-
Notifications
You must be signed in to change notification settings - Fork 0
Expand file tree
/
Copy pathSDC-IC_Mat_Lib.mac
More file actions
6629 lines (6020 loc) · 259 KB
/
SDC-IC_Mat_Lib.mac
File metadata and controls
6629 lines (6020 loc) · 259 KB
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
57
58
59
60
61
62
63
64
65
66
67
68
69
70
71
72
73
74
75
76
77
78
79
80
81
82
83
84
85
86
87
88
89
90
91
92
93
94
95
96
97
98
99
100
101
102
103
104
105
106
107
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
148
149
150
151
152
153
154
155
156
157
158
159
160
161
162
163
164
165
166
167
168
169
170
171
172
173
174
175
176
177
178
179
180
181
182
183
184
185
186
187
188
189
190
191
192
193
194
195
196
197
198
199
200
201
202
203
204
205
206
207
208
209
210
211
212
213
214
215
216
217
218
219
220
221
222
223
224
225
226
227
228
229
230
231
232
233
234
235
236
237
238
239
240
241
242
243
244
245
246
247
248
249
250
251
252
253
254
255
256
257
258
259
260
261
262
263
264
265
266
267
268
269
270
271
272
273
274
275
276
277
278
279
280
281
282
283
284
285
286
287
288
289
290
291
292
293
294
295
296
297
298
299
300
301
302
303
304
305
306
307
308
309
310
311
312
313
314
315
316
317
318
319
320
321
322
323
324
325
326
327
328
329
330
331
332
333
334
335
336
337
338
339
340
341
342
343
344
345
346
347
348
349
350
351
352
353
354
355
356
357
358
359
360
361
362
363
364
365
366
367
368
369
370
371
372
373
374
375
376
377
378
379
380
381
382
383
384
385
386
387
388
389
390
391
392
393
394
395
396
397
398
399
400
401
402
403
404
405
406
407
408
409
410
411
412
413
414
415
416
417
418
419
420
421
422
423
424
425
426
427
428
429
430
431
432
433
434
435
436
437
438
439
440
441
442
443
444
445
446
447
448
449
450
451
452
453
454
455
456
457
458
459
460
461
462
463
464
465
466
467
468
469
470
471
472
473
474
475
476
477
478
479
480
481
482
483
484
485
486
487
488
489
490
491
492
493
494
495
496
497
498
499
500
501
502
503
504
505
506
507
508
509
510
511
512
513
514
515
516
517
518
519
520
521
522
523
524
525
526
527
528
529
530
531
532
533
534
535
536
537
538
539
540
541
542
543
544
545
546
547
548
549
550
551
552
553
554
555
556
557
558
559
560
561
562
563
564
565
566
567
568
569
570
571
572
573
574
575
576
577
578
579
580
581
582
583
584
585
586
587
588
589
590
591
592
593
594
595
596
597
598
599
600
601
602
603
604
605
606
607
608
609
610
611
612
613
614
615
616
617
618
619
620
621
622
623
624
625
626
627
628
629
630
631
632
633
634
635
636
637
638
639
640
641
642
643
644
645
646
647
648
649
650
651
652
653
654
655
656
657
658
659
660
661
662
663
664
665
666
667
668
669
670
671
672
673
674
675
676
677
678
679
680
681
682
683
684
685
686
687
688
689
690
691
692
693
694
695
696
697
698
699
700
701
702
703
704
705
706
707
708
709
710
711
712
713
714
715
716
717
718
719
720
721
722
723
724
725
726
727
728
729
730
731
732
733
734
735
736
737
738
739
740
741
742
743
744
745
746
747
748
749
750
751
752
753
754
755
756
757
758
759
760
761
762
763
764
765
766
767
768
769
770
771
772
773
774
775
776
777
778
779
780
781
782
783
784
785
786
787
788
789
790
791
792
793
794
795
796
797
798
799
800
801
802
803
804
805
806
807
808
809
810
811
812
813
814
815
816
817
818
819
820
821
822
823
824
825
826
827
828
829
830
831
832
833
834
835
836
837
838
839
840
841
842
843
844
845
846
847
848
849
850
851
852
853
854
855
856
857
858
859
860
861
862
863
864
865
866
867
868
869
870
871
872
873
874
875
876
877
878
879
880
881
882
883
884
885
886
887
888
889
890
891
892
893
894
895
896
897
898
899
900
901
902
903
904
905
906
907
908
909
910
911
912
913
914
915
916
917
918
919
920
921
922
923
924
925
926
927
928
929
930
931
932
933
934
935
936
937
938
939
940
941
942
943
944
945
946
947
948
949
950
951
952
953
954
955
956
957
958
959
960
961
962
963
964
965
966
967
968
969
970
971
972
973
974
975
976
977
978
979
980
981
982
983
984
985
986
987
988
989
990
991
992
993
994
995
996
997
998
999
1000
! ###################################################################################################### !
! !
! Copyright 2019 F4E | European Joint Undertaking for ITER and the Development !
! of Fusion Energy (‘Fusion for Energy’). Licensed under the EUPL, Version 1.2 !
! or - as soon they will be approved by the European Commission - subsequent versions !
! of the EUPL (the “Licence”). You may not use this work except in compliance !
! with the Licence. You may obtain a copy of the Licence at: http://ec.europa.eu/idabc/eupl.html !
! Unless required by applicable law or agreed to in writing, software distributed !
! under the Licence is distributed on an “AS IS” basis, WITHOUT WARRANTIES !
! OR CONDITIONS OF ANY KIND, either express or implied. See the Licence permissions !
! and limitations under the Licence. !
! !
! ###################################################################################################### !
! MATLIB,MAT_NAME,MAT_NUMB,PROP1,PROP2,PROP3....
! Defines a material included in the Structural Design Criteria for ITER In-vessel Components (SDC-IC), Appendix A - Material Design Limit Data
! MAT_NAME - material name as indicated below under the title "List of materials". Only needed if MAT_NUMB is not supplied
! MAT_NUMB - material number as indicated below under the title "List of materials". Only needed if MAT_NAME is not supplied
! PROP1,PROP2,...,PROP17 - Properties of the material with the tags indicated below the title "List of properties available" and subsection "List of properties available for each material"
!!!!!!!!!!!!!!!!!!!! How to use this macro !!!!!!!!!!!!!!!!!!!!
!! List of steps
! The macro can be called as an usual ANSYS macro with the command *USE, Name, ARG1, ARG2, ARG3, ARG4,
! The list of steps for the use of the macro it's explained below.
! 1) Select MAT_NAME or MAT_NUMB corresponding to the desired material. Both variables are specified below in the
! section with the title "List of materials" . Only one of the two variables is needed, the other can be left blank.
! MAT_NAME input variable has to be a string parameter. MAT_NUMB input variable has to be a scalar parameter
! The numbers of the material are fixed and this can't be changed.
! Only one material can be defined for each execution of the macro.
! 2) Select the desired properties to be defined in material model. The name of the properties is specified below in the
! section "List of properties available" under the title "List of properties available for each material".
! General information about the properties can be found in the same section under the title "Properties for the material model" and "Other properties".
! There are two type of properties that can be defined: Properties for the material model and Other properties.
! The properties for the material model are included in the material model that ANSYS use to describe the behaviour of the material.
! The Other properties are properties not included in the material model but which may be used for post-processing tasks
! The input properties parameters have to be string parameters.
! Up to 17 properties can be defined in each run of the macro. The combination of the properties has to be coherent. If some properties are not compatible
! an ANSYS error will be raised.
! The numbers of the materials already defined are stored in the variables MAT_TAG, which allows an easy usage of the material (Material assignment, modifications in the material model ...)
! The MAT_TAG variables are specified below in the section with the title "List of materials"
!! Examples of use
! The three lines below produce the same output
! *USE, MATLIB.mac,'304L Stainless Steel',,'EX','C','ALPX','PRXY','KXX','DENS','MISO'
! *USE, MATLIB.mac,,101,'EX', 'ALPX','PRXY','KXX','DENS','MISO'
! *USE, MATLIB.mac,'304L Stainless Steel',101,'EX','ALPX','PRXY','KXX','DENS','MISO'
! Defining material model properties and other properties
! *USE, MATLIB.mac,,107,'ALPX','PRXY','KXX','DENS','BISO','SY_MIN_107','SU_MIN_107'
!!!!!!!!!!!!!!!!!!! List of materials !!!!!!!!!!!!!!!!!!!
! MAT_NUMB - MAT_NAME - MAT_TAG !
! !
! 101 - 304L Stainless Steel - MAT_SS304 !
