Nastran Result Summary - Boeing Huntsville Design Center


MSC Software
CORP
M S C N a s t r a n
Version 2017.1.2-CL511321
AUG 25, 2017
Intel
MODEL P5-4/5417 (A6119137)
Windows 7 Enterprise 6.1 7601
Compiled for 8664 (SINGLE Mode)

Quick Access Links to file Location
Nastran Job Folder D:/Test/Test
f06 File D:\Test\Test\abis8b_chk.f06
log File D:\Test\Test\x06_Reports\x06_abis8b_chk\abis8b_chk.log
f04 File D:\Test\Test\x06_Reports\x06_abis8b_chk\abis8b_chk.f04
Report Folder D:/Test/Test\x06_Reports\x06_abis8b_chk
Main Report FileD:\Test\Test\x06_Reports\x06_abis8b_chk\!abis8b_chk.htm
EXO6 Execution Log D:\Test\Test\x06_Reports\x06_abis8b_chk\abis8b_chk_x06.log



Simulation FATAL Errors Nastran FATAL Errors Description
No FATAL Messages Found.



Warning Messages Warning Messages are not considered Severe Enough to Stop the Nastran Job, but could result in unexpected answers.
No Warning Messages Found.



User Information Messages Echo of User Information Messages.

*** USER INFORMATION MESSAGE 3 (crdb::nastran::Processor::writeInput)
*** USER INFORMATION MESSAGE (WRITE DATA BLOCK PVT, TRAILER[101, 28, 0, 0, 0, 0, 0])

*** USER INFORMATION MESSAGE (WRITE DATA BLOCK CASECC, TRAILER[102, 7, 0, 1762, 0, 0, 0])
*** USER INFORMATION MESSAGE 3 (crdb::nastran::Processor::writeInput)

*** USER INFORMATION MESSAGE 3 (crdb::nastran::Processor::writeInput)
*** USER INFORMATION MESSAGE (WRITE DATA BLOCK GEOM1Q, TRAILER[101, 0, 2048, 8, 0, 0, 0])

*** USER INFORMATION MESSAGE (WRITE DATA BLOCK EPT, TRAILER[101, 4, 768, 0, 1024, 0, 16])
*** USER INFORMATION MESSAGE 3 (crdb::nastran::Processor::writeInput)

*** USER INFORMATION MESSAGE 3 (crdb::nastran::Processor::writeInput)
*** USER INFORMATION MESSAGE (WRITE DATA BLOCK GEOM2, TRAILER[103, 2, 64, 0, 9760, 0, 0])

*** USER INFORMATION MESSAGE (WRITE DATA BLOCK GEOM3, TRAILER[104, 0, 0, 80, 136, 32768, 0])
*** USER INFORMATION MESSAGE 3 (crdb::nastran::Processor::writeInput)

*** USER INFORMATION MESSAGE 3 (crdb::nastran::Processor::writeInput)
*** USER INFORMATION MESSAGE (WRITE DATA BLOCK GEOM1, TRAILER[101, 0, 2048, 8, 0, 0, 0])

*** USER INFORMATION MESSAGE (WRITE DATA BLOCK EDT, TRAILER[103, 0, 0, 0, 0, 0, 4])
1 CCTS LRS ABIS, 194000-0501, OFT MAY 28, 2019 MSC Nastran 8/25/17 PAGE 5

*** USER INFORMATION MESSAGE 3 (crdb::nastran::Processor::writeOutput)
*** USER INFORMATION MESSAGE (WRITE DATA BLOCK OGPWG, TRAILER[101, 0, 0, 0, 0, 0, 1])

*** USER INFORMATION MESSAGE 7570 (GPWG1S)
RESULTS OF RIGID BODY CHECKS OF MATRIX KGG (G-SET) FOLLOW:

*** USER INFORMATION MESSAGE 5293 (SSG3A)

*** USER INFORMATION MESSAGE 3 (crdb::nastran::Processor::writeOutput)
*** USER INFORMATION MESSAGE (WRITE DATA BLOCK OUG1, TRAILER[101, 0, 102014752, 0, 0, 0, 2])

*** USER INFORMATION MESSAGE (WRITE DATA BLOCK OES1X, TRAILER[102, 63, 5, 28, 19, 0, 2])
*** USER INFORMATION MESSAGE 3 (crdb::nastran::Processor::writeOutput)

*** USER INFORMATION MESSAGE 3 (crdb::nastran::Processor::writeOutput)
*** USER INFORMATION MESSAGE (WRITE DATA BLOCK OQG1, TRAILER[102, 0, 102014752, 0, 0, 0, 2])

*** USER INFORMATION MESSAGE (WRITE DATA BLOCK OQMG1, TRAILER[104, 0, 102014752, 0, 0, 0, 2])
1 CCTS LRS ABIS, 194000-0501, OFT MAY 28, 2019 MSC Nastran 8/25/17 PAGE 17





System Information Messages Echo of System Information Messages.

*** SYSTEM INFORMATION MESSAGE 4159 (DFMSA)

Refer to MAXRatio DataBlock





MSC Nastran File Management Section Nastran File Management Section Description

0 N A S T R A N F I L E A N D S Y S T E M P A R A M E T E R E C H O
0


NASTRAN BUFFSIZE=65537 $(C:/APPL/MSC/NASTRAN/20171/CONF/NAST20171.RCF[15])
NASTRAN NLINES=999999 $(C:/APPL/MSC/NASTRAN/20171/CONF/NAST20171.RCF[30])
NASTRAN PARALLEL=6 $(C:/APPL/MSC/NASTRAN/20171/CONF/NAST20171.RCF[31])
$ SUPPRESS WRITING LOAD DATA TO THE XDB, REDUCES SIZE $(C:/APPL/MSC/NASTRAN/2017
$ SUPPRESS WRITING LOAD DATA TO OP2, REDUCES SIZE $(C:/APPL/MSC/NASTRAN/20171/CO
$===============================================================================
$ CCTS LRS ABIS, CC1-194000, ASSEMBLY MODEL
$===============================================================================
$
$ THIS MODEL IS USED FOR THE STRESS ANALYSIS OF 40 PARTS INCLUDED IN THE
$ 194000 ANALYSIS PACKAGE. OTHER RELATED PACKAGES THAT INCLUDE ADJOINING
$ PARTS ARE 193000, 194325, AND 194344. EACH ANALYSIS PACKAGE HAS A
$ FORMAL STRESS REPORT THAT LISTS THE SAFETY MARGINS AND STRESS ANALYSIS
$ DOCUMENTATION.
$
$ MODEL IS DIVIDED INTO 6 MAIN REGIONS.
$
$ REGION NUMBERING SCHEME:
$ ------------------------
$ 1) TUBES_INNER_BAG ----------> 100001-200000
$ 2) TUBES_OUTER_BAG ----------> 200001-300000
$ 3) TUBE_SUPPORT_BRACKETS ----> 300001-700000
$ 4) BRACKET_PARTS_HARDWARE----> 800001-900000
$ 5) MPC ----------------------> 900001-1000000
$ 6) COMMAND VALVE BRACKETS ---> 1000001-3000000
$
$ UPDATE HISTORY:
$ ---------------
$ - 2015: MODEL CREATED BY SHOLA AWOYALE, 2015
$ - 2019_MAY: MODEL UPDATE
$ 1) CHANGED COMMAND VALVE PANELS (6X)
$ 2) CONVERTED FROM FEMAP TO PATRAN
$ 3) ADDED NEW ATCS PANEL AND ATCS VALVE BRACKET (146410)
$
$
$===============================================================================
$NASTRAN SYSTEM(444)=9 $ ALLOW INTEGER IN REAL FIELD
$NASTRAN XMSG=0 $ GIVE EXTENDED ERROR MESSAGES (0=OFF,1=ON)
$NASTRAN INDEX=19 $ SETS INDEXING FOR PATRAN WITH SOL 400
$NASTRAN STPFLG=0 $ KEEP STANDARD SUBCASE/STEP LAYOUT
$NASTRAN OP2NEW=0 $ SET OP2 VERSION INFO (0=OLD, 1=NEW, >2004)
$NASTRAN SEGLOG=1 $ SET STS CONTACT PENALTY LOGIC (0=OLD, 1=NEW, >=2017))
$NASTRAN QRMETH=5 $ CONVERT SHELLS TO CQUADR FORMULATION
$===============================================================================


