title: Презентация на тему: MSC.Nastran 102 2001 - 07

text:
Slide Title
Body Text
Second Level
Third Level
Fourth Level
Fifth Level
Body Text
Second Level
Third Level
Fourth Level
Fifth Level
MSC Corporate Overview Speaker Notes
Q
.
$ SPECIFY STRUCTURAL DIAMPING
$ 3 PERCENT AT 250 HZ. = 1571 RAD/SEC
$
PARAM, G, 0.06
PARAM, W3, 1571.
$
$ APPLY UNTI PRESSURE LOAD TO PLATE
$
LSEQ, 100, 300, 400
$
PLOAD2, 400, 1., 1, THRU, 40
$
$ VARY PRESSURE LOAD (250HZ)
$
TLOAD2, 200, 300, , 0, 0., 8.E-3, 250., -90.
$
$ APPLY POINT LOAD OUT OF PAHSE WITH PRESSURE LOAD
$
TLOAD2, 500, 600, , 0, 0., 8.E-3, 250., 90.
$
DAREA, 600, 11, 3, 1.
$
$ COMBINE LOADS
$
DLOAD, 700, 1., 1., 200, 50., 500
$
$ SPECIFY INTERGRATION TIME STEPS
$
TSTEP, 100, 100, 4.0E-4, 1
$
ENDDATA
0                                                                                SUBCASE 1ML
      POINT-ID =        11
                                             D I S P L A C E M E N T   V E C T O R

       TIME       TYPE          T1             T2             T3             R1             R2             R3
    .0              G       .0             .0             .0             .0             .0             .0
   4.000000E-04     G       .0             .0           -2.173625E-02   1.104167E-02   1.050818E-02    .0
   8.000000E-04     G       .0             .0           -7.204904E-02   2.847414E-02   2.852519E-02    .0
   1.200000E-03     G       .0             .0           -1.433462E-01   4.082027E-02   4.915178E-02    .0
                                                  .
                                                  .
                                                  .
   3.999996E-02     G       .0             .0            1.535974E-02   5.380195E-06  -4.281028E-03    .0
                                                  .
                                                  .
                                                  .
                                                  .
                                                  .
                                                  .
      POINT-ID =        33
                                             D I S P L A C E M E N T   V E C T O R

       TIME       TYPE          T1             T2             T3             R1             R2             R3
    .0              G       .0             .0             .0             .0             .0             .0
   4.000000E-04     G       .0             .0           -1.122398E-02   9.220219E-03   6.138594E-03    .0
   8.000000E-04     G       .0             .0           -4.424753E-02   2.576699E-02   2.014980E-02    .0
   1.200000E-03     G       .0             .0           -1.030773E-01   3.819037E-02   3.922388E-02    .0
   1.600000E-03     G       .0             .0           -1.756290E-01   2.927664E-02   5.577566E-02    .0
   2.000000E-03     G       .0             .0           -2.443317E-01   1.765907E-03   6.761354E-02    .0
                                                  .
                                                  .
                                                  .
   3.839996E-02     G       .0             .0           -4.946285E-02  -3.005945E-05   1.376158E-02    .0
   3.879996E-02     G       .0             .0           -3.729695E-02   1.898671E-05   1.037927E-02    .0
   3.919996E-02     G       .0             .0           -2.121863E-02   3.488552E-05   5.907703E-03    .0
   3.959996E-02     G       .0             .0           -3.002587E-03  -2.227573E-07   8.361285E-04    .0
   3.999996E-02     G       .0             .0            1.535096E-02  -3.032754E-05  -4.274250E-03    .0
ID SEMINAR, PROB4
SOL 112
TIME 30
CEND
TITLE = TRANSIENT RESPONSE WITH TIME DEPENDENT PRESSURE AND POINT LOADS
SUBTITLE = USE THE MODAL METHOD
ECHO = UNSORTED
SPC = 1
SET 111 = 11, 33, 55
DISPLACEMENT(SORT2) = 111
SDAMPING = 100
SUBCASE 1
METHOD = 100
DLOAD = 700
LOADSET = 100
TSTEP = 100
$
OUTPUT (XYPLOT)
XGRID=YES
YGRID=YES
XTITLE= TIME (SEC)
YTITLE= DISPLACEMENT RESPONSE AT LOADED CORNER
XYPLOT DISP RESPONSE / 11 (T3)
YTITLE= DISPLACEMENT RESPONSE AT TIP CENTER
XYPLOT DISP RESPONSE / 33 (T3)
YTITLE= DISPLACEMENT RESPONSE AT OPPOSITE CORNER
XYPLOT DISP RESPONSE / 55 (T3)
$
PLOAD2, 400, 1., 1, THRU, 40
$
$ VARY PRESSURE LOAD (250 HZ)
$
TLOAD2, 200, 300, , 0, 0., 8.E-3, 250., -90.
$
$ APPLY POINT LOAD (250 HZ)
$
TLOAD2, 500, 600,610, 0, 0.0, 8.E-3, 250., -90.
$
DAREA, 600, 11, 3, 1.
DELAY, 610, 11, 3, 0.004
$
$ COMBINE LOADS
$
DLOAD, 700, 1., 1., 200, 25., 500
$
$ SPECIFY INTERGRATION TIME STEPS
$
TSTEP, 100, 100, 4.0E-4, 1
$
ENDDATA
 *** SYSTEM INFORMATION MESSAGE 6916 (DFMSYN)     DECOMP ORDERING METHOD CHOSEN: DEFAULT, ORDERING METHOD USED: MMD *** USER INFORMATION MESSAGE 5010 (LNCILD)     STURM SEQUENCE DATA FOR EIGENVALUE EXTRACTION.     TRIAL EIGENVALUE =  9.433958D+07, CYCLES =  1.545849D+03 NUMBER OF EIGENVALUES BELOW THIS VALUE =     3 *** USER INFORMATION MESSAGE 5010 (LNCILD)     STURM SEQUENCE DATA FOR EIGENVALUE EXTRACTION.     TRIAL EIGENVALUE =  2.281618D+08, CYCLES =  2.404039D+03 NUMBER OF EIGENVALUES BELOW THIS VALUE =     5
 TABLE OF SHIFTS:  (LNNRIGL) SHIFT #        SHIFT VALUE         FREQUENCY, CYCLES     # EIGENVALUES BELOW    # NEW EIGENVALUES FOUND     1.        9.4339576E+07          1.5458490E+03                 3                        6     2.        2.2816176E+08          2.4040393E+03                 5                        0
1    TRANSIENT RESPONSE WITH TIME DEPENDENT PRESSURE AND POINT LOADS          APRIL   8, 1998  MSC.Nastran  4/ 6/98   PAGE    10      USE THE MODAL METHOD                                                                                0                                                                                0
                          E I G E N V A L U E  A N A L Y S I S   S U M M A R Y   (READ MODULE)
                                     BLOCK SIZE USED ......................    7
                                     NUMBER OF DECOMPOSITIONS .............    2
                                     NUMBER OF ROOTS FOUND ................    5
                                     NUMBER OF SOLVES REQUIRED ............    5
1    TRANSIENT RESPONSE WITH TIME DEPENDENT PRESSURE AND POINT LOADS          APRIL   8, 1998  MSC.Nastran  4/ 6/98   PAGE    11      USE THE MODAL METHOD                                                                                0                                                                                R E A L   E I G E N V A L U E S   MODE    EXTRACTION      EIGENVALUE            RADIANS             CYCLES            GENERALIZED         GENERALIZED    NO.       ORDER                                                                       MASS              STIFFNESS        1         1        7.056994E+05        8.400591E+02        1.336996E+02        1.000000E+00        7.056994E+05        2         2        1.878432E+07        4.334088E+03        6.897916E+02        1.000000E+00        1.878432E+07        3         3        2.811467E+07        5.302327E+03        8.438915E+02        1.000000E+00        2.811467E+07        4         4        1.931709E+08        1.389859E+04        2.212030E+03        1.000000E+00        1.931709E+08        5         5        2.234434E+08        1.494802E+04        2.379052E+03        1.000000E+00        2.234434E+08
 POINT-ID =        11                                             D I S P L A C E M E N T   V E C T O R        TIME       TYPE          T1             T2             T3             R1             R2             R3    .0              G       .0             .0             .0             .0             .0             .0   4.000000E-04     G     -3.625017E-15  -1.905611E-15   1.887243E-04  -6.386437E-06   5.199215E-05    .0   8.000000E-04     G     -2.914862E-14  -1.814328E-14   1.956669E-03  -2.026748E-05  -1.663007E-04    .0   1.200000E-03     G     -8.908526E-14  -5.652777E-14   6.887082E-03  -4.435436E-06  -1.612398E-03    .0                                                       .                                                        .                                                        .    3.919996E-02     G      2.885643E-14   1.851072E-14  -2.561149E-03   1.920348E-04   6.726292E-04    .0   3.959996E-02     G     -7.876552E-14  -5.047815E-14   6.422142E-03  -1.141607E-05  -1.799371E-03    .0   3.999996E-02     G     -1.754870E-13  -1.124985E-13   1.438590E-02  -1.381519E-04  -3.964385E-03    .0                                                       .                                                        .                                                        .                                                        .                                                        .                                                        .       POINT-ID =        33                                             D I S P L A C E M E N T   V E C T O R        TIME       TYPE          T1             T2             T3             R1             R2             R3    .0              G       .0             .0             .0             .0             .0             .0   4.000000E-04     G     -2.425735E-15  -3.601817E-15   1.849105E-04   1.747102E-13   5.123477E-05    .0   8.000000E-04     G     -1.846279E-14  -3.116278E-14   1.944596E-03   1.289274E-12  -1.686260E-04    .0                                                       .                                                        .                                                        .    3.839996E-02     G      1.418105E-13   2.481614E-13  -1.858122E-02  -2.107761E-04   5.154297E-03    .0   3.879996E-02     G      8.371286E-14   1.466735E-13  -1.103474E-02  -3.810626E-05   3.082996E-03    .0   3.919996E-02     G      1.725147E-14   3.062306E-14  -2.364378E-03   2.016205E-04   6.607183E-04    .0   3.959996E-02     G     -4.836024E-14  -8.483060E-14   6.404299E-03  -2.743191E-05  -1.795630E-03    .0   3.999996E-02     G     -1.075141E-13  -1.887765E-13   1.423312E-02  -1.733039E-04  -3.950206E-03    .0                                                       .                                                        .                                                        .
0                                                                                SUBCASE 1                              0                             X Y - O U T P U T  S U M M A R Y  ( R E S P O N S E )0 SUBCASE  CURVE FRAME                    XMIN-FRAME/    XMAX-FRAME/    YMIN-FRAME/      X FOR        YMAX-FRAME/      X FOR     ID     TYPE   NO.    CURVE ID.          ALL DATA       ALL DATA       ALL DATA       YMIN           ALL DATA       YMAX0       1  DISP      1       11(  5)      0.000000E+00   3.999996E-02  -1.690216E-01   9.199998E-03   1.497643E-01   6.399998E-03                                          0.000000E+00   3.999996E-02  -1.690216E-01   9.199998E-03   1.497643E-01   6.399998E-030       1  DISP      2       33(  5)      0.000000E+00   3.999996E-02  -1.849363E-01   9.199998E-03   1.606161E-01   6.799998E-03                                          0.000000E+00   3.999996E-02  -1.849363E-01   9.199998E-03   1.606161E-01   6.799998E-030       1  DISP      3       55(  5)      0.000000E+00   3.999996E-02  -2.005836E-01   9.199998E-03   1.734470E-01   6.799998E-03                                          0.000000E+00   3.999996E-02  -2.005836E-01   9.199998E-03   1.734470E-01   6.799998E-03

Q
.
$ SPECIFY STRUCTURAL DIAMPING
$ 3 PERCENT AT 250 HZ. = 1571 RAD/SEC
$
PARAM, G, 0.06
PARAM, W3, 1571.
$
$ APPLY UNTI PRESSURE LOAD TO PLATE
$
LSEQ, 100, 300, 400
$
PLOAD2, 400, 1., 1, THRU, 40
$
$ VARY PRESSURE LOAD (250HZ)
$
TLOAD2, 200, 300, , 0, 0., 8.E-3, 250., -90.
$
$ APPLY POINT LOAD OUT OF PAHSE WITH PRESSURE LOAD
$
TLOAD2, 500, 600, , 0, 0., 8.E-3, 250., 90.
$
DAREA, 600, 11, 3, 1.
$
$ COMBINE LOADS
$
DLOAD, 700, 1., 1., 200, 50., 500
$
$ SPECIFY INTERGRATION TIME STEPS
$
TSTEP, 100, 100, 4.0E-4, 1
$
ENDDATA
0                                                                                SUBCASE 1ML
      POINT-ID =        11
                                             D I S P L A C E M E N T   V E C T O R

       TIME       TYPE          T1             T2             T3             R1             R2             R3
    .0              G       .0             .0             .0             .0             .0             .0
   4.000000E-04     G       .0             .0           -2.173625E-02   1.104167E-02   1.050818E-02    .0
   8.000000E-04     G       .0             .0           -7.204904E-02   2.847414E-02   2.852519E-02    .0
   1.200000E-03     G       .0             .0           -1.433462E-01   4.082027E-02   4.915178E-02    .0
                                                  .
                                                  .
                                                  .
   3.999996E-02     G       .0             .0            1.535974E-02   5.380195E-06  -4.281028E-03    .0
                                                  .
                                                  .
                                                  .
                                                  .
                                                  .
                                                  .
      POINT-ID =        33
                                             D I S P L A C E M E N T   V E C T O R

