ML20213G675
| ML20213G675 | |
| Person / Time | |
|---|---|
| Site: | Point Beach  |
| Issue date: | 11/11/1986 |
| From: | Fay C WISCONSIN ELECTRIC POWER CO. |
| To: | Harold Denton, Lear G Office of Nuclear Reactor Regulation |
| References | |
| CON-NRC-86-107 VPNPD-86-453, NUDOCS 8611180259 | |
| Download: ML20213G675 (100) | |
Text
Wisconsin Electnc eam coune 231 W MICHIGAN.P.O DOX 2046. MILWAUKEE.Wl53201 (414)277-2345 VPNPD-86-453 NRC-86-107 November 11, 1986 Mr. H. R. Denton, Director Office of Nuclear Reactor Regulation U.
S. NUCLEAR REGULATORY COMMISSION Washington, D.
C.
20555 Attention:
Mr. George Lear, Project Director PWR' Project Directorate 1 Gentlemen:
DOCKETS 50-266 AND 50-301 ENERGY ABSORBERS POINT BEACH NUCLEAR PLANT, UNITS 1 AND 2 on October 23, 1986, Wisconsin Electric and Bechtel met with the NRC and Brookhaven National Laboratories (BNL) representatives to discuss our application for using energy absorbers for Point Beach Nuclear Plant.
The twenty-two questions transmitted by your letter dated September 30, 1986 comprised the agenda for the presentation and subsequent discussions.
We are transmitting the following attachments in accordance with the agreements made during the meeting so that BNL may i
proceed with non-linear analysis of the main steam dump l
system for Point Beach Nuclear Plant, Unit 1 using energy l
absorbers:
1.
ME101 Input Listing 2.
ME101 User's Manual 3.
Energy Absorber Loading and Hysteresis Curves for Size E4B5-5 l
i 4.
Earthquake Artificial Time Histories (Horizontal l
and Vertical) h00 5.
Piping Isometric P-107 (Main Steam Outside I
Containment, Unit 1), Revision 5 I l 8611180259 861111 DR ADOCK 05000266 PDR
Mr. H. R. Denton November 11, 1986 Page 2 By separate copy of this letter, Mr. Guiliano DeGrassi of BNL is being provided the above-listed attachments to expedite the exchange of this information.
Wisconsin Electric will provide the formal responses to the twenty-two NRC questions under a separate cover.
Very truly yours, l
C. W. Fy Vice President Nuclear Power Enclosures Copy to Resident Inspector (without enc.)
Guiliano DeGrassi - BNL
NRC NP POINT BEACH NUCLEAR PLANT P-107, MAIN STEAM BYPASS - UNIT 1 GUIDE TO ANALYSIS DATA The enclosed data package provides the necessary information which may be used in performing a confirmatory non-linear time history analysis:
1.
Geometry and See isometric P107, Revision 5 and the ME101 input relevant input listing. Refer to the ME101 users manual for data definitions of the input code. The equivalent linear analysis performed by Bechtel was based on a combined analysis of the main steam and bypass systems.
2.
Support location /
- Refer to isometric P107, Revision 5 and the ME101 l
type input listing.
3.
Energy absorber
- e Refer to the ME101 input listing, loading data curve, and the hysteresis curve provided, All energy absorbers used are of the same size e
(E4B5-5),
e Note that the elastic design is based on the full range of yield displacement, i.e. 2(XY).
l 4.
FSAR seismic design : e 1/2% damping basis e Two component earthquake; Maximum of dX2+Y2' or [Z2,y' 2
e Modal combinations by SRSS 5.
Seismic loadings
- e Design Spectra X = Z, See the ME101 input listing Y
See the ME101 input listing e Artificial Time Histories See the vertical and horizontal data generated from broadened enveloped spectra
O P
ME101 INPUT LISTING k
ME101/K3 DATE 081385 PAGE 1
MEtOi INPUT CA RD 1MA GES LARD 1
11 21 31 41 51 61 71 80 If 8Pil'
+
+
+
+
+
+
.+
+
LOAD CASE (S)
+
NRC HUtlETIN #79-14/ ENERGY ABSORBER REPLACFMENT PROGRAM
......,,,,,,ee...eeeeeeeeeeeee eee,...eeeeeeeeese.....
seee 2
SYSTEM *tlMAINSTEAM) 3 4
- CAL C #1-21 REV1 150 nP IO7(REV 5) 5 SOLVER =EAL.
6 Cit LDCASE=THRM1(S+0) 7 RUN LOCASE=WT1(W+0) 8 RUN LDCASE=SEISOB($+0) 9 RUN LOCASE*SEISDB(S*D) 10 RON ZPA=0N,CMB=CMSRS, 11
/PA TIT =MAINSTEAM OUTSIDE CONTMNT 17 HED EAB DESIGN / ANALYSIS, USER =ANDREWS.
ORIGINAtuR; USER = LEE / DONG, 14 UNITS =2, 16 PROJ POINT BEACH, 7
PROJNO= 10447014, g
PROBN0=1-21/EAB, g
MODES =250, 20 PER=.03, 21 CDEF=CS4, SVDAMP=.OOS, 23 MITER =5, 24 25 SAP 130 88.00 OD=30,THI=.908,LBS/FT=339.825, 26 ANC 5
E=27.9E6,EXP=3.8258, 27 CODE =B31573, g
ATEMP=70.
29 SC=15000, SH=tSOOO, OPRESS*1085 MAT =SAlO6-B,
-5.681 TEE =WTEE, 34 10
-9.84
-2.165064 SIF*2.269, 35 15 1.25
-1.515545 SIF=2.269, 36 20 0.875 OD=8.625.TH1=.406, 2-4-11/16 37 21 LBS/FT=44.827, 38 THl=.812.LBS/FT=569, 39 22 4-8-21/32
-1.29904 OD=30,THI=.908,LBS/FT=339.825, 40 20 25 0.75 DTITLE=EB-1-H20.SEG=2, 41 42 RAD 25 1
43 30 0.75
-1.29904 SIF=2.269, 44 31 2-4-11/16 OD=8.625.THl=.406, LBS/FT=44.827, 45 THl=.812 LBS/FT=569, 40 32 1-8-21/32
-0.866025 OD=30.THI=.908,LBS/FT=339.825, 47 30 35 0,5 DTITLE=EB-1-H20A.SEG=2, 48 es THRM1 SEISOB SEISDB 49 RAD 35 1
-0.866025 SIF=2.269, 50 40 0.5 OD=8.625.TH1=.406, 51 41 2-4-11/16 LBS/FT=44.827.
52 THI=.812,LBS/FT=569, 51 42 1-8-21/32 00=30 THI=.908,LBS/FT=339.825,
-1.732051 54 40 45 1.0 7
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8 05 0550550500505 055050055055500055050 55056 70 056 70 056 7
2222333344444556 66777 78 888 89 999 9
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44 5556667788899 0001 1
0 5
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5 6
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N A
P A
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R 2345678901 2145678901234567890123456789012345678901234 2222222222333333333344444444445555555555666666666677777 5678901 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 11 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 11 1 1 11 1
ME101/K3 DATE 08t385 PAGE 4
SIF=2.269,OD=30.THI=.908, 875 395400 2-0 LBS/FT*339.825, 176 OD=8.625.THI=.406, 177 401 2-4-11/16 LBS/FT=44.827, 17H THI=.812.LBS/Fi=569, 179 402 1-8-21/32 00=30.THI*.908.LPS/FT=339.825 180 400405 t-5 OTITLE=EB-t-Hlo,SEG=2, 181 182 RAD 405 t
SIF=1.3742, 183 410 1-7 ADOWT=318 084 415 1-6 OD=24,THI=.968,LBS/FT=262.52, 185 225500 14-10-1/4 DT I T L E a ( E AB 1 )E B-2-H1. SEG= 2
- 186 FORCE =5817,AA=600
=W
. WT1 187 SPR 500 1
1 HYS=E465-5 188 EAB 500 00=.200.
+0 THRM1 Wit SEIS08
- D SEISDB 1Q9 00=.424, 190 1
191
- SNB 500 TEE =WTEE.SEG=3.
192 505 23-8-3/4 DTITLE=EB-2-H2.
191 510 0 1-1/4 FORCE =7019,AA=1500.
- W WTt 194 SPR 510 t
SIF=5.729.
195 515 1 4-3/4 SIF=5.725.
196 520 6-5 197 525 0-15 JOINT = RED.
198 530 0-10
-O-1.5 OD=18,THI=.75.LBS/FT=157.164, 199 533 0-10
-O-1.5 OD=18.THI=.75,LBS/FT=tS7.164 200 535 21-6 DTITLE=(EAB2)EB-2-H3.SEG=3, 201 202 RAD 535 1
1 203
- SN8 535 1
HYS=E4BS-5.
=0 THRM1 Wit SEISOB 204 EAR 535 DD=.115,
=D SEISDB 205 DDa.229 206 L
207 540 0 21 208 542 1-3 3 OTI= FEASIBLE EAB.
1 HYS=E4BS-4 209
- EAB 542 1
210 545 1-3
-t-3 L
SIF=5.725.SEG=2.
211 550 13-0 DTITLE=EB-2-H4.SEG=2 212 555 8-9 213 RAD 555 1
I 214 RAD 555 SIF=5.725 SEG=2, 215 560 11-6 216 564 0-15
?i7 565 0-6.5 0.5 dOINT= RED, 00=16,THI=.656.LBS/FT=124.689, 218 570 0-6.5
-O-0.5 OTITLE=EB-2-H5.SEG=2 219 575 12-3.75 220 RAD 575 1
DTITLE=(EAB3)EB-2-H6.SEG=2.
221 577 12-7.5 1
HYS=E485-5,
. THRMt WT1 SEISOB 222 EAB 577 DO=_240,
- O 223 DD=.496
- D
. SEISDB 224 DTITLE=(EAB3)EB-2-H6.SEG=2.
225 580 0-5.75 226 RAD 580 t
1 227
- SN8 580 228
- SNUBBER MOVED 19 FT 1-3/4 INCHES SOUTH OF ORIGINAL LOCATION L
229 585 3-8.75 230 590 3
-6.018 L
-12.565 DTITLE=EB-2-H7.SEG=2, 231 595 232
- SNO 595 t 9-t/2 DTITLE=EB-2-H8,SEG=4, P33 600 234 RAD 600 t
i ME101/K3 DATE 081385 PAGE 5
235-.
605 11-1/2 336 610 3 THI=1.312.LBS/FT=1164 237 J15 0 THI=.656.LBS/FT=124.689, TEE =WTEE, 238 239 620 0 TEE =WTEE.
240 625 0 TEE =WTEE.
241 628 10.5 DTITLE=EB-2-H9 242 RAD 628 1
343 RAD 628 1
244 630 1.5 TEE =WTEE.
245
- (REVO) 630 0 TEE =WTEE.DTITLE=EB 246
- * * ( R EVO )R AD 630 1
247
- * * (REVO) RAD 630 1
248 635 0 ADOWi=105 249 630640 1-7-3/8 L
OD=6.625.THI=.280 LBS/FT=26.084 250 251 645 9 L
DTITLE=EG-2-H13.SEG=2 252 650 3-1-5/8 253 RAD 650 1
L 254 655 O-9 255 660 6-1/8 L
?56 665 3 THI=.56.LBS/FT=378.2 257 675 7.51 THI=.28.LBS/FT=26.084 25R 680 -O-3.5 JOINT = RED.
259 OD=10.75.THI=.365 260 685 -O-3.5 LBS/FT=51.072.
261 THI=.73.LBS/FT=622.2.
?62 690 7 THI=.365.LBS/FT=51.072
?63 692 7.49 DTITLE=HB-12-4 i
264 FORCE =2120.AA=900
- W WT1 265 SPR 692 1
?66 695 8.:18 5 ADDWT=56.SEG=2 267 26e ANC 695 0.36 0.t27 L
DD=6.625.THI=.280 269 625700 2 11 LBS/FT=26.084
?70 6 L
?71 702 DTITLE=EB-2-H12.SEG=2 272 704 1-10
'73 RAD 704 1
/
L
??t 706 0-9 275 708 6-1/8 L
276 710 3 THI=.56.LBS/FT=378.2 277 714 7.5 THI=.28.LBS/FT=26.084 278 716 3.5 JOINT = RED.
279 DD=10.75.THI=.365 280 718 3.5 LBS/FT=51.072 281 THI=.73.LBS/FT=622.2 282 720 7 THI=.365.LBS/FT=51.072.
283 721
-O-7.49 DTITLE=HB-12-3, 4
284 FDRCE=2120.AA=900
- W Wil 285 SPR 721 1
286 722 8.385 ADDWT=56 287 288 ANC 722 0.36 0.127 L
00=6.625.THI=.28, 289 620724 4-3 LBS/FT=26.084 290
?91 726 3 L
DTITLE=EB-2-H11.SEG=2 292 728 O-9 j
293 RAD 728 1
5
)
?94 730 0-6
s MF101/K3 DATE 081385 PAGE 6
295 732 6-1/8 L
296 734 3 THI=.56.LBS/FT=378.2.
297 738 7.51 THI=.28 LBS/FT=26.084 278 740 3.5 JOINT = RED.
299 DD=10.75.THI=.365 300 742 -O-3.5 LRS/FT=51.072.
301
'HI=.73.LBS/FT=622.2.
302 744 7 THI=.365.LBS/FT=51.072.
303 745 7.49 DTITLE=HB-12-2, 304 FORCE =1276.AA=520
- W WT1 305 SPR 745 1
306 746 8.385 ADOWT=56, 307 308 ANC 746 0.36 0.127 L
OD=6.625.THI*.28, 309 615748 5-6 LBS/FT=26.084 310 311 750 3 DTITLE=EB-2-H10.SEG=2 312 RAD 750 1
313 752 9 L
314 754 6-1/8 L
315 756 3 THI=.56.LBS/FT=378.2 316 760 7.51 THI=.28.LBS/FT=26.084 317 762 -O-3.5 JOINT = RED, 318 OD=10.75.THI=.365 319.
764
-O-3.5 LBS/FT=51.072 320 THI=.73.LBS/FT=622.2.
321 766 7 THI=.365.LBS/FT=51.072 322 767 7.49 DTITLE=HB-12-1 323 FORCE =1276.AA=520.
- W WT1 324 SPR 767 1
325 768 8.385 ADDWT=56 326 327 ANC 768 0.36 0.127
' 4 L
OD=16.THI=.656 328 505770 LBS/FT=124.689 329 DT I T LE = EB-2-H14. -
. WT1 330 772 2 FORCE =2037.AA=340.
- W 331 SPR 772 1
332 773 0 L
333 774 0 DTITLE=NEW RIGID.SEG=2 9 334 776 335 RAD 776 1 3 L
336 778 337 779 4 5
DTITLE=EB-2H16 338 780 7-9 FORCE =2656.AA=450
+W WT1 339 SPR 780 1
DTITLE=EB-2-H16, 340 781 0-11 1
341 RAD 781 L
342 782 J-O DTITLE=NEW RIGIO.
343
- (REVO) 781 2-0
\\
1 344
- +(REVO) RAD 781 L
345
- ++(REVO) 782 2-0 4 DTITLE=(EAB4)2R-2-4 346 784 HYS=E4BS-5 347 EAB 784 1
- O
. THRM1 WT1 SEIS08 DD=.100
- D SEISDB 348 0D=.157 349 350
- SNB 784 1
j 9-1/2 351 786 f
352 788 3 THI=1.312.LBS/FT=1164 DTITLE=(EABS)EB-2-H11.SEG=2 353 790 9 THI=.656.LBS/FT=124.689 l
354
ME101/K3 DATE 081385 PAGE 7
HYS=E485-5, 355 EAB 79) 1
- O THRM1 WT1 SEISOB DD=.100
'356 0D=.119
- D SEISDB 357
't S R
- SNB 790 1
- 15 9 RAD 790 1
'16 0 792 11-1/2 TEE =WTEE, 361 794 0 TEE =WTEE, 36?
796 0 TEE =WTEE,
- 63 798 0 TEE =WTEE, 364 800 6-1/2 DTITLE=EB-2-H18,SEG=2,
6 5 RAD 800 1
-O-11-1/2 ADOWT=105, 3GG 802 367 798804 7-3/8 L
DD=6.625,THI=.28 LBS/FT=26.084,
'16 9 369 806 11 L
DTITLE=EB-2-H22.SEG=2,
~170 807 1-5/8 17i RAD 807 1
-O-9 17 1 810 9-1/8 L
374 812 8-9 THI=.56.LBS/FT=378.2,
.47 5 81G 1-7.51 00lNT= RED THI=.28, 176 818 O-3.5 LBS/FT=26.084, 377 00=10.75,THI=.365, 278 820 0-3.5 LBS/FT=51.072, 379 THI=.73 LBS/FT=622.2.
3EO 822 2-7 DTITLE=HB-12-8 THI=.365 381 823 1-5.49 LBS/FT=51.072, 382 FORCE =1956,AA=340,
+W WT1 383 SPR 823 1
384 824 10-1.385 ADOWT=56, 385 386 ANC 824 -0.36 0.127 L
OD=6.625,THI=.28, 287 796826 11 LBS/FT=26.084 38R 389 828 8 L
DTITLE=EB2-H21 SEG=2, 390 829 10 391 RAD 829 1
L 392 830 9 393 832 9-1/8 L
SEG=3, 394 834 13-9 THI=.56 LBS/FT=378.2, 395 838 1-7.51 THI=.28,LBS/FT=26.084, 196 840 0-3.5 DTITLE=HB-12-7,
- 19 7 JOINT = RED, 198 FORCE =2649 AA=600.
- W WT1 399 SPR 840 1
OD=10.75 THI=.365, 400 842 0-3.5 LBS/FT=51.072 401 THI=.73,LBS/FT=622.2, 102 844 2-7 THI=.365.LBS/FT=51.072, 403 846 6-6 7/8 ADOWT=56, 404 405 ANC 846 -0.36 0.127 L
00=3.625,THI=.28, 406 794848 3 LBS/FT=26.084, 407 5 S
408 850 DTITLE=EB2-H20,SEG=2, 409 851
-O-6 410 RAD 851 1
-O-9 l
412 854 9-1/8 L
l 413 856 8-9 THI=.56 LBS/FT=378,2 414 860 1-7.51
A ME101/K3 DATE 081385 PAGE 8
t TH1=.28.LBS/FT=26.084 015 862 0-3.5 JOINT = RED.
