title: Презентация на тему: MSC.Nastran 102 2001 - 15

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ID SEMINAR, PROB12SOL 107TIME 5CENDTITLE= TWO-DOF MODEL (IMAC 8, PG 891)SUBTITLE= COMPLEX MODESDISPLACEMENT= ALL $ DEFAULT= REAL, IMAGINARYSPC= 100CMETHOD= 99$BEGIN BULK$$ COMPLEX EIGENVALUE EXTRACTION PARAMETERS$EIGC, 99, HESS, , , , , 4$$ DEFINE GRIDS, MASSES, AND STIFFNESSES$  GRID 1 = EXCITER (X=2, MASS=3)  50K STIFFNESS BETWEEN GRIDS 1 AND 2$  GRID 2 = PILE (X=1, MASS=3)   12.5K STIFFNESS BETWEEN GRIDS 2 AND 3$  GRID 3 = BASE (X=0, FIX BASE)$GRID, 1, , 2., 0., 0.GRID, 2, , 1., 0., 0.GRID, 3, , 0., 0., 0.GRDSET, , , , , , , 23456CELAS2, 1, 50000., 1, 1, 2, 1CELAS2, 2, 12500., 2, 1, 3, 1CONM2, 201, 1, , 3.0CONM2, 202, 2, , 1.5SPC, 100, 3, 1$$ DEFINE DAMPER OF 30 BETWEEN GRIDS 2 AND 3$CVISC, 101, 1, 2, 3PVISC, 1, 30.$ENDDATA
1    TWO-DOF MODEL (IMAC 8, PG 891)                                        NOVEMBER  13, 2001  MSC.NASTRAN  4/ 9/01   PAGE     6      COMPLEX MODES                                                                                0                                                                                C O M P L E X   E I G E N V A L U E   S U M M A R Y0                ROOT     EXTRACTION                  EIGENVALUE                     FREQUENCY              DAMPING                  NO.        ORDER             (REAL)           (IMAG)                (CYCLES)            COEFFICIENT                      1           2         -2.660969E+00    -4.983521E+01          7.931520E+00          1.067907E-01                      2           1         -2.660969E+00     4.983521E+01          7.931520E+00          1.067907E-01                      3           4         -7.339031E+00    -2.360312E+02          3.756553E+01          6.218695E-02                      4           3         -7.339031E+00     2.360312E+02          3.756553E+01          6.218695E-021    TWO-DOF MODEL (IMAC 8, PG 891)                                        NOVEMBER  13, 2001  MSC.NASTRAN  4/ 9/01   PAGE     7      COMPLEX MODES                                                                                0                                                                                1    TWO-DOF MODEL (IMAC 8, PG 891)                                        NOVEMBER  13, 2001  MSC.NASTRAN  4/ 9/01   PAGE     8      COMPLEX MODES                                                                                0                                                                                COMPLEX EIGENVALUE = -2.660969E+00, -4.983521E+01                                       C O M P L E X   E I G E N V E C T O R   NO.          1                                                          (REAL/IMAGINARY)       POINT ID.   TYPE          T1             T2             T3             R1             R2             R30            1      G      1.000000E+00   0.0            0.0            0.0            0.0            0.0                           0.0            0.0            0.0            0.0            0.0            0.00            2      G      8.514119E-01   0.0            0.0            0.0            0.0            0.0                           1.591320E-02   0.0            0.0            0.0            0.0            0.00            3      G      0.0            0.0            0.0            0.0            0.0            0.0                           0.0            0.0            0.0            0.0            0.0            0.01    TWO-DOF MODEL (IMAC 8, PG 891)                                        NOVEMBER  13, 2001  MSC.NASTRAN  4/ 9/01   PAGE     9      COMPLEX MODES                                                                                0                                                                                COMPLEX EIGENVALUE = -2.660969E+00,  4.983521E+01                                       C O M P L E X   E I G E N V E C T O R   NO.          2                                                          (REAL/IMAGINARY)       POINT ID.   TYPE          T1             T2             T3             R1             R2             R30            1      G      1.000000E+00   0.0            0.0            0.0            0.0            0.0                           0.0            0.0            0.0            0.0            0.0            0.00            2      G      8.514119E-01   0.0            0.0            0.0            0.0            0.0                          -1.591320E-02   0.0            0.0            0.0            0.0            0.00            3      G      0.0            0.0            0.0            0.0            0.0            0.0                           0.0            0.0            0.0            0.0            0.0            0.0
1    TWO-DOF MODEL (IMAC 8, PG 891)                                        NOVEMBER  13, 2001  MSC.NASTRAN  4/ 9/01   PAGE    10
      COMPLEX MODES
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                                       C O M P L E X   E I G E N V E C T O R   NO.          3
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      POINT ID.   TYPE          T1             T2             T3             R1             R2             R3
0            1      G     -4.241094E-01   0.0            0.0            0.0            0.0            0.0
                          -3.768431E-02   0.0            0.0            0.0            0.0            0.0
0            2      G      1.000000E+00   0.0            0.0            0.0            0.0            0.0
                           0.0            0.0            0.0            0.0            0.0            0.0
0            3      G      0.0            0.0            0.0            0.0            0.0            0.0
                           0.0            0.0            0.0            0.0            0.0            0.0
1    TWO-DOF MODEL (IMAC 8, PG 891)                                        NOVEMBER  13, 2001  MSC.NASTRAN  4/ 9/01   PAGE    11
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      COMPLEX EIGENVALUE = -7.339031E+00,  2.360312E+02
                                       C O M P L E X   E I G E N V E C T O R   NO.          4
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      POINT ID.   TYPE          T1             T2             T3             R1             R2             R3
0            1      G     -4.241094E-01   0.0            0.0            0.0            0.0            0.0
                           3.768431E-02   0.0            0.0            0.0            0.0            0.0
0            2      G      1.000000E+00   0.0            0.0            0.0            0.0            0.0
                           0.0            0.0            0.0            0.0            0.0            0.0
0            3      G      0.0            0.0            0.0            0.0            0.0            0.0
                           0.0            0.0            0.0            0.0            0.0            0.0
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title: Презентация на тему: MSC.Mvision Workshop 3