       TIME       TYPE          T1             T2             T3             R1             R2             R3
    .0              G       .0             .0             .0             .0             .0             .0
   4.000000E-04     G       .0             .0           -1.122398E-02   9.220219E-03   6.138594E-03    .0
   8.000000E-04     G       .0             .0           -4.424753E-02   2.576699E-02   2.014980E-02    .0
   1.200000E-03     G       .0             .0           -1.030773E-01   3.819037E-02   3.922388E-02    .0
   1.600000E-03     G       .0             .0           -1.756290E-01   2.927664E-02   5.577566E-02    .0
   2.000000E-03     G       .0             .0           -2.443317E-01   1.765907E-03   6.761354E-02    .0
                                                  .
                                                  .
                                                  .
   3.839996E-02     G       .0             .0           -4.946285E-02  -3.005945E-05   1.376158E-02    .0
   3.879996E-02     G       .0             .0           -3.729695E-02   1.898671E-05   1.037927E-02    .0
   3.919996E-02     G       .0             .0           -2.121863E-02   3.488552E-05   5.907703E-03    .0
   3.959996E-02     G       .0             .0           -3.002587E-03  -2.227573E-07   8.361285E-04    .0
   3.999996E-02     G       .0             .0            1.535096E-02  -3.032754E-05  -4.274250E-03    .0
ID SEMINAR, PROB4
SOL 112
TIME 30
CEND
TITLE = TRANSIENT RESPONSE WITH TIME DEPENDENT PRESSURE AND POINT LOADS
SUBTITLE = USE THE MODAL METHOD
ECHO = UNSORTED
SPC = 1
SET 111 = 11, 33, 55
DISPLACEMENT(SORT2) = 111
SDAMPING = 100
SUBCASE 1
METHOD = 100
DLOAD = 700
LOADSET = 100
TSTEP = 100
$
OUTPUT (XYPLOT)
XGRID=YES
YGRID=YES
XTITLE= TIME (SEC)
YTITLE= DISPLACEMENT RESPONSE AT LOADED CORNER
XYPLOT DISP RESPONSE / 11 (T3)
YTITLE= DISPLACEMENT RESPONSE AT TIP CENTER
XYPLOT DISP RESPONSE / 33 (T3)
YTITLE= DISPLACEMENT RESPONSE AT OPPOSITE CORNER
XYPLOT DISP RESPONSE / 55 (T3)
$
PLOAD2, 400, 1., 1, THRU, 40
$
$ VARY PRESSURE LOAD (250 HZ)
$
TLOAD2, 200, 300, , 0, 0., 8.E-3, 250., -90.
$
$ APPLY POINT LOAD (250 HZ)
$
TLOAD2, 500, 600,610, 0, 0.0, 8.E-3, 250., -90.
$
DAREA, 600, 11, 3, 1.
DELAY, 610, 11, 3, 0.004
$
$ COMBINE LOADS
$
DLOAD, 700, 1., 1., 200, 25., 500
$
$ SPECIFY INTERGRATION TIME STEPS
$
TSTEP, 100, 100, 4.0E-4, 1
$
ENDDATA
 *** SYSTEM INFORMATION MESSAGE 6916 (DFMSYN)     DECOMP ORDERING METHOD CHOSEN: DEFAULT, ORDERING METHOD USED: MMD *** USER INFORMATION MESSAGE 5010 (LNCILD)     STURM SEQUENCE DATA FOR EIGENVALUE EXTRACTION.     TRIAL EIGENVALUE =  9.433958D+07, CYCLES =  1.545849D+03 NUMBER OF EIGENVALUES BELOW THIS VALUE =     3 *** USER INFORMATION MESSAGE 5010 (LNCILD)     STURM SEQUENCE DATA FOR EIGENVALUE EXTRACTION.     TRIAL EIGENVALUE =  2.281618D+08, CYCLES =  2.404039D+03 NUMBER OF EIGENVALUES BELOW THIS VALUE =     5
 TABLE OF SHIFTS:  (LNNRIGL) SHIFT #        SHIFT VALUE         FREQUENCY, CYCLES     # EIGENVALUES BELOW    # NEW EIGENVALUES FOUND     1.        9.4339576E+07          1.5458490E+03                 3                        6     2.        2.2816176E+08          2.4040393E+03                 5                        0
1    TRANSIENT RESPONSE WITH TIME DEPENDENT PRESSURE AND POINT LOADS          APRIL   8, 1998  MSC.Nastran  4/ 6/98   PAGE    10      USE THE MODAL METHOD                                                                                0                                                                                0
                          E I G E N V A L U E  A N A L Y S I S   S U M M A R Y   (READ MODULE)
                                     BLOCK SIZE USED ......................    7
                                     NUMBER OF DECOMPOSITIONS .............    2
                                     NUMBER OF ROOTS FOUND ................    5
                                     NUMBER OF SOLVES REQUIRED ............    5
1    TRANSIENT RESPONSE WITH TIME DEPENDENT PRESSURE AND POINT LOADS          APRIL   8, 1998  MSC.Nastran  4/ 6/98   PAGE    11      USE THE MODAL METHOD                                                                                0                                                                                R E A L   E I G E N V A L U E S   MODE    EXTRACTION      EIGENVALUE            RADIANS             CYCLES            GENERALIZED         GENERALIZED    NO.       ORDER                                                                       MASS              STIFFNESS        1         1        7.056994E+05        8.400591E+02        1.336996E+02        1.000000E+00        7.056994E+05        2         2        1.878432E+07        4.334088E+03        6.897916E+02        1.000000E+00        1.878432E+07        3         3        2.811467E+07        5.302327E+03        8.438915E+02        1.000000E+00        2.811467E+07        4         4        1.931709E+08        1.389859E+04        2.212030E+03        1.000000E+00        1.931709E+08        5         5        2.234434E+08        1.494802E+04        2.379052E+03        1.000000E+00        2.234434E+08
 POINT-ID =        11                                             D I S P L A C E M E N T   V E C T O R        TIME       TYPE          T1             T2             T3             R1             R2             R3    .0              G       .0             .0             .0             .0             .0             .0   4.000000E-04     G     -3.625017E-15  -1.905611E-15   1.887243E-04  -6.386437E-06   5.199215E-05    .0   8.000000E-04     G     -2.914862E-14  -1.814328E-14   1.956669E-03  -2.026748E-05  -1.663007E-04    .0   1.200000E-03     G     -8.908526E-14  -5.652777E-14   6.887082E-03  -4.435436E-06  -1.612398E-03    .0                                                       .                                                        .                                                        .    3.919996E-02     G      2.885643E-14   1.851072E-14  -2.561149E-03   1.920348E-04   6.726292E-04    .0   3.959996E-02     G     -7.876552E-14  -5.047815E-14   6.422142E-03  -1.141607E-05  -1.799371E-03    .0   3.999996E-02     G     -1.754870E-13  -1.124985E-13   1.438590E-02  -1.381519E-04  -3.964385E-03    .0                                                       .                                                        .                                                        .                                                        .                                                        .                                                        .       POINT-ID =        33                                             D I S P L A C E M E N T   V E C T O R        TIME       TYPE          T1             T2             T3             R1             R2             R3    .0              G       .0             .0             .0             .0             .0             .0   4.000000E-04     G     -2.425735E-15  -3.601817E-15   1.849105E-04   1.747102E-13   5.123477E-05    .0   8.000000E-04     G     -1.846279E-14  -3.116278E-14   1.944596E-03   1.289274E-12  -1.686260E-04    .0                                                       .                                                        .                                                        .    3.839996E-02     G      1.418105E-13   2.481614E-13  -1.858122E-02  -2.107761E-04   5.154297E-03    .0   3.879996E-02     G      8.371286E-14   1.466735E-13  -1.103474E-02  -3.810626E-05   3.082996E-03    .0   3.919996E-02     G      1.725147E-14   3.062306E-14  -2.364378E-03   2.016205E-04   6.607183E-04    .0   3.959996E-02     G     -4.836024E-14  -8.483060E-14   6.404299E-03  -2.743191E-05  -1.795630E-03    .0   3.999996E-02     G     -1.075141E-13  -1.887765E-13   1.423312E-02  -1.733039E-04  -3.950206E-03    .0                                                       .                                                        .                                                        .
0                                                                                SUBCASE 1                              0                             X Y - O U T P U T  S U M M A R Y  ( R E S P O N S E )0 SUBCASE  CURVE FRAME                    XMIN-FRAME/    XMAX-FRAME/    YMIN-FRAME/      X FOR        YMAX-FRAME/      X FOR     ID     TYPE   NO.    CURVE ID.          ALL DATA       ALL DATA       ALL DATA       YMIN           ALL DATA       YMAX0       1  DISP      1       11(  5)      0.000000E+00   3.999996E-02  -1.690216E-01   9.199998E-03   1.497643E-01   6.399998E-03                                          0.000000E+00   3.999996E-02  -1.690216E-01   9.199998E-03   1.497643E-01   6.399998E-030       1  DISP      2       33(  5)      0.000000E+00   3.999996E-02  -1.849363E-01   9.199998E-03   1.606161E-01   6.799998E-03                                          0.000000E+00   3.999996E-02  -1.849363E-01   9.199998E-03   1.606161E-01   6.799998E-030       1  DISP      3       55(  5)      0.000000E+00   3.999996E-02  -2.005836E-01   9.199998E-03   1.734470E-01   6.799998E-03                                          0.000000E+00   3.999996E-02  -2.005836E-01   9.199998E-03   1.734470E-01   6.799998E-03

Body Text
Second Level
Third Level
Fourth Level
Fifth Level
MSC Corporate Overview Speaker Notes


title: Презентация на тему: MSC.Patran PAT 318 2002 - 00

text:
       PAT318, Section  0, March 2002
Click to edit Master text styles
Second level
Third level
Fourth level
Fifth level
MSC.Software Corporation
2 MacArthur Place
Santa Ana, CA 92707, USA
Tel:  (714) 540-8900
Fax: (714) 784-4056
Web: http://www.mscsoftware.com
United States
MSC.Patran Support
Tel: 1-800-732-7284
Fax: (714) 979-2990
Tokyo, Japan
Tel: 81-3-3505-0266
Fax: 81-3-3505-0914
Munich, Germany
Tel: (+49)-89-43 19 87 0
Fax: (+49)-89-43 61 716
       P/N P3*V2002*Z*Z*Z*SM-PAT318-NT1
PAT318 Course Director:
Abdur.Razzaque@MSCSoftware.com


Презентация на тему: MS-DOS


Презентация на тему: MS Excel


title: Презентация на тему: MSC.Nastran 102 2001 - 08

text:
Slide Title
Body Text
Second Level
Third Level
Fourth Level
Fifth Level
Body Text
Second Level
Third Level
Fourth Level
Fifth Level
MSC Corporate Overview Speaker Notes
.
$
$	cbush1.dat
$
TIME 10
SOL 108
CEND
TITLE = VERIFICATION PROBLEM, FREQ. DEP. IMPEDANCE              BUSHVER
SUBTITLE = SINGLE DOF, CRITICAL DAMPING, 3 EXCITATION FREQUENCIES
ECHO = BOTH
SPC = 1002
DLOAD = 1
DISP = ALL
FREQ = 10
ELFO = ALL
BEGIN BULK
$ CONVENTIONAL INPUT FOR MOUNT
GRDSET,	,	,	,	,	,	,	23456 $ PS
$ TIE DOWN EVERYTHING BUT THE 1 DOF
GRID,	11,	,	0.,	0.,	0.0 	$ GROUND
=,	12,	=,	=,	=,	,	$ ISOLATED DOF
SPC1,	1002	123456	11	$ GROUND
CONM2,	12,	12,	,	1.0	$ THE ISOLATED MASS
$
$	EID	PID	GA	GB	GO/X1	X2	X3	CID
$
CBUSH	1000	2000	11	12				0
$
PBUSH	2000	K	1.0
		B	0.0
$
PBUSHT	2000	K	2001
		B	2002
$
TABLED1, 2001 $ STIFFNESS TABLE
,	0.9	0.81,	1.0,	1.0,	1.1,	1.21	ENDT
TABLED1 2002 $ DAMPING TABLE
,	0.9	.2864789,  1.0,		.318309,   1.1	,	.3501409  ENDT
$CONVENTIONAL INPUT FOR FREQUENCY RESPONSE
PARAM,	WTMASS,	.0253303 $ 1/(2*PI)**2. GIVES FN=1.0
DAREA,	1,	12,	1,	2.  $CAUSES UNIT DEFLECTION
FREQ,	10,	0.9,	1.0,	1.1  $  BRACKET THE NATURAL FREQUENCY
RLOAD1,	1,	1,	,	,	3
TABLED1,3  $  TABLE FOR FORCE VS. FREQUENCY
,	0.9,	0.81,	1.,	1.,	1.1,	1.21,ENDT  $ P = K
ENDDATA
FREQUENCY =  9.000000E-01
	C O M P L E X     D I S P L A C E M E N T
	(REAL/IMAGINARY)

	POINT ID. 	TYPE 	T1 	T2 	T3 	R1 	R2 	R3
0	11	G	.0	.0	.0	.0	.0	.0
			.0	.0	.0	.0	.0	.0
0	12	G	-6.682744E-08	.0	.0	.0	.0	.0
			-1.000000E+00	.0	.0	.0	.0	.0
1	VERIFICATION PROBLEM, FREQ. DEP. IMPEDANCE				BUSHVER	MARCH 20,1997 MSC.Nastran 1/23/97 PAGE 8
	 SINGLE DOF , CRITICAL DAMPING, 3 EXCITATION FREQUENCIES
0
FREQUENCY =  1.000000E+00
	C O M P L E X     D I S P L A C E M E N T
	(REAL/IMAGINARY)

