:54 FEB 10, 2003 CP=

7.351 PAD RESPONSE AT END OF 6.125 DAYS -

NO PAD/ROCK CONSTRAINT NODE SX 27 138.48 1036 136.91 SY

-4.4393

-3. 5174 Sz 152.12 148.78 SXY

-3.4992

-3.0012 SYZ

-2.6595

-3.9136 SXz

-0.66283

-1.1360

F-t ENERCON SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006 NODE SORT REMOVED MINIMUM VALUES OF SX Sheet 42 of 47 SORT ON ITEM=S COMPONENT=X SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

ORDER= 1 KABS= 0 NMAX=

2

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:54 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 6.125 DAYS -

NO PAD/ROCK CONSTRAINT 7.361 NODE SX 626

-154.35 10

-154.14 NODE SORT REMOVED SY

-1.2115

-0.91699 Sz

-145.31

-66. 530 SXY

-1.5803

-1.8844 SYZ SXZ

-0.80210

-9.5406

-0.17290E-01-0.72947 MAXIMUM VALUES OF SZ

=

SORT ON ITEM=S COMPONENT=Z SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

ORDER= 0 KABS= 0 NMAX=

2

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:54 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 6.125 DAYS - NO PAD/ROCK CONSTRAINT 7.371 SXz

-0.66283

-1.0677 NODE SX SY SZ SXY SYZ 27 138.48

-4.4393 152.12

-3.4992

-2.6595 30 132.79

-2.9314 149.67

-5.1556

-2.0468 NODE SORT REMOVED MINIMUM VALUES OF SZ SORT ON ITEM=S SORT COMPLETED FOR COMPONENT=Z 2 VALUES.

ORDER= 1 KABS= 0 NMAX=

2

F.:^

E1NERCON SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006 PRINT S NODAL SOLUTION PER NODE Sheet 43 of 47 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:54 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 6.125 DAYS -

NO PAD/ROCK CONSTRAINT 7.391 SXz

-1.5963

-3.2170 NODE 617 619 SX

-109.75

-110.78 SY

-0. 57142

-0.46729 SZ

-147.28

-147.11 SXY

-0.25007

-0.10968 SYZ

-1.2211

-1.2071 MAXIMUM VALUES OF S1

==-

SORT ON ITEM=S COMPONENT=1 SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

ORDER= 0 KABS= 0 NMAX=

2

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:54 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 6.125 DAYS -

NO PAD/ROCK CONSTRAINT 7.411 NODE S1 27 152.19 30 149.75 NODE SORT REMOVED S2 138.54 132.93 S3

-4.5706

-3.1554 SINT 156.76 152.91 SEQV 150.40 145.23 MINIMUM VALUES OF S3

==-

SORT ON ITEM=S COMPONENT=3 SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

ORDER= 1 KABS= 0 NMAX=

2

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:54 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 6.125 DAYS -

NO PAD/ROCK CONSTRAINT 7.431

ENERCON F

SERVICES, INC. Appendix SPadNC-TH to Calculation PGE-009-CALC-006 Sheet 44 of 47 NODE Si 626

-1.1917 838 -0.99112 S2

-139.28

-128.57 S3

-160.41

-158.22 SINT 159.22 157.23 SEQV 149.77 144.70 NODE SORT REMOVED LCASE 11 LOAD CASE 11 IS LOAD STEP 11 SUBSTEP 1

COMPLEX=

0 FILE= PadNC-Th.111 PAD RESPONSE AT END OF 7.875 DAYS -

NO PAD/ROCK CONSTRAINT COPY LOAD CASE 11 FROM FILE TO DATABASE ESEL FOR LABEL= TYPE FROM 2 TO 2 BY 1

1870 ELEMENTS (OF 8812 DEFINED) SELECTED BY ESEL COMMAND.

SELECT ALL NODES HAVING ANY ELEMENT IN ELEMENT SET.

2376 NODES (OF 10212 DEFINED) SELECTED FROM 1870 SELECTED ELEMENTS BY NELE COMMAND.

MAXIMUM VALUES OF SX

==-

SORT ON ITEM=S COMPONENT=X ORDER= 0 KABS= 0 NMAX=

2 SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:54 FEB 10, 2003 CP=

7.991 PAD RESPONSE AT END OF 7.875 DAYS -

NO PAD/ROCK CONSTRAINT NODE 16 686 SX 124.36 123.49 SY

-12.632

-9.6027 Sz 130.47 128.27 SXY

-5.9337

-5.1316 SYZ

-4.3237

-6.8596 SXz

-0.52056

-0.85729 NODE SORT REMOVED MINIMUM VALUES OF SX

F 1 i ENERCON SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006 Sheet 45 of 47 SORT ON ITEM=S COMPONENT=X SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

ORDER= 1 KABS= 0 NMAX=

2

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:54 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 7.875 DAYS -

NO PAD/ROCK CONSTRAINT 8.002 SXz

-13.423

-13.497 NODE SX SY SZ SXY SYZ 626

-219.67 1.0790

-218.16

-0.39386

-0.71404 838

-218.41 0.13874

-204.64

-0.50244

-0.58385 NODE SORT REMOVED MAXIMUM VALUES OF SZ

==-

SORT ON ITEM=S COMPONENT=Z SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