! 102 - 316L Stainless Steel - MAT_SS316 !
! 103 - 316L (N-IG) Stainless Steel - MAT_SS316_NIG !
! 104 - GRADE 660 Stainless Steel - MAT_SS660 !
! 105 - XM-19 Steel - MAT_XM19 !
! 106 - Alloy 625 - MAT_ALLOY625 !
! 107 - Ti-6Al-4V Alloy - MAT_TI64 !
! 108 - Pure Copper - MAT_CU !
! 109 - Copper-Chromium-Zirconium Alloy - MAT_CUCRZR !
! 110 - Dispersion-Strengthened Copper - MAT_CUAL25=110 !
! 111 - Aluminium-Nickel Bronze - MAT_ALNIBRZ !
! 112 - Alloy 718 - MAT_INCONEL718 !
! 113 - Beryllium - MAT_BERYLLIUM !
! 114 - Tungsten - MAT_TUNGSTEN !
! 115 - CFC EU Grade - MAT_CFC_EU !
! 116 - CFC CX-2002U Grade - MAT_CFC_CX !
!!!!!!!!!!!!!!!!!!! List of properties available !!!!!!!!!!!!!!!!!!!
!! Properties for the material model
! ALPX- Mean,average or secant coefficient of thermal expansion
! CTEX- Instantaneous coefficient of thermal expansion
! EX- Young Modulus
! PRXY- Poisson's ratio
! DENS- Mass density
! KXX- Conductivity
! C- Specific heat
! MELAS- Stress-strain elastic curves. Nonlinear structural, multilinear elastic.
! BISO- Isotropic hardening plasticity. Bilinear stress-strain curves.
! MISO- Isotropic hardening plasticity. Multilinear stress-strain curves.
! BKIN- Kinematic hardening plasticity. Bilinear stress-strain curves.
! KINH- Kinematic hardening plasticity. Multilinear stress-strain curves.
!! Other properties
! SY_MIN - Minimum yield strength
! SY_AV - Average yield strength
! SU_MIN - Minimum tensile strength
! SU_AV - Average tensile strength
! SY_IRR_MIN - Minimum yield strength. Material irradiated
! SY_IRR_AV - Average yield strength. Material irradiated
! SU_IRR_MIN - Minimum tensile strength. Material irradiated
! SU_IRR_AV - Average tensile strength. Material irradiated
! ETOT_MIN - Minimum total elongation
! ETOT_AV - Average total elongation
! EUNIF_MIN - Minimum uniform elongation
! EUNIF_AV - Average uniform elongation
! ETOT_IRR_MIN - Minimum total elongation. Material irradiated
! ETOT_IRR_AV - Average total elongation. Material irradiated
! EUNIF_IRR_MIN - Minimum uniform elongation. Material irradiated
! EUNIF_IRR_AV - Average uniform elongation. Material irradiated
! STRAIN_RUPT_MIN - Minimum true strain at rupture
! STRAIN_RUPT_AV - Average true strain at rupture
! SM - Allowable stress intensity
! SMB - Design stress intensity for bolt materials
! SE_IRR - Allowable stress for the primary plus secondary membrane stress intensity dependent on temperature and neutron fluence. A value of 9.99E+020 indicates that there is no limit for that Dose and Temperature.
! FATIGUE_STRAIN - Fatigue curves for unirradiated material. Number of cycles - Strain amplitude (Strain/2). !! Linear interpolation between cycles can´t be done !!
! FATIGUE_STRESS - Fatigue curves for unirradiated material. Number of cycles - Stress amplitude (Stress/2). !! Linear interpolation between cycles can´t be done !!
! K_CYCL - Coefficient for cyclic stress - strain curves
! m - Coefficient for cyclic stress - strain curves
! K_v - Coefficient for cyclic stress - strain curves
! K_e - Coefficient for cyclic stress - strain curves
!! List of properties available for each material
! 101 - 304L Stainless Steel
! Material model properties: ALPX, CTEX, EX, PRXY, DENS, KXX, C, MELAS ,BISO, MISO, BKIN, KINH
! Other properties: SY_MIN_101, SY_AV_101, SU_MIN_101, SM_101, FATIGUE_STRAIN_101, K_101, m_101, K_e_101, K_v_101
! 102 - 316L Stainless Steel
! Material model properties: ALPX, CTEX, EX, PRXY, DENS, KXX, C, MELAS ,BISO, MISO, BKIN, KINH
! Other properties: SY_MIN_PIP_FORG_102, SY_AV_PIP_FORG_102, SY_MIN_FLAT_102, SY_AV_FLAT_102, SU_MIN_PIP_102, SU_MIN_FLAT_102,SM_102, FATIGUE_STRAIN_102, K_102, m_102, K_e_102, K_v_102
! 103 - 316L (N-IG) Stainless Steel
! Material model properties: ALPX, CTEX, EX, PRXY, DENS, KXX, C, MELAS ,BISO, MISO, BKIN, KINH
! Other properties: SY_MIN_103, SY_AV_103, SU_MIN_103, SU_AV_103, EUNIF_MIN_103, EUNIF_IRR_MIN_103, EUNIF_AV_103, EUNIF_IRR_AV_103, ETOT_AV_103, ETOT_IRR_AV_103, STRAIN_RUPT_AV_103, SM_103, SE_IRR_103, FATIGUE_STRAIN_103, K_103, m_103, K_e_103, K_v_103
! 104 - GRADE 660 Stainless Steel
! Material model properties: ALPX, CTEX, EX, PRXY, DENS, KXX, C, MELAS ,BISO, MISO, BKIN, KINH
! Other properties: SY_MIN_104, SY_AV_104, SU_MIN_104, SU_AV_104, ETOT_AV_104, STRAIN_RUPT_AV_104, SM_STRUCTURAL_104, SMB_NONLEAKTIGHT_JOINTS_104, SMB_LEAKTIGHT_JOINTS_104, FATIGUE_STRESS_104
! 105 - XM-19 Steel
! Material model properties: ALPX, CTEX, EX, PRXY, DENS, KXX, C, MELAS, BISO, MISO, BKIN, KINH
! Other properties: SY_MIN_105, SU_MIN_105, SM_105, SMB_NONLEAKTIGHT_JOINTS_105, SMB_LEAKTIGHT_JOINTS_105, FATIGUE_STRESS_105
! 106 - Alloy 625
! Material model properties: ALPX, EX, PRXY, DENS, KXX, C
! Other properties: SY_MIN_106, SU_MIN_106, SM_106
! 107 - Ti-6Al-4V Alloy
! Material model properties: ALPX, EX, PRXY, DENS, KXX, C, MELAS ,BISO, MISO, BKIN, KINH
! Other properties: SY_MIN_107, SY_AV_107, SU_MIN_107, SU_AV_107, EUNIF_MIN_107, ETOT_MIN_107, STRAIN_RUPT_AV_107, SM_107, SE_107
! 108 - Pure Copper
! Material model properties: ALPX, EX, PRXY, DENS, KXX, C, MELAS_TUBE, MELAS_PLATE, MELAS_ROD ,BISO_TUBE, BISO_PLATE, BISO_ROD, MISO_TUBE, MISO_PLATE, MISO_ROD, BKIN_TUBE, BKIN_PLATE, BKIN_ROD, KINH_TUBE, KINH_PLATE, KINH_ROD
! Other properties: SY_MIN_PLATE_108, SY_MIN_TUBE_108, SY_MIN_ROD_108, SU_MIN_108, EUNIF_AV_108, ETOT_AV_108, STRAIN_RUPT_AV_108, SM_PLATE_108, SM_TUBE_108, SM_ROD_108, FATIGUE_STRAIN_108