	POINT ID. 	TYPE 	T1 	T2 	T3 	R1 	R2 	R3
0	11	G	.0	.0	.0	.0	.0	.0
			.0	.0	.0	.0	.0	.0
0	12	G	-1.046835E-07	.0	.0	.0	.0	.0
			-9.999999E-01	.0	.0	.0	.0	.0
1	VERIFICATION PROBLEM, FREQ. DEP. IMPEDANCE				BUSHVER	MARCH 20,1997 MSC.Nastran 1/23/97 PAGE 9
	 SINGLE DOF , CRITICAL DAMPING, 3 EXCITATION FREQUENCIES
0
FREQUENCY =  1.100000E+00
	C O M P L E X     D I S P L A C E M E N T
	(REAL/IMAGINARY)

	POINT ID. 	TYPE 	T1 	T2 	T3 	R1 	R2 	R3
0	11	G	.0	.0	.0	.0	.0	.0
			.0	.0	.0	.0	.0	.0
0	12	G	-6.855670E-08	.0	.0	.0	.0	.0
			-9.999999E-01	.0	.0	.0	.0	.0
1	VERIFICATION PROBLEM, FREQ. DEP. IMPEDANCE				BUSHVER	MARCH 20,1997 MSC.Nastran 1/23/97 PAGE 10
	 SINGLE DOF , CRITICAL DAMPING, 3 EXCITATION FREQUENCIES
FREQUENCY =  9.000000E-01
	C O M P L E X     F O R C E S   I N   B U S H   E L E M E N T S   ( C B U S H )
	(REAL/IMAGINARY)

	ELEMENT-ID. 	FORCE-X 	 FORCE-Y 	 FORCE-Z 	MOMENT-X 	MOMENT-Y 	MOMENT-Z
0	1000	 1.620000E+00	 .0	.0	.0	.0	.0
		-8.100000E-01	 .0	.0	.0	.0	.0
1	VERIFICATION PROBLEM, FREQ. DEP. IMPEDANCE				BUSHVER	MARCH 20,1997 MSC.Nastran 1/23/97 PAGE 11
	 SINGLE DOF , CRITICAL DAMPING, 3 EXCITATION FREQUENCIES
0
FREQUENCY =  1.000000E+00
	C O M P L E X     F O R C E S   I N   B U S H   E L E M E N T S   ( C B U S H )
	(REAL/IMAGINARY)

	ELEMENT-ID. 	FORCE-X 	 FORCE-Y 	 FORCE-Z 	MOMENT-X 	MOMENT-Y 	MOMENT-Z
0	1000	 2.000000E+00	 .0	.0	.0	.0	.0
		-1.000000E+00	 .0	.0	.0	.0	.0
1	VERIFICATION PROBLEM, FREQ. DEP. IMPEDANCE				BUSHVER	MARCH 20,1997 MSC.Nastran 1/23/97 PAGE 12
	 SINGLE DOF , CRITICAL DAMPING, 3 EXCITATION FREQUENCIES
0
FREQUENCY =  1.100000E+00
	C O M P L E X     F O R C E S   I N   B U S H   E L E M E N T S   ( C B U S H )
	(REAL/IMAGINARY)

	ELEMENT-ID. 	FORCE-X 	 FORCE-Y 	 FORCE-Z 	MOMENT-X 	MOMENT-Y 	MOMENT-Z
0	1000	 2.419999E+00	 .0	.0	.0	.0	.0
		-1.210000E+00	 .0	.0	.0	.0	.0
1	VERIFICATION PROBLEM, FREQ. DEP. IMPEDANCE				BUSHVER	MARCH 20,1997 MSC.Nastran 1/23/97 PAGE 13
	 SINGLE DOF , CRITICAL DAMPING, 3 EXCITATION FREQUENCIES
0

1.0
ID SEMINAR, PROB5
SOL108
TIME30
CEND
TITLE = FREQUENCY RESPONSE DUE TO UNIT FORCE AT TIP
ECHO = UNSORTED
SPC = 1
SET 111 = 11, 33, 55
DISPLACEMENT(SORT2, PHASE) = 111
SUBCASE 1
DLOAD = 500
FREQUENCY = 100
$
OUTPUT (XYPLOT)
$
XTGRID= YES
YTGRID= YES
XBGRID= YES
YBGRID= YES
YTLOG= YES
YBLOG= NO
XTITLE= FREQUENCY (HZ)
YTTITLE= DISPLACEMENT RESPONSE AT LOADED CORNER, MAGNITUDE
YBTITLE= DISPLACEMENT RESPONSE AT LOADED CORNER, PHASE
XYPLOT DISP RESPONSE / 11 (T3RM, T3IP)
YTTITLE= DISPLACEMENT RESPONSE AT TIP CENTER, MAGNITUDE
YBTITLE= DISPLACEMENT RESPONSE AT TIP CENTER, PHASE
XYPLOT DISP RESPONSE / 33 (T3RM, T3IP)
YTTITLE= DISPLACEMENT RESPONSE AT OPPOSITE CORNER, MAGNITUDE
YBTITLE= DISPLACEMENT RESPONSE AT OPPOSITE CORNER, PHASE
XYPLOT DISP RESPONSE / 55 (T3RM, T3IP)
$
 POINT-ID =        11                                       C O M P L E X   D I S P L A C E M E N T   V E C T O R                                                         (MAGNITUDE/PHASE)       FREQUENCY   TYPE         	T1          	T2             	T3             	R1             	R2             	R30  2.000000E+01     G           	.0             	.0          	8.817999E-03   	6.435859E-04   	2.632016E-03      	.0                                	.0             	.0          	356.4954       	176.5664       	176.5000          	.00  4.000000E+01     G           	.0             	.0          	9.404316E-03   	6.434992E-04   	2.795561E-03      	.0                                	.0             	.0          	356.2596       	176.5677       	176.2785          	.0                                                   .                                                    .                                                    . 0  9.799999E+02     G       	.0             	.0          	9.965085E-04   	2.691742E-04   	4.097779E-04    	.0                            	.0             	.0          	187.6832       	7.8008         	15.1581         	.00  1.000000E+03     G       	.0             	.0          	8.803169E-04   	2.354655E-04   	3.317750E-04    	.0                            	.0             	.0          	186.9298       	8.2146         	14.6645         	.0                                                   .                                                    .                                                    .       POINT-ID =        33                                       C O M P L E X   D I S P L A C E M E N T   V E C T O R                                                         (MAGNITUDE/PHASE)       FREQUENCY   TYPE          	T1             	T2             	T3             	R1             	R2             	R30  2.000000E+01     G         	.0             	.0            	8.183126E-03   	5.993296E-04   	2.443290E-03      	.0                              	.0             	.0            	356.4899       	176.5639       	176.4950          	.00  4.000000E+01     G         	.0             	.0            	8.768992E-03   	6.006201E-04   	2.606561E-03      	.0                              	.0             	.0            	356.2376       	176.5565       	176.2581          	.0                                                   .                                                    .                                                    .
0  9.799999E+02     G       	.0             	.0            	6.867234E-04   	3.836353E-04   	5.393046E-04    	.0                              	.0             	.0          	188.0180         	5.5597        	10.0794          	.00  1.000000E+03     G       	.0             	.0            	6.062436E-04   	3.454143E-04   	4.648783E-04    	.0                              	.0             	.0          	186.8358         	5.4959         	8.8514          	.0                                                   .                                                    .                                                    .
1    FREQUENCY RESPONSE DUE TO UNIT FORCE AT TIP                              APRIL   8, 1998  MSC.Nastran  4/ 6/98   PAGE    170                                                                                SUBCASE 1                         0                             X Y - O U T P U T  S U M M A R Y  ( R E S P O N S E )0 SUBCASE  CURVE FRAME                    XMIN-FRAME/    XMAX-FRAME/    YMIN-FRAME/      X FOR        YMAX-FRAME/      X FOR     ID     TYPE   NO.    CURVE ID.          ALL DATA       ALL DATA       ALL DATA       YMIN           ALL DATA       YMAX0       1  DISP      1       11(  5,--)   2.000000E+01   1.000000E+03   1.001178E-04   3.800000E+02   6.794556E-02   1.400000E+02                                          2.000000E+01   1.000000E+03   1.001178E-04   3.800000E+02   6.794556E-02   1.400000E+020       1  DISP      1       11(--, 11)   2.000000E+01   1.000000E+03   1.834655E+02   2.200000E+02   3.564954E+02   2.000000E+01                                          2.000000E+01   1.000000E+03   1.834655E+02   2.200000E+02   3.564954E+02   2.000000E+010       1  DISP      2       33(  5,--)   2.000000E+01   1.000000E+03   4.981586E-05   6.000000E+02   6.858238E-02   1.400000E+02                                          2.000000E+01   1.000000E+03   4.981586E-05   6.000000E+02   6.858238E-02   1.400000E+020       1  DISP      2       33(--, 11)   2.000000E+01   1.000000E+03   1.815143E+02   3.000000E+02   3.564899E+02   2.000000E+01                                          2.000000E+01   1.000000E+03   1.815143E+02   3.000000E+02   3.564899E+02   2.000000E+010       1  DISP      3       55(  5,--)   2.000000E+01   1.000000E+03   2.144667E-04   1.000000E+03   6.896591E-02   1.400000E+02                                          2.000000E+01   1.000000E+03   2.144667E-04   1.000000E+03   6.896591E-02   1.400000E+020       1  DISP      3       55(--, 11)   2.000000E+01   1.000000E+03   6.565820E+00   7.599999E+02   3.580194E+02   7.800000E+02                                          2.000000E+01   1.000000E+03   6.565820E+00   7.599999E+02   3.580194E+02   7.800000E+02
ID SEMINAR, PROB6
SOL 111
TIME30
CEND
TITLE = FREQUENCY RESPONSE WITH PRESSURE AND POINT LOADS
ECHO = UNSORTED
SEALL = ALL
SPC = 1
SET 111 = 11, 33, 55
DISPLACEMENT(PHASE, PLOT) = 111
METHOD = 100
FREQUENCY = 100
SDAMPING = 100
SUBCASE 1
DLOAD = 100
LOADSET = 100
$
OUTPUT (XYPLOT)
$
XTGRID= YES
YTGRID= YES
XBGRID= YES
YBGRID= YES
YTLOG= YES
YBLOG= NO
XTITLE= FREQUENCY (HZ)
YTTITLE= DISPLACEMENT RESPONSE AT LOADED CORNER, MAGNITUDE
YBTITLE= DISPLACEMENT RESPONSE AT LOADED CORNER, PHASE
XYPLOT DISP RESPONSE / 11 (T3RM, T3IP)
YTTITLE= DISPLACEMENT RESPONSE AT TIP CENTER, MAGNITUDE
YBTITLE= DISPLACEMENT RESPONSE AT TIP CENTER, PHASE
XYPLOT DISP RESPONSE / 33 (T3RM, T3IP)
0                                                                                SUBCASE 1                              0                             X Y - O U T P U T  S U M M A R Y  ( R E S P O N S E )0 SUBCASE  CURVE FRAME                    XMIN-FRAME/    XMAX-FRAME/    YMIN-FRAME/      X FOR        YMAX-FRAME/      X FOR     ID     TYPE   NO.    CURVE ID.          ALL DATA       ALL DATA       ALL DATA       YMIN           ALL DATA       YMAX0       1  DISP      1       11(  5,--)   2.000000E+01   1.000000E+03   3.481835E-04   4.400000E+02   1.699121E-01   1.336996E+02                                          2.000000E+01   1.000000E+03   3.481835E-04   4.400000E+02   1.699121E-01   1.336996E+020       1  DISP      1       11(--, 11)   2.000000E+01   1.000000E+03   1.390213E+02   1.000000E+03   3.258276E+02   2.000000E+01                                          2.000000E+01   1.000000E+03   1.390213E+02   1.000000E+03   3.258276E+02   2.000000E+010       1  DISP      2       33(  5,--)   2.000000E+01   1.000000E+03   2.271459E-04   6.600000E+02   1.700317E-01   1.336996E+02                                          2.000000E+01   1.000000E+03   2.271459E-04   6.600000E+02   1.700317E-01   1.336996E+020       1  DISP      2       33(--, 11)   2.000000E+01   1.000000E+03   1.385571E+02   1.000000E+03   3.263339E+02   2.000000E+01                                          2.000000E+01   1.000000E+03   1.385571E+02   1.000000E+03   3.263339E+02   2.000000E+010       1  DISP      3       55(  5,--)   2.000000E+01   1.000000E+03   1.278678E-04   1.000000E+03   1.696787E-01   1.336996E+02                                          2.000000E+01   1.000000E+03   1.278678E-04   1.000000E+03   1.696787E-01   1.336996E+020       1  DISP      3       55(--, 11)   2.000000E+01   1.000000E+03   1.687413E+01   7.001384E+02   3.573561E+02   7.104853E+02                                          2.000000E+01   1.000000E+03   1.687413E+01   7.001384E+02   3.573561E+02   7.104853E+02


title: Презентация на тему: MSC.Nastran 102 2001 - 10

text:
Slide Title
Body Text
Second Level
Third Level
Fourth Level
Fifth Level
Body Text
Second Level
Third Level
Fourth Level
Fifth Level
MSC Corporate Overview Speaker Notes
[Baa]