ORDER= 0 KABS= 0 NMAX=

2

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:54 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 7.875 DAYS - NO PAD/ROCK CONSTRAINT

8. 022 SXz

-0.52056

-0.79402 NODE SX 16 124.36 25 120.66 NODE SORT REMOVED SY

-12.632

-8.1530 SZ 130.47 129. 08 SXY

-5. 9337

-9. 0045 SYZ

-4.3237

-3.3686 MINIMUM VALUES OF SZ SORT ON ITEM=S COMPONENT=Z SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

ORDER= 1 KABS= 0 NMAX=

2

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U

F~^ ENERCON SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006 00245050 VERSION=INTEL NT 20:02:54 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 7.875 DAYS -

NO PAD/ROCK CONSTRAINT Sheet 46 of 47 8.042 SXz

.8290

.6986 NODE 617 619 SX

-182.90

-183.90 SY 0.52607 0.62185 Sz

-219.88

-219.73 SXY

-0.25679

-0.10547 SYZ

-1.1713

-1.1572

-1

-3 MAXIMUM VALUES OF S1 SORT ON ITEM=S COMPONENT=1 SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE 1

ORDER= 0 KABS= 0 NMAX=

2

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:54 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 7.875 DAYS -

NO PAD/ROCK CONSTRAINT

8. 062 NODE S1 16 130.62 25 129.21 NODE SORT REMOVED S2 124.60 121.25 S3

-13.020

-8.8639 SINT 143. 64 138.07 SEQV 140.73 134.27 MINIMUM VALUES OF S3 SORT ON ITEM=S COMPONENT=3 SORT COMPLETED FOR 2 VALUES.

PRINT S NODAL SOLUTION PER NODE ORDER= 1 KABS= 0 NMAX=

2 1

• • • • • ANSYS -

ENGINEERING ANALYSIS SYSTEM RELEASE 6.1 ANSYS/Mechanical U 00245050 VERSION=INTEL NT 20:02:54 FEB 10, 2003 CP=

PAD RESPONSE AT END OF 7.875 DAYS -

NO PAD/ROCK CONSTRAINT 8.082 NODE S1 626 1.0819 625 0.69327 NODE SORT REMOVED S2

-205. 47

-201.40 S3

-232.36

-229. 56 SINT 233.45 230.26 SEQV 221.23 217. 55

ENERCON E SERVICES, INC.

Appendix SPadNC-TH to Calculation PGE-009-CALC-006 Sheet 47 of 47 8812 ELEMENTS (OF 10212 NODES (OF 8812 DEFINED) SELECTED BY EALL COMMAND.

10212 DEFINED) SELECTED BY NALL COMMAND.

EXIT THE ANSYS POSTI DATABASE PROCESSOR

• • • • • ROUTINE COMPLETED *****

CP =

8. 082 EXIT ANSYS WITHOUT SAVING DATABASE NUMBER OF WARNING MESSAGES ENCOUNTERED=

NUMBER OF ERROR MESSAGES ENCOUNTERED=

2 0

___________________________________________________Y___RUN____CO___PLETED__*

I ANSYS RUN COMPLETED I

Release 6.1 UP20020321 INTEL NT Maximum Scratch Memory Used

=

1035636 Words 3.951 MB CP Time (sec) =

Elapsed Time (sec) =

8. 092 11.000 Time =

20:02:55 Date

=

02/10/2003

ENERCON I

SERVICES, INC. Appendix LSPadNC-TH to Calculation PGE-009-CALC-006 Sheet 1 of 7 Originator:

Date:

AS.

C. umminelli March 3, 2003 Appendix LSPadNC-TH This Appendix presents the ANSYS plots of the pad vertical displacements for the unconstrained thermal stress analysis for the individual load steps.

Sheet 2 of 7 F3 I

ENERCON SERVICES, INC.

Appendix LSPadNC-TH to Calculation PGE-009-CALC-006 S-EP=;,

SU'

=E TI.ME =_

-.4"

=~

=f rI2 i

=,

7C5 SNYN =-.0'221 AN l 5: 22:

-. UUizzi

. VJUj3q UV 1

.e4r-04

.CO2612

.0051E7 DELTA T D.0 TO 0.25 DAYS -

NO PAD/ROCK CONSTRAINT

.* UL

.07'722

.0i0277 Figure LSNC Time 0.00 to 0.25 days NCrA1 SCITEO S-EP=2 SUB =7 TIME=2

-SY tA'*<'8 RSYS=C' DEM =. 132f13 SHN =.15C-03 SMX =.067f.4 AN FEEB 10 2;03 15:23 :0

.150-1152

.2-93

.0477

.0*-

75SE

.'22465

.037341 DELTA T 0.25 TO 0.50 DAYS -

NO PAD/ROCK CONSTRAINT

.0551656

.05221F

.5i7C94 Figure LSNC Time 0.25 to 0.50 days

Sheet 3 of 7 IFI1 ENERCON SERVICES, INC.