MSC Nastran File Executive Control Section Nastran Executive Control Section Description

SOL SESTATIC


MSC Nastran File Case Control Section Nastran Case Control Section Description

0 C A S E C O N T R O L E C H O
COMMAND
COUNT
1 $======================================================================= ========
2 $ SET DEFINITIONS
3 $ 11 = COMMAND VALVE PANEL ELEMENTS (SOLID)
4 $ 13 = TUBE SUPPORT BRACKET ELEMENTS (SHELL)
5 $ 15 = ALL BRACKET ELEMENTS
6 $ 21 = ALL TUBE ELEMNENTS (BAR/BEAM)
7 $ 31 = ALL CBUSH ELEMENTS
8 $ 32 = ALL CBUSH GRIDS
9 $ 41 = ALL CVB PART JOINT GRIDS
10 $ 51 = ALL P-CLAMP JOINT SPACER BARS
11 $ 101 = ALL BAR/BUSH ELEMENT
12 $ 102 = ALL BAR/BUSH GRIDS
13 $======================================================================= ========
14 $INCLUDE ../inc/abis2a_sets.dat
15 $======================================================================= ========
16 $ SET DEFINITIONS
17 $ 11 = COMMAND VALVE PANEL ELEMENTS (SOLID)
18 $ 13 = TUBE SUPPORT BRACKET ELEMENTS (SHELL)
19 $ 15 = ALL BRACKET ELEMENTS
20 $ 21 = ALL TUBE ELEMNENTS (BAR/BEAM)
21 $ 31 = ALL CBUSH ELEMENTS
22 $ 32 = ALL CBUSH GRIDS
23 $ 41 = ALL CVB PART JOINT GRIDS
24 $ 51 = ALL P-CLAMP JOINT SPACER BARS
25 $ 101 = ALL BAR/BUSH ELEMENT
26 $ 102 = ALL BAR/BUSH GRIDS
27 $======================================================================= ========
28 $ ELEMENTS (AND CONNECTORS) FOR GROUP : E1_ALL_BRACKETS_CV
29 SET 11 = 1000001 THRU 2108582,2108583
30 $======================================================================= ========
31 $ NODES FOR GROUP : E1_ALL_BRACKETS_CV
32 SET 12 = 800260 THRU 813573,1000001 THRU 1139449,1139518 THRU 1139538,
33 1139573 THRU 1139794,1139847 THRU 1139898,1139977 THRU 1140004,1140041,
34 1140042 THRU 1140081,1140088,1140110 THRU 1140348,1140354 THRU 1140724,
35 1140730 THRU 1141132,1141138 THRU 1149973,1150061 THRU 1161285,1161291,
36 1161292 THRU 1161891,1161980 THRU 1175609,1175632 THRU 1175653,1175687,
37 1175688 THRU 1178784,1179042 THRU 1179319,1179486 THRU 1183173,1183187,
38 1183188 THRU 1186226,1186238 THRU 1186980,1186996 THRU 1200652,1200731,
39 1200732 THRU 1202133,1202282 THRU 1360460,1360503 THRU 1360530,1360547,
40 1360548 THRU 1360853,1361036 THRU 1361056,1361089 THRU 1361209,1361238,
41 1361239 THRU 1361499,1361513 THRU 1363941,1363955 THRU 1364292,1364306,
42 1364307 THRU 1367295,1367370 THRU 1379521,1379527 THRU 1381241,1381253,
43 1381254 THRU 1382474,1382547 THRU 1398792,1398870 THRU 1401903,1402609,
44 1402610 THRU 1407789,1407821 THRU 1411807,1411841 THRU 1412606,1412626,
45 1412627 THRU 1429571,1429654 THRU 1429742,1429911 THRU 1589817,1589858,
46 1589859 THRU 1589883,1589900 THRU 1590209,1590392 THRU 1590410,1590445,
47 1590446 THRU 1590544,1590573 THRU 1590832,1590846 THRU 1593464,1593478,
48 1593479 THRU 1593825,1593839 THRU 1596770,1596850 THRU 1609647,1609653,
49 1609654 THRU 1611313,1611327 THRU 1612606,1612685 THRU 1628936,1629014,
50 1629015 THRU 1632072,1632766 THRU 1638086,1638120 THRU 1641896,1641926,
51 1641927 THRU 1642745,1642767 THRU 1660109,1660189 THRU 1660278,1660376,
52 1660377 THRU 1660428,1660506 THRU 1823261,1823286 THRU 1823301,1823326,
53 1823327 THRU 1823386,1823403 THRU 1823466,1823483 THRU 1823639,1823846,
54 1823847 THRU 1824035,1824062 THRU 1824290,1824304 THRU 1824678,1824692,
55 1824693 THRU 1827456,1827470 THRU 1828841,1828855 THRU 1828953,1829020,
56 1829021 THRU 1847348,1847364 THRU 1871702,1871786 THRU 1873449,1873477,
57 1873478 THRU 1875914,1875944 THRU 1879675,1880422 THRU 1882357,1882454,
58 1882455 THRU 1885184,1885282 THRU 1885953,1885975 THRU 1888796,1888818,
59 1888819 THRU 1897074,1897152 THRU 1898087,1898165 THRU 1960871,1960873,
60 1960874 THRU 2001458,2001460 THRU 2054470,2054513 THRU 2054538,2054555,
61 2054556 THRU 2054872,2055055 THRU 2055073,2055110 THRU 2055213,2055240,
62 2055241 THRU 2055527,2055541 THRU 2058137,2058151 THRU 2058541,2058555,
63 2058556 THRU 2061653,2061731 THRU 2074464,2074470 THRU 2076221,2076233,
64 2076234 THRU 2077474,2077549 THRU 2093580,2093658 THRU 2096760,2097474,
65 2097475 THRU 2102782,2102816 THRU 2106483,2106515 THRU 2107322,2107344,
66 2107345 THRU 2124344,2124428 THRU 2124516,2124623 THRU 2124670,2124749,
67 2124750 THRU 2564523,2564525,2564558 THRU 2564565,2564567,2564592,
68 2564593 THRU 2564609,2564724 THRU 2564740,2564887 THRU 2564893,2564978,
69 2564979 THRU 2564989,2565034 THRU 2566135,2566143 THRU 2566156,2566158,
70 2566159 THRU 2566166,2566168 THRU 2566176,2566196 THRU 2566830,2566865,
71 2566866 THRU 2566920,2567013,2567014,2567015,2567023 THRU 2567032,
72 2567101,2567125 THRU 2567234,2567303 THRU 2567323,2567561 THRU 2584412,
73 2584426 THRU 2584955,2584967 THRU 2585041,2585533,2585704 THRU 2585943,
74 2585990 THRU 2586638,2586809,2586810,2586812,2586813,2586815,2586816,
75 2587471 THRU 2590851,2591441 THRU 2594718,2595046,2595047,2595216,
76 2595217 THRU 2596742,2597100 THRU 2608398,2608453 THRU 2613034,2613169,
77 2613170 THRU 2614403,2614428 THRU 2621238,2621269 THRU 2633073,2633124,
78 2633125 THRU 2686712,2686733 THRU 2689339,2689356 THRU 2695044,2695056,
79 2695057 THRU 2696006,2696017 THRU 2725614,2725641 THRU 2737752,2737962,
80 2737963 THRU 2738631,2738641 THRU 2739136,2739207 THRU 2747148,2747327,
81 2747328 THRU 2751174,2751807 THRU 2766447,2766448
82 $======================================================================= ========
83 $ ELEMENTS (AND CONNECTORS) FOR GROUP : E1_ALL_BRACKETS_TUBE
84 SET 13= 300001 THRU 329911,329912
85 $======================================================================= ========
86 $ NODES FOR GROUP : E1_ALL_BRACKETS_TUBE
87 SET 14= 29 THRU 42,300001 THRU 300468,300470 THRU 300582,300595,
88 300596 THRU 302077,302079 THRU 302156,302161 THRU 302218,302220,