! 109 - Copper-Chromium-Zirconium Alloy
! Material model properties: ALPX, CTEX, EX, PRXY, DENS, KXX, C, MELAS_B, MELAS_C ,BISO_B, BISO_C, MISO_B, MISO_C, BKIN_B, BKIN_C, KINH_B, KINH_C
! Other properties: SY_MIN_A_109, SY_IRR_MIN_A_109, SY_MIN_B_109, SY_AV_B_109, SY_IRR_MIN_B_109, SY_MIN_C_109, SU_MIN_A_109, SU_IRR_MIN_A_109, SU_MIN_B_109, SU_AV_B_109, SU_IRR_MIN_B_109, SU_IRR_AV_B_109, SU_MIN_C_109, SU_IRR_MIN_C_109, STRAIN_RUPT_A_AV_109, STRAIN_RUPT_B_AV_109, STRAIN_RUPT_C_AV_109, SM_A_109, SM_IRR_A_109, SE_IRR_A_109, SM_B_109, SM_IRR_B_109, SE_IRR_B_109, SM_C_109, FATIGUE_STRAIN_109, K_e_109, K_v_109
! 110 - Dispersion-Strengthened Copper
! Material model properties: ALPX, CTEX, EX, PRXY, DENS, KXX, C
! Other properties: SY_MIN_110, SY_IRR_MIN_110,SY_AV_110, SY_IRR_AV_110, SU_MIN_110, SU_IRR_MIN_110, SU_AV_110, SU_IRR_AV_110, EUNIF_AV_110, EUNIF_IRR_MIN_110, STRAIN_RUPT_AV_110, SM_110, SM_IRR_110, FATIGUE_STRAIN_110
! 111 - Aluminium-Nickel Bronze
! Material model properties: ALPX, EX, PRXY, DENS, KXX, C, MELAS_BAR, MELAS_PLATE, MELAS_FORG ,BISO_BAR, BISO_PLATE, BISO_FORG, MISO_BAR, MISO_PLATE, MISO_FORG, BKIN_BAR, BKIN_PLATE, BKIN_FORG, KINH_BAR, KINH_PLATE, KINH_FORG
! Other properties: SY_MIN_BAR_111, SY_MIN_PLATE_111, SY_MIN_FORG_111, SU_MIN_111, EUNIF_MIN_111, EUNIF_AV_111, EUNIF_IRR_MIN_111, ETOT_MIN_111, ETOT_AV_111, ETOT_IRR_MIN_111, STRAIN_RUPT_MIN_111, SM_BAR_111, SM_PLATE_111, SM_FORG_111, FATIGUE_STRAIN_111
! 112 - Alloy 718
! Material model properties: ALPX, EX, PRXY, DENS, KXX, C, MELAS ,BISO, MISO, BKIN, KINH
! Other properties: SY_MIN_112, SY_AV_112, SU_MIN_BOLT_112, SU_MIN_PLATE_112, SU_AV_112, EUNIF_AV_112, ETOT_AV_112, STRAIN_RUPT_AV_112, SM_PLATE_STRUCTURAL_112, SM_BAR_FORG_STRUCTURAL_112, SMB_BAR_NONLEAKTIGHT_JOINTS_112, SMB_BAR_LEAKTIGHT_JOINTS_112, SM_IRR_PLATE_STRUCTURAL_112, SMB_IRR_BAR_NONLEAKTIGHT_JOINTS_112, SMB_IRR_BAR_LEAKTIGHT_JOINTS_112, FATIGUE_STRESS_112
! 113 - Beryllium
! Material model properties: ALPX, EX, PRXY, DENS, KXX, C
! Other properties: SY_AV_113, SU_AV_113, EUNIF_AV_113, ETOT_AV_113
! 114 - Tungsten
! Material model properties: ALPX, EX, PRXY, DENS, KXX, C
! Other properties: SY_STRESSRELIEVED_AV_114, SY_RECRISTALIZED_AV_114, SU_STRESSRELIEVED_AV_114, SU_RECRISTALIZED_AV_114, EUNIF_AV_114, ETOT_STRESSRELIEVED_AV_114, ETOT_ANNEALED_AV_114, STRAIN_RUPT_AV_114
! 115 - CFC EU Grade
! Material model properties: ALPX, ALPY, ALPZ, PRXZ, PRXY, PRYZ, DENS, KXX, KYY, KZZ, C
! 116 - CFC CX-2002U Grade
! Material model properties: DENS, KXX, KYY, KZZ, C
!!!!!!!!!!!!!!!!!!!! Reference documents !!!!!!!!!!!!!!!!!!!!
!! In-vessel Components, SDC-IC
! IDM UID ITER_D_222RHC v3.0
! Version created On/ Version/ Status 12 Sep 2012/ 3.0/ Approved
!! Appendix A, Materials Design Limit Data
! IDM UID ITER_D_222RLN v3.2
! Version created On/ Version/ Status 18 Sep 2012/ 3.2/ Approved
! Author: Miguel Gonzalez Fernandez
! Organization: Fusion For Energy
/PREP7
MAT_NAME=ARG1
MAT_NUMBER=ARG2
! Materials and material numbers are stored in arrays MATNAMES_ARRAY and MATNUMBERS_ARRAY
NUM_MAT=16
MATNAMES_ARRAY=
MATNUMBERS_ARRAY=
PROP_ARRAY=
*dim,MATNAMES_ARRAY,string,40,NUM_MAT
MATNAMES_ARRAY(1,1)='304L Stainless Steel'
MATNAMES_ARRAY(1,2)='316L Stainless Steel'
MATNAMES_ARRAY(1,3)='316L (N-IG) Stainless Steel'
MATNAMES_ARRAY(1,4)='GRADE 660 Stainless Steel'
MATNAMES_ARRAY(1,5)='XM-19 Steel'
MATNAMES_ARRAY(1,6)='Alloy 625'
MATNAMES_ARRAY(1,7)='Ti-6Al-4V Alloy'
MATNAMES_ARRAY(1,8)='Pure Copper'
MATNAMES_ARRAY(1,9)='Copper-Chromium-Zirconium Alloy'
MATNAMES_ARRAY(1,10)='Dispersion-Strengthened Copper'
MATNAMES_ARRAY(1,11)='Aluminium-Nickel Bronze'
MATNAMES_ARRAY(1,12)='Alloy 718'
MATNAMES_ARRAY(1,13)='Beryllium'
MATNAMES_ARRAY(1,14)='Tungsten'
MATNAMES_ARRAY(1,15)='CFC EU Grade'
MATNAMES_ARRAY(1,16)='CFC CX-2002U Grade'
*dim,MATNUMBERS_ARRAY,array,NUM_MAT
MATNUMBERS_ARRAY(1)=101,102,103,104,105,106,107,108,109,110,111,112,113,114,115,116
! If only the number of the material is supplied,the material name MAT_NAME is calculated with the given number
*get,MAT_NAME_TYPE,parm,ARG1,type
*if,MAT_NAME_TYPE,eq,0,then
*do,I,1,NUM_MAT,1
*if,MATNUMBERS_ARRAY(I),eq,MAT_NUMBER,then
IDX=I
*exit
*endif
*enddo
MAT_NAME=MATNAMES_ARRAY(1,IDX)
*endif
! Create parameter NUM_PROP to store the number of properties supplied, wich
! is used in the *DO loops for properties selection inside each material
ARG_INIT=3
*do,I,ARG_INIT,19,1
*if,I,lt,10,then
*get,ARGUMENT_TYPE,parm,ARG%I%,type
*else
*get,ARGUMENT_TYPE,parm,AR%I%,type
*endif
*if,ARGUMENT_TYPE,eq,0,or,ARGUMENT_TYPE,eq,-1,then
*exit
*endif
NUM_PROP=I-ARG_INIT+1
*enddo
! Main body of the material macro.The material and the right properties are selected
! according with input parameters
*if,NUM_PROP,gt,0,then
! Create string array to store the properties given in the macro input parameters
! for later property selection
*dim,PROP_ARRAY,string,40,NUM_PROP
*do,I,1,NUM_PROP,1
INDX=I+ARG_INIT-1
*if,INDX,lt,10,then
PROP_ARRAY(1,I)=ARG%INDX%
*else
PROP_ARRAY(1,I)=AR%INDX%
*endif
*enddo
! If - else structure in order to select the rigth material and properties,
! comparing the material number MAT_NUMBER or the material name MAT_NAME with
! the arrays in which all the material numbers and names are stored, MATNUMBERS_ARRAY and MATNAMES_ARRAY respectively
!------------------------------------------------------------------------------
! Material 101. 304L Stainless Steel.