Appendix LSPadNC-TH to Calculation PGE-009-CALC-006 SUB =c l;ME=`

• _ Y

' AV':,

rM: =.1jMs21 S.YI =.1*61E-;'

ce-, =.0163"'

AN FS.

10 1203 I; '2?:24 X L-

.46 JE-53

.0a3959

.0753T

.5V223

.$-057fz

.003: ' 5 DELTA 7 0.50 TO C.625 DAYS -

NO PAD/ROCK CONSTRAINT

.011074

. oi4lz

.012S43

.014391 Figure LSNC Time 0.50 to 0.625 days 241A.

sc:FTIxn AN SFE-10 25403 S M -=19

.23: 4J FSB =8 T1349=4 JY WI'G!

.RSYSC=

rS *35F7 DELTA 7 0.625 TO 1.125 DAYS -

NO PAD/ROCK CONSTRAINT Figure LSNC Time 0.625 to 1.125 days L.6

Sheet 4 of 7 F

~ ENERCON I 3 SERVICES, INC.

Appendix LSPadNC-TH to Calculation PGE-009-CALC-006 I

N, D k

I S-rp=

j SUP =

,I P1 =

I ':'Y FSY'S=

I SYN =

zSSc =

IL SCBS-ION

= -

3E

=.19: 35 N

FE3 10 2;1)3 1R:2I:5E JI

.001088

.044259

.08743

.130601

.173772

.022674

.065845

.109016

.1521Re

.195357 T 1.125 TO 1.625 DAYS -

NO PAD/ROCK CONSTRAINT Figure LSNC Time 1.125 to 1.625 days 5I' :z SC;U-ION s1:

.r=i SY (AAV)

RSYS=O DHX =. 101347 SXN. 55E-03 SMX =. 1C114 X

.55E-03

.022879

.011717 DELTA T 1.625 TO 2.125 DAYS -

AN FEB 10 2IO3 1? 24:13

.045203

.045203

.C34041

.056365 NO PAD/ROCK CONSTRAINT nasP

.UtIDZ I

.078689

. os.ses Figure LSNC Time 1.625 to 2.125 days

('01

)

Sheet 5 of 7 F'j

[ENERCON Fl 3 SERVICES, INC.

Appendix LSPadNC-TH to Calculation PGE-009-CALC-006

ScDAL SCiZ-IOS S-EP=7 SUB =E IY (AV; RSYS=0 MX =.02?40p 656-E-04 DELV 1'2.2 I, X=.j>2-243 i

I II.

X.

I

_6CE0 l DELTA T 2. 125 '.

AN FEB 10J 2.03

.10611i5

.012145 I

.06155

.Cl2145

.003Dr5

.009125

.015164 rO 2.3'5 DAYS -

NO PADIROCK CONSTRAINT n.sorc

1. weneX

.021204

.0272:3 Figure LSNC Time 2.125 to 2.375 days AN SC1P.1 SCLVRICB FEB 10 2C0b3 SUEp=E 15:24:46 SUB =

TI!5S=E UY WAVJ R SY=0 DX =.'5457 SMB =-.174E-~3 X'E

-. 1764-0

.c'

'Sn

.t23925

.035g 4

.349023 DELA249

.34T95

.254t45 DELTIA T 2.375 TO 3.125 DAYS -

NO PAD/ROCK CONSTRAINT Figure LSNC Time 2.375 to 3.125 days C~f

Sheet 6 of 7 F'j ENERCON I 3SERVICES, INC.

J t 3 Appendix LSPadNC-TH to Calculation PGE-009-CALC-006 IINCA

'S C'.U-ONS SUB =e

..E i

Y =.0223071 SICM =-..11114

-t i x=.Cel;2E2 AN IEE 10

. 03

-. 001114

. ^l041;

.03942

.1I5LE-03

.C0267S

.005206 DELTA T 3.125 TO 4.125 DAYS -

N4O PAD/ROCK CONSTRAINT

.00647

.00fS0e

.007734 Figure LSNC Time 3.125 to 4.125 days MDA3L SCGMION AN SF=l0 10 203 SUB =7 TIME=10 UY WAVO)

RSYS=O DS4X =.037463 0143 =.037463

-. 007154

.002761 12676 2-9

-032505 D.002191

.00N71e

.R17633

.027545

.037463 DELTA T 4.125 TO 6.125 DAYS NO PAD/ROCR CONSTRAINT Figure LSNC Time 4.125 to 6.125 days C,o 5-

Sheet 7 of 7 3

ENERCON SERVICES, INC.

Appendix LSPadNC-TH to Calculation PGE-009-CALC-006 NCDAL SC14 7O';

SUB =Y T IME= 1 DWX9 =.0474?9?

SHN =-.)r5S,71 SMz =.Ft4'439 AN E~B 10 2-03 1-:2: 41

-.OO57I

.C'0598B

.01754B

-. 005971 0c35.17849

. 52E-04

.0:1919

.023779 DELTA T 6.125 TO 7.875 DAYS -

10 PAD/ROCK CONSTRAINT

.035E!B

.04749 Figure LSNC Time 6.125 to 7.875 days COG