89 302221 THRU 302743,302745 THRU 302907,302909 THRU 303143,303145,
90 303146 THRU 311754,311771 THRU 311831,311833 THRU 312187,312189,
91 312190 THRU 315857,315859 THRU 315874,315876 THRU 315881,315883,
92 315884 THRU 315899,315901 THRU 315906,315908 THRU 315923,315925,
93 315926 THRU 317758,317760 THRU 317765,317767 THRU 317904,317906,
94 317907 THRU 317922,317924 THRU 317929,317931 THRU 317946,317948,
95 317949 THRU 320858,320860 THRU 320950,320952 THRU 320977,320980,
96 320981 THRU 321099,321101 THRU 321144,321146 THRU 321584,321586,
97 321587 THRU 321609,321611 THRU 322117,322122 THRU 322241,322243,
98 322244 THRU 322286,322288 THRU 323257,323260 THRU 323379,323381,
99 323382 THRU 323424,323426 THRU 324835,324837 THRU 325295,325297,
100 325298 THRU 325815,325817 THRU 325959,325961 THRU 326795,326797,
101 326798 THRU 326859,326884 THRU 327305,327307 THRU 327316,327318,
102 327319 THRU 327550,327575 THRU 327985,327987 THRU 327997,327999,
103 328000 THRU 328241,328266 THRU 328676,328678 THRU 328688,328690,
104 328691 THRU 328932,328957 THRU 329367,329369 THRU 329379,329381,
105 329382 THRU 329623,329648 THRU 330069,330071 THRU 330080,330082,
106 330083 THRU 330314,330339 THRU 330749,330751 THRU 330761,330763,
107 330764 THRU 330963,800043 THRU 800258,800259
108 $======================================================================= ========
109 $ ELEMENTS (AND CONNECTORS) FOR GROUP : ALL__BRACKETS
110 SET 15 = 300001 THRU 329912,1000001 THRU 2108582,2108583
111 $======================================================================= ========
112 $ ELEMENTS (AND CONNECTORS) FOR GROUP : ALL__TUBES
113 SET 21 = 100001 THRU 102440,200001 THRU 202567,202568
114 $======================================================================= ========
115 $ ELEMENTS (AND CONNECTORS) FOR GROUP : ALL_CBUSH
116 SET 31 = 1001 THRU 1056,1058 THRU 1071,800004,800005,800006
117 $======================================================================= ========
118 $ NODES FOR GROUP : ALL_CBUSH
119 SET 32 = 101 THRU 129,1030 THRU 1100,1116,1120,1124,1125,1126,
120 1129,1130,1131,1132,100291,200380,800002 THRU 800034,813574,
121 813575,813576
122 $======================================================================= ========
123 $ NODES FOR GROUP : N3_ALL_JOINTS_CVB_PARTS
124 SET 41 = 813600 THRU 813605,813617,813618,813637 THRU 813641,813652,
125 813653,813654,813673 THRU 813678,813689,813690,813692,813693,813694,
126 813695,813713,813724,813725,813726,813745 THRU 813750,813761,813762,
127 813769,813770,813788 THRU 813792,832728 THRU 832735,832737 THRU 832741,
128 832742
129 $======================================================================= ========
130 $ NODES FOR GROUP : ALL_SPACER_BARS
131 SET 51 = 111 THRU 118,130,1116,1120,1124,1125,1126,1129,1130,1131,1132,
132 813577 THRU 813582,813583
133 $======================================================================= ========
134 $ ELEMENTS (AND CONNECTORS) FOR GROUP : ALL_BAR
135 SET 101= 1001 THRU 1071,50001 THRU 50024,100001 THRU 102440,200001,
136 200002 THRU 202568,800001 THRU 800016,800020 THRU 800027,800032,
137 800033 THRU 800046,800048 THRU 800072,800074 THRU 800099,800101,
138 800102 THRU 800126,800128 THRU 800153,800155 THRU 800166,800173,
139 800174 THRU 800186,800188 THRU 800199,810145,810146,810147,810148
140 $======================================================================= ========
141 $ NODES FOR GROUP : ALL_BAR
142 SET 102=101 THRU 157,1030 THRU 1100,1116,1120,1124,1125,1126,1129,1130,
143 1131,1132,100001 THRU 100040,100042 THRU 100097,100099 THRU 100107,
144 100109 THRU 100182,100184 THRU 100193,100195 THRU 100300,100302,
145 100303 THRU 100329,100331 THRU 100342,100344 THRU 100359,100361,
146 100362 THRU 100447,100449,100450,100452 THRU 100479,100481 THRU 100640,
147 100642 THRU 100776,100778,100779,100781 THRU 100813,100815 THRU 100942,
148 100944 THRU 100987,100989,100991 THRU 101240,101242 THRU 101288,101290,
149 101291,101292,101294 THRU 101394,101396,101397,101399,101400,101402,
150 101403 THRU 101496,101498,101499,101502,101503,101504,101506,
151 101507 THRU 101761,101763,101764,101766 THRU 101836,101838 THRU 101913,
152 101915 THRU 101919,101921,101922,101923,101927 THRU 102214,102216,
153 102218 THRU 102245,102247 THRU 102440,200001 THRU 200041,200043,
154 200044 THRU 200090,200093 THRU 200168,200170,200171,200173 THRU 200259,
155 200261,200262,200263,200264,200266 THRU 200318,200320 THRU 200375,
156 200377 THRU 200443,200445,200446,200448 THRU 200570,200572 THRU 200611,
157 200613 THRU 200754,200756 THRU 200834,200836,200838 THRU 200924,200926,
158 200927 THRU 200967,200969 THRU 201183,201185 THRU 201272,201274,
159 201275 THRU 201298,201300,201302 THRU 201492,201494 THRU 201511,201513,
160 201514 THRU 201526,201528 THRU 201613,201615,201616,201617,201618,
161 201621 THRU 201638,201640 THRU 201893,201895,201896,201897,201899,
162 201900,201902 THRU 201915,201917 THRU 202067,202070,202071,202072,
163 202074,202076 THRU 202331,202334 THRU 202387,202389 THRU 202451,202453,
164 202454 THRU 202568,800002 THRU 800042,813574 THRU 813598,813600,813601,
165 813602,813603,813606 THRU 813616,813619 THRU 813633,813635 THRU 813640,
166 813642 THRU 813651,813655 THRU 813669,813671 THRU 813676,813679,
167 813680 THRU 813688,813691 THRU 813709,813711,813712,813714 THRU 813723,
168 813727 THRU 813741,813743 THRU 813748,813751 THRU 813760,813771,
169 813772 THRU 813784,813786,813787,813790 THRU 813802,832728 THRU 832734,
170 832735
171 $ 1 | 2 | 3 | 4 | 5 | 6 | 7 | 8 | 9 | 10 |
172 $======================================================================= ========
173 $END OF INCLUDE FILE ../inc/abis2a_sets.dat
174 $======================================================================= ========
175 TITLE = CCTS LRS ABIS, 194000-0501, OFT