! SDC-IC A.S01 Austenitic steel - 304L (EN grade numbers 1.4307, 1.4306)
!------------------------------------------------------------------------------
*if,MAT_NAME,eq,MATNAMES_ARRAY(1,1),or,MAT_NUMBER,eq,MATNUMBERS_ARRAY(1),then
! Define the material tag (MAT_TAG)
MAT_SS304=101
*do,I,1,NUM_PROP,1
! Mean,average or secant coefficient of thermal expansion
*if,PROP_ARRAY(1,I),eq,'ALPX',then
mptemp
mptemp, 1, 20.0, 50.0, 100.0, 150.0, 200.0,
mptemp, 6, 250.0, 300.0, 350.0, 400.0, 450.0,
mptemp, 11, 500.0, 550.0, 600.0, 650.0, 700.0,
mptemp, 16, 750.0, 800.0, 850.0, 900.0, 950.0,
mptemp, 21, 1000.0,
mpdata, ALPX, 101, 1, 1.53e-05, 1.55e-05, 1.59e-05, 1.62e-05, 1.66e-05,
mpdata, ALPX, 101, 6, 1.69e-05, 1.72e-05, 1.75e-05, 1.78e-05, 1.8e-05,
mpdata, ALPX, 101, 11, 1.83e-05, 1.85e-05, 1.87e-05, 1.89e-05, 1.9e-05,
mpdata, ALPX, 101, 16, 1.92e-05, 1.93e-05, 1.95e-05, 1.96e-05, 1.97e-05,
mpdata, ALPX, 101, 21, 1.97e-05,
*endif
! Instantaneous coefficient of thermal expansion
*if,PROP_ARRAY(1,I),eq,'CTEX',then
mptemp
mptemp, 1, 20.0, 50.0, 100.0, 150.0, 200.0,
mptemp, 6, 250.0, 300.0, 350.0, 400.0, 450.0,
mptemp, 11, 500.0, 550.0, 600.0, 650.0, 700.0,
mptemp, 16, 750.0, 800.0, 850.0, 900.0, 950.0,
mptemp, 21, 1000.0,
mpdata, CTEX, 101, 1, 1.53e-05, 1.57e-05, 1.65e-05, 1.71e-05, 1.78e-05,
mpdata, CTEX, 101, 6, 1.83e-05, 1.89e-05, 1.93e-05, 1.98e-05, 2.01e-05,
mpdata, CTEX, 101, 11, 2.05e-05, 2.07e-05, 2.1e-05, 2.11e-05, 2.13e-05,
mpdata, CTEX, 101, 16, 2.13e-05, 2.14e-05, 2.13e-05, 2.13e-05,
*endif
! Young Modulus
*if,PROP_ARRAY(1,I),eq,'EX',then
mptemp
mptemp, 1, 20.0, 100.0, 150.0, 200.0, 250.0,
mptemp, 6, 300.0, 350.0, 400.0, 450.0, 500.0,
mptemp, 11, 550.0, 600.0, 650.0, 700.0,
mpdata, EX, 101, 1, 200.0e9, 193.0e9, 189.0e9, 185.0e9, 180.0e9,
mpdata, EX, 101, 6, 176.0e9, 172.0e9, 168.0e9, 164.0e9, 159.0e9,
mpdata, EX, 101, 11, 155.0e9, 151.0e9, 147.0e9, 142.0e9,
*endif
! Poisson's ratio
*if,PROP_ARRAY(1,I),eq,'PRXY',then
mp, PRXY, 101, 0.3
*endif
! Mass density
*if,PROP_ARRAY(1,I),eq,'DENS',then
mptemp
mptemp, 1, 20.0, 50.0, 100.0, 150.0, 200.0,
mptemp, 6, 250.0, 300.0, 350.0, 400.0, 450.0,
mptemp, 11, 500.0, 550.0, 600.0, 650.0, 700.0,
mptemp, 16, 750.0, 800.0,
mpdata, DENS, 101, 1, 7930.0, 7919.0, 7899.0, 7879.0, 7858.0,
mpdata, DENS, 101, 6, 7837.0, 7815.0, 7793.0, 7770.0, 7747.0,
mpdata, DENS, 101, 11, 7724.0, 7701.0, 7677.0, 7654.0, 7630.0,
mpdata, DENS, 101, 16, 7606.0, 7582.0,
*endif
! Conductivity
*if,PROP_ARRAY(1,I),eq,'KXX',then
mptemp
mptemp, 1, 20.0, 50.0, 100.0, 150.0, 200.0,
mptemp, 6, 250.0, 300.0, 350.0, 400.0, 450.0,
mptemp, 11, 500.0, 550.0, 600.0, 650.0, 700.0,
mptemp, 16, 750.0, 800.0,
mpdata, KXX, 101, 1, 14.28, 14.73, 15.48, 16.23, 16.98,
mpdata, KXX, 101, 6, 17.74, 18.49, 19.24, 19.99, 20.74,
mpdata, KXX, 101, 11, 21.49, 22.24, 22.99, 23.74, 24.49,
mpdata, KXX, 101, 16, 25.25, 26.0,
*endif
! Specific heat
*if,PROP_ARRAY(1,I),eq,'C',then
mptemp
mptemp, 1, 20.0, 50.0, 100.0, 150.0, 200.0,
mptemp, 6, 250.0, 300.0, 350.0, 400.0, 450.0,
mptemp, 11, 500.0, 550.0, 600.0, 650.0, 700.0,
mptemp, 16, 750.0, 800.0,
mpdata, C, 101, 1, 472.0, 485.0, 501.0, 512.0, 522.0,
mpdata, C, 101, 6, 530.0, 538.0, 546.0, 556.0, 567.0,
mpdata, C, 101, 11, 578.0, 590.0, 601.0, 610.0, 615.0,
mpdata, C, 101, 16, 615.0, 607.0,
*endif
! Stress-strain elastic curves. Nonlinear structural, multilinear elastic.
*if,PROP_ARRAY(1,I),eq,'MELAS',then
tb, MELAS, 101, 5, 14
tbtemp, 20
tbpt, , 0.000, 0.0
tbpt, , 0.0001, 20000000.0
tbpt, , 0.0002, 40000000.0
tbpt, , 0.0003001, 60000000.0
tbpt, , 0.0004014, 80000000.0
tbpt, , 0.0005107, 100100000.0
tbpt, , 0.0006544, 120100000.0
tbpt, , 0.0009146, 140100000.0
tbpt, , 0.0015034, 160200000.0
tbpt, , 0.0029031, 180500000.0
tbpt, , 0.0061022, 201200000.0
tbpt, , 0.012963, 222900000.0
tbtemp, 100
tbpt, , 0.000, 0.0
tbpt, , 0.0001036, 20000000.0
tbpt, , 0.0002073, 40000000.0
tbpt, , 0.0003116, 60000000.0
tbpt, , 0.0004246, 80000000.0
tbpt, , 0.0005918, 100100000.0
tbpt, , 0.0009946, 120100000.0
tbpt, , 0.0021924, 140300000.0
tbpt, , 0.0056284, 160900000.0
tbpt, , 0.014545, 182600000.0
tbtemp, 200
tbpt, , 0.000, 0.0
tbpt, , 0.0001081, 20000000.0
tbpt, , 0.0002163, 40000000.0
tbpt, , 0.0003292, 60000000.0
tbpt, , 0.0004957, 80000000.0
tbpt, , 0.001001, 100100000.0
tbpt, , 0.0029749, 120400000.0
tbpt, , 0.009882, 141400000.0
tbpt, , 0.017595, 152700000.0
tbtemp, 300
tbpt, , 0.000, 0.0
tbpt, , 0.0000568, 10000000.0
tbpt, , 0.0001136, 20000000.0
tbpt, , 0.0001705, 30000000.0
tbpt, , 0.0002278, 40000000.0
tbpt, , 0.0002883, 50000000.0
tbpt, , 0.0003623, 60000000.0
tbpt, , 0.0004819, 70000000.0
tbpt, , 0.0007305, 80100000.0
tbpt, , 0.0012973, 90100000.0
tbpt, , 0.0025721, 100300000.0
tbpt, , 0.0052941, 110600000.0
tbpt, , 0.010773, 121300000.0
tbpt, , 0.0211871, 132800000.0
tbtemp, 400
tbpt, , 0.000, 0.0
tbpt, , 0.0000595, 10000000.0
tbpt, , 0.000119, 20000000.0
tbpt, , 0.0001787, 30000000.0
tbpt, , 0.0002397, 40000000.0
tbpt, , 0.0003095, 50000000.0
tbpt, , 0.0004174, 60000000.0
tbpt, , 0.0006539, 70000000.0
tbpt, , 0.0012535, 80100000.0
tbpt, , 0.0027488, 90200000.0
tbpt, , 0.0062313, 100600000.0
tbpt, , 0.0137547, 111500000.0
*endif
! Isotropic hardening plasticity. Bilinear stress-strain curves.
*if,PROP_ARRAY(1,I),eq,'BISO',then
tb, BISO, 101, 5, 2,
tbtemp, 20
tbdata, , 180e6, 61800373
tbtemp, 100
tbdata,, 145e6,34243803
tbtemp, 200
tbdata,, 118e6, 22092872
tbtemp, 300
tbdata,, 100e6, 17459038
tbtemp, 400
tbdata,, 89e6, 19353256
*endif
! Isotropic hardening plasticity. Multilinear stress-strain curves..