416 OD=10.75.THI=.365 417 864 0-3.5 LBS/FT=51.072.
418 THl=.73.LBS/FT=622.2 419 866 2-7 DTITLE=HB-12-6.THI=.365 420 867 1-5.49 LBS/FT=51.072 C21 FORCE =1956.AA=340
+W
. WT1 423 SPR 867 1
423 868 10-1.385 ADOWT=56, C34 435 ANC 868 -0.36 0.127 L
00=6.625.THI= 28, 436 792870 6 LBS/FT=26.084 427 5 OTITLE=EB2-H-19 SEG=2 428 871 439 RAD 871 f
430 872
-O-9 L
431 874 9-1/8 L
432 876 13-9 THI=.56.1BS/FT=378.2.
433 880 1-7.51 THI=.28.LBS/FT=26.084 434 882 0-3.5 DTITLE=HB-12-5.
435 JOINT = RED.
436 FORCE =2649.AA=600
- W WT1 437 SPR 882 1
OD=10.75.THI=.365 438 884 0-3.5 LBS/FT=51.072 439 THI=.73.LBS/FT=622.2.
440 886 2-7 THI=.365.LBS/FT=51.072 441 888 6-6-7/8 ADOWT=56, 402 443 ANC 888 -0.36 0.127 444
- EAB LOADING CURVE 445 HYS=E4BS-6, 1CG Hv5 XV=.142.FY=8790 447 448
.000
.000
.278
.278 556
- 485, 1.03
.703 A49 1.50
.851 2.40.
.990.
3.50 1.07 4.44, 1.12, 450 5.56, 1.14 100.0 1.50, HYS=E485-5 451 His XV=.142.FY=7325 152 453
.000.
.000.
.278
.278.
.556 485 1.03
.703, 454 1.50
.R51, 2.40.
.990, 3.50.
1.07 4.44, 1.12, 455
- f. 56 1.14 100.0.
1.50.
HYS=E485-3 456 Hv5 XV=.142.FV=4395
.iS7 438
.000
.000
.278.
.278.
.556 485 1.03
.703, 459 1.50
.851, 2.40.
.990.
3.50 1.07 4.44, 1.12 460 5.56 1.14, 100.O.
1.50.
TITLE = ENV AUX (S) 488-AUX (C) 6.
461 462 ACE 2.5'8 CONT 105' OBE 463 ACE LDNAME=SEIS08 464 ACF TYP=3. POI =20.CDAMP=.OOS.
465 ACE DIR=X+Z 466 ACf 467
.1000.
.0000
.5700
.0428 1.1500
.1016 46R 1.3000
.1193 1.5000.
.1668 1.5500
.5487.
469
- 1. 7eXX).
1.7000 1.8200.
1.7000, 2.0000 1.5382.
470 2.3300.
1.3200 2.3400, 1.3200, 2.9800
.8542 471 3.7590.
.4600 4.1000.
.4348 6.0000
.6900 472 7.6000
.6900 8.0000
.3200 10.1000,
.1751 473 11.0000
.1700 100.0000
.1700 DIR=Y 474 ACE
ME101/K3 DATE 081385 PAGE 9
475
.1000
.0063
.3400
.0200
.5000
.0306 476
.6700,
.0433, 1.0000
.0670 1.2500
.0830.
477 1.6700.
.1166 2.0000
.1333, 2.5000
.1533.
478 3.3300.
.1866, 5.0000
.2000.
6.6700
.1866.
479 10.0000
.1333, 12.5000.
.1000.
14.2850
.0830 480 16.6700.
.0666 20.0000
.0533 25.0000
.0400.
481 100.0000
.0333 100.0010
.0333 482 EOA TITLE = ENV AUX (S) 48'-AUX (C) 6.
483 ACE 2.5'& CONT 105' DBE(2OBE).
484 ACE LDNAME=SEISDB.
485 ACE TYP=3. POI =20.CDAMP=.OOS.
. 486 ACE DIR=X+2 487 ACE 488 1000
.0000
.5700.
.0956, 1.1500
.2032 489.
1.3000.
.2386 1.5000
.3336, 1.5500 1.0974 490 1.7000.
3.4000.
1.8200.
3.4000 2.0000, 3.0764 491 2.3300 2.6400 2.3400 2.6400 2.9800 1.7084 492 3.7500.
.9200 4.1000.
.8696 6.0000, 1.3800 493 7.6000 1.3800, 8.0000
.6400.
10.1000
.3502, 494 11.0000
.3400.
100.0000
.3400.
DIR=Y 495 ACE 496
.1000.
.0126
.3400
.0400.
.5000.
.0612.
497 6700.
.0866 1.0000
.1340 1.2500
.1660.
498 1.6700.
.2332, 2.0000
.2666, 2.5000.
.3066 3.3300.
.3732, 5.0000.
.4000, 6.6700.
.3732, 499.
10.0000.
.2666 12.5000.
.2000 14.2850.
.1660 500 501 16.6700.
.1332, 20.0000.
.1066 25.0000
.0800 502 100.0000.
.0666.
100.0010.
.0666 503 E0A INCLUO=NTt 504 SLA LEVEL =8 INCLUO=WT1+SEIS08 505 OLA LEVEL =C.INCLUD=WT1+SEISDB 506 OLA LEVEL =D.INCLUO=WT1+SEISOB 507 OLA INCLUO=THRM1+WT1 508' TEA LIST =THRM1*WT1+SEIS08+SEISDB 509 RLS 510 END
+
+
+
+
+
+
+
+
+.
510 CARDS IN INPUT DECK 483 CARDS IN LOAD CASE THRM1 503 CARDS IN LOAD CASE WT1 483 CARDS IN LOAD CASE SEIS08 483 CARDS IN LOAD CASE SEISDB O WARNINGS O ERRORS O FATAL ERRORS SFREE WORKER.
U: 12O433 filename not known to this run.
l
- FREF SLPACH.
W: 120433 filename not known to this run.
l l
i l
- XOT.M
'ME101.ME1011 THRM1
1 i
ENERGY ABSORBER LOADING CURVE Size E4B5-5 Deformation (in)
Force (1b.)
0.0000 0
0.0395 2036 0.0790 3553 0.1463 5149 j-0.2130 6234 0.3408 7252 0.4970 7838 O.6305 8204 0.7895 8351 Elastic Design:
Yield displacement (XY) =.142" Yield force (FY)
= 7325 lb.
I 4
i 1
I i
1
-~-
-,.., ~,.. _ ~. - -.. -, - - _
.~ -.
ENERGY ABSORBER HYSTERESIS CURVE Size E4B5-5 9
g_
O 7-6-
5-4-
3-2-
nnh 1-bj 0 O
d O 3
. [t 2 26
_3 _
' c
-0.8
-0. 6
-0.4
-0.2 O
O.2 0.4 0.6 0.8 DEFORMATION (IN.)
O a
ARTIFICAL TIME HISTORY GENERATED FROM BROADENED ENVELOPED DBE SEISMIC SPECTRA HORIZONTAL COMPONENT
(
00801-1
I CE980 VER A2 DATE 102386 PAGE 58 rien -HisinP r iOffU I?EACH HORIZONTAL CYCLE 6
+++ TIME HISTORY ***
ACCELERATION TIMT (G'S)
E LEC D t000
.D 0900
.026613
.024057
.020716
.017568
.015024
.013331
.011827
.010163
.008591
.006217
.002489 i
.1200
. 07)SO0
.002378
.004801
.007041
.008435
.009101
.007587
.006785
.004223
.001849
.000484
.002164 j
.3400
.0u5570
.009647
.011711
.012511
.012726
.011788
.013068
.011496
.009991
.009456
.008487
.006765
.WO
.095179
.003106
.0C2940
.002598
.000959
.001970
.003060
.007084
.008693
.009497
.O10278
.008731
}
. tPOO
.010925
.012172
.011960
.009196
.083170
.015606
.014153
.017172
.018014
.021789
.019707
.020504 u000
.013789
.017063
.0C9691
.002612
.013267
.018542
.024436
.035942
.033805
.038238
.032839
.030802
.7290
.02S706
.025911
.022169
.019616
.020537
.023359
.026160
.026377
.023648
.021216
.018448
.010518 "4Co
.001019
.018028
.022139
.026037
.031523
.036036
.041193
.037257
.030E07
.028954
.027745
.023378
- E 00
.01951G
.017489
.012797
.011160
.005404
.006867 000986
.006723
.012774
.022749
.026053
.025303 t u$ n 024774
.033983
.026622
.029096
.025961
.029968
.027038
.025876
.025411
.024947
.013920
.019841 J000
.016517
.015266
.011146
.010584
.012789
.007918
.006557
.007491
.000403
.001561
.001817
.001150 12' o
.Ogo999
.011551
.011724
.011608
.016783
.024653
.040887
.049506
.058544
.070871
.072565
.077054
'.14ou
.07P273
.072235
.063841
.045403
.0240f9
.000560
.018862 046017
.059960
.065474
.070426
.064757
- f' o
.059532
.03803G
.028810
.016245
.009803
.003199
.010393
.014332
.019799
.030176
.057516
.073692
- 1. r.c ' A
.03U1G9
.069850
.051046
.039877
.0f0172
.089422
.052667
.080597
.094063
.110278
.106687
.099083 1.9000
.071760
.054764
.029390
.003174
.010126
.013989
.021041
.019862
.001317
.014060
.017383
.031291 1 92 4
.071052
.020504
.000418
.013020
.033203
.044127
.058394
.070316
.067333
.065596
.072486
.075229
. 41029
.007190
.007279
.031341
.047252 0
? e4< o 092583
.084819
.082776
.095511
.104753
.083989
.069468 16 > >
.065274
.071012
.072819
.067407
.062020
.076014
.061362
.057454
.066183
.068646
.078764
.094509
?e'H
.116333
.120579
.110899
.112929
.075434
.061307
.026851
.006024
.045455
.079908
.091504
.099676 4090
.110648
.102028
.099876
.074716
.042993
.051416
.039632
.040889
.055860
.061444
.068409
.077275 r290
.081654
.082237
.O79813
.060787
.053623
.044002
.024258
.012843
.026752
.031098
.054514
.049855 J.6400
.034949
.036383
.020811
.014174
.036424
.066062
.080566
.089661
.107601
.117493
.146929
.139323
?.7600
.154912
.153000
.163789
.167280 179386
.187915
.134451
.107067
.105972
.077678
.055578
.051111 2.H800
.015607
.017495
.001379
.012098
.015651
.038512
.063481 103477
.134839
.160298
.179395
.186289 3.0000
.1191SG
.186681
.169205
.1478b3
.152686
.f49674
.136880
.f46223
.141225
.145216 147189
.156271 1 1200
.145436
.141093
.123308
.081163
.049459
.006087
.040948
.084512
.135381
.152713
.186487
.211007 3.2400
.215348
.219808
.219132
.192760
.192761
.196932
.197575
.212293
.190796
.194806
.173417
.149254 3.3600
.112105
.072257
.039109
.006702
.044819
.104048
.150613 148309
.187265
.200362
.222101
.220177 3.4800
.2251G4
.213405 183824
.189238
.190143
.186908
.192299
.205086
.194191
.171849 149229
.141946 3.6000
.102847
.008492
.020428
.003853
.043455
.054928
.075382
.072632
.092433
.097189
.094229
.098002 3.7200
.121350
.135654
.154461
.178510
.199257
.211970
.228903
.227526
.203030
.190931
.170917
.151398 3.8400
.125522
.084924
.067346
.044728
.047227
.036093
.018999
.016213
.010487
.011795
.025776
.073642 3.9600
.101077
.136181
.178869
.192812 185200
.194335
.198313
.186770
.182717
.165916
.155140
.154950 i
4.0800
,127587
.118011
.100112
.110903
.082337
.O53534
.002609
.022682
.073279
.122690
.160704
.209678 l
4. 2O(O
.224699
.236380
.231892
.219339
.202801
.163663
.1602O4
.144545
.127867
.082982
.065933
.059018 4.3200
.049095
.038713
.013842
.006500
.034226
.048262
.054761
.086513
.089976
.086474
.093231
.085223 4.4400
.094946
.088352
.099950
.081882
.072811
.073446
.069890
.043499
.026931
.038570
.O32826
.049758 i
4.5600
.045132
.O51854
.073506
.088898
.088197
.104698
.109704
.108930
.095704
.068739
.033226
.000180 4.6R00
.046898
.092010
.117057
.149688
.169177
.183512
.184582
.190157
.193992
.187330
.184197
.161814 4.8000
.141703
.134545
.118373
.119543 109890
.083341
.089071
.094538
.081147
.058987
.050463
.022287 4.9200
.OO3G99
.048834
.094438
.125459
.157030
.189636
.185048 169335
.179043
.157575
.147973
.139677 5.0400
.138038
.123944
.100053
.089270
.O81855
.097031
.067247
.062061
.049782
.018594
.011919
.032592 j
5.1600
.053G5G 089083
.114294
.131992
.139276
.128197
.116168
.115153
.101277
.071850
.045828
.034236 5.2800
.026373
.018215
.023233
.003033
.018798
.024263
.036960
.027723
.039861
.023955
.019659
.013075 5.4000
.01803G
.030738
.079701
.094519
.089166
.118002
.119716
.087960
.057617
.025888
.006411
.023500 5.52CO
.049033
.043433
.039416
.034051
.024598
.003515
.033484
.051244
.072369
.092626
.084630
.066618 5.6400
.056933
.015614
.002368
.030654
.035175
.055723
.058732
.046997
.030716
.045739
.030221
.003870 5.7600
.011689
.022076
.034569
.034430
.037852
.036194
.015622
.011598
.004096
.029336
.030649
.043363 5.8800
.0G0201
.065587
.062156
.052588
.052520
.052854
.076076
.068292
.068986
.093140
.096475
.089456 6.0000
.091210
.080723
.05G713
.044280
.024288
.039648
.026995
.034121
.041495
.041202
.030379
.035692 6.1200
.001574
.033267
.058588
.081391 108374
.146848
.f59033
.155475
.143193
.115967
.096536
.069383 6.2400
.037229
.006701
.002546
.009615
.016147
.019694
.026164
.019634
.017182 002805
.008339
.011980 6.3600
.003644
.013286
.006742
.003551
.009273
.046991
.031427
.032888
.051209
.051756
.055833
.056385 1
l
e CE980 VER A2 DATE 102386 PAGE 60 il"r-HISTORV PulNT BEACH HORIZONIAL 13,68u0
.054689
.056203
.050583
.052942
.063257
.088848
.105689
.130860
.172772
.186543
.191126
.189577 i
- 13. P OC O
.185292
.155403 127579
.081981
.049330
.038613
.016781
.003498
.014523
.000756
.005323
.008726 13.9200
.006522
.024853
.042309
.062728
.096101
.105029
.108171 109832
.097587
.071067
.050409
.Ot7527 14.0400
.005782
.020726
.033961
.042360
.023750
.006249
.008272
.035059
.053186
.064160
.060478
.063128 14.frOO
.062630
.063079
.055912
.040336
.041183
.050344
.060960
.065775
.071047
.057874
.060010
.057193 11 2000
.044829
.026525
.015720
.009542
.030590
.044624
.052935
.071249
.082353
.101128
.127299
.150131 14.4000
.175671
.207418
.227611
.236523
.244215
.235730
.217688
.189828
.149975
.112814
.086414
.067226 t1.5200
.049610
.032334
.003595
.019525
.037641
.070011
.109258
.138709
.t80467
.226594
.265559
.295603 14 6400
.327040
.340857
.345360
.351905
.299049
.252005
.207371
.134965
.073406
.003541
.013574
.033275 11.7600
.023247
.030822
.020581
.016284
.021085
.021298
.066871
.105685
.158678
.205984
.247957
.275876 14.8800 277229
.279811
.271227
.247250
.224746
.190178
.19G317
.170232 153049
.124684
.121288
.078481 15.0000
.09348G
.066938
.053692
.031376
.022696
.040519
.068185
.088324
.111023
.t13918
.148757
.149683 15.1200
.160774
.141998
.130650
.130569
.111467
.112123
.109642
.105704
.097205
.105506 091351
.084V27 15.2400
.079534
.062949
.062675
.047262
.027889
.015585
.006597
.000572
.009423
.001547
.005387
.029379 15.3600
.026417
.055264
.077967
.09f229
.117t19
.f32544
.130952
.129852
.112247
.090702
.069012
.053019 15.4800
.039455
.014808
.015904
.005086
.014710
.011691
.010850
.023798
.012532
.009272
.026679
.029218 1
15.6000
.021629
.036993
.033191
.041799
.040425
.037724. 040453
.04269G
.034303
.035306
.025306
.020662 15.7200
.018481
.021465
.035816
.049245
.039102
.033426
.019715
.032457
.025863
.021344
.031770
.045108 15.8400
.069926
.080924
.093863
.108248
.105741
.180542
.O89898
.063570
.029969
.009902
.040089
.06b996 15.9600
.090285
.099403
.125671
.109163
.113280
.106423
.098604
.094674
.087450
.084272
.085700
.086674 16.6300
.087941
.093120
.097919
.08806S
.076539
.046870
.032001
.018560
.004551
.016114
.038640
.O78382 16.2000
.094956
.104261 114983
.119034
.125469
.133383
.129961 138051
.f42573
.t37045
.114721
.112957 16.3200
.114220
.115553
.087919
.068870
.043916
.018132
.003643
.006109 051395
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.106593 16.4400
.141406
.155639
.154252
.169554
.154726
.153376
.146788
.113522
.109832
.106446
.072743
.070928 16.5600
.043504
.038961
.019246
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.011765
.002740
.Of2917
.026532
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.064946 16.6800
.t02369
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.192347
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i" tt'
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.169994 to 7lo 1%P'60
.140731
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.022235
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- M7 to
.118410
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oP o i ? *. rA
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20.'
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i 1
a A
l CE980 VER A2 OATE 102386 PAGE 62 TIME-HISTORY POINT BE ACH HORIZON 14L 28,0809
.Of2529
.Of0605
.006799
.007395
.001441
.001436
.004331
.002672
.002298
.002963
.003499
.003490 2 8. 2 XO
.001038
.000627
.001173
.000466
.003228
.003551
.004814
.002484
.002837
.001682
.002328
.002349
?S.32Co
.004066
.004505
.004050
.005845
.007379
.008454
.008272
.010729
.011377
.011267
.011287
.011117 28.14CO
.010168
.009445
.009958
.000005
.007934
.006850
.006927
.005073
.002641
.002104
.000513 004353 28.56 M
.004729
.005420
.OOG260
.006416
.006525
.007082
.006012
.005748
.006618
.007954
.009188
.011036-1 2 8. Get o
.012480
.081962
.Of3255
.012276
.010234
.008745
.006504
.003588
.001373
.000521
.000500
.001104 28.8000 001423
.00119G
.001291
.001160
.002347
.0034G4
.003097
.007188
.008948
.012404
.013909
.016105 28.9209
.015912
.015786
.015999
.015811
.014945
,01191G
.011190
.010025
.007917
.004733
.004104
.000356 29.0400
.002043
.003724
.005719
.006648
.007138
.007652
.006997
.006474
.005371
.005996
.004813
.005569 29.1f.00
.005885
.007149
.009644
.008896
.008870
.009212.