176 $======================================================================= ========
177 ECHO = NONE
178 $RIGID = LAGR
179 RIGID = LINEAR
180 AUTOSPC(RESIDUAL,NOPRINT) = YES
181 GROUNDCHECK = YES
182 $======================================================================= ========
183 DISPLACEMENT(PLOT) = ALL
184 SPCFORCES(PLOT) = ALL
185 STRESS(PLOT) = 15
186 FORCE(PLOT) = 101
187 MPCFORCE(PLOT) = ALL
188 $BOUTPUT(PLOT) = NONE
189 $----------------------------------------------------
190 $ RESULT SUMMARY TABLE REQUESTS, LINEAR
191 $----------------------------------------------------
192 $MAXMIN(DEF) DISP MAGT MAXA(5) BRIEF
193 $MAXMIN(DEF) SPCF T1 T2 T3 MAGT R1 R2 R3 MAGR ALL(5) BRIEF
194 $MAXMIN(DEF) FORCE(BAR,6,7,8) MAXA(5) BRIEF
195 $MAXMIN(DEF) FORCE(BEAM,6,7,8) MAXA(5) BRIEF
196 $MAXMIN(DEF) STRESS(QUAD4,7,8,9,15,16,17) MINA(5) MAXA(3) FULL
197 $MAXMIN(DEF) STRESS(QUAD4C,9,11,17,19) MAXA(3) BRIEF
198 $MAXMIN(DEF) STRESS(TETRA, 8,13) MAXA(5) BRIEF
199 $MAXMIN(BOTH,CENTER,FIBER) = ALL
200 $======================================================================= ========
201 $ PRIMARY LOAD CASES (7X)
202 $======================================================================= ========
203 SUBCASE 101
204 SUBTITLE = MAC_GX47
205 SPC = 2
206 LOAD = 3105
207 SUBCASE 102
208 SUBTITLE = MAC_GY47
209 SPC = 2
210 LOAD = 3107
211 SUBCASE 103
212 SUBTITLE = MAC_GZ47
213 SPC = 2
214 LOAD = 3109
215 $------------------------------------------
216 SUBCASE 201
217 SUBTITLE = TUBE_BEND_FORCES
218 SPC = 2
219 LOAD = 3111
220 $------------------------------------------
221 SUBCASE 301
222 SUBTITLE = THERMAL_BLOWDOWN
223 SPC = 2
224 TEMPERATURE(LOAD) = 3101
225 SUBCASE 302
226 SUBTITLE = THERMAL_COLD
227 SPC = 2
228 TEMPERATURE(LOAD) = 3102
229 SUBCASE 303
230 SUBTITLE = THERMAL_HOT
231 SPC = 2
232 TEMPERATURE(LOAD) = 3103
233 $======================================================================= ========
234 $ LOAD CASE COMBINATIONS (27X)
235 $======================================================================= ========
236 $-----------------------------------------------------------
237 $ MAC LOAD COMBINATIONS (.5,1,.5), NO PRESSURE, NO THERMAL
238 $-----------------------------------------------------------
239 $ SUBCOM 411
240 $ SUBTITLE = MAC_COMBO_515(+++)
241 $ SUBSEQ = 0.5,1.,0.5, 0., 0.,0.,0.
242 $ SUBCOM 412
243 $ SUBTITLE = MAC_COMBO_515(---)
244 $ SUBSEQ = -0.5,-1.,-0.5, 0., 0.,0.,0.
245 $ SUBCOM 413
246 $ SUBTITLE = MAC_COMBO_515(++-)
247 $ SUBSEQ = 0.5,1.,-0.5, 0., 0.,0.,0.
248 $ SUBCOM 414
249 $ SUBTITLE = MAC_COMBO_515(--+)
250 $ SUBSEQ = -0.5,-1.,0.5, 0., 0.,0.,0.
251 $ SUBCOM 415
252 $ SUBTITLE = MAC_COMBO_515(+-+)
253 $ SUBSEQ = 0.5,-1.,0.5, 0., 0.,0.,0.
254 $ SUBCOM 416
255 $ SUBTITLE = MAC_COMBO_515(-+-)
256 $ SUBSEQ = -0.5,1.,-0.5, 0., 0.,0.,0.
257 $ SUBCOM 417
258 $ SUBTITLE = MAC_COMBO_515(+--)
259 $ SUBSEQ = 0.5,-1.,-0.5, 0., 0.,0.,0.
260 $ SUBCOM 418
261 $ SUBTITLE = MAC_COMBO_515(-++)
262 $ SUBSEQ = -0.5,1.,0.5, 0., 0.,0.,0.
263 $ $-----------------------------------------------------------
264 $ $ MAC LOAD COMBINATIONS (.5,.5,1), NO PRESSURE, NO THERMAL
265 $ $-----------------------------------------------------------
266 $ SUBCOM 421
267 $ SUBTITLE = MAC_COMBO_551(+++)
268 $ SUBSEQ = 0.5,0.5,1., 0., 0.,0.,0.
269 $ SUBCOM 422
270 $ SUBTITLE = MAC_COMBO_551(---)
271 $ SUBSEQ = -0.5,-0.5,-1., 0., 0.,0.,0.
272 $ SUBCOM 423
273 $ SUBTITLE = MAC_COMBO_551(++-)
274 $ SUBSEQ = 0.5,0.5,-1., 0., 0.,0.,0.
275 $ SUBCOM 424
276 $ SUBTITLE = MAC_COMBO_551(--+)
277 $ SUBSEQ = -0.5,-0.5,1., 0., 0.,0.,0.
278 $ SUBCOM 425
279 $ SUBTITLE = MAC_COMBO_551(+-+)
280 $ SUBSEQ = 0.5,-0.5,1., 0., 0.,0.,0.
281 $ SUBCOM 426
282 $ SUBTITLE = MAC_COMBO_551(-+-)
283 $ SUBSEQ = -0.5,0.5,-1., 0., 0.,0.,0.
284 $ SUBCOM 427
285 $ SUBTITLE = MAC_COMBO_551(+--)
286 $ SUBSEQ = 0.5,-0.5,-1., 0., 0.,0.,0.
287 $ SUBCOM 428
288 $ SUBTITLE = MAC_COMBO_551(-++)
289 $ SUBSEQ = -0.5,0.5,1., 0., 0.,0.,0.
290 $ $-----------------------------------------------------------
291 $ $ MAC LOAD COMBINATIONS (1,.5,.5), NO PRESSURE, NO THERMAL
292 $ $-----------------------------------------------------------
293 $ SUBCOM 431
294 $ SUBTITLE = MAC_COMBO_155(+++)
295 $ SUBSEQ = 1.,0.5,0.5, 0., 0.,0.,0.
296 $ SUBCOM 432
297 $ SUBTITLE = MAC_COMBO_155(---)
298 $ SUBSEQ = -1.,-0.5,-0.5, 0., 0.,0.,0.
299 $ SUBCOM 433
300 $ SUBTITLE = MAC_COMBO_155(++-)
301 $ SUBSEQ = 1.,0.5,-0.5, 0., 0.,0.,0.
302 $ SUBCOM 434
303 $ SUBTITLE = MAC_COMBO_155(--+)
304 $ SUBSEQ = -1.,-0.5,0.5, 0., 0.,0.,0.
305 $ SUBCOM 435
306 $ SUBTITLE = MAC_COMBO_155(+-+)
307 $ SUBSEQ = 1.,-0.5,0.5, 0., 0.,0.,0.
308 $ SUBCOM 436
309 $ SUBTITLE = MAC_COMBO_155(-+-)
310 $ SUBSEQ = -1.,0.5,-0.5, 0., 0.,0.,0.
311 $ SUBCOM 437
312 $ SUBTITLE = MAC_COMBO_155(+--)
313 $ SUBSEQ = 1.,-0.5,-0.5, 0., 0.,0.,0.
314 $ SUBCOM 438
315 $ SUBTITLE = MAC_COMBO_155(-++)
316 $ SUBSEQ = -1.,0.5,0.5, 0., 0.,0.,0.
317 $ $-----------------------------------------------------------
318 $ $ PRESSURE PLUS THERMAL BLOWDOWN
319 $ $-----------------------------------------------------------
320 $ SUBCOM 501
321 $ SUBTITLE = BLOWDOWN_PRESSURE
322 $ SUBSEQ = 0.,0.,0., 1., 1.,0.,0.
323 $ $-----------------------------------------------------------
324 $ $ PRESSURE PLUS HOT SOAK
325 $ $-----------------------------------------------------------
326 $ SUBCOM 502
327 $ SUBTITLE = HOT_PRESSURE
328 $ SUBSEQ = 0.,0.,0., 1., 0.,0.,1.
329 $ $-----------------------------------------------------------
330 $ $ PRESSURE PLUS COLD SOAK
331 $ $-----------------------------------------------------------
332 $ SUBCOM 503
333 $ SUBTITLE = COLD_PRESSURE
334 $ SUBSEQ = 0.,0.,0., 1., 0.,1.,0.
335 $======================================================================= ========


