Презентация на тему: MS EXCEL ОСНОВЫ РАБОТЫ


Презентация на тему: MS Excel(Электронные таблицы)


title: Презентация на тему: MSC.Nastran 101 2006 - 2

text:
Click to edit Master title style
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Second level
Third level
Fourth level
Fifth level
MSC Confidential
Body Text
Second Level
Third Level
Fourth Level
Fifth Level
MSC Corporate Overview Speaker Notes
Hand Calculation
HAND CALCULATION
1
2
3
ka
kb
U1 , P1
U3 , P3
U2 , P2
100
200
Element 100
Element 200
N x N
g
A
B
V
WB
WA
X
Y
Z
W3B
W1B
W3A
+
W2B
W2A
PB
PA
W1A
OFFT
X2
X1
CBAR
X3
GB
PID
EID
GA
W3B
W1B
W3A
+
W2B
W2A
PB
PA
W1A
OFFT
X2
X1
CBAR
X3
GB
PID
EID
GA
Offset
Offset
Basic
BOO
Global
Offset
Basic
BOG
Offset
Global
Basic
BGO
Global
Global
Basic
BGG
Offset
Offset
Global
GOO
Global
Offset
Global
GOG
Offset
Global
Global
GGO
Global
Global
Global
GGG
End B Offset
End A Offset
Orientation Vector
String
$
$
Field
Contents
~Aw / A
~Af  / 2A
1/2
9/10
5/6
.5
.5
.5
.5
6.
14.
I
8
39
PBARL
NSM
-etc-
DIM9
DIM8
DIM7
DIM6
DIM5
DIM4
DIM3
DIM2
DIM1
TYPE
GROUP
MID
PID
PBARL
10
9
8
7
6
5
4
3
2
1

.5
.5
.5
.5
6.
14.
I
8
39
PBARL
NSM
-etc-
DIM9
DIM8
DIM7
DIM6
DIM5
DIM4
DIM3
DIM2
DIM1
TYPE
GROUP
MID
PID
PBARL
10
9
8
7
6
5
4
3
2
1


Презентация на тему: MS Excel : основы работы


title: Презентация на тему: MSC.Patran PAT 318 2002 - 03

text:
        PAT318, Section  3, March 2002
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Second level
Third level
Fourth level
Fifth level
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Second level
Third level
Fourth level
Fifth level


title: Презентация на тему: MS WINDOWS. Копирование, перемещение объектов. Корзина. Удаление и восстановление

text:
1.
2.
3.
4.
5.


title: Презентация на тему: MS OFFICE В ШКОЛЕ

text:
Microsoft Word
Microsoft Excel
Microsoft PowerPoint
Microsoft Access
Microsoft Outlook
Microsoft Word


title: Презентация на тему: MS Office

text:
Click to edit Master title style
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Second level
Third level
Fourth level
Fifth level
Click to edit Master title style
Click to edit Master text styles
Second level
Third level
Fourth level
Fifth level
Click to edit Master title style
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Second level
Third level
Fourth level
Fifth level
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Second level
Third level
Fourth level
Fifth level
900igr.net
MICROSOFT® BUSINESS CERTIFICATION
Improving the Workplace Study, Sean Gyll, PhD
Post Certification Survey, Certiport 2008
Post Certification Study, Certiport 2008
Preventing Bad  Hires White Paper, IDC 2007
Improving the Workplace Study, Sean Gyll, PhD
Post Certification Study, Certiport 2008
Post Certification Survey, Certiport 2008
Improving the Workplace Study, Sean Gyll, PhD

http://www.microsoft.com/learning/mcp/mct/benefits.mspx

Sonya Andrews sonyaa@microsoft.com
Debbie Collins is a consultant to Microsoft and Certiport, and a worldwide authority on Microsoft certification.


title: Презентация на тему: MSC.Patran PAT 318 2002 - 23

text:
Stress-Life Analysis (SLF)
Strain-Life Crack Initiation (CLF)
Multiaxial Strain-Life (MLF)
Frequency Domain Fatigue (FLF)
Crack Growth LEFM (FCG)
        PAT318, Section 23, March 2002
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Second level
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Fifth level
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Second level
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Fourth level
Fifth level
0
10
20
30
-10
-5
0
5
10
rear g2(g)
A04.DAC
secs
0
10
20
30
-10
-5
0
5
10
rear g2(g)
3A04.DAC
secs
Screen 1
PSDs of input & output
Cross-Power Spectra between input & output
Gain, phase & coherence relationships
0
4174
Range
Total plot of file STRAIN
224.2
0
    Cycles
10.67
0
    Damage  %
Cycle
Damage
o
h
r
t
Kt = 0.22 +         1
                    -------------------
                   (r/t)   . (h/t)
0.2
0.4
stress
d
d/4
d/8
r
o
o
o
A
A
B
M
M
Kt is at point B (15 deg from vertical)
N.B. Kt at point A is constant = 1.6
d
r
t
M
M
s
Nominal stress = M / ( 3.142 d   / 32 )
In this case r / d = 0.1
3
Stress-Life Analysis (SLF)
Strain-Life Crack Initiation (CLF)
Multiaxial Strain-Life (MLF)
Frequency Domain Fatigue (FLF)
Crack Growth LEFM (FCG)
Stress-Life Analysis (SLF)
Strain-Life Crack Initiation (CLF)
Multiaxial Strain-Life (MLF)
Frequency Domain Fatigue (FLF)
Crack Growth LEFM (FCG)


title: Презентация на тему: MS Word мәтіндік процессоры туралы жалпы түсінік

text:
1.
2.
3.
4.
5.
6.
1.
2.
3.
4.
5
MS WORD


title: Презентация на тему: MSC.Patran PAT 318 2002 - 19

text:
         PAT318, Section 19, March 2002
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Second level
Third level
Fourth level
Fifth level
©nCode International 1998
Fatigue Theory for Engineers
smax = Kts
Kt=3
Kt=(1+2a/b)
da
---
dN
DK
TCY
MDB
KSN
CRG


title: Презентация на тему: MSC.Patran PAT 318 2002 - 16

text:
        PAT318, Chapter 16, March 2002
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Second level
Third level
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Fifth level
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Second level
Third level
Fourth level
Fifth level
©nCode International 1998
S
t
r
e
s
s
A
m
p
l
i
t
u
d
e
N
o
t
c
h
e
d
S
h
a
f
t
U
n
n
o
t
c
h
e
d
S
h
a
f
t
Log (fatigue life)
Log(Stress)
Log(Life)
Steel or Ti
Al alloy
or steel in seawater
P
P
P
_
A
A
Static Limitations
1
m
m+2
constant amplitude loading
in clean air
S
t
r
e
s
s

r
a
n
g
e

(
s
0
)

l
o
g

s
c
a
l
e
Endurance N (cycles) - log scale
Effective curve obtained under variable amplitude
loading, equivalent to changing slope of sr - N curve
above N = 10
10
7
(
s
0
)
1
1
1
s
n
o
m
n
o
m
s
%
5
.
0
60000
300
=
=

100 MPa
å
=
i
f
i
N
N
n
1
N
1
N
1
S
1
S
1
n
1
%
5
.
0
60000
300
=
=

100 MPa
å
=
i
f
i
N
N
LIFE
Un-Safe
Un-Safe
s
s
a
e
m
u
S
S
+
=
1
2
s
s
a
e
m
u
S
S
+
æ
è
ç
ö
ø
÷
=
1
s
s
a
m
u
e
S
S
=
=
=
=
s
m
=
0

Kf = 1 + ( Kt  - 1 ) / ( 1 + a / r )
1E3
1E4
1E5
1E6
1E7
1E8
200
400
600
800
1000
SMOOTH
Kt=3, Kf=2.67
Cross Plot of Data : KFEFFECT
NOTCHED
UNNOTCHED
Life(Cycles)
Amplitude(MPa)
Kf
+
=
S-N Data Plot
MANTEN_SN
SRI1: 3162  b1: -0.2  b2: 0    E: 2.034E5  UTS: 600
1E1
1E2
1E3
1E4
Stress Range (MPa)
1E0
1E1
1E2
1E3
1E4
1E5
1E6
1E7
1E8
1E9
Life (Cycles)
f
\
S
e
s
a
---    1
s
m
s
u
¤
 (                         )
=
This sort of approach is incorporated into a British Standard Design Code BS7608.  Here is an example of one weld class from that standard.  The stress used is the nominal stress on the joint, i.e. it is independent of the detailed geometry of the weld.
Most fatigue tests are conducted at R=-1.  If we have cycles with other R values we should make corrections to the stress range in order to be able to compare the cycles to the S-N curve determined at R=-1.
Of the two methods described here, the Goodman method is more popular because it is more conservative.
This factor may be calculated using the graph shown above.
Other effects that should be considered are loading type (e.g. bending vs tension) size effects and stress gradient effects.
For instance, for correcting for size effects in shafts, an equation such as:
C(size) = 1.189*d^(-0.097)
can be used to determine the correction factor for size effect, relative to tests on an 8 mm bar.  This recognises that the probability of finding a bad defect rises as you increase the size of the component.
The effect of surface roughness is typically accounted for by applying a reduction factor to the stress at the endurance or fatigue limit.  On a log-log plot, the slope of the stress life curve is adjusted, with the stress at 1000 cycles being unaffected.


title: Презентация на тему: Мультикастинг

text:
RPF (Reverse Path Forwarding)
CBT (Core Based Trees)


Презентация на тему: MS Project


title: Презентация на тему: MSC.Nastran 101 2006 - 5

text:
AUTOSPC

AUTOSPC
section5_1.bdf
section5_1.bdf

 G R I D   P O I N T   S I N G U L A R I T Y   T A B L E
0                             POINT    TYPE   FAILED      STIFFNESS       OLD USET           NEW USET
                               ID            DIRECTION      RATIO     EXCLUSIVE  UNION   EXCLUSIVE  UNION
                                1        G      4         0.00E+00          BF       F         SB       S    *
                                1        G      5         0.00E+00          BF       F         SB       S    *
                                1        G      6         0.00E+00          BF       F         SB       S    *
                                2        G      4         0.00E+00          BF       F         SB       S    *
                                2        G      5         0.00E+00          BF       F         SB       S    *
                                2        G      6         0.00E+00          BF       F         SB       S    *
                                3        G      4         0.00E+00          BF       F         SB       S    *
                                3        G      5         0.00E+00          BF       F         SB       S    *
                                3        G      6         0.00E+00          BF       F         SB       S    *

section5_3.bdf
section5_3.bdf
section5_3.bdf

THE FOLLOWING DEGREES OF FREEDOM HAVE FACTOR DIAGONAL RATIOS GREATER THAN
      1.00000E+07 OR HAVE NEGATIVE TERMS ON THE FACTOR DIAGONAL.
0                                                                                SUBCASE 1
0
         GRID POINT ID       DEGREE OF FREEDOM   MATRIX/FACTOR DIAGONAL RATIO        MATRIX DIAGONAL

              13                                      R2                                           1.71146E+13                                       2.13419E+02
 ^^^ USER   FATAL   MESSAGE 9050 (SEKRRS)
 ^^^ RUN TERMINATED DUE TO EXCESSIVE PIVOT RATIOS IN MATRIX KLL.
 ^^^ USER ACTION:  CONSTRAIN MECHANISMS WITH SPCI OR SUPORTI ENTRIES OR SPECIFY PARAM,BAILOUT,-1 TO  CONTINUE THE RUN WITH MECHANISMS.

$        SID    GRID  DOF  A1    GRID  DOF   A2
MPC      1       145     1      -1.      146     1       1.
MPC      1       145     2      -1.      146     2       1.

RSSCON
ELSUM
$ file maxmin.dat
sol 101
cend
title = cantilever beam model
subtitle = OLOAD OUTPUT
spc = 1
disp=all
maxmin(vmag=2,disp,spcf)=all
subcase 1
label = pload1
load = 1
subcase 2
label = load in x, y, and z
load = 2
begin bulk
pload1,1,1,fy,fr,0.,1.,1.,1.
=,=,*(1),==
=(6)
force,2,9,,1.,1.,1.,1.
PARAM   GRDPNT  0
PARAM   POST    -1
$
cord2r,1,,0.,0.,0.,0.,1.,0.
,1.,0.,1.
GRID    1       0       0.0     0.0     0.0     0
GRID    2       0       12.5    0.0     0.0     0
GRID    3       0       25.     0.0     0.0     0
GRID    4       0       37.5    0.0     0.0     0
GRID    5       0       50.     0.0     0.0     0
GRID    6       0       62.5    0.0     0.0     0
GRID    7       0       75.     0.0     0.0     0
GRID    8       0       87.5    0.0     0.0     0
GRID    9       0       100.    0.0     0.0     1
$
CBEAM   1       1       1       2               1.
CBEAM   2       1       2       3               1.
CBEAM   3       1       3       4               1.
CBEAM   4       1       4       5               1.
CBEAM   5       1       5       6               1.
CBEAM   6       1       6       7               1.
CBEAM   7       1       7       8               1.
CBEAM   8       1       8       9               1.
$
SPC     1       1       123456  0.0
$
PBEAML  1       1               BAR
        1.      2.
$
MAT1    1       1.+7            .3      .1
$
ENDDATA
0          *** T1 ***   D I S P L A C E M E N T   M A X / M I N   V A L U E   S U M M A R Y          RESULTS FOR SUBCASE       1
  MAXMIN OPTIONS: SET=ALL, CID=BASIC, VMAG=2, VMAG=2, COMP=T1
  POINT ID. TYPE   CID          ***TMAG***           T2               T3               R1               R2               R3
        1     G   BASIC        0.000000E+00     0.000000E+00     0.000000E+00     0.000000E+00     0.000000E+00     0.000000E+00
        2     G   BASIC        5.404634E-02     0.000000E+00     0.000000E+00     8.251953E-03     0.000000E+00     0.000000E+00
        8     G   BASIC        1.563420E+00     0.000000E+00     0.000000E+00     2.495117E-02     0.000000E+00     0.000000E+00
        9     G   BASIC        1.875780E+00     0.000000E+00     0.000000E+00     2.500000E-02     0.000000E+00     0.000000E+00
        9     G        1       0.000000E+00     0.000000E+00     1.875780E+00     1.767767E-02    -1.767767E-02     0.000000E+00