.008832
.00768G
.006471
.004095
.002755
.000877
- 29. 2 SCW)
.001072
.001355
.000996
.001233
.001749
.001891
.001474
.001308
.000102
.000762
.000543
.000315 29.4000
.000401
.000131
.009441
.001489
.002780
.003870
.004358
.004342
.003870
.003483
.003003
.002278 29.5200
.001997
.001636
.001534
.001587
.001449
.001631
.001573
.001262
.000986
.000786
.000147
.000838 29.6400
.000803
.000768
.000572
.000804
.000580
.000343
.000396
.000198
.000019
.000105
.000080
.000280 29.7EOO
.000343
.000775
.009690
.000548
.000828
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.000169
.000145
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.000095
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.000227
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.000171
.000118
.000045
.000001
.000024
,000001 t
30.0000 000000 MhlMUM ACCELERATION
.351905 G'S AT 14.6700 SEC 4
4 6.6450 SUP-SECONOS
+*. f!ME *** TIME ',PINI IN OtRIVIN'1 THE SPECTRA
=
i i
i l
l
\\
i t
I!
i CE980 VER A2 DATE 102386 PAGE 64 TIML-HISTORY FOINT BEACH HORIZONTAL 4
38.2287 6.0843 1.3800 1.3801
.01 5.9000 40.6275 6.4600 1.3800 1.3788
.09 14.9000 43.1767 6.8718 1.3800
-1.3801
.01 6.7900 45.8860 7.3030 1.3800
-1.3799
.01 17.1600 49.7652 7.7612 1.0772 1.0750
.20 14.8700 51.8252 8.2482
.6020
.6038
.30 14.6200 55.0771 8.7658
.52G3
.5273
.19 7.5000 58.5330 9.3158
.4507
.4540
.73 14.6400 G2.2059 9.9003
.3750
.4201
-10.73 14.6600 CG.1092 10.5216
.3453 3760
-8.16 14.8600 70.2574 11.1818
.3400
.3428
.82 14.6750 74.6659 11.8834
.3400
.3453-
-l.53 14.6300 79.3510 12.6291
.3400
.3502
-2.91 14.8850 81.3301 13.4215
.3400
.3600
-5.55 14.8750 83.6216 14.2637
.3400
.3577
-4.95 14.6550 95.2452 15.1587
.3400
.3492
-2.63 14.6400 101.221G 16.1099
.3400
.3483
-2.38 14.6400 107.5731 17.1207
.3400
.3483
-2.37 14.6500 111.3231 18.1950
.3400
.3472
-2.06 14.G450 l
121.4966 19.33G7
.3400
.3483
-2.39 14.6450 123.1202 20.5501
.3400
.3523
-3.48 14.6433 131.2223 21.839G
.3400
.3525
-3.53 14.6700 145.8327 23.2099
.3400
.3538
-3.91 14.6700 151.9831 24.6663
.3400
.3520
-3.40 14.6500 164.7083 26.2141
.3400
.3481
-2.33 14.6700 175.0133 27.8589
.3400
.3492
-2.64 14.6700 1PG.02C9 29.G070
.3400
.3487
-2.50 14.6700 197.6997 31.4648
.3400
.3526
-3.57 14.6550 210.1000 33.4392
.3400
.3500
-2.86 14.6700
??3.238G 35.537M
.3400
.3495
-2.73 14.6725 237 29T4 37 7673
.3400
.3545
-4.10 14.6550 2 52.1 L' O r.
40.1371
.3400
.3505
-2.99 14.6540 269 0101 42.6556
.3400
.3568
-4.70 14.6700 234 9 :11.:
45.3322
.3400
.3542
-4.00 14.6720 3O? 70'1 48.1767
.3400
.3497
-2.78 14.6580 321 6973 51.1997
.3400
.3511
-3.17 14.6717 J11.HP17 54.4123
.3400
.3558
-4.44 14.6700 363.1361 57.32GG
.3400
.3544
-4.07 14.6717 104 134:
61.4551
.3400
.3572
-4.82 14.6671 410.1GT' 65.1113
.3400
.3545
-4.08 14.6629 1'16 11T' 69.4094
.3400
.3570
-4.75 14.6686 493 5 7 a 'i 71.7647
.3400
.3562
-4.54 14.6650 1
41?. ! 6U 7R.3933
.3400
.3575
-4.90 14.6700 523 1G81 83.3123
.3400
.3510
-3.14 14.6700 536 114'.
88.5400
.3400
.3525
-3.56 14.6644 591 2221 94.0957
.3400
.3567
-4.67 14.6710 G?n 3N t 100.0000
.3400
.3525
-3.54 14.6700 100.00 %
t' A < l M lt.1 Di r r E R t.tK.E =
rt OT a**
1 l' LOT CRFATED (TIME HISTORY FOR CYCLE 6)
I'l o t ++*
1 PLOT 15) CRLATED (RESPONSE SPECTRA FOR CYCLE 6)
ARTIFICAL TIME HISTORY GENERATED FROM BROADENED ENVELOPED DBE SEISMIC SPECTRA VERTICAL COMPONENT 1
I 00801-1
CE980 VER A2 DATE 102386 PAGE 58 T tf tr -H1%IWI 00lfil BEACH VERTICAL CYCLE -
6 TIME HISTORY ACCELERATION F I rn (G'S) 4 Nf 6 6 (E O
.O^O000
.004296
.005021
.005369
.005630
.006124
.007258
.007974
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. Or T5 2 8
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?4W M o432
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.002173
.002737
.002087
.004382
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.005339
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.001239
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. I mo
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.002O28
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.001793
.000659
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~%o
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- M
. O'T1 14
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' 1400
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.017678
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- 5. m o
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- f. W M
. fy4790
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? 2900
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.009237
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.'.1000
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.012938
.008933
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.009697 5200
.047568
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.000164
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?.6400
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.003648 000077
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.015295 1.2400
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.010582
- 3600
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.009064
.007782
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.033088
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.013357
.016289
.022381
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3.0000
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.014666 3.9600
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.015040 4.0800
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.013986
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.041999
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.003196
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.021824 1.3200
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.036876
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.018778
.018395
.006778 4.4400
.012660
.007325
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.012421
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.011661
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.009865 4.5600
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.016261
.002939
.004015 4.6800
.016589
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.035750 042O34
.043477
.048945
.044335
.043871
.049115
.050805
.051977
.041312 4.8000
.031234
.034118
.023356
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CE980 VER A2 DATE 102386 PAGE 59 T ip E-ttl5IORY POINT DLACH VERTICAL 3
6.4POO
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CE980 VER A2 DATE 102386 PAGE 60 Tl"F-PISTOR(
POINT BEACH VERTICAL 1'.6800
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i CE980 VER A2 DATE 102386 PAGE 62-TIME.HtSTORY POINT BEACH VERTICAL 28.0809
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.i 6.6450 SUP-SECONDS TIME SPFNI IN DERIVING THE SPECTRA
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CE9BO VER A2 DATE 102386 PAGE 63 Tire-H1510R( POINT BE Allt VERTICAL TARGET VS CALCULATr0 SPECTRAL ACCELERATION (G'S) FOR DAMPING =
.005 +++
CYCLE 6
1ARGET CALCULATED FREOUENCY FREOUIN(.y ACCELERATION ACCELERATION DIFFERENCE TIME (RAD /5EC)
( C PF. )
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CE980 VER A2 DATE 102386 PAGE 64 TitME-HISTORY POINT BEACH VERTICAL 38.2287 6.0843
.3817
.3818
.00 8.5500 40.6275 6.4660
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-34.28 8.2975 223.28RC 35.5374
.0766 1128
-32.12 15.3275 2 3 7, 2 0 "* ".
37.7673
.0760
.1043
-27.13 10.2750 252.199'i 40.1371
.0754
.1036
-27.22 16.7160 268.0131 42.6556
.0748
.1023
-26.87 14.9440 293 93t?
45.3322
.0742
.1025
-27.56 10.2720 302 7079 48.1767
.0737
.1038
-29.06 15.0260 321 697H 51.1997
.0731
.0887
-17.57 15.0217 311.4837 54.1123
.0725
.O961
-24.58 4.1967 341,334' 57.8266
.0719
.0900
-20.12 7.8200 3* G.174.-
G1.4551
.0713
.0820
-13.04 17.3714 410.3G74 65.3113
.0707
.0752
-5.93 10.2686 4PG 117:
69.4094
.0701 0732
-4.23 14.6686 467.17PR 73.7647
.0695
.0752
-7.47 14.6650 41? 360' 78.2933
.0690
.0682 1.13 14.6675 521.164 i R3.3123
.0684
.0705
-3.07 14.6633 556.314-
88.5400
.0678
.0761
-10.89 14.6622
o f ??>l 94.0957
.0672
.0667
.69 14.6700 GJ9 320' 100.0000
.0666
.0650 2.45 14.6700 34.28 7.
f1 A.s t r.e m D i r r E R E NC E
=
l't oi i* 1 PLOT CRE ATED (TIME HISTORY FOR CYCLE 6)
FLot **
1 PLOT ( S ) CREATED (RESPONSE SPECTRA FOR CYCLE 6) l l
CE980 VER A2 DATE 102386 PAGE 65 61 r'<
felftti f I At il VII'T f C AI 10
= fl I C i f Ill? f!llf1Pf P f)T I TERATION CYCLES (UMPL E IF D
' ' Iii l'R ilJ T 1 1
l l
6
/
O e
ME101 INPUT DESCRIPTION
)
ME101 Devolep.f;nt I
Spncificaticn with
.... COPYRIGHTED AND CONFIDENTIAL Input & Methodology SECTION I DATA P REP ARATI-)N COORDIN ATE SYSTEMS _
follow the right hand rule Global and local both coordinate systems coordinates respectively.
and are symbolized by (X,Y,Z) and ( a,b, c)
Both are cartesian systems of coordinates.
Global Coordinate. System (X,Y, Z)
The y-axis is Any point may be chosen as the origin of the system.
in parallel with gravity and points upward.
F, Y
C My v
O a
5 g Un Mg
\\
X Z
E n F,
Local Coordinate Systems ( a,b, c) for various elements is The orientation o f local coordinate systems explained below:
~.
i.
ME101 D3valopm:nt Specification with
.... COPYRIGHTED AND CONFIDENTIAL Input & Methodology the local coordinate to E, For a bend, traversed from B llows:
system at any point on the bend is as fo Bend.
In the plane of the bend and in the forwardto direction of the tangent a-axis:
(bend traversal) the bend at the point In the plane of the bend and toward the center b-axis:
of curvature.
from Established by the right-hand rule c-axis:
and b-axes.
a-E
[
i l
BEND l
1
~- D e
traversed from B to E, the local coordinate Tangent.
For a tangent, is as follows:
any point on the tangent system at Along the axis of the pipe and in the direction a-ax s:
from B to E from a-Established by the right-hand rule b-axis:
and c-axes Lies along the line of intersection of the
- 1) a plane perpendicular c-axis:
following two planes:a plane parallel to X-Z and 2) it to a-axis,Its positive direction is such that plane.
Z-axis.
a positive projection on the makes The following are special cases:
E xcep tions_.
is not valid when the The above definition for c-axisFor this special case, the a-axis lies in Y-Z plane.
c-axis is arbitrarily assumed to coincide with the X-axis.
ME101 DSvolopm:nt Sp cification with Input & Methodology
,,.. COPYRIGHTED AND CONFIDENTIAL J4 - nay, Avea the local coordinate system is as follows:
For a restraint, Restraint i
from Along the axis of the restraint and in the direct on f structure t.he point of pipe attachment to the point o a-axis:
attachment.
the local coordinate system is as follows:
For a component.,
Component and end (E)
Along the line connecting the beginning (B)in the direc a-axis:
points of the connponent d c-axes.
Established by the right-hand rule f rom the a-an b-axis:
defaults to the same as of tangent.
Established by input, c-axis A
N(
,s' 4
w A
i AT FMO cf 'ut SEAM f'l At FEE :rven tu r.AI!
A Ast$ 3181 TI:
N
,J M. ~ {
~
A WED IN Af SE:!M4f4G CF ?NE SEAM Af FACE VIE POSITIVE A AXI$ DIRg;?!OH es:tesA, excw r:=:ts f
i l
6 I-3
ME101 Dtv@lopmant Specificction with
.... COPYRIGHTED AND CONFIDENTIAL Input & Methodology INFtyI CCDING FORM is an input data coding form, in which the data Shown in Fig. (I-1)
- 50) is fixed format in the sense entered on left hand side (up to col.The data entries on the right enat data goes in specific columns.
f ree format means that hand side (cal. 51-80) are f ree f ormat.
- Here, required to be in specific columns.
the parameters defined are notdata coding form are defined as follows:
Various entries in the input Data Descriotion Col.
field I
I 1-3 Ident1iles the general Element type tag type af data entry.
4-9 The FRCM data point Data Paint Numoers 1
(col. 4-6) and To data point (Col.
7-9) designate geometrical locations in the piping system.
10-42 Three fields each with Increments columns are used for garameters associated with the global X,Y,I j
i coordinates of the piping systemu.
I I
43-49 Descrices a tend or curved
- hadius pipe element.
(See page I-31anx-1)
J l
If LIG E1,
=2, a non-blank 50 l
i Mass eritry in this field designates a mass paint in the system.
If EIGEN I
= 1 all data paints in the system will be considereo i
as mass points.
Additional piping 51-60 Derines s pecific
, parameters associated and loading data with piping system.
(Keywords)
)
79-60 Assaclate data cards with i
i
- -Optians corticular load cases.
t
i ameoH or<0o5as3o a
i mooo* ro;;1lo3 cPn#
oO' <.NHo o
yHo yg>1 ssecn m %fyoaoHO$
t o
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O M tf i I,
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- lll, gllI8, I
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ME101 Davalopmant Spacification with
.... COPYRIGHTED AND CONFIDENTIAL Input & Methodology monarks The data point numbers may be defined by any alphanumeric characters e
(i.e. 5, 35, 15).
If an element extends f rom the lausdodiately preceding TO data poin no his rule is entry should be made la the FROM field. The one excep e
h hored anchor and the current element continues throug as follows:
element (see remarks for the ANC card).
data The unit of length for the entries in the X, Y and 2 in e
sed in except for the ANC card, where imposed displacements must be expres inches if UKLY = ENGLSH, and in millimeters if UKEY = METRIC (see description of UKEY on the CTL card).
If Units.= 1 or 2, the user may specify the pipe geometry (X, Y, increments and radius entries) of an inch) units. Examples of such entries are shown below:
Decimal Equivalents _
Entry (ft)
(in) 10-3-1/2 10.292 123.5 4
-0.333
-4 0-10.5
.875 10.5 f
The same type of input may also be used for the radius field. Because o it is not advisable to use both types of entries in type of entry closure errors, describing closed-loop piping. Tne (fsst-inches-fraction) is i' legal if UNITS = 3.
[fieldconsistsof The general format of data entry in the additional Jac
' " data definitions" separated by cosanas. A "datrdefinition" consists of a e
keyword, followed by an equal sign, followed by the keyword value.
Continuation cards may be used for additional data. A continuation card must have Col. 1-9 blank. Except for the keywords TITLE, PROBNO, PR and USER, a data definition must appear on one cards it may not start on l
one card and continue on the next.
definition" input may be prepared
_It-is important to note that the " data
' using either the English or the Metric System of Units, even though th 1
e f
input units specified in the description of the various data sections o i
p this manual correspond to the English system. The corresponding Metr c units associated with each data section are presented in Appendix (g).
The data point number of a tangent intersection point of a bend should e
not appear as a FROM entry, Do not put blank lines or cards in the input data.
e I
I-5
=L.
ME101 Davolopmsnt Spscification with COPYRIGHTED AND CONFIDEN"IAL Input & Methodology g OPTIONS EftB MULTpLS LOADING CONDITIONS ANDMR GM i i In general, a series of load analyses must be performed on a p p ng f
system in.)rder to analyze its performance under a variety o Examples are as follows:
condition';.
Apply multiple thermal loads to the same piping system.
Perform dead load analysis f or full and empty pipes.
condition for different load cases.
Vary restraint (RAD)
Vary pipe characteristic (size, thickness, etc).
The data cards that apply only to a particular load case are identified by an asterisk in column 79, followed by the runThis is refer a
toentification in column 80.
'The run identification may be either num&ric or alphabetic.
bl A data card is applied to a load case by listing its *-option la e d after the load case name defined by the LDCASE keyword on a RUN ca a star-option are assumed to apply to all load All data cards withoutAll data cards which have a star option which is not c ase s.
on a RUN card, are ignored.
SIA, OLA, TEA,PBA, CMB, STD, RLS,
- -options must not be used on any RUN, CTL or ZPA card.
l l
l l
l l
l I
I
=,---,-c-----rmw eeie-'--r
,-,-------->-,v=-
w w*+-ww-y er.-e g----+-
+--w.w-ye m sc. e - w g-g-7
---wrw w www--
w=
.u
ME101 Davelopmsnt Specification with Input. & Methodology
.... COPYRIGHTED AND CONFIDENTIAL
)
ORDER OF DATA DECK t
An ME101 data deck must start with a RUN or HED 1.
card.
The ME101 deck consists of 6 separate sections.CTL, RCL, RUN, HED, ZP 2.
The control section cards:
SAP, ANC, CMP, BLANK, CCC, RAD,
2.1 2.2 The geometry section cards:
RAR, SNB, SPR, SPD, FOR, MOM and OLD TIM 2.3 The tima history section cards:
ACE, E0A The acceleration section cards:
SLA, OLA TEA, PBA, CMB, RLS, STO 2.4 2.5 The combination section cards:
END 2.6 The end of deck card:
The user can only place *-options on geometry cards and the HED c 3.
All ME101 problems should not be stacked, i.e., each separate ME problem needs a set of control cards. See Section II for additio 4.
information.
All restrain elements (RAD, RAR, SNB, SPR, SPD) and applied force or moments (FOR, OLD, MOM) should appear freediately following t S.
on which they were defined. The ANC card should also inmediately the data point unless it is at the beginning of a branch.
The order of cards should be prepared as follows:
6.
Control section cards Geor.etry section cards Time history section cards Response Spectrum Acceleration section cards Combination section cards End of deck card.