MSC Nastran Bulk Data Summary Section Nastran Bulk Data Summary Description

Model Volume/Weight Breakdown can be triggered using (in Case Control Section):

ELSUM(EIDSUM)=ALL
Model Summary
Entity TypeNumber in Model
MAT111
CTRIA3348
GRAV3
PSOLID7
SPC14
CBUSH74
CTETRA1118528
FORCE223
TEMP15501
PBEAM6
CORD2R121
CONM221
SPCADD1
LOAD4
CQUAD429564
PBUSH72
MDLPRM1
PARAM4
CBEAM5213
GRID1821692
PBEAML29
TEMPD3
PSHELL11
RBE2164


Nastran Element Geometry Tests Summary Nastran Element Geometry Tests Description
Summary Of Tests List of Elements Tests Performed
Elem Type Skew Angle Aspect/Taper Ratio Min Int. Angle Max Int. Angle Surf/Face Warp Factor Offset Ratio Edge Pt Lenght Ratio Edge Pt Angle Limit Jacobian Determinant
BEAMN/AN/AN/AN/AN/A0N/AN/AN/A
TRIA30N/AN/A0N/AN/AN/AN/AN/A
QUAD402000N/AN/AN/AN/A
TETRAN/A0N/AN/AN/AN/A5484697
N/A IN THE ABOVE TABLE INDICATES TESTS THAT ARE NOT APPLICABLE TO THE ELEMENT TYPE AND WERE NOT PERFORMED.

QUAD4 ELEMENT ID 300991 PRODUCED LARGEST TAPER RATIO OF 0.51 (TOLERANCE = 0.50).
TETRA ELEMENT ID 1306178 PRODUCED LARGEST EDGE POINT LR OF 0.37 (TOLERANCE = 0.50).
TETRA ELEMENT ID 805494 PRODUCED SMALLEST EDGE POINT ANGLE OF 134.78 (TOLERANCE = 150.00).
TETRA ELEMENT ID 1191859 PRODUCED SMALLEST VERTEX DET(JAC) -UWM 6828- OF 0.00 (TOLERANCE = 0.00).



Ouptout From Grid Point Weight Generator (GPWG) The Grid Point Weight Generator (GPWG)
Triggered by :
PARAM,GRDPNT,n
Represents the total system Model Mass/Weigth Inertia Matrices
Reference Point The Reference Point is triggered by:

PARAM,GRDPNT,n

Nastran computes mass properties relative to grid point with identifier grid.

If this grid point does not exist (or 0), Nastran computes mass properties relative to the origin of the basic coordinate system
0
Rigid Body Mass Matrix The Rigid Body Mass Matrix shows the rigid body mass matrix Mrr with respect to the reference point.

It relates the inertia loads to the rigid body accelerations about the reference point.

| M33 | R33 |
| R33T | J33 |

M33 is the mass matrix.
It usually is a diagonal matrix with the mass on the diagonal.

R33 is the matrix of static moments about the reference point.

J33 is the matrix of moments of inertia about the reference point.
1.052261E+02-2.623348E-177.447761E-17-1.910224E-151.849039E+03-9.390829E+02
-2.623348E-171.052261E+023.325118E-17-1.849039E+03-4.116150E-142.393142E+04
7.447761E-173.325118E-171.052261E+029.390829E+02-2.393142E+04-1.441071E-14
-1.910224E-15-1.849039E+039.390829E+024.883417E+05-2.071645E+05-4.417606E+05
1.849039E+03-4.116150E-14-2.393142E+04-2.071645E+055.751141E+063.720220E+04
-9.390829E+022.393142E+04-1.441071E-14-4.417606E+053.720220E+045.635836E+06
S [S] shows the transformation matrix from the principal mass axes to the basic coordinate system.

If no directional scalar masses have been defined this should be an identity matrix.
1.000000E+000.000000E+000.000000E+00
0.000000E+001.000000E+000.000000E+00
0.000000E+000.000000E+001.000000E+00
Direction The Mass System (S) shows the masses in the three directions and the locations of the center of mass.

The locations are the distances, in the basic coordinate system, of the center of mass from the reference point.

If no directional scalar masses have been input, all masses should be identical.
Mass system (S)MassX (CG)Y (CG)Z (CG)
X1.052261E+02-1.815351E-178.924427E+001.757205E+01
Y1.052261E+022.274285E+02-3.911719E-161.757205E+01
Z1.052261E+022.274285E+028.924427E+00-1.369499E-16
I(S) I(S) shows the moments of inertia about the center of mass with respect to the basic coordinate system.
4.474695E+05-6.409731E+032.123630E+04
-6.409731E+032.759600E+05-5.370381E+04
2.123630E+04-5.370381E+041.847658E+05
I(Q) I(Q) shows the transformation matrix from the principal directions to the basic coordinate system.
3.007488E+05
4.492020E+05
1.582445E+05
Q Q shows the principal moments of inertia.
-2.065441E-029.969122E-017.575912E-02
-9.086861E-011.288425E-02-4.172811E-01
-4.169687E-01-7.745996E-029.056142E-01




OLOAD Resultant Table Output Nastran Calls OLOAD The SUM of Externally Generated Loading on the Structure
(such as inertial loading or applied loads)

Loads are Summarized by SUBCASEs.

OLOAD are calculated relative to the Basic Coord System Origin.
SubCasesType T1T2 T3R1 R2R3
101FX 4.945628E+03 ---- ---- ---- 8.690484E+04 -4.413689E+04
101FY ---- -1.375825E-15 ---- 9.486595E-14 ---- -3.256781E-13
101FZ ---- ---- 5.124614E-15 -2.277208E-13 -1.218577E-12 ----
101MX ---- ---- ---- 0.000000E+00 ---- ----
101MY ---- ---- ---- ---- 0.000000E+00 ----
101MZ ---- ---- ---- ---- ---- 0.000000E+00
101Totals 4.945628E+03 -1.375825E-15 5.124614E-15 -1.328548E-13 8.690484E+04 -4.413689E+04
SubCasesType T1T2 T3R1 R2R3
102FX -2.144596E-15 ---- ---- ---- -1.423639E-13 4.807381E-13
102FY ---- 4.945628E+03 ---- -8.690484E+04 ---- 1.124777E+06
102FZ ---- ---- -1.942970E-14 4.681926E-14 4.609340E-12 ----
102MX ---- ---- ---- 0.000000E+00 ---- ----
102MY ---- ---- ---- ---- 0.000000E+00 ----
102MZ ---- ---- ---- ---- ---- 0.000000E+00
102Totals -2.144596E-15 4.945628E+03 -1.942970E-14 -8.690484E+04 4.466976E-12 1.124777E+06
SubCasesType T1T2 T3R1 R2R3
103FX 1.632111E-16 ---- ---- ---- -5.519870E-13 2.185293E-13
103FY ---- -1.873984E-15 ---- 4.192208E-13 ---- -4.490576E-13
103FZ ---- ---- 4.945628E+03 4.413689E+04 -1.124777E+06 ----
103MX ---- ---- ---- 0.000000E+00 ---- ----
103MY ---- ---- ---- ---- 0.000000E+00 ----
103MZ ---- ---- ---- ---- ---- 0.000000E+00
103Totals 1.632111E-16 -1.873984E-15 4.945628E+03 4.413689E+04 -1.124777E+06 -2.305283E-13
SubCasesType T1T2 T3R1 R2R3
201FX 1.088749E+03 ---- ---- ---- -1.359389E+04 -1.970080E+04
201FY ---- 3.131226E+02 ---- 9.365904E+03 ---- 7.176638E+04
201FZ ---- ---- 3.491436E+02 -2.095469E+03 -7.272821E+04 ----
201MX ---- ---- ---- 0.000000E+00 ---- ----
201MY ---- ---- ---- ---- 0.000000E+00 ----
201MZ ---- ---- ---- ---- ---- 0.000000E+00
201Totals 1.088749E+03 3.131226E+02 3.491436E+02 7.270436E+03 -8.632210E+04 5.206559E+04
SubCasesType T1T2 T3R1 R2R3
301FX -5.721344E-12 ---- ---- ---- 6.675533E+04 -2.704317E+04
301FY ---- -2.290231E-12 ---- 8.913252E+04 ---- 2.704317E+04
301FZ ---- ---- 1.151662E-12 -8.913252E+04 -6.675533E+04 ----
301MX ---- ---- ---- 0.000000E+00 ---- ----
301MY ---- ---- ---- ---- 0.000000E+00 ----
301MZ ---- ---- ---- ---- ---- 0.000000E+00
301Totals -5.721344E-12 -2.290231E-12 1.151662E-12 3.492460E-09 7.130438E-10 -6.039045E-10
SubCasesType T1T2 T3R1 R2R3
302FX 3.600908E-12 ---- ---- ---- 2.578636E+04 -1.044628E+04
302FY ---- 9.078467E-12 ---- 3.443025E+04 ---- 1.044628E+04
302FZ ---- ---- 4.124759E-13 -3.443025E+04 -2.578636E+04 ----
302MX ---- ---- ---- 0.000000E+00 ---- ----
302MY ---- ---- ---- ---- 0.000000E+00 ----
302MZ ---- ---- ---- ---- ---- 0.000000E+00
302Totals 3.600908E-12 9.078467E-12 4.124759E-13 3.419700E-10 9.968062E-10 -2.008164E-09
SubCasesType T1T2 T3R1 R2R3
303FX -1.095099E-11 ---- ---- ---- -1.759256E+04 7.126900E+03
303FY ---- 1.148796E-12 ---- -2.348980E+04 ---- -7.126900E+03
303FZ ---- ---- 6.398773E-13 2.348980E+04 1.759256E+04 ----
303MX ---- ---- ---- 0.000000E+00 ---- ----
303MY ---- ---- ---- ---- 0.000000E+00 ----
303MZ ---- ---- ---- ---- ---- 0.000000E+00
303Totals -1.095099E-11 1.148796E-12 6.398773E-13 -2.000888E-10 4.620233E-10 2.722118E-09