*if,PROP_ARRAY(1,I),eq,'MISO',then
tb, PLASTIC, 101, 5, 4, MISO
tbtemp, 20
tbpt, , 0.002869, 180000000.0
tbpt, , 0.0061022, 201200000.0
tbpt, , 0.012963, 222900000.0
tbtemp, 100
tbpt, , 0.002976, 145000000.0
tbpt, , 0.0056284, 160900000.0
tbpt, , 0.014545, 182600000.0
tbtemp, 200
tbpt, , 0.0027415, 118000000.0
tbpt, , 0.009882, 141400000.0
tbpt, , 0.017595, 152700000.0
tbtemp, 300
tbpt, , 0.002535, 100000000.0
tbpt, , 0.0052941, 110600000.0
tbpt, , 0.010773, 121300000.0
tbpt, , 0.0211871, 132800000.0
tbtemp, 400
tbpt, , 0.0025711, 89000000.0
tbpt, , 0.0062313, 100600000.0
tbpt, , 0.0137547, 111500000.0
*endif
! Kinematic hardening plasticity. Bilinear stress-strain curves.
*if,PROP_ARRAY(1,I),eq,'BKIN',then
tb, BKIN, 101, 5, 2,
tbtemp, 20
tbdata, , 180e6, 61800373
tbtemp, 100
tbdata,, 145e6,34243803
tbtemp, 200
tbdata,, 118e6, 22092872
tbtemp, 300
tbdata,, 100e6, 17459038
tbtemp, 400
tbdata,, 89e6, 19353256
*endif
! Kinematic hardening plasticity. Multilinear stress-strain curves.
*if,PROP_ARRAY(1,I),eq,'KINH',then
tb, PLASTIC, 101, 5, 4, KINH
tbtemp, 20
tbpt, , 0.002869, 180000000.0
tbpt, , 0.0061022, 201200000.0
tbpt, , 0.012963, 222900000.0
tbtemp, 100
tbpt, , 0.002976, 145000000.0
tbpt, , 0.0056284, 160900000.0
tbpt, , 0.014545, 182600000.0
tbtemp, 200
tbpt, , 0.0027415, 118000000.0
tbpt, , 0.009882, 141400000.0
tbpt, , 0.017595, 152700000.0
tbtemp, 300
tbpt, , 0.002535, 100000000.0
tbpt, , 0.0052941, 110600000.0
tbpt, , 0.010773, 121300000.0
tbpt, , 0.0211871, 132800000.0
tbtemp, 400
tbpt, , 0.0025711, 89000000.0
tbpt, , 0.0062313, 100600000.0
tbpt, , 0.0137547, 111500000.0
*endif
! Other properties
! Minimum yield strength: Sy_min
*if,PROP_ARRAY(1,I),eq,'SY_MIN_101',then
*dim, SY_MIN_101, table, 11,,, TEMP
*taxis, SY_MIN_101(1), 1, 20.0, 100.0, 150.0, 200.0, 250.0, 300.0, 350.0, 400.0, 450.0,
*taxis, SY_MIN_101(10), 1, 500.0, 550.0,
SY_MIN_101(1)=180000000.0, 145000000.0, 130000000.0, 118000000.0, 108000000.0, 100000000.0, 94000000.0, 89000000.0, 85000000.0, 81000000.0, 80000000.0,
*endif
! Average yield strength: Sy_av
*if,PROP_ARRAY(1,I),eq,'SY_AV_101',then
*dim, SY_AV_101, table, 11,,, TEMP
*taxis, SY_AV_101(1), 1, 20.0, 100.0, 150.0, 200.0, 250.0, 300.0, 350.0, 400.0, 450.0,
*taxis, SY_AV_101(10), 1, 500.0, 550.0,
SY_AV_101(1)=225000000.0, 181250000.0, 162500000.0, 147500000.0, 135000000.0, 125000000.0, 117500000.0, 111250000.0, 106250000.0, 101250000.0, 100000000.0,
*endif
! Minimum tensile strength: Su_min
*if,PROP_ARRAY(1,I),eq,'SU_MIN_101',then
*dim, SU_MIN_101, table, 9,,, TEMP
*taxis, SU_MIN_101(1), 1, 20.0, 100.0, 150.0, 200.0, 250.0, 300.0, 350.0, 400.0, 450.0,
SU_MIN_101(1)=460000000.0, 410000000.0, 380000000.0, 360000000.0, 350000000.0, 340000000.0, 340000000.0, 337000000.0, 331000000.0,
*endif
! Average tensile strength: Su_av
*if,PROP_ARRAY(1,I),eq,'SU_AV_101',then
*endif
! Allowable stress intensity: Sm
*if,PROP_ARRAY(1,I),eq,'SM_101',then
*dim, SM_101, table, 11,,, TEMP
*taxis, SM_101(1), 1, 20.0, 100.0, 150.0, 200.0, 250.0, 300.0, 350.0, 400.0, 450.0,
*taxis, SM_101(10), 1, 500.0, 550.0,
SM_101(1)=120000000.0, 120000000.0, 117000000.0, 106000000.0, 97000000.0, 90000000.0, 85000000.0, 80000000.0, 76500000.0, 73000000.0, 72000000.0,
*endif
! Fatigue curves for unirradiated material
*if,PROP_ARRAY(1,I),eq,'FATIGUE_STRAIN_101',then
*dim, FATIGUE_STRAIN_101, table, 20,2,, N,TEMP
*taxis, FATIGUE_STRAIN_101(1,1), 1, 1.00E+01, 2.00E+01, 4.00E+01, 1.00E+02, 2.00E+02, 4.00E+02, 1.00E+03, 2.00E+03, 4.00E+03,
*taxis, FATIGUE_STRAIN_101(10,1), 1, 1.00E+04, 2.00E+04, 4.00E+04, 1.00E+05, 2.00E+05, 4.00E+05, 1.00E+06, 5.00E+06, 1.00E+07, 5.00E+07,
*taxis, FATIGUE_STRAIN_101(20,1), 1, 1.00E+08
*taxis, FATIGUE_STRAIN_101(1,1), 2, 20, 450,
FATIGUE_STRAIN_101(1,1)= 4.291E-02, 2.755E-02, 1.931E-02, 1.331E-02, 1.057E-02, 0.863E-02, 0.698E-02, 0.59E-02, 0.498E-02, 0.399E-02, 0.341E-02,
FATIGUE_STRAIN_101(12,1)=0.301E-02, 0.267E-02, 0.25E-02, 0.238E-02, 0.225E-02, 0.203E-02, 0.192E-02, 0.169E-02, 0.165E-02
FATIGUE_STRAIN_101(1,2)=2.552E-02, 1.931E-02, 1.485E-02, 1.08E-02, 0.869E-02, 0.715E-02, 0.578E-02, 0.488E-02, 0.412E-02, 0.33E-02, 0.282E-02,
FATIGUE_STRAIN_101(12,2)= 0.249E-02, 0.221E-02, 0.207E-02, 0.197E-02, 0.186E-02, 0.168E-02, 0.159E-02, 0.14E-02, 0.136E-02
*endif
! K - Coefficient for cyclic stress - strain curves
*if,PROP_ARRAY(1,I),eq,'K_101',then
*dim,K_101,table, 3,,,TEMP
*taxis, K_101(1), 1, 20, 300, 550
K_101(1)= 711.9E+06, 638.7E+06, 638.7E+06
*endif
! m - Coefficient for cyclic stress - strain curves
*if,PROP_ARRAY(1,I),eq,'m_101',then
*dim,m_101,table, 3,,,TEMP
*taxis, m_101(1), 1, 20, 300, 550
m_101(1)= 0.351, 0.31, 0.31
*endif
! K_e - Coefficient for cyclic stress - strain curves
*if,PROP_ARRAY(1,I),eq,'K_e_101',then
*dim, K_e_101, table,7 ,14 ,, TEMP,STRESS
*taxis, K_e_101(1,1), 1, 20, 300, 350, 400, 450, 500, 550
*taxis, K_e_101(1,1), 2, 100E+06, 200E+06, 300E+06, 400E+06, 500E+06, 600E+06, 700E+06, 800E+06, 900E+06,
*taxis, K_e_101(1,10), 2, 1000E+06, 1100E+06, 1200E+06, 1300E+06, 1400E+06
K_e_101(1,1)= 1.04, 1.02, 1.02, 1.02, 1.02, 1.02, 1.02
K_e_101(1,2)= 1.12, 1.09, 1.09, 1.09, 1.09, 1.09, 1.08
K_e_101(1,3)= 1.21, 1.19, 1.18, 1.18, 1.18, 1.17, 1.17
K_e_101(1,4)= 1.3, 1.28, 1.28, 1.27, 1.27, 1.27, 1.26