9 I-7
ME101 Devolopmsnt spscification with
.... COPYRIGHTED AND CONFIDENTIAL Input & Methodology ORDER OF DATA DECK (Cont'd)
Example:
9RUN 9 ADO P$*ME101.RUN1 RUN LOCASE=SEIS1 LOCASE=WT1 RUN TITLE =MY ME101 JOB, HED Control USER =ME101 USER, Section UNI =1, M00=20, ANC 5 00=24, THICK =.8 Geometry 10 1
LBS/FT=12 Section 15 1
20 1
ANC 20 DIRXON=X+Y+Z, TYP=0 Acceleration ACE.1,.1,.2,.1,.3,.5 Section E0A Cortination OLA Section SLA End Section END SADO P$*ME101.RUN2 9 FIN NOTES:
The UNITS keyword on the HED card and the TYPE keyword on the ACE card are 1.
required.
The two RUN cards have been entered to request a weight and a seismic 2.
analysis. Since the DIRXON keyword was used on the ACE card, this will be a (ynamic seismic analysis.
The 00 and THICK keywords are required on the first card in the geometry l
3.
section.
See pages I-4 and I-5 for more complete infomation on fomat of data 1
4 input and Section II for control caN descriptions.
i I-8 I
ME101 D0valopm:nt Spscification with
.... COPYRIGHTED AND CONFIDENTIAL Input & Methodology CLASS A KEYWORDS _
These keywords are l ent tags.
A group of keywords is valid fer a number of e em Class A keywcrds are generally applicable to a Class A keywords need not be redefined for each tegned as Class A keywords.
for All unit definitials in parentrases in the text series of pipe elenants.
Howew.r, all !wywords can also be if there is no change.
h CTL card (also see class A keywords are in english units. defined in metric u;1i Appendix g for all unit definiticus).
Description Keyword 0
(UF). Default = 70 F, Ambient temperature Applicable only to ASME Section III CODE values.
ATEMP CLASS Bend and tee flexibility factors are calculated in accordance with
=1 ASME Sec. III Subsection NB.
Bend flexibility factors and stress intensification factors for
=2 piping components are calculated III in accordance with ASME Sec.
Subsections NC and ND.
(see REMARKS for Default).
Piping code parameter CODE Compute bend flexibility factors, tee flexibility factors, and.
~
= SC374 moment ccmbinations per ASME Sec.
Subsection NB or NC/ND III, 1974, as determined by CLASS.
Compute bend flexibility factors,
= B31573 stress intensification factors, and moment combinations per ANSI 331.1 Summer 1973 Addenda.
Compute bend flexibility factors,
= SC3W75 tee flexibility factors, and momen III combinations per AShE Sec. 1974 Winter 1975 Addenda Sub-section NB or NC/ND as determined by CLASS.
Direction cosines of uniformly distributed be values rust
- COSFX, Direction cosines may be specified three load.
All
- COSFY, specified.
COSFI in terms of their relative values.
l i
I-9
ME101 D;volop=cnt Spacificntion with
.... COPYRIGHTED AND CONFIDENTIAL Input & Methodology The total weight per unit Density (lb/in ).
DENS length / metal cross sectional area.
Design pressure (psi).
DPRESS 7
Default value = 2.79 x 10 psi.
Young's Modulus (psi).
E Thermal expansion strain in in/100 f t.
EXP Weight per unit length in Ib/ft.
LBS/FT Weight per unit length in ib/in.
LBS/IN or LBS Weight per unit length in kg/ meter.
KG /M Weight per unit length in kg/ millimeter.
KG/MM (See REMAP.KS f or valid values)
Material type.
MAT (1 to 12 characters)
Poisson's ratio.
Def ault value = 0.3.
MU Outside diameter of pipe cross section (in).
OD Peak operating pressure (psi).
PPRESS Internal pressure (psi).
PREES Basic material allowable stress at minimum (cold) temperature (psi). Default = 15,000 psi SC l
Basic material allowable stress at maximum (hot) temperature (psi). Default = 15,000 psi SH Operating temperature (*F).
TEMP Thermal expansion strain (mils /in).
THERM Pipe wall thickness (in).
THICK Uniformly distributed load in specified system of units, as defined on HED card, (lb/in or lb/f t).
UFL also be If UFL is specified, the direction cosines must REMARKS _:
e specified.
is used for pressure stiffening The internal pressure (PRESS) for computing flexibility f actors at bends and elbows e
effect according to ASME BPV Code Section III Sub-section NB.
I-10
ME101 DOvalCpm%nt Specification with
.... COPYRIGHTED AND CONFIDENTIAL Input & Methodology
- versa, EXP is substitute for THERM and vice e
The effect of DENS is added with the effect of LBS/FT (or LBS/IN).
See Appendix (a).
e If the keywords CODE and CLASS do not appear in the data CODE = SC374 and CLASS = 1 are e
used.
for a description of the See Appendix (i) difference between CODE = SC374 and CODE =
e SC3W75.
ATEMP and MAT is The set of keywords TEMP, substitute for EXP/ THERM and vice versa, e
a strain is calculated from Thermal expansionthe Table of Nominal Coefficients of e
Section III, Expansion, ASME 1977 Division 1, Appendix I when MAT and TEMP are specified.
See appendix (s).
fall within the range TEgP and AfEMP must e
70 F - 800 F.
Young's Modulus can also be provided from the See page ASME table when MAT is specified.
e I-CTL-1 for explanation of the MTABLE keyword.
The valid values for material type follow:
e SA106-B SA106-C SA106-A SA312-IP304 SA312-TP304H SA312-TP304L SA312-TP304N SA312-TP309 SA312-TP310 SA312-TP316 SA312-TP316H SA312-TP316L S.t312-TP347 SA312-TP347H SA312-TP348 SA312-TP348H SA333-1 SA333-9 SA335-P1 SA335-P2 SA335-P5 SA335-P7 SA335-P9 SA335-P11 SA335-P12 SA335-P21 SA335-P22 SA376-TP304 SA376-TP304H SA376-TP304N SA376-TP316 SA376-TP316H SA376-TP316N SA376-TP321 SA376-TP321H SA376-TP347 SA376-TP347H SA376-TP348 SA430-FP316N for the value of the thermal expansion (s)
Refer to appendix Modulus used by the above Material tyce.
strain and Young' is scecified, the thermal strain If other material type (THERM or EXP) and Young's Modulus must be specified.
I-ll
ME101 DOvolopmsnt Spscificction with
.... COPYRIGHTED AND CONFIDENTIAL Input & Methodology Remarks _ (Cont'd)
Only one of the LBS/IN, LBS/FT, KG/PN, KG/M should be specified.
e The unit for EXP, LBS/IN, LBS/FT, KG/M, KG/MM are fixed re5ardless of e
The keyword "CCDE" is intended to extract the SIF, flexibility factors, and calculate stresses according to a particular code addendum. This code e
parameter (i.e., SC374, SC3W76, etc. ) can be used for other addenda long as the ASME Section III methodology is the same. If other adden modified values for SIF, manual input can be used to comply with the appropriate code.
O I-12
ME101 D;Volopm:nt Sp;cification with Input & Methodology
.... COPYRIGHTED AND CONFIDENTIAL ELEMENT TAGS AND ASSOCIATED KEYWORDS _
l ment tags Further discussion will explain the use of various e eMany keywords are valid and their associated valid keywords.In the description of keywords, tag.
for more than one element the underlined are default values.
d categories, All the key words have been classified into two broaClass A keywords are generally be re-defined Class A and Class B keywords. applicable to a series of pipe element for each element if there is no change.
keywords.
are not Class A keywords are classified as Class B o
in english
)
All unit definitions in parentheses in the text areall keywords can also be units.
- However, (See Table g 2, by specifying UKEY = METRIC on the CTL card.
for all unit definitions.)
Appendix (g) e
ME101 D&velopmsnt Specification with
.... COPYRIGHTED AND CONFIDENTIAL Input & Methodology l
Blank. (no entry in cols. 1-3)
Element Type Tag:
Describe a straight or curved pipe element.
Purpose:
FROM field may be left blank, except if t Data Field Data Point Numbers point was Anchor. The TO field must always have an en Global offsets of the 70 dats point relative to the FROM Increment data point in the specified system of units.
Enter the bend radius in the specified system of unit if the TO data point is a tangent intersection point. The Bend radius following shorthand notation may be used for the bend radius (nominal diameter notation is always considered in the dimensions according to ANSI B16.9,1971):
short radius bend (1.0 x nominal dia.)
t long radius bend (1.5 x nominal dia.)
S=
N-D bend (N x nominal dia.) where, N is a positive L=
ND =
integer 6 9.
(For Metric unit, do not use shorthand notation.)
If EIGEN=2, a non-blank entry in this field designates a hass mass point in the system.
s Additional Piping and Loading Data:
Any class A data keywords may be entered. The following Clas also be specified.
Cescription i
Class B Keyword f
Additional weight (lb).
ADOWT Direction cosines of the c-axis with respect to the can be used to describe local coordinate COSCX, COSCY system of any straight member. (c-axis re-orientati global axes COSCZ prohibited when the a-axis lies in the may also be specified in terms of their relative values.
Def ault values are explained on page I-2. See remarks.
I-BLANK-1
ME101 Davolopmant Specificction with
.... COPYRIGHTED AND CONFIDENTIAL Input & Methodology 1
Descriotion T
Class E Keyword i
I 1
Mass release, applicable only if i
i i
g cyp hEL i
EIGEN = 2 under element tage, " HEC" I
I I
l j
Release mass in X direction j
i
=X I
Felease mass in Y direction i
I
=Y I
Release mass in I direction i
i
=Z I
l i
=x+Y Belease mass in X and Y 1
direction, etc.
i i
l 1
l i
Reinf orcement drea to De used for l
i i
calculation of tee flexibility f actor 1
FIAAEA*
I NE-36 87. 5 o f the ASME i
i per parag.
a j
1 Section III Code (in ),
\\
I 1
Pad or saddle thickness used to cal-I i
1 l
PTHICK 1
culate tee stress intensity factors 1
119.6.4 of ANSI B31.1 or i
1 I
per para.
I ASME Section III Subsections NC and ND.
i 1
l i
i i
j Tee type W61 ding tee per ANSI E16.9 l
l TEE i
=WIEE Reinforced f abricated tee i
1
=RTEE Unreinforced fabricated tee l
i
=UTEE j
=EF ANC H Eranch cannection 1
i l
i JGINT l
= REC Feduce r I
i
=ETWELD Eutt weld l
=TEF 300 tapered transition I
i
=FLhtLC Fillet weld 1
i i
I See ASoE Section III 1974 Subsection i
i FF NC-3673, fig. NC36 73 (o) - 2 (in).
i i
Cef aults to 1/2 the CD of branch pipe.
i 1
l l
Cone angle (degrees) fo r ca lcula tior.
l 1
l ALFA of reducer stress intensificatian 1
i facto r.
Just not_ exceed _ijf.
l 1
f 1
i I
Alsmaten, of adjoining pipe sections i
1 DELTA used in calculating stress intensi-i j
fication factors f or tutt welds and i
i taperec transitions (in).
I I
i i
I Generates equally spaced da ta points, 1
SEG4NT I
SEGMJT - the number of equal length i
I l
I segments desirec.
l 1
I l
ME101 D3Volcpm:nt Specification with
.... COPYRIGHTED AND CONFIDENTIAL Input & Methodology Stress intensification factor to be used The stress SIF in calculating stresses.
intensification factor is applied to the data point, not the entire member, except for a bend.
Member flexibility factor. Applied only FLX to curved members.
Translational release of the element TRELB at the beginning of the element.
=A release in a-direction release in b-direction
=B
=C release in c-direction
= A+B release in a-and b-direc-tions, etc.
Rotational release of the element at RRELB the beginning of the element.
release about a-direction
=A release about b-direction
=B
=C release about c-direction
= A+B release about a-and b-direc-tions, etc.
Translational release of. the element TRELE at the end of the element.
Rotational release of the element at RREL the end of the element.
Title for this data point.
OTITLE Title for the tangent ending at this ETITLE data point and beginning at the previous data point.
-I Remarks:
The length of a straight pipe element, before segmentation, that is preceded and/or followed by a bend is computed by e
subtracting [ bend radius x tan (1/2 bend angle. The mass point flag for new data points generated by SEGMNT will be the same as the mass flag for the data point defined e on the card with SEGMNT. e _ Subscriots of potnts generated by the SEGMNT keyword' will be
ME101 Dav@lopmnnt specification with .... COPYRIGHTED AND CONFIDENTIAL Input & Methodology f Release at a point means the point has zero stiffness in the direction o e the release. See appendix (c). RRELB, TRELE and RRELE should not be entered at the tangent e
- PELB, intersection points.
is defined to be of ZERO length if it is less than 0.001 ft. long, and of SMALL length if it is less than OD/10 long. The prog A tangent e length always delete ZERO length tangents and it will try to delete SMALL tangents. 5-D The entry ND in the BEND RADIUS field may be used to specify a 3-D or e bend. TITLE DTITLE and ETITLE may be up to 12 characters (alpha numeric). The D i The ETITLE will be printed in all tables which contain this data po nt. e will be printed in all tables in which the tangent occurs. d DTITLE and ETITLE may not occur on a tangent intersection point an ETITLE can not be used to label a bend (elbow). e ETITLE may not occur on a segmented element. e If JOINT = RED and ALFA is not specified, the stress intensification e factor of the reducer will be 2.0. the adjacent tangents If the data point is a tangent intersection point, must be long encugh to accomodate the bend. the mass of the bend intersection point is a mass point, will be divided equally to be lumped at each end of the bend. If a tangent e for bends is divided into two equal weights at the Additional weight beginning and end points of the bend. For straight members, it is lump e at the data point. intersection For a bend, note that the TO data point must be the tangent e point. It is not on the actual pipe. The data point number of a tangent intersection point of a bend may never e appear as a FROM entry. I-BIANK-4
j ME101 D3valopmsnt Spscificction with Input & Methodology .... COPYRIGHTED AND CONFIDENTIAL J \\ 1 \\ Default Values ] l Stress Intensification j Data Needed i j l i j Eactors to be Calculated i i 1 1 1 i 1 i I 1 l 1 I I l I WTEE I 1 i PTHIK 1 0 l 1 UTEE I FF i BRANC H OD / 2 i, 1 RTEE l 4 EF ANCH i ALF A* 1 1 CELTA i 1/ 3 2 in *
- 1 1
FED i DELTA i 1/32 in *
- I 1
ETWELD l i TEP 1 i i FLWELD 1 1 _A 1 See Remark, See NC-4 233 of Sectlan III of the ASME SPV Code. . ~ - - _ _ _ - -,. - - - -.