1    CANTILEVER BEAM MODEL                                                 FEBRUARY  13, 2001  MSC.NASTRAN  1/17/01   PAGE    12
      OLOAD OUTPUT
0

0          *** R1 ***   D I S P L A C E M E N T   M A X / M I N   V A L U E   S U M M A R Y          RESULTS FOR SUBCASE       1
  MAXMIN OPTIONS: SET=ALL, CID=BASIC, VMAG=2, VMAG=2, COMP=R1
  POINT ID. TYPE   CID              T1               T2               T3           ***RMAG***           R2               R3
        1     G   BASIC        0.000000E+00     0.000000E+00     0.000000E+00     0.000000E+00     0.000000E+00     0.000000E+00
        2     G   BASIC        5.404634E-02     0.000000E+00     0.000000E+00     8.251953E-03     0.000000E+00     0.000000E+00
        8     G   BASIC        1.563420E+00     0.000000E+00     0.000000E+00     2.495117E-02     0.000000E+00     0.000000E+00
        9     G   BASIC        1.875780E+00     0.000000E+00     0.000000E+00     2.500000E-02     0.000000E+00     0.000000E+00
        9     G        1       0.000000E+00     0.000000E+00     1.875780E+00     1.767767E-02    -1.767767E-02     0.000000E+00
GEOMCHECK

1    MSC.NASTRAN JOB CREATED ON 28-JUL-05 AT 11:18:00                          JULY  28, 2005  MSC.NASTRAN  9/23/04   PAGE     4

0
     TOLERANCE LIMITS ARE:  SA =  60.00, IA(MIN) =  30.00, IA(MAX) = 150.00, WF =   0.05, TR =   0.50 (FLAG = LIMIT VIOLATED)
 ELEMENT TYPE    ID          SKEW ANGLE      MIN INT. ANGLE    MAX INT. ANGLE    WARPING FACTOR      TAPER RATIO
    QUAD4           1        45.00 ++++        45.00            135.00              0.00              0.00
    QUAD4           2        45.00 ++++        45.00            135.00              0.00              0.00
    QUAD4           3        45.00 ++++        45.00            135.00              0.00              0.00
    QUAD4           4        45.00 ++++        45.00            135.00              0.00              0.00
    QUAD4           5        45.00 ++++        45.00            135.00              0.00              0.00
1    MSC.NASTRAN JOB CREATED ON 28-JUL-05 AT 11:18:00                          JULY  28, 2005  MSC.NASTRAN  9/23/04   PAGE     5

0

                            E L E M E N T   G E O M E T R Y   T E S T   R E S U L T S   S U M M A R Y
                                        TOTAL NUMBER OF TIMES TOLERANCES WERE EXCEEDED
                                  ASPECT/       MINIMUM       MAXIMUM     SURFACE/FACE                 EDGE POINT     JACOBIAN
     ELEMENT TYPE  SKEW ANGLE    TAPER RATIO  INTER. ANGLE  INTER. ANGLE   WARP FACTOR  OFFSET RATIO  LENGTH RATIO  DETERMINANT
         QUAD4          80             0             0             0             0           N/A           N/A           N/A

         N/A IN THE ABOVE TABLE INDICATES TESTS THAT ARE NOT APPLICABLE TO THE ELEMENT TYPE AND WERE NOT PERFORMED.
         FOR ALL ELEMENTS WHERE GEOMETRY TEST RESULTS HAVE EXCEEDED TOLERANCES,

         QUAD4    ELEMENT ID        1 PRODUCED SMALLEST SKEW ANGLE       OF      45.00 (TOLERANCE =       60.00).
MAT1    1       3.E+7           0.3$FORCE   1       2               2500.   0.0     -1.0    0.0$SPC1    1       156     3SPC1    2       2       3$ENDDATA
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Second level
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Fifth level
MSC Confidential
Body Text
Second Level
Third Level
Fourth Level
Fifth Level
MSC Corporate Overview Speaker Notes
R3
R2
R1
T3
T2
T1
GRID 99
R3
R2
R1
T3
T2
T1
HEXA Element
GRID 99
R3
R2
R1
T3
T2
T1
R3
R2
R1
T3
T2
T1
GRID 99
Solid
Bar
GRID 99
R3
R2
R1
T3
T2
T1
GRID 99
GRID 99
1.2745e+6
6
100.
20.
2.4671e+6
7
0.
20.
1.2842e+6
6
0.
0.
K6ROT
SNORM
n
R=10
Z
246
246
246
2
2
246
246
246
20.
100.
20.
0.
20.
0.
SNORM
K6ROT
0.1000
0.2000
0.3000
0.4000
0.5000
0.6000
0.7000
0.8000
0.9000
1.0000
0.
1.e+1
1.e+2
1.e+3
1.e +4
1.e +5
1.e +6
K6ROT
4x4
2x2
1
20
60
o
t = 2
R = 46
150
1N
X
y
Z
R = 14

GRID 1
                                1        G      6         0.00E+00          BF       F         SB       S    *
                                2        G      6         0.00E+00          BF       F         SB       S    *
                                3        G      6         0.00E+00          BF       F         SB       S    *
                                4        G      6         0.00E+00          BF       F         SB       S    *
                               62        G      4         0.00E+00          BF       F         SB       S    *
                               62        G      5         0.00E+00          BF       F         SB       S    *
                               62        G      6         0.00E+00          BF       F         SB       S    *
                               63        G      4         0.00E+00          BF       F         SB       S    *
                               63        G      5         0.00E+00          BF       F         SB       S    *
                               63        G      6         0.00E+00          BF       F         SB       S    *
                               64        G      4         0.00E+00          BF       F         SB       S    *
                               64        G      5         0.00E+00          BF       F         SB       S    *
                               64        G      6         0.00E+00          BF       F         SB       S    *
GRID 13
 *** USER WARNING MESSAGE 5487 (EBCHKD)
     ORIENTATION VECTOR DEFINED FOR THE ELEMENT ID =       7 IS NEARLY PARALLEL, IT MAY GIVE POOR RESULTS.
 *** USER WARNING MESSAGE 5487 (EBCHKD)
     ORIENTATION VECTOR DEFINED FOR THE ELEMENT ID =       8 IS NEARLY PARALLEL, IT MAY GIVE POOR RESULTS.
 *** USER WARNING MESSAGE 5487 (EBCHKD)
     ORIENTATION VECTOR DEFINED FOR THE ELEMENT ID =       9 IS NEARLY PARALLEL, IT MAY GIVE POOR RESULTS.
 *** USER WARNING MESSAGE 5487 (EBCHKD)
     ORIENTATION VECTOR DEFINED FOR THE ELEMENT ID =      10 IS NEARLY PARALLEL, IT MAY GIVE POOR RESULTS.
 *** USER WARNING MESSAGE 5487 (EBCHKD)
     ORIENTATION VECTOR DEFINED FOR THE ELEMENT ID =      11 IS NEARLY PARALLEL, IT MAY GIVE POOR RESULTS.
 *** USER WARNING MESSAGE 5487 (EBCHKD)
     ORIENTATION VECTOR DEFINED FOR THE ELEMENT ID =      12 IS NEARLY PARALLEL, IT MAY GIVE POOR RESULTS.
 *** USER WARNING MESSAGE 5487 (EBCHKD)
     ORIENTATION VECTOR DEFINED FOR THE ELEMENT ID =      13 IS NEARLY PARALLEL, IT MAY GIVE POOR RESULTS.
 *** USER WARNING MESSAGE 5487 (EBCHKD)
     ORIENTATION VECTOR DEFINED FOR THE ELEMENT ID =      14 IS NEARLY PARALLEL, IT MAY GIVE POOR RESULTS.
 *** USER FATAL MESSAGE 2026 (EMG)
     ELEMENT        7 GEOMETRY YIELDS UNREASONABLE MATRIX.
 *** USER FATAL MESSAGE 2026 (EMG)
     ELEMENT        8 GEOMETRY YIELDS UNREASONABLE MATRIX.
 *** USER FATAL MESSAGE 2026 (EMG)
     ELEMENT        9 GEOMETRY YIELDS UNREASONABLE MATRIX.
 *** USER FATAL MESSAGE 2026 (EMG)
     ELEMENT       10 GEOMETRY YIELDS UNREASONABLE MATRIX.
 *** USER FATAL MESSAGE 2026 (EMG)
     ELEMENT       11 GEOMETRY YIELDS UNREASONABLE MATRIX.
 *** USER FATAL MESSAGE 2026 (EMG)
     ELEMENT       12 GEOMETRY YIELDS UNREASONABLE MATRIX.
 *** USER FATAL MESSAGE 2026 (EMG)
     ELEMENT       13 GEOMETRY YIELDS UNREASONABLE MATRIX.
 *** USER FATAL MESSAGE 2026 (EMG)
     ELEMENT       14 GEOMETRY YIELDS UNREASONABLE MATRIX.
$ bar elements follow
CBAR     1       1       1       2       0.      1.      0.
CBAR     2       1       2       3       0.      1.      0.
CBAR     3       1       3       4       0.      1.      0.
CBAR     4       1       4       5       0.      1.      0.
CBAR     5       1       5       6       0.      1.      0.
CBAR     6       1       6       7       0.      1.      0.
CBAR     7       1       8       9       0.      1.      0.
CBAR     8       1       9       10      0.      1.      0.
CBAR     9       1       10      12      0.      1.      0.
CBAR     10      1       12      1       0.      1.      0.
CBAR     11      1       14      15      0.      1.      0.
CBAR     12      1       15      16      0.      1.      0.
CBAR     13      1       16      18      0.      1.      0.
CBAR     14      1       18      7       0.      1.      0.
CBAR     15      1       10      21      0.      1.      0.
CBAR     16      1       21      22      0.      1.      0.
CBAR     17      1       22      23      0.      1.      0.
CBAR     18      1       23      24      0.      1.      0.
CBAR     19      1       24      25      0.      1.      0.
CBAR     20      1       25      16      0.      1.      0.
a
b
a
b
u
u
u
u
u
*** USER INFORMATION MESSAGE 5293 (SSG3A)
    FOR DATA BLOCK KLL
    LOAD SEQ. NO.             EPSILON              EXTERNAL WORK      EPSILONS LARGER THAN 0.001 ARE FLAGGED WITH ASTERISKS
                1                      -1.3760919E-13          3.6560133E+04

0 RESULTANTS ABOUT ORIGIN OF SUPERELEMENT BASIC COORDINATE SYSTEM IN SUPERELEMENT BASIC SYSTEM COORDINATES.

0                                                  OLOAD    RESULTANT
  SUBCASE/    LOAD
  DAREA ID    TYPE       T1            T2            T3            R1            R2            R3
0        1     FX   -3.900000E+03     ----          ----          ----       0.000000E+00  3.744000E+05
               FY       ----      -4.500000E+03     ----       0.000000E+00     ----      -1.296000E+06
               FZ       ----          ----       0.000000E+00  0.000000E+00  0.000000E+00     ----
               MX       ----          ----          ----       0.000000E+00     ----          ----
               MY       ----          ----          ----          ----       0.000000E+00     ----
               MZ       ----          ----          ----          ----          ----       0.000000E+00
             TOTALS -3.900000E+03 -4.500000E+03  0.000000E+00  0.000000E+00  0.000000E+00 -9.216000E+05
0       20     FX    0.000000E+00     ----          ----          ----       0.000000E+00  0.000000E+00
               FY       ----      -1.818989E-12     ----       0.000000E+00     ----       9.313226E-10
               FZ       ----          ----       0.000000E+00  0.000000E+00  0.000000E+00     ----
               MX       ----          ----          ----       0.000000E+00     ----          ----
               MY       ----          ----          ----          ----       0.000000E+00     ----
               MZ       ----          ----          ----          ----          ----       0.000000E+00
             TOTALS  0.000000E+00 -1.818989E-12  0.000000E+00  0.000000E+00  0.000000E+00  9.313226E-10
0       30     FX    0.000000E+00     ----          ----          ----       0.000000E+00  0.000000E+00
               FY       ----      -2.123938E+03     ----       0.000000E+00     ----      -6.116941E+05
               FZ       ----          ----       0.000000E+00  0.000000E+00  0.000000E+00     ----
               MX       ----          ----          ----       0.000000E+00     ----          ----
               MY       ----          ----          ----          ----       0.000000E+00     ----
               MZ       ----          ----          ----          ----          ----       0.000000E+00
             TOTALS  0.000000E+00 -2.123938E+03  0.000000E+00  0.000000E+00  0.000000E+00 -6.116941E+05
RESULTANTS ABOUT ORIGIN OF SUPERELEMENT BASIC COORDINATE SYSTEM IN SUPERELEMENT BASIC SYSTEM COORDINATES.