Maximum (Pivot) Ratio Table Output Pivot Ratio is a measure of numeric ill-Conditioning in the model potentieally due to:
  • Rigid body motions due to inadequate constraints
  • Mechanisms due to DOF mismatch between dissimilar element types
  • Very stiff elements near flexible elements
  • Very distorted elements
  • Unreasonable material properties
  • Etc...

  • Maximum (Pivot) Ratio Table Output4.685209E+04




    Epsilon Value Output In a static analysis, the equation

    Ku = P

    is solved for the displacements (u).

    Subsequently, residual loads can be computed from

    DP = Ku - P

    Because of numerical roundoff, the residual loads will not be zero For each subcase, a normalized value of the residual load is given by

    epsilon = (uT . DP)/(uT . P)

    A value of epsilon less than about 10-9 is generally considered acceptable.
    Large values of epsilon indicate an ill-conditioned model, possibly due to rigid body motions or mechanisms.
    SubcasesEpsilon External Work
    1 -1.3492765E-11 2.5268093E+01
    2 -1.1151891E-10 6.4288313E+01
    3 -2.8933065E-11 5.0519139E+01
    4 -6.4617461E-12 1.8911968E+02
    5 -3.7499086E-13 9.6534427E+03
    6 -3.8007517E-13 1.4404236E+03
    7 -3.3767467E-13 6.7045310E+02




    SPC Forces Resultant Table Output Nastran Calls SPC Forces Resultants The SUM of Reaction Forces
    generated by the Structure at the Boundary Conditions

    Loads are Summarized by SUBCASEs.
    SubCasesType T1T2 T3R1 R2R3
    101FX -4.945628E+03 ---- ---- ---- -8.267889E+04 4.254763E+04
    101FY ---- 2.742370E-09 ---- 1.324886E+02 ---- 1.517843E+03
    101FZ ---- ---- 2.865595E-09 -6.582429E+01 -3.544174E+03 ----
    101MX ---- ---- ---- -6.666428E+01 ---- ----
    101MY ---- ---- ---- ---- -6.817762E+02 ----
    101MZ ---- ---- ---- ---- ---- 7.142449E+01
    101Totals -4.945628E+03 2.742370E-09 2.865595E-09 -2.828524E-07 -8.690484E+04 4.413689E+04
    102FX -1.100767E-08 ---- ---- ---- -3.507359E+02 -1.850874E+03
    102FY ---- -4.945628E+03 ---- 8.443672E+04 ---- -1.122460E+06
    102FZ ---- ---- 9.063370E-09 1.566190E+03 2.009893E+02 ----
    102MX ---- ---- ---- 9.019265E+02 ---- ----
    102MY ---- ---- ---- ---- 1.497466E+02 ----
    102MZ ---- ---- ---- ---- ---- -4.664781E+02
    102Totals -1.100767E-08 -4.945628E+03 9.063370E-09 8.690484E+04 -1.688636E-06 -1.124777E+06
    103FX 7.262827E-09 ---- ---- ---- 2.094054E+03 -5.234430E+02
    103FY ---- -1.541262E-08 ---- -1.892529E+03 ---- 2.184894E+02
    103FZ ---- ---- -4.945628E+03 -4.220470E+04 1.122341E+06 ----
    103MX ---- ---- ---- -3.966004E+01 ---- ----
    103MY ---- ---- ---- ---- 3.419042E+02 ----
    103MZ ---- ---- ---- ---- ---- 3.049536E+02
    103Totals 7.262827E-09 -1.541262E-08 -4.945628E+03 -4.413689E+04 1.124777E+06 -3.300470E-06
    201FX -1.088749E+03 ---- ---- ---- 4.078055E+03 2.004496E+04
    201FY ---- -3.131226E+02 ---- -1.326242E+04 ---- -7.211902E+04
    201FZ ---- ---- -3.491436E+02 6.409149E+03 8.226705E+04 ----
    201MX ---- ---- ---- -4.171678E+02 ---- ----
    201MY ---- ---- ---- ---- -2.300795E+01 ----
    201MZ ---- ---- ---- ---- ---- 8.482928E+00
    201Totals -1.088749E+03 -3.131226E+02 -3.491436E+02 -7.270436E+03 8.632210E+04 -5.206559E+04
    301FX -2.232207E-08 ---- ---- ---- -2.687432E+03 8.931942E+02
    301FY ---- 6.544894E-09 ---- -1.398863E+03 ---- -6.166774E+02
    301FZ ---- ---- -3.288073E-08 1.240911E+03 2.910496E+03 ----
    301MX ---- ---- ---- 1.579518E+02 ---- ----
    301MY ---- ---- ---- ---- -2.230635E+02 ----
    301MZ ---- ---- ---- ---- ---- -2.765167E+02
    301Totals -2.232207E-08 6.544894E-09 -3.288073E-08 2.493896E-06 7.179337E-06 1.124599E-06
    302FX -8.688204E-09 ---- ---- ---- -1.038106E+03 3.450245E+02
    302FY ---- 2.617753E-09 ---- -5.403549E+02 ---- -2.382111E+02
    302FZ ---- ---- -1.268535E-08 4.793410E+02 1.124271E+03 ----
    302MX ---- ---- ---- 6.101385E+01 ---- ----
    302MY ---- ---- ---- ---- -8.616534E+01 ----
    302MZ ---- ---- ---- ---- ---- -1.068133E+02
    302Totals -8.688204E-09 2.617753E-09 -1.268535E-08 9.762168E-07 2.768029E-06 4.581230E-07
    303FX 5.885170E-09 ---- ---- ---- 7.082403E+02 -2.353905E+02
    303FY ---- -1.703086E-09 ---- 3.686533E+02 ---- 1.625179E+02
    303FZ ---- ---- 8.665140E-09 -3.270270E+02 -7.670260E+02 ----
    303MX ---- ---- ---- -4.162627E+01 ---- ----
    303MY ---- ---- ---- ---- 5.878570E+01 ----
    303MZ ---- ---- ---- ---- ---- 7.287264E+01
    303Totals 5.885170E-09 -1.703086E-09 8.665140E-09 -6.645159E-07 -1.893321E-06 -3.003608E-07




    Maximum SPC Forces Table SPC Forces Maximum Results Table Shows maximum responses across the entire Subcases and Grids for each component.