ME101 DLvolopm3nt Specification with COPYRIGHTED AND CONFIDENTIAL Input & Methodology ACE Element Tvoe Tag Describe earthquake acceleration response spectrism. Purpose Additional Piping and Loading Data: Description Class B Keyword Up to 54 alphanumeric characters (blanks included) may be specified as earthquake TITLE identification. I I Period (sec.) - acceleration (g); =0 use linear interpolation for period TYPE i Period (sec.) - acceleration (g); l =1 use logarithmic interpolation for j period Frequency (cps) - acceleration (g); =2 use linear interpolation for frequency } Frequency (cps) - acceleration (g); =3 logarithmic interpolation for frequency l Direction of response spectra curve. l DIRXON X direction =X X and Z are the same curve as speci- = X+Z i fied, etc. Percentage to be used in determining CLOSE definition of closely spaced modes. j Default - 10.0 percent. l Modal su=mation option. i COEF i { = SRSS_ Square root of the sum of the squares method l' = CS4 Closely spaced modes su=mation according to Eq. 4 of Regulatory Guide 1.92 l accelerations Static Seismic analysis input X-ACC in the X, Y and Z directions given in g's. Y-ACC { Z-ACC l Earthquake type f or dual damping response i EQK spectra seismic analysis according to j Regulatory Guide 1.61 (see Appendix o). = OBE Operating Basis Earthquake = SSE Safe shutdown Earthquake i i P i
ME101 Davalopmsnt Specification with Input & Methodology .... COPYRIGHTED AND CONFIDENTIAL i Description class s Keyword i Modal damping value for dual damping response DCURVE spectra seismic analysis according to Regulatory Guide 1.61 (see appendix 0). =1 for 1% of critical damping =2 for 2% of critical damping =3 for 3% of critical damping j = SEISxx where "xx" is a 1 or 2 character LONAME identifier. LDNAME specifies the name of a seismic load and matches the name of a load request on the LOCASE keyword on the RUN card. Defines curves for multiple response spectra RSNAME analysis. = name of up to six alphanumeric characters (as identified by ANC, RAD or SNS cards). The four control frequencies for response spectra FA, FB, FC, FD extrapolation in descending order. Applies to a specific direction of the response spectra curve and as such must follow the "DIRXON=" keywo rd. The four control periods for response spectra PA, PB, PC, PD extrapolation in ascending order. Applies to a specific direction of the response spectra curve and as such must follow the "DIRXON=" keyword. Damping value for response spectra. Must be given when CC411=YES is specified on the HED CDAMP l card. i Remarks: The spectral curve values follow the ACE card (s). The period or frequency i comes first, followed by the corresponding acceleration value. The period o or frequency values must be input in ascending order. Values may be entered in columns 10 through 80. A conna separates two entries. Maximum of 200 spectral curve points may be input for each direction. The ( total number of points entered may vary for each direction. o I-ACE-2 c
ME101 Dsv@lopmsnt spacification with i .... COPYRIGHTED AND CONFIDENTIAL Input & Methodology Remarks (Cont'd) Xeywords 'CLOSE' and 'COEF' are used in conjunction with the o keyword (see appendix b). Spectra must be specified in all three directions for dynamic ana o For static seismic analysis, do not input any response spectra data. o For static seismic analysis the user must enter accelerations for all directions even though some acceleration values are set to zero. o An E0A card must be inserted after each set of ACE card complete acceleration load (that is, each set which contains DIR o all directions or X-ACC, Y-ACC and Z-ACC keywords). The keywords EQK and DCURVE must both be specified for a dual d o response spectra analysis, Neither EQK nor DCURVE keywords should.be used on the ACE card non-dual damping response spectra analysis. o For a dual damping response spectra analysis, two response spectra curv one for each damping value required by R. G.1.61, must be defined for o each direction in which earthquake motion is desired. The ACE cards response spectra curve data must satisfy the following conditions: Two set of ACE cards must be input, one for each of the two damping values. Each set contains all ACE cards necessary to define the input 1. for one damping value, e.g., TITLE =---, ACE EQK=---, DCURVE=----, ACE CLOSE=---, COEF=---, ACE TYPE =---, ACE DIRXON = X ACE (response spectra curve data) DIRXON = Y ACE (response spectra curve data) DIRXON = Z ACE (response spectra curve data) E0A I-ACE-3
ME101 Dsvolopmsnt Spscification with .... COPYRIGHTED AND CONFIDENTIAL Input & Methodology Remarks (Cont'd) TITLE =---, ACE DCURVE=----, ACE TYPE =---, DIRXON = X ACE (response spectra curve data) DIRXON = Y ACE (response spectra curve data) DIRXON = Z ACE (response spectra curve data) E0A A set must be completely defined before starting the definition of the 2. second set. If there are more than one seismic load case, all ACE cards and response spectra curve data corresponding to the same seismic load i 3. case must be acilacent. If the EQK, CLOSE, COEF, TYPE and LONAME keywords are specified on both sets of dual damping response spectra curves, then the values I 4. must be the same for these keywords on both sets. The values of OCURVE must comply with R. G.1.61, i.e., if EQK = OBE, 5. ( DCURVE = 1 or 2, and if EQK = SSE, OCURVE = 2 or 3. i If any one of the above conditions is not satisfied a fatal error wil occur. LDNAME must be the same as one of the seismic load case names def o the LDCASE keywoni on the RUN card, If LONAE is not specified then the name of the first acceleration load will be the same as the name of the first seismic load case requested on o RUN card (see LDCASE keyword on RUN card, page I-RUN-1). If LONAME is specified on any SEISxx acceleration load it must be o specified on all others. s I-ACE-4
ME101 Davolopmsnt Specification with .... COPYRIGHTED AND CONFIDENTIAL Input & Methodology Remarks (Cont'd) i TYPE must be the same for all curves in a load case. o LDNAME is not required when RSNAME is specified unless the curve is to be o used for both SEISxx and MRSxx load cases. Control frequencies (FA, FB, FC, FD) or periods (PA, PB, PC, PO) are required only if extrapolation of input spectral curve is to be done for o applying Code Case 411 modal damping values (i.e., CC411=YES and IN HED card). If both, control frequencies and control periods are given, control o periods will be ignored, j If control frequencies and periods are not specified, they will be o detennined (if needed) as follows: FA = Zero oerfod frequency. FB =./FA
- FC FC = Frequency at which the response spectrum has maximum accelerat F0 = The second lowest frequency specified for the response spectnan All four control frequencies or periods need not be input. The missing values will be calculated, as above, automatically by the program, but o
those that are input must be in the required order (i.e., FA > FB > FC) FD and PA < PB < PC < PD), Control frequencies (FA, FB, FC and FD), when specified, must not exceed the cut-off frequency (inverse of PERIOD on HED card). o Control periods (PA, PB, PC and PD), when specified, must not be less than o the cut-off period (PERIOD on HED card). CDAMP is required only when CC411=YES is specified on the HED card, o The following exangle illustrates the setup of ACE cards when CC411=YES and INTP=I are used on the HED card and a seismic analysis is to be o perfonned (i.e., LOCASE=SEISxx on the RUN card): ACE TITLE =---, ACE TYPE =--, CLOSE=---, COEF= ---, ACE LDNAME=----, CDAMP= ----, ACE DIRXON = X (response spectra curve data) ACE DIRXON = Y I-ACE-5 - - - - - - * - ~ -, - .,,_.m-_ e
ME101 D;Valopmant Specification with Input & Methodology .... COPYRIGHTED AND CONFIDENTIAL Remarks _ (Cont'd) (response spectra curve data) DIRXON = Z ACE (response spectra curve data) E0A (repeat the above set with identical TYPE, CLOSE, COEF. and LONAM dif ferent C0 AMP values and curve data for as many damping values as desi red). All X-direction curves must have identical number of ggints and similarly for Y-and Z-direction curves. COAMP values must be in increasing order, The following example illustrates the setup of ACE cards when CC411=YES and INTP=I are used on the HED card and a multiple response spectra o analysis is to be performed (i.e., LOCASE=MtSxx on the RUN card): ACE TITLE =---, TYPE =---, CLOSE=---, COEF=---, ACE RSNAME=---, CDAMP=----, ACE ACE DIRXON = X (response spectra curve data) ACE DIRXON = Y (response spectra curve data) ACE DIRXON = Z (response spectra curve data) E0A (repeat the above set with identical TYPE, CLOSE, COEF and RSNAME different C0 AMP valuws and curve data for as many damping values as desired). (Then repeat all of the above for as many RSNAME as desired.) For a given RSNAME and DIRXON, all curves must have identical number of points. For a given, RSHAME, the C0 AMP values must be in increasing order. I-ACE-6
1 ME101 D;v31CpmOnt f Specification with .... COPYRIGHTED AND CONFIDENTIAL Input & Methodology Element Type Tam ANC Describe an anchor Purpose Data Field Enter the data point number in the TO field, leave Data Point Number the FROM field balnk. Global components of the imposed thermal anchor displacement in inches or mm, depending on UKEY Increment on the CTL card. (See appendix (g)). Additional Piping and Loading Data: The following Class Any Class A keywords may be entered on the ANC card. B keywords may also be entered: Class B Keyword i Description Additional weight (ib) ADDWT cosines of the a-axis with respect to the COSAX,COSAY,COSAZ-Direction Only non-zero values need be specified. global axes. Direction cosines may also be specified in terms of their relative values. Default is COSAX = 1 (see remark). Direction cosines of the e-axis with respect to the COSCX,COSCY,COSCZ Only non-zero values need to be global axes. Direction cosines may also be specified specified. in terms of their relative values. Default is i COSCZ = 1 (see remark). Translation flexibilities (in/lb) in local coordinates. KA, KB, KC Rotational flexibilities (angular unic/in-lb) in i RA, RB, RC local coordinates. External anchor rotation (angular units) in global ROT-X, ROT-Y, ROT-Z ? coordinates. t Translational stif fnesses of the anchor (1b/in). AA, AB, AC in-lb Rotational stiffnesses of the anchor (a lar unit}' l ARA. ARE, ARC i Seismic movements (in) in global coordinates DX, DY, DZ I-ANC-1
ME101 D;VolepmOnt specification with .... COPYRIGHTED AND CONFIDENTIAL Input & Methodology Description ]~ClassBKeyword Name of phase for DX, DY, DZ of the anchor (up to 6 alphanumeric PHASE Also see appendix (k). characters). (See Title of this anchor point. DTITLE remarks). (sec.) to be added to Delayed time the time history function identified DELAY by the TIM card. Default = 0. Multiplicative constant for the time history function identified by the MULTI TIM card. Default = 1. A label of up to three alphanumeric characters identifying the TIM card TACC set which de' scribes an acceleration time history function. A label of up to three alphanumeric characters identifying the TIM card TARr set which describes a rotational acceleration time history function. A label of up to three alphanumeric characters identifying the TIM card TDIS set which describes a displacement time history function. A label of up to three alphanumeric characters identifying the TIM card TBar i set which describes a rotational time history function. displacement A '.abel of up to six alphanumeric R20eE characterr identifying a set of curves fcr multiple response spectra analysis. Multiplicative constant for multiple RSFACT response spectra acceleration s. Default = 1. Remarks (or stiffn If neither translation nor rotational flexibilities are entered, the data point is defined as an anchor point e ' Direction cosines need not rigidly connected to " ground". be entered.
~ ME101 D;volcpacnt Specification with Input & Methodology .... COPYRIGHTED AND CONFIDENTIAL pamarks__ (Ocnt'd) If some or all of the translational and rotationalfle o is defined as an anchor point elastically connected to defined are considered to be rigid connections to " ground". " ground". d, The direction cosines of the a-and c-axes must be enter KB, KC and vice versa. AA, AB, AC are substitutes for KA, RB, RC Similarly, ARA, ARB, ARC are substitutes for RA, o and vice versa. (FRASE) are allowed. A maximum of 10 different phases o If the user specifies direction cosines of the a-axis,ified the direction cosines of the c-axis must also be spec o and vice versa, The a-axis and c-axis must be parpendicular to w o the program will adjust the direction cosines of the .1 radian. c-axis. In-line Anchor input is described on page I-5. o in 'HED' card. Angular unit is defined by keyword 'ARU' o (see page I-HED-2), (alphanumeric). This DTITLE may be up to 12 characterstitle will be printed in all repo o DTITLE may only be used if the anchor point is the beginning o of a branch. must be specified for seismic anchor PHASE and DX, DY, D: o movement analysis. A TIM card must use the same keyword (TACC, TART, TDIS, orSee pa and label as specified on the ANC card. o TROT) TACC and TART are not compatible with TDIS and TROT in the Use *-options to define more o same run (LDCASE=TIMExx). than one type of time history analysis. Time history functions are in the local A direction. To specify functions in more than one direction, use(for TART or TROT). o RAD cards (for TACC or TDIS) or RAR cards and label An ACE card must use the same keyword (RSNAME) as specified on the ANC card. See page I-ACE-2. o Multiple response spectrum analysis does not require specification o However, if it is not specified a warning message o RSNAME for every ANC. will print for user infonnation, b/V&J1
ME101 D0valcpm:nt Specificntien with Input & Methodology .... COPYRIGHTED AND CONFIDENTIAL Element Tvoe Taq: CCC Check internally computed global coordinates agalDSt user-Spec 1fied global coordinates. P ur pose Data Field Enter data Foint number in the TO field. Data Numoers Increments X,Y,Z global coordinates of data point. Additional Piping and Loading Cata: 1 Descriotion 1 Class e Keyword' 1 l l l Tolerance f or coordinate check (in units l-1 TC LAR i 1 o f the coordinate). Default value = 1.0 l 1 l l inch. i 1 i i CooRD J =X Check X coordinate only. I I =x+ Y Check X ans Y coordinates. I i i = X+ Y+ Z Checx X, Y, Z coordinates. j I I -g i - l Femarks: If tne coordinate check exceeds the specified tolerance, a diagnostic will te issued and execution inhitited. Cnly 10 cards with element tag 'CCC' are permitted in ene I input decx. I I I
ME101 D;volep;cnt specificatien with .... COPYRIGHTED AND CONFIDENTIAL Input & Methodology Element Type Tag: CM8 Algebraic Codination of Loadcases
Purpose:
Leave Col. 4-50 blank. i Data Field: Additional Piping and Loading Data:
== Description:== 1. Genersi There are no class A or 8 keywords on CM8 cards. Instead the CM8 card i consists of algebraic load coeination equations. The algebraic coeination of loadcases is defined by an algebraic equatici in Cols. 51 through 80. The left hand side of "=" is the algebraic coeination of loadcases, i 2. Algebraic Operators for SAP Solver The valid algebraic operators are: j + addition subtraction maximum r l minimum square root of the sum of squares (SRSS) ABS () absolute value n* scalar multiplication resultant maximun resultant minimum 3. Simple Equations for SAP Solver The following shows how the operators are used to form codined loadcaset C1 through C10: C1=L1+L2 addition of L1 and L2 C2=L1-L2 subtraction of L2 from L1 l C34.14L2 maximum of L1 and L2 C4=Ll#L2 minimum of L1 and L2 r C5=LI$L2 SRSS,(L12 + L2 })/2 2 l C6=-L1 negative of L1 l C7= ABS (L1) absolute value of L1 I-CM8-1
ME101 DOvolopm:nt specificcticn with .... COPYRIGHTED AND CONFIDENTIAL Input & Methodology scalar multiplication of L1 where n is any positive real numer expressed in integer, or decimal notation C8=n*L1 (scientific notation is not allowed) resultant maxima of L1 and L2 C9=L1 L2 resultant minima of L1 and L2 C10=L1;L2 where C1,..... C10 are coeined loadcases, L1 and loadcases names. 4. Complex Equations for SAP Solver The following are the valid algebraic coeinations of L1, L2, L3: +L1+L2+L3+... El&C24E34E.. LitL2fL3#.. LI$L2$L3$... L1:L2:L3... L1;L2;L3;... where L1, L2, L3,... must be one of the following: a loadcase, L, defined on a RUN, RCL or preceding CMB card, 1) ii) n*L where L is defined in (i), iii) 13S(L) where L is defined in (i), iv) n* ABS (L) where L is defined in (i), Any fom of algebraic combination that includes a tem rPL immediately followed by a negative sign (e.g., MYCOM8 = 2.5*WT1 - THRM1) must not be used. It must be broken up into two or more simpler combinations. Examples: l a) C1 = THRM1#WT1 C2 = THRM24THRM3 I C3 = SEIS01 $5AM1 C4 = -2.*C1+3*C2 VERIFY = C4-C3+SEIS02 b) RESMAX=SEIS01:10*SEIS02 It may be necessary to use two or more CMB cards to define a codined loadcase. I-CMB-2
ME101 DOVolcpment Specification with Input & Methodology .... COPYRIGHTED AND CONFIDENTIAL Reearks: The right handside of "=" may use one or more input if nes, o Comined loadcases specified on the STD carti (see page I-STD-1) will have o results printed in the " Actions on Supp' orts and Anchors", " Joint 01 splacements", " Direction Cosines and Glottal Fort:es and Monents", " Stresses and Local Forces and Moments" and " Effective Accelerations" reports. Loadcases used on the right side of the "a" must have been defined on a o RUN card or recalled from a previous master file by the RCL car 11 or defined on the left side of the "=" on a previous CMB card. Combinations are performed in the order in which they are irput. CM8 o general cominations are performed before stress check Q/A calculations. (SLA, OLA, TEA, PBA). o
- -options may not be used on the CM8 card.
o Loadcases created through CM8 may be used as input to stress Q/A reports (SLA, OLA, TEA and PSA) provided that they confonn to the naming convention for loadcases for Q/A reports. (See Appendix r). Special restraints such as SNS, SPR and SPD are codined in the ways as o described in Appendix r. 1 i 1-CM8-3
ME101 DOvc1cp2Ont Specification with Input & Methodology .... COPYRIGHTED AND CONFIDENTIAL CNP Elament Tyce Tag Used to model memoers with non-circular cross Purpose section. Data Field If this element is a continuation of the the FROM field may be left Data Point Numbers previous element, Enter the data point identification blank. number in the Tc field. Global o f f sets of the TO data point relative Increments to the EFCM data point in the specified system of units. If EIGEh=2, a nod-clank entry in this field in the system. . tass designates a mass point Additional Piping and Loading Data: The f ollowing Class B Any class A data keywords may te entered. keywords may also be specified. class 3 1(eyword._ cescriction Additional weight (1b). ADDWT a Component area (in ). AFEA Component weignt (lt). CNPTWT of the c-axis with respect COSCX, COSCY, COSCZ Direction cosines OnAy non-zero values need bo the global axes. to be specliied. Direction cosines may also be specified in terms of their relative Cef ault values are explained on page value s. l I-3.
- 4 ass release applicaole only if EIGEN=2 under l
DYNREL e le me nt tag ' HED'. Release mass in the gictal X =X direction. helease mass in the global Y i =Y direction. l seAease v. ass in the global Z =1 direction. M
ME101 D;volopm:nt Specification with Input & Methodology .... COPYRIGHTED AND CONFIDENTIAL Eelease mass in the global X, Y X+Y = direction. etc. Moment of inertia about the b-and c-axes I-B, I-C (in*). l l Torsional constant ( in * ). I J-O is polar moment of inertia for a circular l J-O section only. a Ef fective shear area about the b-axis (in ). I means shear deflection is neglected. SHEARE Default (in2). I Effective shear area about the c-axis Def ault means shear deflection is neglected. SHEARC Translational release of the component at the l TRZLB teginning of the component. j release in a-direction =A release in n-direction I =B release in c-direction =C release in a-and b-directions, l = A+B i etc. at the Rotational release of the compor.ent FRELB Leginning of the component. release about a-cirection =A =B releasa about c-direction =C release about c-direction = A+B release about a-and b-directions etc. Translational release of the component at the TRELE end of the compcnent. Rotational release of the component at the end RAELE of the component. Title of this data point. l DTITLE Title of the component element ending on this data point and beginnning on the FROM point 01 ETITLE previous point.
ME101 Davolopm:nt Specification with .... COPYRIGHTED AND CONFIDENTIAL Input & Methodology Component modal damping value for dual damping response spectra seismic analysis (see DCURVE Appendix o). f or higher damping value, i.e., =H 2% damping for OEE or 31 damping for SSE. for lour damping value, i.e., =L 15 damping for OEE or 25 damping f or SSE. default values: = H if current input value of OD is > 12.75 in. = L if current input value of OD is 5 12.75 in. or if CD has not been specified on any previous input card. Remarks: is applied as a unif orm load for Compment weight (CMPTWT)For dynamic analysis, one half of the i + dead wight analysis. component weight le lumped at each end. is lumped at the data point. Additional weight (ACCWT) The data point number of a tangent intersection point should not appear as a FROM entry. l and J-O must be entered.
- AREA, I-B, I-C, The material properties E and MU are handled in the same way I
as for piping elements. l Release at a point means the point has zero stif fness in the direction of the release. See Appendix (c). The DTITLE and ETITLE may be 12 characters (alphanumeric). ETITLE is printed in all reports which would list theThe components. data points. The class A keywords L85/FT and LBS/IN are not applied to componen i e
- elements, calculated for component elements.