K_e_101(1,5)= 1.39, 1.38, 1.37, 1.37, 1.36, 1.36, 1.35
K_e_101(1,6)= 1.47, 1.47, 1.47, 1.46, 1.45, 1.45, 1.44
K_e_101(1,7)= 1.55, 1.56, 1.56, 1.55, 1.54, 1.54, 1.53
K_e_101(1,8)= 1.62, 1.65, 1.64, 1.64, 1.63, 1.62, 1.61
K_e_101(1,9)= 1.7, 1.73, 1.73, 1.72, 1.71, 1.7, 1.69
K_e_101(1,10)= 1.77, 1.81, 1.81, 1.8, 1.79, 1.78, 1.77
K_e_101(1,11)= 1.83, 1.89, 1.88, 1.87, 1.86, 1.85, 1.84
K_e_101(1,12)= 1.9, 1.97, 1.96, 1.95, 1.94, 1.93, 1.92
K_e_101(1,13)= 1.96, 2.04, 2.03, 2.02, 2.01, 2, 1.99
K_e_101(1,14)= 2.02, 2.11, 2.1, 2.09, 2.08, 2.07, 2.06
*endif
! K_v - Coefficient for cyclic stress - strain curves
*if,PROP_ARRAY(1,I),eq,'K_v_101',then
*dim, K_v_101, table,7 ,14 ,, TEMP,STRESS
*taxis, K_v_101(1,1), 1, 20, 300, 350, 400, 450, 500, 550
*taxis, K_v_101(1,1), 2, 100E+06, 200E+06, 300E+06, 400E+06, 500E+06, 600E+06, 700E+06, 800E+06, 900E+06,
*taxis, K_v_101(1,10), 2, 1000E+06, 1100E+06, 1200E+06, 1300E+06, 1400E+06
K_v_101(1,1)= 1.03, 1.02, 1.02, 1.02, 1.02, 1.02, 1.02
K_v_101(1,2)= 1.08, 1.06, 1.06, 1.06, 1.06, 1.06, 1.06
K_v_101(1,3)= 1.13, 1.12, 1.11, 1.11, 1.11, 1.11, 1.11
K_v_101(1,4)= 1.17, 1.16, 1.16, 1.16, 1.16, 1.15, 1.15
K_v_101(1,5)= 1.2, 1.2, 1.2, 1.2, 1.19, 1.19, 1.19
K_v_101(1,6)= 1.23, 1.23, 1.23, 1.23, 1.23, 1.22, 1.22
K_v_101(1,7)= 1.26, 1.26, 1.26, 1.25, 1.25, 1.25, 1.25
K_v_101(1,8)= 1.28, 1.28, 1.28, 1.28, 1.27, 1.27, 1.27
K_v_101(1,9)= 1.3, 1.3, 1.3, 1.3, 1.29, 1.29, 1.29
K_v_101(1,10)= 1.31, 1.32, 1.32, 1.31, 1.31, 1.31, 1.31
K_v_101(1,11)= 1.32, 1.33, 1.33, 1.33, 1.33, 1.33, 1.32
K_v_101(1,12)= 1.34, 1.35, 1.34, 1.34, 1.34, 1.34, 1.34
K_v_101(1,13)= 1.35, 1.36, 1.36, 1.35, 1.35, 1.35, 1.35
K_v_101(1,14)= 1.36, 1.37, 1.37, 1.36, 1.36, 1.36, 1.36
*endif
*enddo
*endif
!------------------------------------------------------------------------------
! Material 102. 316L Stainless Steel.
! SDC-IC A.S02 Austenitic steel - 316L (EN grade numbers 1.4404, 1.4435)
!------------------------------------------------------------------------------
*if,MAT_NAME,eq,MATNAMES_ARRAY(1,2),or,MAT_NUMBER,eq,MATNUMBERS_ARRAY(2),then
! Define the material tag (MAT_TAG)
MAT_SS316=102
*do,I,1,NUM_PROP,1
! Mean,average or secant coefficient of thermal expansion
*if,PROP_ARRAY(1,I),eq,'ALPX',then
mptemp
mptemp, 1, 20.0, 50.0, 100.0, 150.0, 200.0,
mptemp, 6, 250.0, 300.0, 350.0, 400.0, 450.0,
mptemp, 11, 500.0, 550.0, 600.0, 650.0, 700.0,
mptemp, 16, 750.0, 800.0, 850.0, 900.0, 950.0,
mptemp, 21, 1000.0,
mpdata, ALPX, 102, 1, 1.53e-05, 1.55e-05, 1.59e-05, 1.62e-05, 1.66e-05,
mpdata, ALPX, 102, 6, 1.69e-05, 1.72e-05, 1.75e-05, 1.78e-05, 1.8e-05,
mpdata, ALPX, 102, 11, 1.83e-05, 1.85e-05, 1.87e-05, 1.89e-05, 1.9e-05,
mpdata, ALPX, 102, 16, 1.92e-05, 1.93e-05, 1.95e-05, 1.96e-05, 1.97e-05,
mpdata, ALPX, 102, 21, 1.97e-05,
*endif
! Instantaneous coefficient of thermal expansion
*if,PROP_ARRAY(1,I),eq,'CTEX',then
mptemp
mptemp, 1, 20.0, 50.0, 100.0, 150.0, 200.0,
mptemp, 6, 250.0, 300.0, 350.0, 400.0, 450.0,
mptemp, 11, 500.0, 550.0, 600.0, 650.0, 700.0,
mptemp, 16, 750.0, 800.0, 850.0, 900.0, 950.0,
mptemp, 21, 1000.0,
mpdata, CTEX, 102, 1, 1.53e-05, 1.57e-05, 1.65e-05, 1.71e-05, 1.78e-05,
mpdata, CTEX, 102, 6, 1.83e-05, 1.89e-05, 1.93e-05, 1.98e-05, 2.01e-05,
mpdata, CTEX, 102, 11, 2.05e-05, 2.07e-05, 2.1e-05, 2.11e-05, 2.13e-05,
mpdata, CTEX, 102, 16, 2.13e-05, 2.14e-05, 2.13e-05, 2.13e-05,
*endif
! Young Modulus
*if,PROP_ARRAY(1,I),eq,'EX',then
mptemp
mptemp, 1, 20.0, 100.0, 150.0, 200.0, 250.0,
mptemp, 6, 300.0, 350.0, 400.0, 450.0, 500.0,
mptemp, 11, 550.0, 600.0, 650.0, 700.0,
mpdata, EX, 102, 1, 200.0e9, 193.0e9, 189.0e9, 185.0e9, 180.0e9,
mpdata, EX, 102, 6, 176.0e9, 172.0e9, 168.0e9, 164.0e9, 159.0e9,
mpdata, EX, 102, 11, 155.0e9, 151.0e9, 147.0e9, 142.0e9,
*endif
! Poisson's ratio
*if,PROP_ARRAY(1,I),eq,'PRXY',then
mp, PRXY, 102, 0.3
*endif
! Mass density
*if,PROP_ARRAY(1,I),eq,'DENS',then
mptemp
mptemp, 1, 20.0, 50.0, 100.0, 150.0, 200.0,
mptemp, 6, 250.0, 300.0, 350.0, 400.0, 450.0,
mptemp, 11, 500.0, 550.0, 600.0, 650.0, 700.0,
mptemp, 16, 750.0, 800.0,
mpdata, DENS, 102, 1, 7930.0, 7919.0, 7899.0, 7879.0, 7858.0,
mpdata, DENS, 102, 6, 7837.0, 7815.0, 7793.0, 7770.0, 7747.0,
mpdata, DENS, 102, 11, 7724.0, 7701.0, 7677.0, 7654.0, 7630.0,
mpdata, DENS, 102, 16, 7606.0, 7582.0,
*endif
! Conductivity
*if,PROP_ARRAY(1,I),eq,'KXX',then
mptemp
mptemp, 1, 20.0, 50.0, 100.0, 150.0, 200.0,
mptemp, 6, 250.0, 300.0, 350.0, 400.0, 450.0,
mptemp, 11, 500.0, 550.0, 600.0, 650.0, 700.0,
mptemp, 16, 750.0, 800.0,
mpdata, KXX, 102, 1, 14.28, 14.73, 15.48, 16.23, 16.98,
mpdata, KXX, 102, 6, 17.74, 18.49, 19.24, 19.99, 20.74,
mpdata, KXX, 102, 11, 21.49, 22.24, 22.99, 23.74, 24.49,
mpdata, KXX, 102, 16, 25.25, 26.0,
*endif
! Specific heat
*if,PROP_ARRAY(1,I),eq,'C',then
mptemp
mptemp, 1, 20.0, 50.0, 100.0, 150.0, 200.0,
mptemp, 6, 250.0, 300.0, 350.0, 400.0, 450.0,
mptemp, 11, 500.0, 550.0, 600.0, 650.0, 700.0,
mptemp, 16, 750.0, 800.0,
mpdata, C, 102, 1, 472.0, 485.0, 501.0, 512.0, 522.0,
mpdata, C, 102, 6, 530.0, 538.0, 546.0, 556.0, 567.0,
mpdata, C, 102, 11, 578.0, 590.0, 601.0, 610.0, 615.0,
mpdata, C, 102, 16, 615.0, 607.0,
*endif
! Stress-strain elastic curves. Nonlinear structural, multilinear elastic.