0                                                  SPCFORCE RESULTANT
  SUBCASE/    LOAD
  DAREA ID    TYPE       T1            T2            T3            R1            R2            R3
0        1     FX    3.900000E+03     ----          ----          ----       0.000000E+00  0.000000E+00
               FY       ----       4.500000E+03     ----       0.000000E+00     ----       9.216000E+05
               FZ       ----          ----       0.000000E+00  0.000000E+00  0.000000E+00     ----
               MX       ----          ----          ----       0.000000E+00     ----          ----
               MY       ----          ----          ----          ----       0.000000E+00     ----
               MZ       ----          ----          ----          ----          ----       0.000000E+00
             TOTALS  3.900000E+03  4.500000E+03  0.000000E+00  0.000000E+00  0.000000E+00  9.216000E+05
0       20     FX    0.000000E+00     ----          ----          ----       0.000000E+00  0.000000E+00
               FY       ----       7.275958E-12     ----       0.000000E+00     ----       2.095476E-09
               FZ       ----          ----       0.000000E+00  0.000000E+00  0.000000E+00     ----
               MX       ----          ----          ----       0.000000E+00     ----          ----
               MY       ----          ----          ----          ----       0.000000E+00     ----
               MZ       ----          ----          ----          ----          ----       0.000000E+00
             TOTALS  0.000000E+00  7.275958E-12  0.000000E+00  0.000000E+00  0.000000E+00  2.095476E-09
0       30     FX   -3.410605E-12     ----          ----          ----       0.000000E+00  0.000000E+00
               FY       ----       2.123938E+03     ----       0.000000E+00     ----       6.116941E+05
               FZ       ----          ----       0.000000E+00  0.000000E+00  0.000000E+00     ----
               MX       ----          ----          ----       0.000000E+00     ----          ----
               MY       ----          ----          ----          ----       0.000000E+00     ----
               MZ       ----          ----          ----          ----          ----       0.000000E+00
             TOTALS -3.410605E-12  2.123938E+03  0.000000E+00  0.000000E+00  0.000000E+00  6.116941E+05
RESULTANTS ABOUT ORIGIN OF SUPERELEMENT BASIC COORDINATE SYSTEM IN SUPERELEMENT BASIC SYSTEM COORDINATES.

0                                                  SPCFORCE RESULTANT
  SUBCASE/    LOAD
  DAREA ID    TYPE       T1            T2            T3            R1            R2            R3
0        1     FX    3.900000E+03     ----          ----          ----       0.000000E+00  0.000000E+00
               FY       ----       4.500000E+03     ----       0.000000E+00     ----       9.216000E+05
               FZ       ----          ----       0.000000E+00  0.000000E+00  0.000000E+00     ----
               MX       ----          ----          ----       0.000000E+00     ----          ----
               MY       ----          ----          ----          ----       0.000000E+00     ----
               MZ       ----          ----          ----          ----          ----       0.000000E+00
             TOTALS  3.900000E+03  4.500000E+03  0.000000E+00  0.000000E+00  0.000000E+00  9.216000E+05
0       20     FX    0.000000E+00     ----          ----          ----       0.000000E+00  0.000000E+00
               FY       ----       7.275958E-12     ----       0.000000E+00     ----       2.095476E-09
               FZ       ----          ----       0.000000E+00  0.000000E+00  0.000000E+00     ----
               MX       ----          ----          ----       0.000000E+00     ----          ----
               MY       ----          ----          ----          ----       0.000000E+00     ----
               MZ       ----          ----          ----          ----          ----       0.000000E+00
             TOTALS  0.000000E+00  7.275958E-12  0.000000E+00  0.000000E+00  0.000000E+00  2.095476E-09
0       30     FX   -3.410605E-12     ----          ----          ----       0.000000E+00  0.000000E+00
               FY       ----       2.123938E+03     ----       0.000000E+00     ----       6.116941E+05
               FZ       ----          ----       0.000000E+00  0.000000E+00  0.000000E+00     ----
               MX       ----          ----          ----       0.000000E+00     ----          ----
               MY       ----          ----          ----          ----       0.000000E+00     ----
               MZ       ----          ----          ----          ----          ----       0.000000E+00
             TOTALS -3.410605E-12  2.123938E+03  0.000000E+00  0.000000E+00  0.000000E+00  6.116941E+05
*** USER INFORMATION MESSAGE 5293 (SSG3A)
    FOR DATA BLOCK KLL
    LOAD SEQ. NO.             EPSILON              EXTERNAL WORK      EPSILONS LARGER THAN 0.001 ARE FLAGGED WITH ASTERISKS
                1                      -1.3760919E-13          3.6560133E+04

146
145
-1.0*Ux145 + 1.0*Ux146 = 0.0
-1.0*Uy145 + 1.0*Uy146 = 0.0
Bulk Data
Case Control
RSSCON,110,GRID,46,101,102,47,108,109
46
101
47
102
109
108
ALPHA
CMB
CMA
CNB
CNA
GB
GA
EID
RBAR
ALPHA
CMB
GB
GA
EID
RBAR1
ALPHA
CMC
CMB
GC
GB
GA
EID
RTRPLT1

ALPHA
CMB
CMA
GB
GA
EID
RROD
CB
GB
GA
EID
RJOINT
GEOMCHECK
= A/4
Ai
A/2
H
D1
D2
Q4_IAMIN
Q4_IAMAX
T3_SKEW
T3_IAMAX
ELmax
ELmin
ELmax
ELmin
ELmax
ELmin
a                    b
L1
L2
45o
                                        M O D E L   S U M M A R Y

                                   NUMBER OF GRID     POINTS   =      102

                                   NUMBER OF CQUAD4   ELEMENTS =       80

 *** USER INFORMATION MESSAGE 7555 (GMTSTD)
     FINITE ELEMENT GEOMETRY CHECK RESULTS EXCEED TOLERANCE LEVELS FOR THE FOLLOWING ELEMENTS.  METRIC VALUES THAT EXCEED
     TEST TOLERANCE LIMITS ARE IDENTIFIED BY ONE OF THE FOLLOWING FLAGS PLACED TO THE RIGHT OF THE METRIC VALUE.
        "++++" FOR TEST RESULTS EXCEEDING TOLERANCES.  INFORMATIONAL ONLY.  PROBLEM SOLUTION CONTINUES.  (DEFAULT FLAG)
        "IGNR" FOR TEST RESULTS EXCEEDING TOLERANCES.  INFORMATIONAL ONLY.  PROBLEM SOLUTION CONTINUES.
        "WARN" FOR TEST RESULTS EXCEEDING TOLERANCES.  INFORMATIONAL ONLY.  PROBLEM SOLUTION CONTINUES.
        "FAIL" FOR TEST RESULTS EXCEEDING TOLERANCES.  SEVERE ERROR.        PROBLEM SOLUTION TERMINATES.
     USER ACTION: USE THE GEOMCHECK (EXECUTIVE CONTROL STATEMENT) KEYWORD=VALUE TO CHANGE TOLERANCE VALUES IF DESIRED.
     A MAXIMUM OF          5 SKEW ANGLE (SA)       TOLERANCE LIMIT VIOLATIONS WILL BE IDENTIFIED BY THE FLAG "++++"
                             PLACED AFTER THE VALUE METRIC FOR THE TEST.
     A MAXIMUM OF        100 MIN INT. ANGLE (IA)   TOLERANCE LIMIT VIOLATIONS WILL BE IDENTIFIED BY THE FLAG "++++"
                             PLACED AFTER THE VALUE METRIC FOR THE TEST.
     A MAXIMUM OF        100 MAX INT. ANGLE (IA)   TOLERANCE LIMIT VIOLATIONS WILL BE IDENTIFIED BY THE FLAG "++++"
                             PLACED AFTER THE VALUE METRIC FOR THE TEST.
     A MAXIMUM OF        100 WARPING FACTOR (WF)   TOLERANCE LIMIT VIOLATIONS WILL BE IDENTIFIED BY THE FLAG "++++"
                             PLACED AFTER THE VALUE METRIC FOR THE TEST.
     A MAXIMUM OF        100 TAPER RATIO (TR)      TOLERANCE LIMIT VIOLATIONS WILL BE IDENTIFIED BY THE FLAG "++++"
                             PLACED AFTER THE VALUE METRIC FOR THE TEST.
     USER INFORMATION: THE MAXIMUM MESSAGE COUNT FOR ANY ONE ELEMENT ERROR TEST COULD BE EXCEEDED BY THE
     CUMULATIVE EFFECT OF ALL THE MESSAGES GENERATED FOR ALL OF THE DIFFERENT TESTS PERFORMED.
1    MSC.NASTRAN JOB CREATED ON 28-JUL-05 AT 11:18:00                          JULY  28, 2005  MSC.NASTRAN  9/23/04   PAGE     4

0
     TOLERANCE LIMITS ARE:  SA =  60.00, IA(MIN) =  30.00, IA(MAX) = 150.00, WF =   0.05, TR =   0.50 (FLAG = LIMIT VIOLATED)
 ELEMENT TYPE    ID          SKEW ANGLE      MIN INT. ANGLE    MAX INT. ANGLE    WARPING FACTOR      TAPER RATIO
    QUAD4           1        45.00 IGNR        45.00            135.00              0.00              0.00
    QUAD4           2        45.00 IGNR        45.00            135.00              0.00              0.00
    QUAD4           3        45.00 IGNR        45.00            135.00              0.00              0.00
    QUAD4           4        45.00 IGNR        45.00            135.00              0.00              0.00
    QUAD4           5        45.00 IGNR        45.00            135.00              0.00              0.00
1    MSC.NASTRAN JOB CREATED ON 28-JUL-05 AT 11:18:00                          JULY  28, 2005  MSC.NASTRAN  9/23/04   PAGE     5

0

                            E L E M E N T   G E O M E T R Y   T E S T   R E S U L T S   S U M M A R Y
                                        TOTAL NUMBER OF TIMES TOLERANCES WERE EXCEEDED
                                  ASPECT/       MINIMUM       MAXIMUM     SURFACE/FACE                 EDGE POINT     JACOBIAN
     ELEMENT TYPE  SKEW ANGLE    TAPER RATIO  INTER. ANGLE  INTER. ANGLE   WARP FACTOR  OFFSET RATIO  LENGTH RATIO  DETERMINANT
         QUAD4          80             0             0             0             0           N/A           N/A           N/A

         N/A IN THE ABOVE TABLE INDICATES TESTS THAT ARE NOT APPLICABLE TO THE ELEMENT TYPE AND WERE NOT PERFORMED.
         FOR ALL ELEMENTS WHERE GEOMETRY TEST RESULTS HAVE EXCEEDED TOLERANCES,

         QUAD4    ELEMENT ID        1 PRODUCED SMALLEST SKEW ANGLE       OF      45.00 (TOLERANCE =       60.00).
1    MSC.NASTRAN JOB CREATED ON 28-JUL-05 AT 11:18:00                          JULY  28, 2005  MSC.NASTRAN  9/23/04   PAGE     4

0
     TOLERANCE LIMITS ARE:  SA =  60.00, IA(MIN) =  30.00, IA(MAX) = 150.00, WF =   0.05, TR =   0.50 (FLAG = LIMIT VIOLATED)
 ELEMENT TYPE    ID          SKEW ANGLE      MIN INT. ANGLE    MAX INT. ANGLE    WARPING FACTOR      TAPER RATIO
    QUAD4           1        45.00 WARN        45.00            135.00              0.00              0.00
    QUAD4           2        45.00 WARN        45.00            135.00              0.00              0.00
    QUAD4           3        45.00 WARN        45.00            135.00              0.00              0.00
    QUAD4           4        45.00 WARN        45.00            135.00              0.00              0.00
    QUAD4           5        45.00 WARN        45.00            135.00              0.00              0.00
1    MSC.NASTRAN JOB CREATED ON 28-JUL-05 AT 11:18:00                          JULY  28, 2005  MSC.NASTRAN  9/23/04   PAGE     5

0

                            E L E M E N T   G E O M E T R Y   T E S T   R E S U L T S   S U M M A R Y
                                        TOTAL NUMBER OF TIMES TOLERANCES WERE EXCEEDED
                                  ASPECT/       MINIMUM       MAXIMUM     SURFACE/FACE                 EDGE POINT     JACOBIAN
     ELEMENT TYPE  SKEW ANGLE    TAPER RATIO  INTER. ANGLE  INTER. ANGLE   WARP FACTOR  OFFSET RATIO  LENGTH RATIO  DETERMINANT
         QUAD4          80             0             0             0             0           N/A           N/A           N/A

         N/A IN THE ABOVE TABLE INDICATES TESTS THAT ARE NOT APPLICABLE TO THE ELEMENT TYPE AND WERE NOT PERFORMED.
         FOR ALL ELEMENTS WHERE GEOMETRY TEST RESULTS HAVE EXCEEDED TOLERANCES,

         QUAD4    ELEMENT ID        1 PRODUCED SMALLEST SKEW ANGLE       OF      45.00 (TOLERANCE =       60.00).
1    MSC.NASTRAN JOB CREATED ON 28-JUL-05 AT 11:18:00                          JULY  28, 2005  MSC.NASTRAN  9/23/04   PAGE     4

0
     TOLERANCE LIMITS ARE:  SA =  60.00, IA(MIN) =  30.00, IA(MAX) = 150.00, WF =   0.05, TR =   0.50 (FLAG = LIMIT VIOLATED)
 ELEMENT TYPE    ID          SKEW ANGLE      MIN INT. ANGLE    MAX INT. ANGLE    WARPING FACTOR      TAPER RATIO
    QUAD4           1        45.00 FAIL        45.00            135.00              0.00              0.00
    QUAD4           2        45.00 FAIL        45.00            135.00              0.00              0.00
    QUAD4           3        45.00 FAIL        45.00            135.00              0.00              0.00
    QUAD4           4        45.00 FAIL        45.00            135.00              0.00              0.00
    QUAD4           5        45.00 FAIL        45.00            135.00              0.00              0.00
1    MSC.NASTRAN JOB CREATED ON 28-JUL-05 AT 11:18:00                          JULY  28, 2005  MSC.NASTRAN  9/23/04   PAGE     5