Stress is not o
ME101 DOvGltpmOnt Sp0cification with .... COPYRIGHTED A!!D CONFIDENTIAL Input & Methodology i CTL Element Type Tag: Control of processing for a ME101 run
Purpose:
Leave Col. 4-50 blank. Data Field: Additional Piping and Loading Data: Description clas s a Keywo rd ' Use the value of Young's Modulus, E, at 70* F MTABLE =E from the ASME 1977 code, Section III, Division 1, Appendix I, Table I-6.0 for material (s) specified by MAT keyword (s). See Appendix (s). Generate a tape at run completion containing the SAVE = YES results of load analyses and recalled load cases. Do not generate a tape of the results of load = NO analysis. SOLVER = SAP Use SAP solver. SAP solver not available for: (a) time history analysis (b) multiple response spectra analysis (c) ASME PVRC Code Case 411 %dal damping Class A and Class B keywords provided in i UXEY = ENGLSH_ English units. Class A and Class B keywords provided in = METRIC Metric units. Remarks
- -options may not be used on this card.
o When SAVE = YES is specified a report is printed at the end of the run containing the tape number and a description of the contents of the tape. o t I-CTL-1 I
ME101 Dev01cp;Cnt Sp0cificction with .... COPYRIGHTED AND CONFIDENTIAL Input & Methodology Remark _s (Cont'd) For more detailed instruction on the SAVE keyword, see Appendix (q). e is required when ICABLE = E Material type (MAT keyword, see page I-10) is specified. See page I-il for valid values of MAT. e is specified, the Young's At any point where the class A keyword "E" Modulus provided in the material table is no longer applied. e If neither ! CABLE = E nor the E keyword are specified, the default e 7 value for E is 2.79 x 10 psi, Details of the UKEY keyword and other information associated with th units of the input data are presented in Appendix (g). e t I l I-CTL-2
ME101 D0volopm:nt specificction with Input & Methodology .... COPYRIGHTED AND CONFIDENTIAL us DLD Element Type Taq: Define which forcing function is applied Purpose at a data point. Data Field Enter data point number at which the force Data Numbers function is applied in the To field. Global components of a vector describing the line of action if the forcing function. Increments Additional Piping and Loading Data Description Class B Keyword to be added to the Delayed time (sec.) forcing function as defined by the TIM DELAY card. Default = 0. Multiplicative constant for the forcing function as defined by the TIM card. l MULTI Default = 1. A label of up to three alphanumeric characters indetifying the TIM card set TFOR which describes the time history forcing function. Remarks The DLD cards should be placed immediately behind the card i that first defines the data point. e i DLD on TINP will move to the beginning of the bend. e A TIM card must use the same keyword TFOR and label as specified on the DLD card. See page I-TIM-1. e t j Do not specify TACC, TART, TDIS or TROT in a load case Use *-options to f e which has force function analysis. define more than one type of time history analysis, i -. - ~ _... _ - - _ - -, _. - -. - - -... -
t t E*"$t ...: COPYRIGHTED AND CONFIDENTIAL.... p jf jo w Input & Methodology Element Type Tag: EAB Restraint against displacement with energy absorbing
Purpose:
capability. Data Field: Enter data point number at which the restraint acts in the Data Numbers TO field. Enter global components of a vector describing the positive Increment direction along the line of action of the restraint. Additional Piping and Loading Data: uescription ciass n Keyworc Ir.itial translational flexibility of the restraint XA (in/lb) DISP Displacement (in) FORCE Preload force (lb) Initial translational stiffness of the restraint (lb/in) AA g DX, DY, DZ Seismic movements (in) in global coordinates. Name of phase for DX, DY, DZ of the rettraint (up to 6 PHASE alphanumeric characters). Also see appendix (k). Delayed time (sec) to be added to the time history DELAY function identified by the TIM card. Default = 0. Multiplicative constant for the time history function MULTI identified by the TIM card. Default = 1. A label of up to three alphanumeric characters TACC identifying the TIM card set which describes an acceleration time history function. A label of up to three alphanumeric characters t TDIS identifying the TIM card set which describes a displacement time history function. A label of up to six alphanumeric characters identifying RSNAME a set of curves for multiple response spectra analysis. (continued) I-EAB-1 1
iffc to th .... COPYRIGHTED AND CONFIDENTIAL.... p Input & Fiethodelcgy Description p ass a Keyword hitiplicative constant for multiple response spectra RSFACT accelerations. Default = 1. I Label of the loading curve for this device. HYS Label of the S-value curve for this device. SVA STRAIN Design peak strain. Design peak defomation (in). DD Design secant stiffness (Ib/in) SS Percentage tolerance of force for device dimension DTF selections. Default a 55. I l Percentage tolerance of displacement for device dimensio n DTD selections. Default = 55. 6 psi. Initial Young's modulus. Default = 29.0 x 10 EEAB Remarks: The EAB cards should be placed ismediately behind the card that first e defines the data point. EAB on TINP will move to the beginning of the bend. e AA is a substitute for KA and vice versa. e For skew restrafrits the DX seismic movements will be multiplied by the cosine of the angle between the X axis and the line of action of the e restraint. Similarly for DY and DI (see appendix k), A maximum of 10 different phases (PHASE) are allowed. e I-EAB-2 .r.- __,y ,m,_ _. _,.. -. _ -. _,,,,.. ,..,c, ,,g_--_,
iffcaionwth .... COPYRIGHTED AND CONFIDENTIAL.... p Input & Methodology Remarks (Cont'd) PHASE and appropriate DX DY. DZ must be specified for seismic anchor e movement analysis. A TIM card must use the same keyword (TACC or TDIS) and label as spe o on the EAB card. See Page I-TIM-1. The displacement time history acts along the line of action of the restraint as defined in the increment field. e An ACE card must use the same keyword (RSNAME) and label as specified on e the EAB card. See page I-ACE-2. TACC is not compatible with TDIS in the same run (LDCASE=TIExx). Use (
- -options to define more than one type of time history analysis, e
Multiple response spectrum analysis does not require specification of RSHAME for every EAB; however, if it is not specified a warning message e will print for user information. Actual loading curve is required for direct-integration time history e analysis. Womalized loading curve is required for single and multiple response e spectra analysis, q The hysteresis normalized loading curve, HYS card, must be specified. e I-EAB-3
4= f t .... COPYRIGHTED AND CONFIDENTIAL.... p cif c io t Input & Methodology Remarks (Cont'd) If the normalization factors can be calculated for the EA8 as above, the e EAB is considered " determined". If the normalization factors cannot be calculated for the EAB, the EAB is e (- Considered " undetermined". gQn undetermined" EAB, the exact hysteresis characteristic is e (a) secant stiffness ("55=") must be input.(b) if design peak str 1.0 el'y. For a " determined" EAB, the exact hysteresis characteristic is known: e (a) if design peak deformation ("D0=") is given, the design peak strain (" STRAIN =") and the secant stiffness ("55=") will be calculated by the program (input values of these two keywords will be ignored). (b) if design peak deformation ("DC=") is not given b is given the design peak defor1 nation and the secant stiffness ("SS=") will be calculated by the program (input secant stiffness value will be ignored). I-EAB-4 ' ' ' - " ' - * - - - - - ~ -., _ _ _,
pme .... COPYRIGHTED AND CONFIDENTIAL.... Specif c ion w th Input & Methodology Remarks (Cont'd) (c) if design peak deformation ("DD=") and design peak strain (" STRA have not been given but the secant stiffness has been given, the design peak deformation and design peak strain will be calculated by the program. (d) if design peak deformation ("DD="), design peak strain (" STRAIN =") and secant stiffness ("SS=") are all not J ven, the design peak strain i will be assumed to be equal to 7.0.ey and the case (b) will apply. Normalized S-value curve is required for single and multiple response e spectra analysis. If the S-value curve is required but not input, it will be generated from o the supplied loading curve. Response spectra curves referenced by the EAS restraint must have dampin value specified (i.e., use CDAMP keyword on ACE card). e If interpolation of the spectral curves is used (i.e. INTP=I on HED card) to obtain acceleration for particular modal damping, spectral curve for e each direction must be given for at least two damping values (CDAMP keyword on ACE cards). I fs I I l I e I-EAB-5
1 ME101 D;volopmsnt Spscification with Input & Methodology .... COPYRIGHTED AND CONFIDENTIAL END ElEme.nt TVDe T&a: Defines the end of a problem input deck. Pur pose Leave Col. 4-80 blank. Data field h errark s: All problem decxs must have the EhD card as its last card. each separate problems should not te stacked, i.e., See Section I-4 MI101 problem needs a set of control cards. AZ101 far the 3rder of other cards. e t l I I
.. o
ME101 D,volopm:nt Specification with . COPYRIGHTED AND CONFIDENTIAL Input & Methodology EOA Element Type Taq: Marks the end of an acceleration Purpose load. Leave Col. 4-80 blank. Data Field Remarks: l follow the set of ACE cards which The EOA card must define a complete acceleration load (that is each set o of ACE cards which contains DIRXON keyword keywords). 1 l l s
ME101 D&volopmsnt Specification with .... COPYRIGHTED AND CONFIDENTIAL Input & Methodology Element Type Tag: FOR Externally applied force
Purpose:
Data Field: Leave the FROM field blank. Enter data point number at Data Numbers which the force acts in the To field. Enter global components of a vector describing line of Increment action of the force. Additional Piping and Loading Data Class B Keyword Description FORCE Applied force (lb) Cost parameter value. This parameter is used to specify the cost of placing a support in a feasible direction. CPV Remarks: FOR cards should be placed immediately behind the card that defines e the data point. intersection point, the line of action When FOR is used at a tangent of force should be parallel to either the tangent before the bend or e the tangent after the bend. If a Specify CPV only under the option LOCASE = FOR in the RUN card.
- ram value of CPV is specified but no FORCE value is specified, the pr e
(SAP Solver only). will assume a default value of 1000 lbs. A CPV value is optional under LDCASE = FOR. CPV value is not used in the ME101 solution, but is saved on the user specified file under HED e card. (SAP Solver only). See appendices 1 and m. e l ? hd.A/e Cw , A V. C to.. -)3 J ; ' 'I-FO R-1 \\
i i ME101 Development .... COPYRIGHTED AND CONFIDENTIAL.... Specification with Input & Methodology Element Type Tag: HED Describe problem identification infomation and control
Purpose:
parameters. Leave Col. 4 - 50 blank. Data Field: Additional Piping and Loading Data: Description Class B Keyword Up to 54 characters of alphanumeric information, TITLE terminated by a coma. Up to 12 characters of alphanumeric information PROJNO identifying the project number, teminated by a coma. PROBN0' Up to 12 characters of alphanumeric information identifying user, terminated by a coma. Unit of length for coordinate increments and bend radius. UNITS =1 Unit of length is inches =2 Unit of length is feet =3 Unit of length is millimeters Number of modes to be used for dynamic analysis. MODES Method of calculation used by SAP solver. EIGEN Determinant search, subspace iteration or shifted =1 subspace iteration =3 Subspace iteration =4 Determinant search ( =6 Shifted subspace iteration l l Name of a FORTRAN file on which the output results of FILE specified analyses are to be saved. Tolerance (in) for closing loops. Default = 1.0 in. LOOPTL Percentage to be used in determining definition of CLOSE closely spaced modes. Default = 10.0 percent. Modal sumation option COEF = SRSS Square root of the sum of the squares method = T Closely spaced modes sumation according to Eq. 4 of Regulatory Guide 1.92. ((.ontinued) I-HED-1 1 ~
- """-m------w--.,
l ME101 Development .... COPYRIGHTED AND CONFIDENTIAL.... Specification with Input & Methodology i Description Class B Keyword PLTR = NOPLTR = ZETA (see page 11-1 and II-2) CALCOMP 1036 and direct PLOT FILE to the Norwalk = CLA queue for plotting. = CSF CALCOMP 1036 and direct PLOT FILE to the S.F. queue for plotting. CALCOMP and direct PLOT FILE to requested site = CAL for plotting. RMS-600 and direct PLOT FILE to requested site = RMS for plotting. l PLOT = NOPLOT = GEOP Produce a Geometry Plot 3 i = GEON Produce a Geometry Plot with data point numbers, g = GE0B Produce both Geometry Plot and Geometry Plo data point numbers. v l Three characters for the remote siteid. See PLOT TABLE SUWRY under " Remarks" for legal values. { SITE Minimum period to be considereu for response spectrum PERIOD analysis (sec). Def ault = 0.03 sec. Modal synthesis option for response spectrum analysis. J SYNTH l =0 X+Y Response Spectrum I+Y Response Spectrum l Local member force superposition. (Global member forces are not printed.) =2 X+Y Response Spectrum I+Y Response Spectrum Global member force superposition. (Local member forces and stresses are not printed.). (continued) I-HED-2
ME101 Development Specification with .... COPYRIGHTED AND CONFIDENTIAL.... Input & Methodology Class B Keyword Description =3 Same as 0 and 2 =4 X+Y+Z Response spectrum Local and global member force superposition. ARd = DEGREE angular unit in DEGREES for input and output. = RAD angular unit in RADIANS for input and output. EDIT Input data check =0 Edit and run =T Check data only PUNCH = FL Gives punched card output for element local forces and moments. (See Output Description Page III-60). Defaults to no punched card output. XYZOUT = YES Gives independent output for three accelerations printed by X-ACC, Y-ACC and Z-ACC keywords on the ACE card. = NO, No independent output is printed. DAMP Fraction of critical damping to be used for time history analysis. Default = 0. MDAMP Rayleigh constant for mass matrix to be used for time history analysis. Default = 0. KDAMP Rayleigh constant for stiffness matrix to be used for time history analysis. Default = 0. TZERO Initial time for time history analysis (sec). Default = 0. TFIN End time for time history modal analysis. t l DT Time increment for time history analysis (sec) i i TPER Minimum period (sec) to be considered for time history analysis. Default = 0.001. (continued) I-HED-3
P .... COPYRIGHTED AND CONFIDENTIAL....' p cif ca io Input & Methodology vescr ipt ion Liass u Keyworo The method used to combine different level of response spectrum from each phase of the building (as defined by GROUP the KEYWORD RSNAPI). It is recomended to use the ABS option for multiple support excitation response spectrum analysis. For other option, consult your area office's user representative. Def ault value = ABS (Absolute sumation). Only final results output for multiple MRSOUT = SHORT response spectra analysis. Individual and final results output for = LONG multiple response spectra analysis. Type of input for acceleration time history ADATA = GLOBAL data. = LOC AL Turn on or off absolute sumation of = OFF DC directions for response spectrum analysis (SAP solver only, for EAL solver it is k~ = ON necessary to use OPTIONAL DATA - see user support for details.) Max. no. of iterations allowed for either each non-linear time history analysis step, or iterative l MITER response spectra analysis. Default = 5. Max. absolute tolerance value of forces (Ib) in TOLF convergence test. Max, absolute tolerance value of displacements (in) in TOLD convergence test. Max. percentage error of displacements in convergence MXERR test. Default = 0.01 (i.e. 1%) System damping coefficient. Def ault = 0.02 (i.e. 2%). SYDAMP Max, allowable damping coefficient. Default = 0.30 (i.e. MXDAMP 30%) (continued) I-HED-4
\\ ME101 Development .... COPYRIGHTED AND CONFIDENTIAL.... Specification with Input & Methodology Class B Keyword' Description Extrapolation of response spectra curves INTP =E-according to control frequencies. =I Interpolate response spectra from a family of Curves. CC411 = YES Calculate modal damping per ASME PVRC Code Case 411. Do not use ASME PYRC Code Case 411 for = NO--- calculating modal damping. Remarks: If MODES is nonzero, frequencies and mode shapes of the system will be o calculated. If response spectrum analysis is to be performed, MODES must be specified. If a dynamic seismic run is requested (LDCASE=SEISxx) in the RUN card then o MODES must be nonzero. A fatal error will occur if EIGEN = 2 for a run containing a dual damping o
- analysis, The number of modes to be adopted in computation by the program is the o
i minimum of modes determined by the options MODES and PERIOD. The EIGEN keyword is ignored when the EAL solver is used. l o EAL solver uses iterative solution with automatic thift which is the most efficient eigenvalue solution available in ME101, When EIGEN=6 or EIGEN = 1 with MODE greater than 50 is specified, the o eigen extraction of the " shifted subspace iteration" is used. The large I values of MODES (i.e., MODE 100) will become insignificant as compared to the required " cut-off" PERIOD. However, the large value of MODES should be reasonable upper bound (i.e. recommended to be less than 400) to avoid the unforeseen input error, for example by specifyTng E=28.3 instead of E=28.3E6. With the current BEC UNIVAC billing algorithm, the eigen solution cost should be within the linear portion of the number of modes to be extracted, s With SAP solver the file name specified by the keyword " FILE" is. y o restricted to a total of six or less characteys and must start with an alphabetic symbol. The first two characters @f the FILE name cannot be numeric. The following names must not be used for the FILE entry: MASTER, SCRACH, SAPDATA. I-HED-5
ME101 Development .... COPYRIGHTED AND CONFIDENTIAL.... Specification with Input & Methodology Remarks (Cont'd) In order to save the output from several star option runs from SAP solver, a separate file must be specified for each option; these files cannot have the same name. If these catalogued mass storage files are no longer required, the user should delete the files with the control card: 90ELETE,C NAE. where NAME is the entry for the FILE keyword. The keywords LDCASE=FOR and FILE can be used to save results on mass o storage files that are used as input to the SLAM (ME110) program. See appendices (1) and (m) for further discussions. When the FILE keyword is specified, the results are not saved for SAM, o EFWT, or SEIS (dynamic) cases, o The UNITS keyword must be specified, SYN =4 is the only option for loadcases to be used in a SOLVER =EAL, loading o combination (CMB), restraint load sunnary (RLS), or stress check summary (0LA), or when zero period acceleration effect is considered in the analysi s. Modes must be specified for time history modal analysis, o DT is specified at most once for time history modal or direct time o integration analysis. If it is omitted, time steps will be internally generated at 1/8 minimum period for modal analysis. It is the user's responsibility to select reasonably small time step for direct integration. The time step for direct time integration must be generally significantly smaller than that allowed with modal analysis, The TFIN keyword must be specified for time history modal analysis. o For time history analysis, if POAMP and/or KDAPF is specified, then DAMP o will be ignored. CC411=YES is available only with EAL solver. It cannot be used if dual o damping is specified (ref: "EQK=" and "0 CURVE =" keywords on ACE cards). When CC4hl=YES is specified, INTP=E means that the spectral curve o correspohding to the ASME PYRC Code Case 411 modal damping values will be extrapolated from the input spectral curve for a specific damping value. When CC411=YES is specified, INTP=I means that the spectral curve o corresponding to the ASME PVRC Code Case 411 modal damping values will be interpolated using a family of input spectral curves for tarious damping L values. I-HED-6
O k***IUP**"2 .... COPYRIGHTED AND CONFIDENTIAL Specification with Input & Methodology Remarks (Cont'd) PLOT TABLE
SUMMARY
e PLTR CALCOMP SITE CITY KEYWORD MODEL KEYWORD SIZE.LINE. PLACE Ann Arbor CAL TOT 2 AAl Warrow Online ~ AAl At AA/7 Ann Arbor RMS ED1 At EDh/? Edmonton RMS gal At Gait /LL Gaithersburg RMS hcl At DEL /4 Houston RMS London CAL 1012 UKl Narrow Online UK) At Bechtel hcuse RMS London 1051 LY1 Narrow Online Louisville CAL LV1 At Water /10 Louisville RMS Norwalk CAL 1036 N01 Narrow Cnline N01 At BLD/42/LL Norwalk RMS Palo Verde CAL 1036 PV1 Narrow Online San Francisco CAL 1055 SF1 Narrow Online SF1 At 350/3/968 San Francisco RMS SF2 At 50/15/A51 San Francisco RMS At Main /10/E21 SF3 San Francisco RMS SF4 Meet /35/B19 San Francisco RMS SF5 At Main /2/Cl4 San Francisco RMS Some of the plotting devices in the above table may not be currently available. Users are advised to check with DP User Support for questions \\,. on status of equipment, CLOSE and/or CCEF on the HED card will override CLCSE and/or CCEF on any o ACE cards, Direction must be specified for acceleration time history data in global coordinates (ADATA= GLOBAL). See DIRXCN keyword for the TIM card, page o I-TIM-1. When DC=0N, the absolute summation of directions is done prior to the modal combination. This option should only be used by the Diablo Canyen e Project. Keywords MITER, TOLF, TOLD, MXERR, SYDAMP, MXDAMP and only when EAB type (energy absorbing) restraints are used. e If INTP=1 is specified, at least two spectra curves must be suppliec fer e each direction and RSNAME. When INTP=1 is specified, user-input or def ault values e minimum and maximum damping values (CDAMP on ACE cards) for the sup; respense spectra curves. ( I-HED-7 = -
.... COPYRIGHTED AND CONFIDENTIAL.... p if ca i th Input & Methodology Element Type Tag: HYS To specify the loading curve for energy absorbing
Purpose:
restraints. Data Field: Leave Col. 4-50 blank. Additional Data: Class B Keyword Description l = Label for the loading curve (1 - 6 characters) HYS NORM = YES If a normalized loading curve. = NO If an actual loading curve. Normalization factor for displacement (in). XY Normalization factor for force (lb). FY Remarks Loading curve coordinates (displacement, force pairs) are specified on cards immediately following the HYS card. Coordinate values are input in e columns 10 thru 80 with coma used as a separator between entries. Coordinates of the first point on a loading curve should always be 0., O. If the user leaves this out, the program will generate the 0., O. point e internally, The program will always generate one extra (last) point on the loading e curve to extend it out far (to 20 times the displacement value of the last l point input by the user) using the slope of the last segment of the curve. Total number of points (including the program generated one or two points e as described above) on the loading curve must not exceed 20. 1 If slope of the loading curve does not decrease with each segment, it e shall be consioered "not nice" and a warning will be issued. Norwalization factors, if given, will be used if the loading curve is I e j required to be transformed from normalized to actual or vice-versa. i I-HYS-1 l
ME101 Davolopmnnt specification with .... COPYRIGHTED AND CONFIDENTIAL Input & Methodology MGM _ Element Tvoe Tag: Externally applied moment P ur pose Data Field which the mome.nt Enter data point number at Data Numbers acts in the TC field. Enter global corponents of a vector describing Ir.crements line of action of the moment. Additional Piping and Loading Data: I Descriction j Cla ss B Keyward Applied moment (ft-lb) _\\ MOMENT Femarks: d that mod cards snould be placed immediately behind the car defines the data point. intersection point, the line o a tangent When MGM is used atshould be parallel to either the tangent action of moment before the cend or the tangent af ter the bend.