*if,PROP_ARRAY(1,I),eq,'MELAS',then
tb, MELAS, 102, 5, 16
tbtemp, 20
tbpt, , 0.000, 0.0
tbpt, , 0.0001, 20000000.0
tbpt, , 0.0002, 40000000.0
tbpt, , 0.0003, 60000000.0
tbpt, , 0.0004008, 80000000.0
tbpt, , 0.0005066, 100100000.0
tbpt, , 0.0006336, 120100000.0
tbpt, , 0.0008326, 140100000.0
tbpt, , 0.0012349, 160200000.0
tbpt, , 0.002139, 180400000.0
tbpt, , 0.0041581, 200800000.0
tbpt, , 0.0084526, 221900000.0
tbpt, , 0.0170658, 244100000.0
tbtemp, 100
tbpt, , 0.000, 0.0
tbpt, , 0.0001036, 20000000.0
tbpt, , 0.0002072, 40000000.0
tbpt, , 0.0003111, 60000000.0
tbpt, , 0.0004176, 80000000.0
tbpt, , 0.0005414, 100100000.0
tbpt, , 0.0007399, 120100000.0
tbpt, , 0.0011906, 140200000.0
tbpt, , 0.0023532, 160400000.0
tbpt, , 0.0052689, 181000000.0
tbpt, , 0.0120611, 202400000.0
tbpt, , 0.0180475, 213800000.0
tbtemp, 200
tbpt, , 0.000, 0.0
tbpt, , 0.0001081, 20000000.0
tbpt, , 0.0002162, 40000000.0
tbpt, , 0.0003256, 60000000.0
tbpt, , 0.0004492, 80000000.0
tbpt, , 0.0006626, 100100000.0
tbpt, , 0.0012661, 120200000.0
tbpt, , 0.0031852, 140400000.0
tbpt, , 0.0088007, 161400000.0
tbpt, , 0.0144829, 172500000.0
tbtemp, 300
tbpt, , 0.000, 0.0
tbpt, , 0.0000568, 10000000.0
tbpt, , 0.0001136, 20000000.0
tbpt, , 0.0001704, 30000000.0
tbpt, , 0.0002274, 40000000.0
tbpt, , 0.000285, 50000000.0
tbpt, , 0.0003454, 60000000.0
tbpt, , 0.0004156, 70000000.0
tbpt, , 0.0005133, 80000000.0
tbpt, , 0.0006788, 90100000.0
tbpt, , 0.0009953, 100100000.0
tbpt, , 0.0016214, 110200000.0
tbpt, , 0.0028401, 120300000.0
tbpt, , 0.0051301, 130700000.0
tbpt, , 0.0092637, 141300000.0
tbpt, , 0.0164322, 152500000.0
tbtemp, 400
tbpt, , 0.000, 0.0
tbpt, , 0.0000595, 10000000.0
tbpt, , 0.000119, 20000000.0
tbpt, , 0.0001786, 30000000.0
tbpt, , 0.0002384, 40000000.0
tbpt, , 0.0002997, 50000000.0
tbpt, , 0.0003679, 60000000.0
tbpt, , 0.0004591, 70000000.0
tbpt, , 0.0006153, 80000000.0
tbpt, , 0.0009323, 90100000.0
tbpt, , 0.0016067, 100200000.0
tbpt, , 0.0030131, 110300000.0
tbpt, , 0.0058181, 120700000.0
tbpt, , 0.0111427, 131500000.0
tbpt, , 0.0207729, 142900000.0
*endif
! Isotropic hardening plasticity. Bilinear stress-strain curves.
*if,PROP_ARRAY(1,I),eq,'BISO',then
tb, BISO, 102, 5, 2,
tbtemp, 20
tbdata, , 190e6, 42674920.28
tbtemp, 100
tbdata,, 165e6, 34025091.91
tbtemp, 200
tbdata,, 127e6, 28412862.8
tbtemp, 300
tbdata,, 113e6, 23690231.83
tbtemp, 400
tbdata,, 103e6, 18356062.57
*endif
! Isotropic hardening plasticity. Multilinear stress-strain curves.
*if,PROP_ARRAY(1,I),eq,'MISO',then
tb, PLASTIC, 102, 5, 4, MISO
tbtemp, 20
tbpt, , 0.003089, 190000000.0
tbpt, , 0.0041581, 200800000.0
tbpt, , 0.0084526, 221900000.0
tbpt, , 0.0170658, 244100000.0
tbtemp, 100
tbpt, , 0.0030043, 165000000.0
tbpt, , 0.0052689, 181000000.0
tbpt, , 0.0120611, 202400000.0
tbpt, , 0.0180475, 213800000.0
tbtemp, 200
tbpt, , 0.0028622, 137000000.0
tbpt, , 0.0088007, 161400000.0
tbpt, , 0.0144829, 172500000.0
tbtemp, 300
tbpt, , 0.0026832, 119000000.0
tbpt, , 0.0051301, 130700000.0
tbpt, , 0.0092637, 141300000.0
tbpt, , 0.0164322, 152500000.0
tbtemp, 400
tbpt, , 0.0026928, 108000000.0
tbpt, , 0.0058181, 120700000.0
tbpt, , 0.0111427, 131500000.0
tbpt, , 0.0207729, 142900000.0
*endif
! Kinematic hardening plasticity. Bilinear stress-strain curves.
*if,PROP_ARRAY(1,I),eq,'BKIN',then
tb, BKIN, 102, 5, 2,
tbtemp, 20
tbdata, , 190e6, 42674920.28
tbtemp, 100
tbdata,, 165e6, 34025091.91
tbtemp, 200
tbdata,, 127e6, 28412862.8
tbtemp, 300
tbdata,, 113e6, 23690231.83
tbtemp, 400
tbdata,, 103e6, 18356062.57
*endif
! Kinematic hardening plasticity. Multilinear stress-strain curves.