0

                            E L E M E N T   G E O M E T R Y   T E S T   R E S U L T S   S U M M A R Y
                                        TOTAL NUMBER OF TIMES TOLERANCES WERE EXCEEDED
                                  ASPECT/       MINIMUM       MAXIMUM     SURFACE/FACE                 EDGE POINT     JACOBIAN
     ELEMENT TYPE  SKEW ANGLE    TAPER RATIO  INTER. ANGLE  INTER. ANGLE   WARP FACTOR  OFFSET RATIO  LENGTH RATIO  DETERMINANT
         QUAD4          80             0             0             0             0           N/A           N/A           N/A

         N/A IN THE ABOVE TABLE INDICATES TESTS THAT ARE NOT APPLICABLE TO THE ELEMENT TYPE AND WERE NOT PERFORMED.
         FOR ALL ELEMENTS WHERE GEOMETRY TEST RESULTS HAVE EXCEEDED TOLERANCES,

         QUAD4    ELEMENT ID        1 PRODUCED SMALLEST SKEW ANGLE       OF      45.00 (TOLERANCE =       60.00).
1    MSC.NASTRAN JOB CREATED ON 28-JUL-05 AT 11:18:00                          JULY  28, 2005  MSC.NASTRAN  9/23/04   PAGE     6

0
 *** USER FATAL MESSAGE 7555 (EMGPRO)
     EMG MODULE TERMINATING DUE TO SEVERE FAILURE OF ELEMENT GEOMETRY CHECK TESTS.  THE ELEMENT TYPES, ELEMENT IDS AND FAILING
     TESTS ARE IDENTIFIED ON PREVIOUS PAGES WITH THE FLAG "FAIL" PLACED AFTER THE VALUE METRIC OF THE TEST THAT FAILED.
 ^^^ USER   WARNING MESSAGE 9031 (ERRPH1)
 ^^^ NOGO ENCOUNTERED IN SUBDMAP    SEMG
SUBCASE 1    +   SUBCASE 2       =       SUBCOM 3
A
C
+
=
B
C
-
=
B
A
C
AUTOSPC

AUTOSPC
section5_1.bdf
section5_1.bdf

 G R I D   P O I N T   S I N G U L A R I T Y   T A B L E
0                             POINT    TYPE   FAILED      STIFFNESS       OLD USET           NEW USET
                               ID            DIRECTION      RATIO     EXCLUSIVE  UNION   EXCLUSIVE  UNION
                                1        G      4         0.00E+00          BF       F         SB       S    *
                                1        G      5         0.00E+00          BF       F         SB       S    *
                                1        G      6         0.00E+00          BF       F         SB       S    *
                                2        G      4         0.00E+00          BF       F         SB       S    *
                                2        G      5         0.00E+00          BF       F         SB       S    *
                                2        G      6         0.00E+00          BF       F         SB       S    *
                                3        G      4         0.00E+00          BF       F         SB       S    *
                                3        G      5         0.00E+00          BF       F         SB       S    *
                                3        G      6         0.00E+00          BF       F         SB       S    *

section5_3.bdf
section5_3.bdf
section5_3.bdf

THE FOLLOWING DEGREES OF FREEDOM HAVE FACTOR DIAGONAL RATIOS GREATER THAN
      1.00000E+07 OR HAVE NEGATIVE TERMS ON THE FACTOR DIAGONAL.
0                                                                                SUBCASE 1
0
         GRID POINT ID       DEGREE OF FREEDOM   MATRIX/FACTOR DIAGONAL RATIO        MATRIX DIAGONAL

              13                                      R2                                           1.71146E+13                                       2.13419E+02
 ^^^ USER   FATAL   MESSAGE 9050 (SEKRRS)
 ^^^ RUN TERMINATED DUE TO EXCESSIVE PIVOT RATIOS IN MATRIX KLL.
 ^^^ USER ACTION:  CONSTRAIN MECHANISMS WITH SPCI OR SUPORTI ENTRIES OR SPECIFY PARAM,BAILOUT,-1 TO  CONTINUE THE RUN WITH MECHANISMS.

$        SID    GRID  DOF  A1    GRID  DOF   A2
MPC      1       145     1      -1.      146     1       1.
MPC      1       145     2      -1.      146     2       1.

RSSCON
ELSUM
$ file maxmin.dat
sol 101
cend
title = cantilever beam model
subtitle = OLOAD OUTPUT
spc = 1
disp=all
maxmin(vmag=2,disp,spcf)=all
subcase 1
label = pload1
load = 1
subcase 2
label = load in x, y, and z
load = 2
begin bulk
pload1,1,1,fy,fr,0.,1.,1.,1.
=,=,*(1),==
=(6)
force,2,9,,1.,1.,1.,1.
PARAM   GRDPNT  0
PARAM   POST    -1
$
cord2r,1,,0.,0.,0.,0.,1.,0.
,1.,0.,1.
GRID    1       0       0.0     0.0     0.0     0
GRID    2       0       12.5    0.0     0.0     0
GRID    3       0       25.     0.0     0.0     0
GRID    4       0       37.5    0.0     0.0     0
GRID    5       0       50.     0.0     0.0     0
GRID    6       0       62.5    0.0     0.0     0
GRID    7       0       75.     0.0     0.0     0
GRID    8       0       87.5    0.0     0.0     0
GRID    9       0       100.    0.0     0.0     1
$
CBEAM   1       1       1       2               1.
CBEAM   2       1       2       3               1.
CBEAM   3       1       3       4               1.
CBEAM   4       1       4       5               1.
CBEAM   5       1       5       6               1.
CBEAM   6       1       6       7               1.
CBEAM   7       1       7       8               1.
CBEAM   8       1       8       9               1.
$
SPC     1       1       123456  0.0
$
PBEAML  1       1               BAR
        1.      2.
$
MAT1    1       1.+7            .3      .1
$
ENDDATA
0          *** T1 ***   D I S P L A C E M E N T   M A X / M I N   V A L U E   S U M M A R Y          RESULTS FOR SUBCASE       1
  MAXMIN OPTIONS: SET=ALL, CID=BASIC, VMAG=2, VMAG=2, COMP=T1
  POINT ID. TYPE   CID          ***TMAG***           T2               T3               R1               R2               R3
        1     G   BASIC        0.000000E+00     0.000000E+00     0.000000E+00     0.000000E+00     0.000000E+00     0.000000E+00
        2     G   BASIC        5.404634E-02     0.000000E+00     0.000000E+00     8.251953E-03     0.000000E+00     0.000000E+00
        8     G   BASIC        1.563420E+00     0.000000E+00     0.000000E+00     2.495117E-02     0.000000E+00     0.000000E+00
        9     G   BASIC        1.875780E+00     0.000000E+00     0.000000E+00     2.500000E-02     0.000000E+00     0.000000E+00
        9     G        1       0.000000E+00     0.000000E+00     1.875780E+00     1.767767E-02    -1.767767E-02     0.000000E+00

1    CANTILEVER BEAM MODEL                                                 FEBRUARY  13, 2001  MSC.NASTRAN  1/17/01   PAGE    12
      OLOAD OUTPUT
0

0          *** R1 ***   D I S P L A C E M E N T   M A X / M I N   V A L U E   S U M M A R Y          RESULTS FOR SUBCASE       1
  MAXMIN OPTIONS: SET=ALL, CID=BASIC, VMAG=2, VMAG=2, COMP=R1
  POINT ID. TYPE   CID              T1               T2               T3           ***RMAG***           R2               R3
        1     G   BASIC        0.000000E+00     0.000000E+00     0.000000E+00     0.000000E+00     0.000000E+00     0.000000E+00
        2     G   BASIC        5.404634E-02     0.000000E+00     0.000000E+00     8.251953E-03     0.000000E+00     0.000000E+00
        8     G   BASIC        1.563420E+00     0.000000E+00     0.000000E+00     2.495117E-02     0.000000E+00     0.000000E+00
        9     G   BASIC        1.875780E+00     0.000000E+00     0.000000E+00     2.500000E-02     0.000000E+00     0.000000E+00
        9     G        1       0.000000E+00     0.000000E+00     1.875780E+00     1.767767E-02    -1.767767E-02     0.000000E+00
GEOMCHECK

1    MSC.NASTRAN JOB CREATED ON 28-JUL-05 AT 11:18:00                          JULY  28, 2005  MSC.NASTRAN  9/23/04   PAGE     4

0
     TOLERANCE LIMITS ARE:  SA =  60.00, IA(MIN) =  30.00, IA(MAX) = 150.00, WF =   0.05, TR =   0.50 (FLAG = LIMIT VIOLATED)
 ELEMENT TYPE    ID          SKEW ANGLE      MIN INT. ANGLE    MAX INT. ANGLE    WARPING FACTOR      TAPER RATIO
    QUAD4           1        45.00 ++++        45.00            135.00              0.00              0.00
    QUAD4           2        45.00 ++++        45.00            135.00              0.00              0.00
    QUAD4           3        45.00 ++++        45.00            135.00              0.00              0.00
    QUAD4           4        45.00 ++++        45.00            135.00              0.00              0.00
    QUAD4           5        45.00 ++++        45.00            135.00              0.00              0.00
1    MSC.NASTRAN JOB CREATED ON 28-JUL-05 AT 11:18:00                          JULY  28, 2005  MSC.NASTRAN  9/23/04   PAGE     5

0

                            E L E M E N T   G E O M E T R Y   T E S T   R E S U L T S   S U M M A R Y
                                        TOTAL NUMBER OF TIMES TOLERANCES WERE EXCEEDED
                                  ASPECT/       MINIMUM       MAXIMUM     SURFACE/FACE                 EDGE POINT     JACOBIAN
     ELEMENT TYPE  SKEW ANGLE    TAPER RATIO  INTER. ANGLE  INTER. ANGLE   WARP FACTOR  OFFSET RATIO  LENGTH RATIO  DETERMINANT
         QUAD4          80             0             0             0             0           N/A           N/A           N/A

         N/A IN THE ABOVE TABLE INDICATES TESTS THAT ARE NOT APPLICABLE TO THE ELEMENT TYPE AND WERE NOT PERFORMED.
         FOR ALL ELEMENTS WHERE GEOMETRY TEST RESULTS HAVE EXCEEDED TOLERANCES,

         QUAD4    ELEMENT ID        1 PRODUCED SMALLEST SKEW ANGLE       OF      45.00 (TOLERANCE =       60.00).
MAT1    1       3.E+7           0.3$FORCE   1       2               2500.   0.0     -1.0    0.0$SPC1    1       156     3SPC1    2       2       3$ENDDATA
AUTOSPC

AUTOSPC
section5_1.bdf
section5_1.bdf

 G R I D   P O I N T   S I N G U L A R I T Y   T A B L E
0                             POINT    TYPE   FAILED      STIFFNESS       OLD USET           NEW USET
                               ID            DIRECTION      RATIO     EXCLUSIVE  UNION   EXCLUSIVE  UNION
                                1        G      4         0.00E+00          BF       F         SB       S    *
                                1        G      5         0.00E+00          BF       F         SB       S    *
                                1        G      6         0.00E+00          BF       F         SB       S    *
                                2        G      4         0.00E+00          BF       F         SB       S    *
                                2        G      5         0.00E+00          BF       F         SB       S    *
                                2        G      6         0.00E+00          BF       F         SB       S    *
                                3        G      4         0.00E+00          BF       F         SB       S    *
                                3        G      5         0.00E+00          BF       F         SB       S    *
                                3        G      6         0.00E+00          BF       F         SB       S    *

section5_3.bdf
section5_3.bdf
section5_3.bdf

THE FOLLOWING DEGREES OF FREEDOM HAVE FACTOR DIAGONAL RATIOS GREATER THAN
      1.00000E+07 OR HAVE NEGATIVE TERMS ON THE FACTOR DIAGONAL.
0                                                                                SUBCASE 1
0
         GRID POINT ID       DEGREE OF FREEDOM   MATRIX/FACTOR DIAGONAL RATIO        MATRIX DIAGONAL

              13                                      R2                                           1.71146E+13                                       2.13419E+02
 ^^^ USER   FATAL   MESSAGE 9050 (SEKRRS)
 ^^^ RUN TERMINATED DUE TO EXCESSIVE PIVOT RATIOS IN MATRIX KLL.
 ^^^ USER ACTION:  CONSTRAIN MECHANISMS WITH SPCI OR SUPORTI ENTRIES OR SPECIFY PARAM,BAILOUT,-1 TO  CONTINUE THE RUN WITH MECHANISMS.

$        SID    GRID  DOF  A1    GRID  DOF   A2
MPC      1       145     1      -1.      146     1       1.
MPC      1       145     2      -1.      146     2       1.