ME101 D3valopmsnt specification with .... COPYRIGHTED AND CONFIDENTIAL Input & Methodology Element Type Tag: 0LA Request Occasional Load Analysis; eqn. 9 NC-3600 or egn.
Purpose:
12 831.1 Data Field: Leave Col. 4-50 blank. Additional Piping and Loading Data: class B Keyword i Description LEVEL =B =C LEVEL indicates the level of service limit at =D specified in ASME Section III,1977, NC3611.1 A list of load case names, separated by a "+". These ar< INCLUD used to calculate the resultant moment used in this analysis, e.g., INCLUD=SEISl+WT1 A list of load case names, separated by a "+". These ar EXCLUD not considered in the calculations for this analysis. Remarks: l
- -options may not be used on this card.
o Every load case name should be the same naming convention as a name o specified by LDCASE on a RUN card (see page I-RUN-1). Either EXCLUD or INCLUD keyword is required if there are more than or o weight load case or more than one seismic load case. Either EXCLUD or INCLUD may be specified but not both. o For each level of service limit, only one set of OLA cards is allowe o See appendix (p) for further infomation. o I-OLA-1
ME101 Dsvalopmsnt Spacification with Input & Methodology .... COPYRIGHTED AND CONFIDENTIAL Element Type Tag: PSA Pipe Break Location Analysis; eqn. 9 NC-3600 or egn.12
Purpose:
831.1 Leave Col. 4-50 blank. Data Field: Additional Piping and Loading Data: class B Keyword De scription The multiplier of the right hand side of eqns 9 + 10 (NC3600) or 12 + 13 (831.1). FPB defaults to 0.8. FPS FSAM = 1 or 2 the multiplier of the moment due to SAM analysis. A list of load case names, separated by a "+". These art INCLUD used to calculate the resultant moment used in this analysis, e.g., INCLUD=THRM1+SEIS1+WT1+ SAM A list of load case names, separated by a "+". These ar EXCLUD not considered in the calculations for this analysis. Remarks: -options may not be used on this card, o Every load case name should be the same naming convention as a name specified by LDCASE on a RUN card (see page I-RUN-1). o Either EXCLUD or INCLUD may be specified but not both, o For more detailed explanation of EXCLUD and INCLUD, see the remarks o under OLA and TEA (pages I-OLA-1 and I-TEA-1), See appendix (p) for further infonnation. o e I-PBA-1
ME101 D;velopmsnt Specification with .... COPYRIGHTED AND CONFIDENTIAL Input & Methodology Element Type Tag RAD Useu for translational Restraint against displacement. Purpose restraint, or an imposed displacement. Data Field Enter data point number at which the restraint Data Numbers acts in the TO field. Enter global components of a vector describing the positive direction along the line of action of the Increment restraint. Additional Piping and Loading Data: Description Class B Keyword Translational flexibility of the restraint (in/lb). KA Displacement (in). DISP Preload force (lb). FORCE Translational stiffness of the restraint (lb/in). AA Seismic movements (in) in global coordinates. DX, DY, DZ Name of phase for DX, DY, DZ of the restraint (up to 6 alphanumeric characters). Also see appendix (k). PHASE Delayed time (sec.) to be added to the time history 1 Default = 0. DELAY function identified by the TIM card. i Multiplicative constant for the time history function MULTI identified by the TIM card. Default = 1. A label of up to three alphanumeric characters TACC identifying the TIM card set which describes an l acceleration time history function. A label of up to three alphanumeric characters TDIS identifying the TIM card set which describes a ( displacement time history function. I A label of up to six alphanumeric characters identifying a set of curves for multiple response spectra analysis. RSNAME Multiplicative constant for multiple response spectra RSFACT accelerations. Default = 1.
ME101 D5volopmsnt Sptcification with .... COPYRIGHTED AND CONFIDENTIAL Input & Methodology Remarks _: If KA (or AA) is not specified, the restraint is assumed to be o rigid. The RAD cards should be placed imediately behind the card that first defines the data point. o RAD on TINP will nove to the beginning of the bend. o AA is a substitute for KA and vice versa. o For skew restraints the DX seismic movements will be multiplied by th cosine of the angle between the X axis and the line of action of the o Similarly for DY and OZ (see appendix (k)). restraint. A maximum of 10 different phases (PHASE) are allowed. o PHASE and appropriate OX, OY, DZ must be specified for seismic anc o movement analysis. A TIM card must use the same keyword (TACC or TDIS) and label on the RAD card. See Page I-TIM-1. o The displacement time history acts along the line of action of the re-straint as defined in the increment field, o An ACE card must use the same keyword (RSNAME) and label as spec on the RAD card. See page I-ACE-2. o TACC is not compatible with TOIS in the same run (LOCASE=TIMExx). Use
- -options to define more than one type of time history analysis, o
Multiple response spectrum analysis does not require specification of RSNAME for every RAD; however, if it is not speficted a warning message o will print for user information. (, ,e W: "..co n%q h '. %.u. ? 2...T,, i %. s [; n.,. ~ m.,ba c t I-RAD-2
i ME101 Davolopment Spacification with Input & Methodology .... COPYRIGHTED AND CONFIDENTIAL RAR Element Type Tao Used for a rotational Restraint against rotation. Purpose restraint or ir:gesed rotation. Data Field Enter data point nunber at which the restraint acts Data Ntrbers in the To field. Enter global ccrponents of a vector describing the positive direction along the line of action of the Increent restraint. AMitional Piping and Ioading Data: Description i Class B Keyword Ibtational flexibility of the restraint (angular unit / PA in-lb). I I Ibtation (angular unit). Pctr A; plied mment (ft-lb). MCr e ir Rotational stiffness of the restraint (in-lb/ APA angular unit). to be aMari to the time Delayed time (sec.) J history function identified by the TIM card. l DEIAY Default = 0. Maltiplicative constant for the time history furctior I MLT TI identified by the TIM card. Default = 1. A label of up to three alphanumeric characters identifying the TIM card set which describes a TART rotational acceleration ti::e history function, j A label of up to three alphantmeric characters identifying the TIM card set which describes a i Taor rotational displaceent time history function. annarks_: is not specified, the restraint is assumed to be rigid. If PA (or APA) e PAR cards should be placed mmediately bePand tra card that first de / e the data point. ABA is a substitute for FA and vice versa. e The positive direction for runents and rotations about the line the restraint are defined by the right-hand rule. e
ME101 D0volopmsnt spscification with Input & Methodology .... COPYRIGHTED AND CONFIDENTIAL Ne to the beginning of the band. RAR on TINP will m: o A m2mnt at a rigid restraint will be ignored. o d An angular unit is defined by kepcId 'ARU' on the 'HED' car. o (See page I-HED-2). ified A TIM card must use the same keyword (TART or TRCTI) and label as O on the RAR card. See page I-TL%-1. f action The rotational displacernent time history acts along the line o of the restraint as defined in the incrermnt field. o TART is not cmpatible with TRctr in the same run o l
ME101 Davolopment specification with .... COPYRIGHTED AND CONFIDENTIAL Input & Methodology Element Type Tag _: RCL To recall load cases from a tape created by tne SAYE J
Purpose:
keyword on the CTL card. \\ Leave Col. 4-50 blank. Data Field: Additional Piping and Loading Data: class B Keyword I Descrf ption TAPE Tape nuirter. The name of a load case on the tape. LOCASE Recall every load case on the tape = ALL = TRID4xx Thermal load case name = WTxx Weight load case name = EFWTxx Effective Weight load case name Seismic Anchor Movement load case name = SAMxx = SEISxx Seismic lead case name = FOR Individual Force load case name = SEFVxx Free Vibration load case name "xx" is the 1 or 2 alphanumeric character identifier for j each separate load case. l The new name of the load case on the tape in the curren-RENAME run. = THRMxx Thennal load case name = WTxx Weight load case name = EFWTxx Effective Weight load case name Seismic Anchor Movement load case name = SAMxx = SEISxx Seismic load case name = FOR Individual Force load case name = SEFVxx Free Vibration load case name "xx" is the 1 or 2 alphanumeric character identifier fc each separate load case. The default is not to change the load case name. Remarks: The RCL card recalls load cases which were previously saved by use c the SAVE keyword on the CTL card (see page I-CTL-1). o l l I-RCL-1 l l
ME101 Dsvolopmant Specification with Input & Methodology .... COPYRIGHTED AND CONFIDENTIAL Remarks (Cont'd): The user has the option of recalling every load case on a tape, b using LDCASE=ALL, or recalling any number of individual cases o The option LDCASE=ALL is available with S solver individual cases must be recalled, Only one occurance of each of the keywords may appear on a o The TAPE keyword must appear on an RC o is optional for both solvers. RENAME can not be used on the same RCL card with L o In order to recall every load case on a tape and to rename any o these load cases, use a sequence of RCL cards, o RENAME must be specified if there 'is a na o on the RUN card or on another RCL card. For each tape recalled, a report is printed listing the tape number, the load cases requested and a description of each load case. o
- -options are not allowed on this card.
o l I-RCL-2
ME101 Development specification with Input & Methodology .... COPYRIGHTED A!iD COliFIDENTIAL RLS Element Type Tag: Produce one restraint load sumary for each designated
Purpose:
loadcase and/or combined loadcase. Leave Col. 4-50 blank. Data Field: Additional Piping and Loading Data: class 5 Keyword i Description Loadcases to be listed on RLS report LIST LIST =CASEl+ CASE 2..., where CASE 1, CASE 2 are loadcases created by the RUN, or CMB cards. Default = no RLS report is printed Remarks: Any number of RLS cards may be input. Each RLS card will pr o separate restraint load sumary report. The list of loadcases may be continued on additional lines, e.g., o LIST =CASEl+ CASE 2 RLS + CASE 3+ CASE 4 The RLS card only produces the sumary of restraint loads. CM should be used for the algebraic combination of restraint loads o page I-Cle-1). If RLS is not specified no restraint load sumary will be printed. o
- -options may not be used on this card, o
RLS load cases must have the same geometry (except for r o Dynamic load case names can only be listed on RLS car i o I-RLS-1 l
ME101 Davolopmsnt Spscification with Input & Msthodology . COPYRIGHTED AND CONFIDENTIAL 5 RUN Element Type Tag: To request load analysis.
Purpose:
Leave Col. 4-50 blank. Data Field: Additional Piping and Loading Datas Note l Class B Keyword Description f Thermal analysis = TNRMxx LDCASE = WTxx(list) Weight analysis Effective Weight calculation = EFWTxx(list) Seismic Anchor Movement analysis = SAMxx(list) = SEISxx(list) Seirmic or static seismic analysis Individual Force analysis for = FOR(list) MEllo (SLAM) only = SEFVxx(list) Free Vibration analysis = TIMExx(list) Time History analysis Multiple response spectra analysis = MRSxx(list) "xx" is a 1 or 2 alphanumeric character identifier for each separate load case selected by the user. " LIST" is a series of one character alphanumeric labels separated by "+" which specify *-options to be included in a load analysis (e.g., A + B + C + 4). " LIST" must not begin with an "E". Remarks: l
- -options may not be used on this card.
e If no RUN cards are specified, no load analysis will be performed. e If LDCASE=FOR is specified, then each force card acts as an indivi load case to be analyzed. These load cases are then called FOR001, e FOR002, etc. A RUN card with LDCASE keyword is required for each load analysis. Fo a seismic analysis with two sets of ACE cards (or four sets of ACE e two RUN cards cards for a dual damping response spsetra analysis), with LDCASE=SEISxx are required. I-RUN-1
ME101 Dsvalopment .... COPYRIGHTED AND CONFIDENTIAL specification with Input & Methodology Remarks (cont'd) o The LDCASE keyword can only appear once per RUN card, Each load analysis requested by LDCASE will include all the cards o without a *-option and all the cards with a *-option which are specified in the list following the load case name. For example: RUN LDCASE = WT1(A) RUN LDCASE = THRMI(B+C) RUN LDCASE = THRM.l(B) HED ANC 5
- A ANC 5.1.2.3
- B THERM = 2.0
- C is equivalent to:
RUN LDCASE = WTl HED ANC 5 and RUN LDCASE = THRMI HED ANC 5.1.2.3 THERM = 2.0 and RUN LDCASE = THRKJ HED ANC 5.1.2.3 The n-th seismic load name (SEISxx) appearing in the card sequence o will be the LDNAE of the n-th set of ACE cards unless LDNAME is specified in the ACE cards. If LDNAME is spectfied in the ACE cards, it must be identical with an entry of LDCASE. See page I-ACE-2 for LDNAE information. l Do not run individual force analysis (LDCASE=FOR) with any other load o analysis (used for SLAM E110 only). l o Individual force analysis (LDCASE=FOR) can only be done by the SAP l solver (SOLVER = SAP on the CTL card). l I-RU N-2
ME101 Dsvalopment Spscification with Input & Methodology .... COPYRIGHTED AND CONFIDENTIAL SAP Element Tvoe Tag: Specify the origin of global coordinate system Purpose Data Field Enter reference data point number in the To Data Numbers field. Z coordinates of reference Enter global X, Y, Increments data point number. Femarks: the first data point If a SAP data card is not present, f the encountered in the input stream is taken as the origin o global coordinate system. Only one SAP card may be used. The SAP card can appear anywhere after the HED card and before ACE cards. - ~ - _ _ _,
ME101 D&velopmsnt spscification with Input & Mathodology .... COPYRIGHTED AND CONFIDENTIAL SLA Element Type Tag: Request Sustained Load Analysis; egn. 8 NC-3600 or eqn.
Purpose:
11 831.1 Leave Col. 4-50 blank. Data Field: Additional Piping and Loading Data: class B Keyword ! Description The load case name used to calculate the resultant INCLUD moment for this analysis, e.g, INCLUD=WTl A list of load case names, separated by a "+". These at not considered in the calculations for this analysis. EXCLUD Remarks:_
- -options may not be used on this card.
o Every load case name should be the same as a name spec on a RUN card (see page I-RUN-1) or by RENAME (or LDCA o card (see page I-RCL-1). Both EXCLUD and INCLUD keywords are not required if there o weight load case. Either EXCLUD or INCLUD may be specified but not both. o Only one set of SLA is pennitted. o See appendix (p) for further information. o I-SLA-1
1 ME101 Dtvalopmnnt Spscification with Input & Methodology .... COPYRIGHTED AND CONFIDENTIAL SNB EltEnent TWe Tag Restraint against displamment in This element is used Snubber: seismic or dynamic analysis.for translational r Purpose loading condition as indicated in the risnarks below. Data Field Enter data point number at which the snutber Data Ntrnbers acts in the 70 field. Enter global cmponents of a vector describing the positive direction along the line of action of the Increment snubber. Additional Piping and Icading Data Description Class B Keyword I Translational flexibility of the snubber (in/lb). i KA Translational stif fness of the snubber (lb/in). I AA Seismic novinnent (in) in global coortlinates. DX, DY, DZ Nane of phase for DX, DY, DZ of the snubber restraint (up to six alphanuneric characters). l PHASE Also see Appendix (k). to be aMai to the time I Delayed time (sec.) DELAY f history function identified by the TIM card. l l Default = 0. j Multiplicative constant for the time history function identified by the TIM card. METI Default = 1. A label of up to three alphanumeric charac+m identifying the TIM card set which describes an TACC l leration time history function. I ac A label of up to three alphanumeric characters ( l identifying the TIM card set which describes a TDIS l displacement time history function. Multiplicative a:nstant for multiple respnse Defau1t = 1. RSFACT spectra accelerations. A lahal of up to six alphantrneric characters identifying a set of curves for nultiple BSNAME response spectra analysis. e-- a-----
ME101 D;volopmInt spacification with .... COPYRIGHTED AND CONFIDENTIAL Input & Methodology 1 Remarks The relationship between the snubber and the loading cenditten is e as follows: SNUBBER RESTRAINT (SNB) LOAD CONDITION _ No restraint Weight No restraint Thermal Separate Load No restraint LDCASE=FOR If KA and AA Snubber stiffness = AA or 1/KA. are not specified, snubber is assumed rigid. Seismic Effective Weight Seismic Anchor Movement Static Seismic Time History The SNB cards should be placed innediately behind first defines the data point. e the card that SNB on TINP will move to the beginning of the benc e AA is a substitute for KA and vice versa. e For skew snubbers, the DX seismic movements will be multiplied by the cosine of the angle e between the X-axis and the line of action of the snubber restraint, similarly for DY and DZ (see Appendix (k)). (PHASE) are alle A maximum of 10 different phases e and A TIM card must use the same keyword (TDIS) See page label as specified on the SNB card. e I-TIM-1. The displacement time history acts along the line of action of the restraint as defined in e the increment field, TACC is not compatible with TDIS in the same rur (LDCASE=TIMExx). Use *-option to define more e than one type of time history analysis, An ACE card must use the same keyword (RSNAME) and label as specified on the SNB card. e See page I-ACE-2. Multiple response spectrum analysis does not i l require specification of RSNAME for every SNB. e However, if it is not specified a warning mess: will print for user information. l x-s9-2
ME101 Dsvolopmnnt Specification with .... COPYRIGHTED AND CONFIDENTIAL Input & Methodology Tvoe Taq SPD _ Ele me nt Eigid restraint against Spring hanger:in weight analysis. 'Ihis Purpose displacement is used for translational element restraint which varies with loading condition as indicated in the remarks below. Data Field Enter data point number at which the Data Nambers spring hanger acts in the To field. Enter global components of a vector Increment describing the line of action of the spring hanger. The relationship between the SPD spring hanger conditions and Remarxs: tne loading condition is as f ollows: Strina Hancer (SPDL Load Condition Stif fness is assumed rigid. Weignt No restraint. Thermal No restraint. Seismic No restraint. Ef fective Weight No restraint. Seismic Anchor Movement No restraint. Static Seismic No restraint. l Separate Load (LDCASE=FOR) The SPD cards should te placed immediately cehind the card I i first defines the data point. tha t SPD on TINP will move to the beginning of the bend.