*if,PROP_ARRAY(1,I),eq,'KINH',then
tb, KINH, 102, 5, 16
tbtemp, 20
tbpt, , 0.003089, 190000000.0
tbpt, , 0.0041581, 200800000.0
tbpt, , 0.0084526, 221900000.0
tbpt, , 0.0170658, 244100000.0
tbtemp, 100
tbpt, , 0.0030043, 165000000.0
tbpt, , 0.0052689, 181000000.0
tbpt, , 0.0120611, 202400000.0
tbpt, , 0.0180475, 213800000.0
tbtemp, 200
tbpt, , 0.0028622, 137000000.0
tbpt, , 0.0088007, 161400000.0
tbpt, , 0.0144829, 172500000.0
tbtemp, 300
tbpt, , 0.0026832, 119000000.0
tbpt, , 0.0051301, 130700000.0
tbpt, , 0.0092637, 141300000.0
tbpt, , 0.0164322, 152500000.0
tbtemp, 400
tbpt, , 0.0026928, 108000000.0
tbpt, , 0.0058181, 120700000.0
tbpt, , 0.0111427, 131500000.0
tbpt, , 0.0207729, 142900000.0
*endif
! Other properties
! Minimum yield strength: Sy_min
*if,PROP_ARRAY(1,I),eq,'SY_MIN_PIP_FORG_102',then
*dim, SY_MIN_PIP_FORG_102, table, 11,,, TEMP
*taxis, SY_MIN_PIP_FORG_102(1), 1, 20.0, 100.0, 150.0, 200.0, 250.0, 300.0, 350.0, 400.0, 450.0,
*taxis, SY_MIN_PIP_FORG_102(10), 1, 500.0, 550.0,
SY_MIN_PIP_FORG_102(1)=190000000.0, 165000000.0, 150000000.0, 137000000.0, 127000000.0, 119000000.0, 113000000.0, 108000000.0, 103000000.0, 100000000.0, 98000000.0,
*endif
*if,PROP_ARRAY(1,I),eq,'SY_MIN_FLAT_102',then
*dim, SY_MIN_FLAT_102, table, 11,,, TEMP
*taxis, SY_MIN_FLAT_102(1), 1, 20.0, 100.0, 150.0, 200.0, 250.0, 300.0, 350.0, 400.0, 450.0,
*taxis, SY_MIN_FLAT_102(10), 1, 500.0, 550.0,
SY_MIN_FLAT_102(1)=220000000.0, 166000000.0, 152000000.0, 137000000.0, 127000000.0, 118000000.0, 113000000.0, 108000000.0, 103000000.0, 100000000.0, 98000000.0,
*endif
! Average yield strength: Sy_av
*if,PROP_ARRAY(1,I),eq,'SY_AV_PIP_FORG_102',then
*dim, SY_AV_PIP_FORG_102, table, 11,,, TEMP
*taxis, SY_AV_PIP_FORG_102(1), 1, 20.0, 100.0, 150.0, 200.0, 250.0, 300.0, 350.0, 400.0, 450.0,
*taxis, SY_AV_PIP_FORG_102(10), 1, 500.0, 550.0,
SY_AV_PIP_FORG_102(1)=243200000.0, 211200000.0, 192000000.0, 175360000.0, 162560000.0, 152320000.0, 144640000.0, 138240000.0, 131840000.0, 128000000.0, 125440000.0,
*endif
*if,PROP_ARRAY(1,I),eq,'SY_AV_FLAT_102',then
*dim, SY_AV_FLAT_102, table, 11,,, TEMP
*taxis, SY_AV_FLAT_102(1), 1, 20.0, 100.0, 150.0, 200.0, 250.0, 300.0, 350.0, 400.0, 450.0,
*taxis, SY_AV_FLAT_102(10), 1, 500.0, 550.0,
SY_AV_FLAT_102(1)=281600000.0, 212480000.0, 194560000.0, 175360000.0, 162560000.0, 151040000.0, 144640000.0, 138240000.0, 131840000.0, 128000000.0, 125440000.0,
*endif
! Minimum tensile strength: Su_min
*if,PROP_ARRAY(1,I),eq,'SU_MIN_PIP_102',then
*dim, SU_MIN_PIP_102, table, 9,,, TEMP
*taxis, SU_MIN_PIP_102(1), 1, 20.0, 100.0, 150.0, 200.0, 250.0, 300.0, 350.0, 400.0, 500.0,
SU_MIN_PIP_102(1)=490000000.0, 430000000.0, 410000000.0, 390000000.0, 385000000.0, 380000000.0, 380000000.0, 380000000.0,380000000.0,
*endif
*if,PROP_ARRAY(1,I),eq,'SU_MIN_FLAT_102',then
*dim, SU_MIN_FLAT_102, table, 9,,, TEMP
*taxis, SU_MIN_FLAT_102(1), 1, 20.0, 100.0, 150.0, 200.0, 250.0, 300.0, 350.0, 400.0, 500.0,
SU_MIN_FLAT_102(1)=520000000.0, 430000000.0, 410000000.0, 390000000.0, 385000000.0, 380000000.0, 380000000.0, 380000000.0, 380000000.0,
*endif
! Average tensile strength: Su_av
*if,PROP_ARRAY(1,I),eq,'SU_AV_102',then
*endif
! Allowable stress intensity: Sm
*if,PROP_ARRAY(1,I),eq,'SM_102',then
*dim, SM_102, table, 12,,, TEMP
*taxis, SM_102(1), 1, 20.0, 50.0, 100.0, 150.0, 200.0, 250.0, 300.0, 350.0, 400.0,
*taxis, SM_102(10), 1, 450.0, 500.0, 550.0,
SM_102(1)=127000000.0, 127000000.0, 127000000.0, 127000000.0, 123000000.0, 114000000.0, 107000000.0, 102000000.0, 97000000.0, 93000000.0, 90000000.0,
SM_102(12)=88000000.0,
*endif
! Fatigue curves for unirradiated material
*if,PROP_ARRAY(1,I),eq,'FATIGUE_STRAIN_102',then
*dim, FATIGUE_STRAIN_102, table, 20,6,, N,TEMP
*taxis, FATIGUE_STRAIN_102(1,1), 1, 1.00E+01, 2.00E+01, 4.00E+01, 1.00E+02, 2.00E+02, 4.00E+02, 1.00E+03, 2.00E+03, 4.00E+03,
*taxis, FATIGUE_STRAIN_102(10,1), 1, 1.00E+04, 2.00E+04, 4.00E+04, 1.00E+05, 2.00E+05, 4.00E+05, 1.00E+06, 5.00E+06, 1.00E+07, 5.00E+07,
*taxis, FATIGUE_STRAIN_102(20,1), 1, 1.00E+08
*taxis, FATIGUE_STRAIN_102(1,1), 2, 20, 450, 500, 550, 600, 650
FATIGUE_STRAIN_102(1,1)= 4.291E-02, 2.755E-02, 1.931E-02, 1.331E-02, 1.057E-02, 0.863E-02, 0.698E-02, 0.59E-02, 0.498E-02, 0.399E-02, 0.341E-02,
FATIGUE_STRAIN_102(12,1)=0.301E-02, 0.267E-02, 0.25E-02, 0.238E-02, 0.225E-02, 0.203E-02, 0.192E-02, 0.169E-02, 0.165E-02
FATIGUE_STRAIN_102(1,2)=2.552E-02, 1.931E-02, 1.485E-02, 1.08E-02, 0.869E-02, 0.715E-02, 0.578E-02, 0.488E-02, 0.412E-02, 0.33E-02, 0.282E-02,
FATIGUE_STRAIN_102(12,2)= 0.249E-02, 0.221E-02, 0.207E-02, 0.197E-02, 0.186E-02, 0.168E-02, 0.159E-02, 0.14E-02, 0.136E-02
FATIGUE_STRAIN_102(1,3)= 2.459E-02, 1.841E-02, 1.403E-02, 1.007E-02, 0.805E-02, 0.659E-02, 0.532E-02, 0.449E-02, 0.38E-02, 0.304E-02, 0.26E-02,
FATIGUE_STRAIN_102(12,3)= 0.229E-02, 0.203E-02, 0.19E-02, 0.181E-02, 0.171E-02, 0.154E-02, 0.146E-02, 0.129E-02, 0.125E-02
FATIGUE_STRAIN_102(1,4)= 2.361E-02, 1.748E-02, 1.316E-02, 0.933E-02, 0.741E-02, 0.605E-02, 0.487E-02, 0.412E-02, 0.348E-02, 0.278E-02, 0.238E-02,
FATIGUE_STRAIN_102(12,4)= 0.21E-02, 0.186E-02, 0.174E-02, 0.166E-02, 0.157E-02, 0.141E-02, 0.134E-02, 0.118E-02, 0.115E-02
FATIGUE_STRAIN_102(1,5)= 2.26E-02, 1.652E-02, 1.231E-02, 0.859E-02, 0.678E-02, 0.552E-02, 0.445E-02, 0.376E-02, 0.317E-02, 0.254E-02, 0.217E-02,
FATIGUE_STRAIN_102(12,5)= 0.192E-02, 0.17E-02, 0.159E-02, 0.151E-02, 0.143E-02, 0.129E-02, 0.122E-02, 0.108E-02, 0.105E-02
FATIGUE_STRAIN_102(1,6)= 2.155E-02, 1.553E-02, 1.139E-02, 0.787E-02, 0.618E-02, 0.502E-02, 0.404E-02, 0.342E-02, 0.289E-02, 0.231E-02, 0.198E-02,
FATIGUE_STRAIN_102(12,6)= 0.174E-02, 0.154E-02, 0.145E-02, 0.138E-02, 0.13E-02, 0.117E-02, 0.111E-02, 0.098E-02, 0.095E-02
*endif
! K - Coefficient for cyclic stress - strain curves
*if,PROP_ARRAY(1,I),eq,'K_102',then
*dim,K_102,table, 4,,,TEMP
*taxis, K_102(1), 1, 20, 300, 550, 600
K_102(1)= 711.9E+06, 638.7E+06, 638.7E+06, 628.2E+06
*endif
! m - Coefficient for cyclic stress - strain curves
*if,PROP_ARRAY(1,I),eq,'m_102',then
*dim,m_102,table, 4,,,TEMP
*taxis, m_102(1), 1, 20, 300, 550, 600
m_102(1)= 0.351, 0.31, 0.31, 0.248