RSSCON
ELSUM
$ file maxmin.dat
sol 101
cend
title = cantilever beam model
subtitle = OLOAD OUTPUT
spc = 1
disp=all
maxmin(vmag=2,disp,spcf)=all
subcase 1
label = pload1
load = 1
subcase 2
label = load in x, y, and z
load = 2
begin bulk
pload1,1,1,fy,fr,0.,1.,1.,1.
=,=,*(1),==
=(6)
force,2,9,,1.,1.,1.,1.
PARAM   GRDPNT  0
PARAM   POST    -1
$
cord2r,1,,0.,0.,0.,0.,1.,0.
,1.,0.,1.
GRID    1       0       0.0     0.0     0.0     0
GRID    2       0       12.5    0.0     0.0     0
GRID    3       0       25.     0.0     0.0     0
GRID    4       0       37.5    0.0     0.0     0
GRID    5       0       50.     0.0     0.0     0
GRID    6       0       62.5    0.0     0.0     0
GRID    7       0       75.     0.0     0.0     0
GRID    8       0       87.5    0.0     0.0     0
GRID    9       0       100.    0.0     0.0     1
$
CBEAM   1       1       1       2               1.
CBEAM   2       1       2       3               1.
CBEAM   3       1       3       4               1.
CBEAM   4       1       4       5               1.
CBEAM   5       1       5       6               1.
CBEAM   6       1       6       7               1.
CBEAM   7       1       7       8               1.
CBEAM   8       1       8       9               1.
$
SPC     1       1       123456  0.0
$
PBEAML  1       1               BAR
        1.      2.
$
MAT1    1       1.+7            .3      .1
$
ENDDATA
0          *** T1 ***   D I S P L A C E M E N T   M A X / M I N   V A L U E   S U M M A R Y          RESULTS FOR SUBCASE       1
  MAXMIN OPTIONS: SET=ALL, CID=BASIC, VMAG=2, VMAG=2, COMP=T1
  POINT ID. TYPE   CID          ***TMAG***           T2               T3               R1               R2               R3
        1     G   BASIC        0.000000E+00     0.000000E+00     0.000000E+00     0.000000E+00     0.000000E+00     0.000000E+00
        2     G   BASIC        5.404634E-02     0.000000E+00     0.000000E+00     8.251953E-03     0.000000E+00     0.000000E+00
        8     G   BASIC        1.563420E+00     0.000000E+00     0.000000E+00     2.495117E-02     0.000000E+00     0.000000E+00
        9     G   BASIC        1.875780E+00     0.000000E+00     0.000000E+00     2.500000E-02     0.000000E+00     0.000000E+00
        9     G        1       0.000000E+00     0.000000E+00     1.875780E+00     1.767767E-02    -1.767767E-02     0.000000E+00

1    CANTILEVER BEAM MODEL                                                 FEBRUARY  13, 2001  MSC.NASTRAN  1/17/01   PAGE    12
      OLOAD OUTPUT
0

0          *** R1 ***   D I S P L A C E M E N T   M A X / M I N   V A L U E   S U M M A R Y          RESULTS FOR SUBCASE       1
  MAXMIN OPTIONS: SET=ALL, CID=BASIC, VMAG=2, VMAG=2, COMP=R1
  POINT ID. TYPE   CID              T1               T2               T3           ***RMAG***           R2               R3
        1     G   BASIC        0.000000E+00     0.000000E+00     0.000000E+00     0.000000E+00     0.000000E+00     0.000000E+00
        2     G   BASIC        5.404634E-02     0.000000E+00     0.000000E+00     8.251953E-03     0.000000E+00     0.000000E+00
        8     G   BASIC        1.563420E+00     0.000000E+00     0.000000E+00     2.495117E-02     0.000000E+00     0.000000E+00
        9     G   BASIC        1.875780E+00     0.000000E+00     0.000000E+00     2.500000E-02     0.000000E+00     0.000000E+00
        9     G        1       0.000000E+00     0.000000E+00     1.875780E+00     1.767767E-02    -1.767767E-02     0.000000E+00
GEOMCHECK

1    MSC.NASTRAN JOB CREATED ON 28-JUL-05 AT 11:18:00                          JULY  28, 2005  MSC.NASTRAN  9/23/04   PAGE     4

0
     TOLERANCE LIMITS ARE:  SA =  60.00, IA(MIN) =  30.00, IA(MAX) = 150.00, WF =   0.05, TR =   0.50 (FLAG = LIMIT VIOLATED)
 ELEMENT TYPE    ID          SKEW ANGLE      MIN INT. ANGLE    MAX INT. ANGLE    WARPING FACTOR      TAPER RATIO
    QUAD4           1        45.00 ++++        45.00            135.00              0.00              0.00
    QUAD4           2        45.00 ++++        45.00            135.00              0.00              0.00
    QUAD4           3        45.00 ++++        45.00            135.00              0.00              0.00
    QUAD4           4        45.00 ++++        45.00            135.00              0.00              0.00
    QUAD4           5        45.00 ++++        45.00            135.00              0.00              0.00
1    MSC.NASTRAN JOB CREATED ON 28-JUL-05 AT 11:18:00                          JULY  28, 2005  MSC.NASTRAN  9/23/04   PAGE     5

0

                            E L E M E N T   G E O M E T R Y   T E S T   R E S U L T S   S U M M A R Y
                                        TOTAL NUMBER OF TIMES TOLERANCES WERE EXCEEDED
                                  ASPECT/       MINIMUM       MAXIMUM     SURFACE/FACE                 EDGE POINT     JACOBIAN
     ELEMENT TYPE  SKEW ANGLE    TAPER RATIO  INTER. ANGLE  INTER. ANGLE   WARP FACTOR  OFFSET RATIO  LENGTH RATIO  DETERMINANT
         QUAD4          80             0             0             0             0           N/A           N/A           N/A

         N/A IN THE ABOVE TABLE INDICATES TESTS THAT ARE NOT APPLICABLE TO THE ELEMENT TYPE AND WERE NOT PERFORMED.
         FOR ALL ELEMENTS WHERE GEOMETRY TEST RESULTS HAVE EXCEEDED TOLERANCES,

         QUAD4    ELEMENT ID        1 PRODUCED SMALLEST SKEW ANGLE       OF      45.00 (TOLERANCE =       60.00).
MAT1    1       3.E+7           0.3$FORCE   1       2               2500.   0.0     -1.0    0.0$SPC1    1       156     3SPC1    2       2       3$ENDDATA
AUTOSPC

AUTOSPC
section5_1.bdf
section5_1.bdf

 G R I D   P O I N T   S I N G U L A R I T Y   T A B L E
0                             POINT    TYPE   FAILED      STIFFNESS       OLD USET           NEW USET
                               ID            DIRECTION      RATIO     EXCLUSIVE  UNION   EXCLUSIVE  UNION
                                1        G      4         0.00E+00          BF       F         SB       S    *
                                1        G      5         0.00E+00          BF       F         SB       S    *
                                1        G      6         0.00E+00          BF       F         SB       S    *
                                2        G      4         0.00E+00          BF       F         SB       S    *
                                2        G      5         0.00E+00          BF       F         SB       S    *
                                2        G      6         0.00E+00          BF       F         SB       S    *
                                3        G      4         0.00E+00          BF       F         SB       S    *
                                3        G      5         0.00E+00          BF       F         SB       S    *
                                3        G      6         0.00E+00          BF       F         SB       S    *

section5_3.bdf
section5_3.bdf
section5_3.bdf

THE FOLLOWING DEGREES OF FREEDOM HAVE FACTOR DIAGONAL RATIOS GREATER THAN
      1.00000E+07 OR HAVE NEGATIVE TERMS ON THE FACTOR DIAGONAL.
0                                                                                SUBCASE 1
0
         GRID POINT ID       DEGREE OF FREEDOM   MATRIX/FACTOR DIAGONAL RATIO        MATRIX DIAGONAL

              13                                      R2                                           1.71146E+13                                       2.13419E+02
 ^^^ USER   FATAL   MESSAGE 9050 (SEKRRS)
 ^^^ RUN TERMINATED DUE TO EXCESSIVE PIVOT RATIOS IN MATRIX KLL.
 ^^^ USER ACTION:  CONSTRAIN MECHANISMS WITH SPCI OR SUPORTI ENTRIES OR SPECIFY PARAM,BAILOUT,-1 TO  CONTINUE THE RUN WITH MECHANISMS.

$        SID    GRID  DOF  A1    GRID  DOF   A2
MPC      1       145     1      -1.      146     1       1.
MPC      1       145     2      -1.      146     2       1.

RSSCON
ELSUM
$ file maxmin.dat
sol 101
cend
title = cantilever beam model
subtitle = OLOAD OUTPUT
spc = 1
disp=all
maxmin(vmag=2,disp,spcf)=all
subcase 1
label = pload1
load = 1
subcase 2
label = load in x, y, and z
load = 2
begin bulk
pload1,1,1,fy,fr,0.,1.,1.,1.
=,=,*(1),==
=(6)
force,2,9,,1.,1.,1.,1.
PARAM   GRDPNT  0
PARAM   POST    -1
$
cord2r,1,,0.,0.,0.,0.,1.,0.
,1.,0.,1.
GRID    1       0       0.0     0.0     0.0     0
GRID    2       0       12.5    0.0     0.0     0
GRID    3       0       25.     0.0     0.0     0
GRID    4       0       37.5    0.0     0.0     0
GRID    5       0       50.     0.0     0.0     0
GRID    6       0       62.5    0.0     0.0     0
GRID    7       0       75.     0.0     0.0     0
GRID    8       0       87.5    0.0     0.0     0
GRID    9       0       100.    0.0     0.0     1
$
CBEAM   1       1       1       2               1.
CBEAM   2       1       2       3               1.
CBEAM   3       1       3       4               1.
CBEAM   4       1       4       5               1.
CBEAM   5       1       5       6               1.
CBEAM   6       1       6       7               1.
CBEAM   7       1       7       8               1.
CBEAM   8       1       8       9               1.
$
SPC     1       1       123456  0.0
$
PBEAML  1       1               BAR
        1.      2.
$
MAT1    1       1.+7            .3      .1
$
ENDDATA
0          *** T1 ***   D I S P L A C E M E N T   M A X / M I N   V A L U E   S U M M A R Y          RESULTS FOR SUBCASE       1
  MAXMIN OPTIONS: SET=ALL, CID=BASIC, VMAG=2, VMAG=2, COMP=T1
  POINT ID. TYPE   CID          ***TMAG***           T2               T3               R1               R2               R3
        1     G   BASIC        0.000000E+00     0.000000E+00     0.000000E+00     0.000000E+00     0.000000E+00     0.000000E+00
        2     G   BASIC        5.404634E-02     0.000000E+00     0.000000E+00     8.251953E-03     0.000000E+00     0.000000E+00
        8     G   BASIC        1.563420E+00     0.000000E+00     0.000000E+00     2.495117E-02     0.000000E+00     0.000000E+00
        9     G   BASIC        1.875780E+00     0.000000E+00     0.000000E+00     2.500000E-02     0.000000E+00     0.000000E+00
        9     G        1       0.000000E+00     0.000000E+00     1.875780E+00     1.767767E-02    -1.767767E-02     0.000000E+00

1    CANTILEVER BEAM MODEL                                                 FEBRUARY  13, 2001  MSC.NASTRAN  1/17/01   PAGE    12
      OLOAD OUTPUT
0

0          *** R1 ***   D I S P L A C E M E N T   M A X / M I N   V A L U E   S U M M A R Y          RESULTS FOR SUBCASE       1
  MAXMIN OPTIONS: SET=ALL, CID=BASIC, VMAG=2, VMAG=2, COMP=R1
  POINT ID. TYPE   CID              T1               T2               T3           ***RMAG***           R2               R3
        1     G   BASIC        0.000000E+00     0.000000E+00     0.000000E+00     0.000000E+00     0.000000E+00     0.000000E+00
        2     G   BASIC        5.404634E-02     0.000000E+00     0.000000E+00     8.251953E-03     0.000000E+00     0.000000E+00
        8     G   BASIC        1.563420E+00     0.000000E+00     0.000000E+00     2.495117E-02     0.000000E+00     0.000000E+00
        9     G   BASIC        1.875780E+00     0.000000E+00     0.000000E+00     2.500000E-02     0.000000E+00     0.000000E+00
        9     G        1       0.000000E+00     0.000000E+00     1.875780E+00     1.767767E-02    -1.767767E-02     0.000000E+00
GEOMCHECK

1    MSC.NASTRAN JOB CREATED ON 28-JUL-05 AT 11:18:00                          JULY  28, 2005  MSC.NASTRAN  9/23/04   PAGE     4

0
     TOLERANCE LIMITS ARE:  SA =  60.00, IA(MIN) =  30.00, IA(MAX) = 150.00, WF =   0.05, TR =   0.50 (FLAG = LIMIT VIOLATED)
 ELEMENT TYPE    ID          SKEW ANGLE      MIN INT. ANGLE    MAX INT. ANGLE    WARPING FACTOR      TAPER RATIO
    QUAD4           1        45.00 ++++        45.00            135.00              0.00              0.00
    QUAD4           2        45.00 ++++        45.00            135.00              0.00              0.00
    QUAD4           3        45.00 ++++        45.00            135.00              0.00              0.00
    QUAD4           4        45.00 ++++        45.00            135.00              0.00              0.00
    QUAD4           5        45.00 ++++        45.00            135.00              0.00              0.00
1    MSC.NASTRAN JOB CREATED ON 28-JUL-05 AT 11:18:00                          JULY  28, 2005  MSC.NASTRAN  9/23/04   PAGE     5

0

                            E L E M E N T   G E O M E T R Y   T E S T   R E S U L T S   S U M M A R Y
                                        TOTAL NUMBER OF TIMES TOLERANCES WERE EXCEEDED
                                  ASPECT/       MINIMUM       MAXIMUM     SURFACE/FACE                 EDGE POINT     JACOBIAN
     ELEMENT TYPE  SKEW ANGLE    TAPER RATIO  INTER. ANGLE  INTER. ANGLE   WARP FACTOR  OFFSET RATIO  LENGTH RATIO  DETERMINANT
         QUAD4          80             0             0             0             0           N/A           N/A           N/A

         N/A IN THE ABOVE TABLE INDICATES TESTS THAT ARE NOT APPLICABLE TO THE ELEMENT TYPE AND WERE NOT PERFORMED.
         FOR ALL ELEMENTS WHERE GEOMETRY TEST RESULTS HAVE EXCEEDED TOLERANCES,

         QUAD4    ELEMENT ID        1 PRODUCED SMALLEST SKEW ANGLE       OF      45.00 (TOLERANCE =       60.00).
MAT1    1       3.E+7           0.3$FORCE   1       2               2500.   0.0     -1.0    0.0$SPC1    1       156     3SPC1    2       2       3$ENDDATA
WARP = h / [0.5*(D1+D2)]
D1
D2