t ME101 DevGlopmsnt Specification with Input & Methodology .... COPYRIGHTED AND CONFIDENTIAL SPR Element Tvoe Tao Restraint against Spring hanger: This element is used for dis placement. P urpose which preloaded translational restraint varies with loading condition as indicated in the remarks below. Data Field Inter data point number at which the spring hanger acts in the To field. Data Numoers Enter global components of a vector cescribing the line of action of the Increment spring hanger. Additional Piping and Loading Cata U Cescriction Cla ss-E Keyword Translational flexibility of the spring hanger t KA (in/lt). DISP DisplaceFent (in). l Preload force (lb). ~ FCRCc Translational stif fness of the spring tange'r, AA (lc /in)'. Selsmic movesekt (in) in global coordinates. DX, DY, C; ; ~ JY, DZ of thef$estraint Name of phase f or CX, Also se P HAS E (up to six alpnana.Teric characters).< Appendix ( k ) ~. Femarks: Ine relationship between the SPR spring hanger, preload force, and the loading condition is as follows: s -s -+ w
- 7.. -
g. ---.y g-- y, ~ - -
ME101 Davalopmsnt Specification with . COPYRIGHTED AND CONFIDENTIAL Input & Methodology Scrinc Hanagg__ f SPRL and Freload Force Ioad Condition Stif fness = AA or 1/KA. Weight If KA and AA are not specified, KA = Separate Load (LDCASE= FOE) 0 is assumed 1.e., rigid. Preload Force is included. If Stif fness = AA or 1/FA. Thermal FA and AA are not s pecified, Setsmic FA=0 is assumed. No seismic Anchor Movement preload force. static Seismic No restraint. No preload force. Eifective height Tae SPE cards should be placed immediately behind the card first defines the data point. that SPR on TINP will move to tne beginning of the bend. 'AA is a substitute f or KA and vice versa. s For skew spring hangers, the DX seismic movc similarly fcr DY and DZ tne line of action of the restraint, (see Appendix (k)). m' O l e v m1 O
ME101 Dsvalopmunt Specification with Input & Methodology .... COPYRIGHTED AND CONFIDENTIAL Element Type Tag: STD Produce a printout of the " Action on Supports and
Purpose:
Anchors", " Joint Oisplacements", "Of rection Cosines and Global Forces and Moments", " Stress and Local Forces and Moments", and "Ef fective Accelerations" reports for each loadcase. Leave Col. 4-50 blank. Data Field: Additional Piping and Loading Data: class a Keyword Description List of combined loadcases, each name separated by '+', LIST to be printed, e.g. LIST =CASEl+ CASE 2+... where CASE 1, CASE 2,..., are combined loadcases appearing on CMB cards. LIST =ALL will cause all loadcases appearing on CM8 carc to be printed. Default = ALL. i Remarks., Only one STD card is allowed. 'o
- 0nly loadcases produced by CMB are pemitted (see page I-CMB-1).
o The list of combined loadcases may use one or more input lines, e.g. o STD LIST =CASEl+ CASE 2 + CASE 3+ CASE 4 i
- option is not allowed on STD cards, o
If STD is not specified, reports will be printed for all combined o loadcases. I-STD-1
ME101 Development Spacification with Input & Methodology .... COPYRIGHTED AND CONFIDENTIAL TEA Element Type Tag: Request Thermal Expansion Analysis; egn.10a NC-3600 or
Purpose:
egn.13 or 14 831.1 Leave Col. 4-50 blank. Data Field: Additional Piping and Loading Data: Class B Keyword ' Description = 1 or 2, the multiplier of the moment due to SAM FSAM analysis. Default is 1.0. A list of load case names, separated by a "+". These are INCLUD used to calculate the resultant moment used in this analysi s, e.g., INCLUD=THRMl+THRM2+5AM1 A list of load case names, separated by a "+". These ar EXCLUD not considered in the calculations for this analysis. Remarks:
- -options may not be used on this card.
o Every load case name should be the same as a name specified by on a RUN card (see page I-RUN-1) or by RENAME (or LDCASE) on o l card (see page I-RCL-1). EXCLUD may be used to restrict the consideration of SAM, WT or any THRM load cases from the TEA (Thermal Expansion Analysis). o INCLUD may be used to include specific THRM load cases in TEA the THRM load cases need to be included in TEA, the INCLUD keywo o not be specified, If WT load case is not present, then only equation 10 ( ASME NC-3 and/or 13 (ANSI B31.1) will be considered in TEA. o If SAM load case is not present, it is assumed to be zero, o Either EXCLUD or INCLUD may be specified but not both, o Only one set of TEA is permitted. o See appendix (p) for further infonnation. o I-TEA-1 \\
ME101 Dsv@lopmsnt Spscification with .... COPYRIGHTED AND CONFIDENTIAL Input & Methodology Remarks:_ f i f l l 1 L l I-TEA-2
ME101 D3valopm2nt specificntion with ,... COPYRIGHTED AND CONFIDENTIAL Input & Methodology TIM Element Type Tag: Describe a time history function. Purpose Additional Piping and Loading Data: Description Class B Keyword Defines an acceleration (G) time history TACC function. = label of up to three alphanumeric characters (as identified by ANC, RAD or SNB card). Initial condition of displacement for CD acceleration time history (in).* Initial condition of velocity for acceleration CV time history (in/sec).* Defines a rotational acceleration (rad /sec ) TART time history function. = label of up to three alphanumeric characters (as identified by ANC or RAR card). Initial condition of angular displacement for angular acceleration time history (rad).* CAD Initial condition of angular velocity for angular acceleration time history (rad /sec).* CAV Defines a displacement (in) time history function. TDIS = label of up to three alphanumeric characters (as identified by ANC, RAD or SNB card). Defines a pressure / force (lb) time history TFOR function. = label of up to three alphanumeric characters (as identified by OLD card). Defines a rotational (rad) displacement time TR0T history function. = label of up to three alphanumeric characters (as identified by ANC or RAR card). Direction of global acceleration data. DIRXON =X X direction =X+Z X and Z are the same as specified, etc.
- MULTI, defined on ANC or restraint cards, is also applied to initial
.m
ME101 Dsvalopmunt Specification with .... COPYRIGHTED AND CONFIDENTIAL Input & Methodology JS - Januarv i+4e RENMK_S We :::'ie value Se t::ne history function values follow the TIM cards. l ce value. (seconds), cxzes first follCWed by the corres;cndmg a:m ituValues may be e 71,ne :ncst be input in ascarsiing crder. A cxmma separates tw entries. 10 th:cugh 80. f d by There is a max 2.mn of 10,000 cxrren time values e For exariple: IlrASE = "I ME01 pm TF3 = 10 HED 100... 'ITCR = 2 c Q 100 200... T!CR = 1 CLD 200... ';TtR = 2, CEU& = 1 300. 0.D 300... TEUR = 1 '1"M0,0, 1,10, 10,19, 50,19 TEER = 2 T::M 0,0, .5,4, 2,4, 4,0 C.'D
- he :h: d :=e h stery re::rd n :n 2ere are 9 cxrren tire values:uue ::
node 300) OE.AY=1 at 0, .5, 1, 1.5, 2, 3, 4, 5, 10 For Data Point 100: time function defired as 0,0 .5,4 1,4 1.5,4 2,4 3,2 4,0 5,0 10,0 For Data Point 200: tire function defired as i 0,0 .5,5 1,10 1.5,10.5 2,11 3,12 4,13 5,14 10,19 For Data Point 300: ti:ne function defined as 0,0 .5,0 1,0 1.5,4 2,4 3,4 4,2 5,0 10,0 TIM cards ttust be placed before AG cards, e e See appendix (u) for further information. O MXCN is recuired for acceleratien data in global coordinates ( ADATA= GLOBAL cn the HED carc or assumed by default). e l 1-Tr4-2
ME101 Davolopmsnt spscification with Input & Methodology ....CCFYRIGHTED AND CONFIDENTIAL se n y arv. Remarks: i For a restraint against displacement or rotation in one direct on, d h orresponding where a global acceleration function is applie, t e c e DIRXOti must be specified. For skewed restraints at least one corresponding DIRXON must be specified. CD and CV keywords must be specified for accelerat e 50 and below. (TACC). See caution on page IV-49, history (TART). If the time history response is calculated over a greater time period function the program uses the last e than that defined by the input i specified amplitude as a constant value over th ) and the and care should be taken in specifying the cutoff time (TFIN acceleration input function. See appendix (u) page IV-50 for more information. is a Piping response analysis with discretized acceleration input if input is theoretically unacceptable method of analysis. Howeve e solution can be achieved. This statement applies to all programs which use integration of acceleration to obtain solution of displacement stress, etc. and it is not particular to ME101 only. In case of rigid base acceleration the stress is based on relative displacements and d. the significance of the integration inaccuracy is diminishe I-TIM-3
ME101 Davalopm3nt spncification with Input & Methodology .... COPYRIGHTED AND CONFIDENTIAL 29A f tiement Type rag: To control processing of the Zero Period Acceleration / I
Purpose:
effect Leave Col. 4-50 blank. Cata Field: Additional Piping and Loading Data: Description [ClassBKeyword Find maximum resultant of dynamic and correspondin static seismic load cases. Mass correction not =ENVL CEB included. Find SRSS of dynamic and corresponding static seismic load cases. Mass correction not includ =SRSS Find SRSS of dynamic and the " mass correction" loadcases. The " mass correction" load case is =CMSRS described in Appendix (t). Cutoff period (sec.) for finding acceleration for static CUTCFF seismic analysis. Print realts for combined effect only. Print results for combined effect and effect due NO PRINT ,=YES 2PA on reaction loads and local forces and stres = =CN Turn on or off the Zero ZPA Period Acceleration effect for =CFF all dynamic cases in the run. If CUTCFF is not specified, the value of PERIOD on the HED Remarks: e used, or its def ault of 0.03 sec. X, Y and I accelerations for the static seismi e of interpolation depends on the value of the TYPE keyword on t l card. For dual damping cases, the highest cutoff accelerations of the two s of response spectra will be used for the static seismic analysis, e
- -options are not allowed on the IPA card.
e See appendix (t) for further information. e The Effective Acceleration Report will not consider the effect of ZP e PRINT = YES can only be used for EAL runs, e f I-ZPA-1
ME101 DSv31opmant Sp;cificction with Input f. Methodology .... COPYRIGHTED AND CONFIDENTIAL Remarks:
ME101 Development specification with ,,,,copyRICHTED AND CONFIDENTIAL Input & Methodology Ele ment Tvoe Tag Comment card for input decks. Purpose Iiema rks: 4-80 for the pur pose Any information can be entered in Col. of documenting input decks. in the Any number of comment cards can be entered anywh .~ They have no other effect. input deck. printout of the input deck. t
l ~ I) I 20S5 RETEA.JE TABLE
- g
'he is11owing cross-reference table shove which itees will be considered for each type of load analysis, 2E i LOAD CASE 33 j S Seismic Time p Thermal Weight Effwt S.A.M. SEISax Nistory o g iSourca Action (Keyword) THRMxx FOR WTxx EFWTxx SAMxx NRSxx TipEtru I Element a No No Yes Yes No Yes Yes o rangent Weight (DENS LB/FT. LB/1M) Additional Weight (ADOWT) No No Yes Yes No Yes Tea' , Bend Uniformly Distributed Loads (UFL) No No Yes No No No No 7 er Thermal Strains (THERM) Yes No No No No No No - p ii Component Weight (DENS. LB/FT LB/IN No No No No No No No g (CW) Additional Weight (ADDWT) No No Yes Yes No Yes Yes [ l Uniformly Distributed Imade (UFL) No No Yes No No No No l Thermal Strains (THERM) Yes No No No No No No l Anchor Translational Displacements Yes No No No No No No (ANC) (Disp X. Y. Z fields) Rotational Displacements (ROT-X. Yes No No No No No No ROT-Y. ROT-Z) Translational Springs (KA. KB. KC) Yes Yes Yes Yes Yes Yes Yes Rotational Springs (RA. RB. RC) Yes Yes Yes Yes Yes Yes Yes l Differential Seismic Motion (DX. DY No No No No Yes No No l DZ. PNASE) j Displacemeit Time History (TDIS. TROT) No No No No No No Yes Acceleration Time History (TACC. TART) No No No No No No Yes I Response Spectra Name (RSNAME) No No No No No Yes No l i! Ractroint Translational SprinRs (KA) Yes Yes Yes Yes Yes Yes Yes (RAD) Preload Force (FURCE) No Yes Yes No No No no .-. tn 2 l Translational Displacement (DISP) Yes No No No No No No 5AC 5 C. O i Differential Seismic Motton (DX, DY. No No No No Yes No No
- o. 2 a Displacement Time History (TDIS)
No No No No No No Yes 22@ l DZ. FNASE) 1, Acceleration Time History (TACC) No No No No No No Yes % C. *._, l Response Spectra Name (RSNAME) No No No No No Yes No l@@ $1k i R2straint Rotational Spring (RA) Yes Yes Yes Yes Yes Yes Yes gp3 (RAR) Inittal Noment (NON) No Yes Yes No No No No y7 Rotattonal Displacement (ROT) Yes No No No No No No Displacement Time History (TROT) No No No No No No Yes l Acceleration Time History (TART) No No No No No No Yes l 1-TABLE-1
f t 01055 EFERENCE TAILE - Continued 'o LOAD CACE O Selsmic Ties y Thermal Neight E?fut S.A.M. SE ISxx History THf84mx Fm WYux EFW'un SAmin MISec YllExx Source Element Action (Keyword) M O Yes Yes Yes No No No No Externally Applied Force (FCRCE) Force O (FOR) Yes No Yes No No No No Q Moment Externally Applied Dbmont (NDENTI s: 91 m (1993 o No No No No No Yes No Q Spectrwe Response Spectre d (ACE) ? Yes Yes No No No No Restraint Translaticael Springs (KA, AA) No Yes No No No No (EAB) Preload Force (FORCEI Yes No No No No No Translational DIspimt (DISP) No No No Yes No No Dif forential Selsmic Motion (DX, DY. DZ PHASE) No No No No No Yes l Displacement Tlee History (TDIS, DELAY Mr Tl) y l Acceleration Tlee History (TMX;, IELAY. MA.Til No ,5 y No No No No Yes No No No Yes No Response Spectre Name & Factor (R$NAIE, R$ FACT) No "4 Yes Yes Yes Yes Yes Yes Device Loeding Curve (NYS) No j$ No No No Yes No Device S-Velve Curve (SVA) No [ No Yes Yes Yes No Design Peak Strein (STRAINI No ,5 g No Yes Yes Yes No Design Peak Deformation (DDI No f '- No Yes Yes Yes No Secent Stiffness (SSI Yes S,* Yes Yes Yes Yes No Device Dimenslons (Y. L. A. NI No yj No No No Yes No Design Tolerance for Force (DIF) l No 3,T No No No Yes No Design Tolerance for Displacement (DTDI Yes Yes Yes Yes No Yes ~wx Young's Modulus (EEA8) e< som nas u y,, yg y,g yg y,, yjow l c Yes Yes Z Yes Yes Yes Yes Yes '+ Q " Loading Curve Label (NYS) No No Yes Yes Yes Yes 0* p @ l (HYSI Normellastion (NORM) Normellsetton Factors (XY, FY) 2m< o r+ e $ o' o" No No No No Yes No No No No No Yes No S3 S-V:lue curve Label (SVA) (SVAl Normaltration (NORN) O, 3. 3 No No No No Yes No Normellretion Factors (XY, FYI 0$" j w I l-TAritt-2 i
01055 NFEMM:E TAKE - Continued LOAD CASE 4 n Setemic Tlas o Thermal Neight Effet 5.A.N. SElsax ltistory u5 Soerce THRMex FGt WTux [FWTux SAMax letScc TlExx c) Element Action (Kevuord) k Yes Yes Yes No Yes Yes Yes Restrciat Translational Springs (KAl No Yes Yes No No No ido Yes No No No No No No Proloed Force (FGICE) (SPR) Translational Displemeent (Dl5PI O No No No No Yes No No Dif ferential Selsmic Motion (DX, DY, DZ, PHASE) o 2 No No Rlgid No No No No 2 300 Class 8 Keyword Restralnt o Restrclxt i l (SPD) 2 No No No No No No Yes d> Force Time History (TFat) f Dynamic ' Force (DLD) f No No No No No No Yes Tlas Function Time History Function defintflon (1015,1 ROT, TFDR, TMX;,1 ART) ITINI Remarks FDR. la load cose names, xx Is any two chorectors identifier. An Identifier is permitted on all load case names except l o 5.A.N. denotes seismic enchor movement onelysis. l o is assumed to be rigid. If KA and AA are not specified, restraint lencept EAB) For EAB, KA or AA must be given (or be derivable from toeding curwel for THietxx and WTxx lood cases. O ~ us 1 3Vm "O (D w q r1 5 3: cu < ID r+ @ r O' 5' O 3 'O OK3 O e+ rt 8 -T AftE-3
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NUMBER OF PAGES: APERTURE CARD /HARD COPY AVAILABLE FROM RECORD SERVICES BRANCH,TipC FT5 492-8939 (26 OR MORE OVEASIZE ORAWINGS) i 1 -}}