    This does not correspond to the results at a single Grid.
    SubCasesT1 T2T3 R1R2 R3
    101 2.0599611E+02 1.5828521E+02 2.7045061E+02 4.0566716E+01 1.2668762E+02 8.2690276E+01
    102 5.8008419E+02 4.3868103E+02 5.1155319E+02 1.2465340E+02 7.8517829E+01 2.2536432E+02
    103 5.8163057E+02 2.9185976E+02 5.2462146E+02 5.5160646E+01 1.3864793E+02 7.6670027E+01
    201 1.1660054E+02 3.8048455E+02 3.4910938E+02 6.7426530E+01 1.6245588E+02 7.0851049E+01
    301 5.7990244E+02 2.8005362E+02 2.7686831E+02 1.2804088E+02 5.2410002E+01 1.2465802E+02
    302 2.2400564E+02 1.0817956E+02 1.0694913E+02 4.9459833E+01 2.0245019E+01 4.8153098E+01
    303 1.5282628E+02 7.3804746E+01 7.2965295E+01 3.3743625E+01 1.3812022E+01 3.2852114E+01




    Maximum Displacement Results Table Maximum Displacement Results Table Shows maximum responses across the entire Subcases and Grids for each component.

    Results Table Show maximum responses across the entire Subcases and Grids for each component.

    This does not correspond to the results at a single Grid.
    SubCasesT1 T2T3 R1R2 R3
    1018.6830677E-024.2312851E-022.3937428E-022.7578110E-024.0168894E-021.4979430E-02
    1025.5076625E-021.8178256E-017.5079730E-025.6689990E-029.2039930E-022.3553668E-02
    1036.0952212E-026.3738029E-021.5487495E-011.6354608E-012.3029070E-017.1811542E-02
    2015.8419538E-026.8795264E-022.0090521E-011.0745040E-011.4570298E-015.4221818E-02
    3019.4649443E-022.1370542E-011.9622967E-012.2565352E-013.2151228E-018.8539556E-02
    3023.6561337E-028.2550469E-027.5799910E-028.7165801E-021.2419427E-013.4201200E-02
    3032.4943716E-025.6319479E-025.1713957E-025.9468257E-028.4730673E-022.3333529E-02




    Maximum Applied Loads Results Table Total Applied Loads Applied on the Structure

    Loads are Summarized by SUBCASEs.

    Results Table Show maximum responses across the entire Subcases and Grids for each component.

    This does not correspond to the results at a single Grid.
    SubCasesT1 T2T3 R1R2 R3
    1012.8999000E+028.3266727E-163.1710745E-150.0000000E+000.0000000E+000.0000000E+00
    1027.7715612E-162.8999000E+022.1316282E-140.0000000E+000.0000000E+000.0000000E+00
    1032.6906645E-152.8421709E-142.8999000E+020.0000000E+000.0000000E+000.0000000E+00
    2016.0900000E+027.0838563E+026.8878032E+020.0000000E+000.0000000E+000.0000000E+00
    3012.3910207E+043.9640013E+044.1543023E+040.0000000E+000.0000000E+000.0000000E+00
    3029.2360728E+031.5312207E+041.6047305E+040.0000000E+000.0000000E+000.0000000E+00
    3036.3012459E+031.0446646E+041.0948161E+040.0000000E+000.0000000E+000.0000000E+00




    MPC Forces Resultant Table Output Nastran Calls MPC Forces Resultants The SUM of Forces
    generated generated within MPCs or Rigid Elements

    Loads are Summarized by SUBCASEs.
    SubCasesType T1T2 T3R1 R2R3
    101FX -6.708190E-12 ---- ---- ---- -8.085246E+02 4.578296E+02
    101FY ---- 2.297051E-13 ---- -6.280637E+01 ---- -5.481104E+02
    101FZ ---- ---- -3.659295E-13 2.102564E+01 8.985715E+02 ----
    101MX ---- ---- ---- 4.178074E+01 ---- ----
    101MY ---- ---- ---- ---- -9.004694E+01 ----
    101MZ ---- ---- ---- ---- ---- 9.028084E+01
    101Totals -6.708190E-12 2.297051E-13 -3.659295E-13 4.558487E-11 -1.011813E-11 -3.000196E-10
    102FX -4.560796E-13 ---- ---- ---- -2.132165E+02 8.581099E+02
    102FY ---- 3.570477E-13 ---- 4.555446E+02 ---- -2.923217E+02
    102FZ ---- ---- -2.486900E-13 -6.341186E+02 -9.002009E+01 ----
    102MX ---- ---- ---- 1.785739E+02 ---- ----
    102MY ---- ---- ---- ---- 3.032366E+02 ----
    102MZ ---- ---- ---- ---- ---- -5.657882E+02
    102Totals -4.560796E-13 3.570477E-13 -2.486900E-13 4.445155E-11 -5.640004E-10 4.756657E-10
    103FX -8.346657E-13 ---- ---- ---- -7.701569E+02 -1.000958E+02
    103FY ---- 1.139755E-12 ---- 1.049229E+03 ---- -2.685085E+02
    103FZ ---- ---- -4.809486E-12 -8.950650E+02 2.078660E+02 ----
    103MX ---- ---- ---- -1.541642E+02 ---- ----
    103MY ---- ---- ---- ---- 5.622909E+02 ----
    103MZ ---- ---- ---- ---- ---- 3.686043E+02
    103Totals -8.346657E-13 1.139755E-12 -4.809486E-12 8.674306E-11 1.735145E-09 -8.765255E-11
    201FX -6.895595E-13 ---- ---- ---- -1.982077E+02 -8.411138E+01
    201FY ---- 2.875478E-13 ---- -1.306354E+02 ---- 1.152789E+02
    201FZ ---- ---- 2.660094E-13 -4.119000E+01 -1.637489E+02 ----
    201MX ---- ---- ---- 1.718254E+02 ---- ----
    201MY ---- ---- ---- ---- 3.619566E+02 ----
    201MZ ---- ---- ---- ---- ---- -3.116749E+01
    201Totals -6.895595E-13 2.875478E-13 2.660094E-13 -1.121947E-11 -8.131451E-11 -6.511414E-11
    301FX -1.595057E-12 ---- ---- ---- 3.516465E+02 -4.139861E+02
    301FY ---- 7.815970E-14 ---- 2.001376E+02 ---- 3.090299E+02
    301FZ ---- ---- 5.222489E-13 3.549257E+02 1.484213E+02 ----
    301MX ---- ---- ---- -5.550633E+02 ---- ----
    301MY ---- ---- ---- ---- -5.000678E+02 ----
    301MZ ---- ---- ---- ---- ---- 1.049562E+02
    301Totals -1.595057E-12 7.815970E-14 5.222489E-13 -7.298695E-11 4.785079E-10 1.380158E-10
    302FX 4.130030E-13 ---- ---- ---- 1.358346E+02 -1.599152E+02
    302FY ---- -1.705303E-13 ---- 7.730949E+01 ---- 1.193726E+02
    302FZ ---- ---- 4.574119E-13 1.371013E+02 5.733242E+01 ----
    302MX ---- ---- ---- -2.144107E+02 ---- ----
    302MY ---- ---- ---- ---- -1.931670E+02 ----
    302MZ ---- ---- ---- ---- ---- 4.054266E+01
    302Totals 4.130030E-13 -1.705303E-13 4.574119E-13 -1.568878E-11 -4.229150E-11 -9.251266E-12
    303FX -4.635181E-14 ---- ---- ---- -9.267219E+01 1.091010E+02
    303FY ---- -3.275158E-13 ---- -5.274386E+01 ---- -8.144109E+01
    303FZ ---- ---- -9.414691E-14 -9.353637E+01 -3.911464E+01 ----
    303MX ---- ---- ---- 1.462802E+02 ---- ----
    303MY ---- ---- ---- ---- 1.317868E+02 ----
    303MZ ---- ---- ---- ---- ---- -2.765995E+01
    303Totals -4.635181E-14 -3.275158E-13 -9.414691E-14 -1.011813E-11 2.766853E-11 3.709033E-11



    Job Performance Analysis Section Job Performance Analysis Description

    Identifies if any parameter should be changed.

    Checks BUFFSIZE Used against Installation Doc Requirements

    Checks Mem used against Mem available at runtime

    Checks SMem used against Hiwater Mem and Available

    Checks Numbers of CPU used for SMP if machine has more CPUs avaialble.

    BUFFSIZE Check
    BUFFSIZE Value Used65537
    Minimum BUFFSIZE Value65540
    Memory Check
    Total Hardware Memory (GB)63.675
    Memory Available at Run Time (GB)56.091
    Memory Allocated (mem) for Nastran (GB)0.0
    Memory Used - HIWATER (GB)24.836
    Min Recommended Memory (mem) Value (GB) 53.3
    Scratch Memory Check
    Scratch Memory (smem) Allocated (GB) 0.0
    Total Scratch I/O Used (GB) 50.4
    Min Recommended Scratch Memory (smem) Value (GB)25.786
    Shared Memory Parallelization (SMP) Check
    Processors Availalble8
    Processors Used6
    If the above results are obtained after initial tuning was performed,
    job performance might still be improved but more RAM is required
    Estimated Free RAM at runtime requirement to improve simulation time is : 64.1 GB
    Recommended Nastran Arguments (Ref Doc - App C - Keywords)
    mode=i8 buffsize=65540 mem=53.29gb smem=25.79gb par=4






    Nastran f04 File Echo Nastran f04 File Description
    MachineModel Operating SystemSolver Version Build DateRun Date
    Intel P5-4/5417 (A6119137) Windows 7 Enterprise 6 i8 V2017.1.2 AUG 25, 2017 MAY 28, 2019
    Start TimeStop TimeElapsed I/O (MB)Del (MB) CPU SecDel CPU
    9:27:259:40:5713:3257135.00.0995.90.0
    Memory Spill (SWAP) Check
    If Required Memory is Less than Memory Required to Avoid Spill, jobtime may be excessively long.
    Consider increasing Nastran memory.
    MINIMUM MEMORY REQUIREMENT (MB)MEMORY AVAILABLE (MB) MEMORY REQRD TO AVOID SPILL (MB)MEMORY USED BY BEND (MB)
    520.4086303718088.06610107 918.8079833980
    Parallel Processing Summary
    CPU 1CPU 2 CPU 3CPU 4 CPU 5CPU 6 CPU 7CPU 8
    52.7151.6551.3650.7950.2649.73
    MASTER Directory Loaded in Memory
    TypeSize (MB)
    USER OPENCORE (HICORE)0.0617065429688
    EXECUTIVE SYSTEM WORK AREA6.103515625e-005
    MASTER(RAM)7.62939453125e-006
    SCRATCH(MEM) AREA0.000381469726563
    TOTAL MSC NASTRAN MEMORY LIMIT0.248725891113
    Memory HI-Water
    HIWATER MEMORY USED (GB)HIWATER DISK USED (GB)
    24.836178600837.381
    DATABASE USAGE STATISTICS
    LOGICAL DBSETS
    DBSETALLOCATED (BLOCKS) BLOCKSIZE (WORDS)USED (BLOCKS) USED (%)
    MASTER209715265536600.00
    DBALL20971526553640.00
    OBJSCR1677721681924540.00
    SCRATCH419440465536970.00
    DBSET FILES
    FILEALLOCATED (BLOCKS)ALLOCATED (GB)HIWATER (BLOCKS)HIWATER (GB)I/O TRANSFERRED (GB)
    MASTER20971521024.005000.2440.252
    DBALL20971521024.0040.0020.004
    OBJSCR167772161024.004540.0280.032
    MEMFILE0.00.00.00.00.0
    SCRATCH20971521024.008238040.22546.453
    SCR30020971521024.002079310.1538.639


    Nastran log File Echo Nastran log File Description
    Logfile Header Logfile Header
    SMEM100
    BPOOL24451MB
    BUFFSIZE65537
    AUTH'1700@msc1.lic.boeing.com;1700@msc2.lic.boeing.com;1700@msc3.lic.boeing.com'
    PARALLEL6
    MEM0.0 MB
    NPROC8
    DBS'c:/scratch/abis8b_chk.T16300_19'
    NEWDEL'c:/appl/msc/nastran/20171/msc20171/win64i8/sss'
    NLINES999999
    SCR1tb
    Shell Section Shell Section
    FPEyes
    Current DirD:\__CCTS_OFT\__Parts_In_Work_Toby\_Part_Folders\4.194000_LRS_ABIS\__ASSY_194000-0501\analysis\fea\runs\2.chk
    Executablec:\appl\msc\nastran\20171\msc20171\win64i8\analysis.exe
    MSC_MSGstderr
    MSC_ISHELLPATHC:\appl\MSC\Nastran\20171\msc20171\actran\win64\Actran_17.1.b.97631\bin;C:\appl\MSC\Nastran\20171\msc20171\nast;c:\appl\sat.software\nastran\alters\2017
    ArchKywd:
    Cmd Line C:\appl\MSC\Nastran\20171\msc20171\win64i8\nastran.exe D:\__CCTS_OFT\__Parts_In_Work_Toby\_Part_Folders\4.194000_LRS_ABIS\__ASSY_194000-0501\analysis\fea\runs\2.chk\abis8b_chk.bdf
    Time Cmdc:\appl\msc\nastran\20171\msc20171\win64i8\msctime
    SCA_RESOURCE_DIRc:\appl\msc\nastran\20171\msc20171\res
    SCA_SERVICE_CATALOGc:\appl\msc\nastran\20171\msc20171\res\SCAServiceCatalog.xml
    Current Ressources Limits Current Ressources Limits
    Virtual Memory (MB)8388607
    Paging file size available (MB)122674
    Physical Memory Available (MB)57437
    Physical Memory (MB)65203
    Paging file size (MB)130405
    Virtual Memory Available (MB)8388552
    System Configuration System Configuration
    Config number15
    Executablestandard
    Raw model ID15
    Clock freq.5567 MHz
    Number of CPUs8
    HostnameA6119137.se.nos.boeing.com
    Bytes per word8
    PlatformIntel Windows 7 Enterprise 6.1 7601 (Windows Compute Cluster)
    Physical memory (MB)65203 MB
    Virtual memory (MB)130405 MB
    Numeric format64-bit little-endian IEEE.
    Architecturewin64i8
    Remote shell cmd"c:/appl/msc/nastran/20171/msc20171/win64i8/mscrmtcmd.exe" (Windows non-CCS nodes, UNIX)
    ModelP5-4/5567
    Disk block size512 bytes (64 words)
    Authorization Authorization
    UserT 1555.439 seconds ( 0:25:55.439)
    Date End09:40:58
    LAPI VersionLAPI 10.1.8-3298 (FLEXlm 11.9.0.0)
    CEID563FFF2D-3654D4D5
    Acquired[' Acquired 250 licenses for Group CAMPUS (MSC Nastran) from license server on host msc1.lic.boeing.com', ' Acquired 120 licenses for Group CAMPUS (MSC Nastran Parallel) from license server on host msc1.lic.boeing.com']
    SysT 202.083 seconds ( 0:03:22.083)
    DOF10930152
    DisplayA6119137
    License files1700@msc1.lic.boeing.com
    User9 seconds ( 0:25:55.439)
    MSC Id025041000001 (ethernet) (Intel)
    Date StartTue May 28 09:27:22 2019
    RealT 821.201 seconds ( 0:13:41.201)
    Host NameA6119137 (user NorrisT1, display A6119137)


    MSC Software Disclaimer Note Disclaimer
    Copyright (c) 2011 MSC.Software Corporation

    WARNING. This computer program is the confidential information and trade secret of MSC.Software Corporation. It is not to be disclosed or distributed to any third party, without the express written consent of MSC.Software legal department. Use or disclosure within MSC.Software is strictly limited to authorized members of the MSC.Software technical team on a need-to-know basis.