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MVI320, Workshop 3, August 2001
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The figure shows three major trends in the plot, the steel (the right point), the titanium alloy (the middle point) and the aluminum alloys (the left set of points).
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Now, close the cross plot window and exit MVISION.
a.	Click File/Close All Cross Plots.
b.	Clear all Search or Design Criteria by selecting Clear then Apply.
c.	Change the Choose a Material Set to Work With to List ALL Materials.
d.	Finally, exit MVISION by
	File/Exit MVISION.
e.	This ends the exercise.
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All settings for each open databank are saved when MVISION is exited. By clearing the Search Criteria and closing the Data Viewer, the next time you run MVISION and open this databank, all settings will be cleared.
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All settings for each open databank are saved when MVISION is exited. By clearing the Search Criteria and closing the Data Viewer, the next time you run MVISION and open this databank, all settings will be cleared.
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title: Презентация на тему: MSC.Nastran 102 2001 - 17

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ID NAS102, WORKSHOP13SOL 109TIME 100CEND TITLE= SIMPLE CAR MODEL WITH NOLINEARSUBTITLE= SPRINGS AND DAMPERS RUNNING OVER A BUMPLABEL= SOL 109, CONSTANT DELTA TIMESEALL= ALL SPC= 100TFL= 100NONLINEAR = 100DLOAD = 100TSTEP = 100DISPLACEMENT(PLOT)= ALLNLLOAD(PLOT)= ALL$OUTPUT(XYPLOT)CSCALE=1.3XAXIS= YESYAXIS= YESXGRID LINES= YESYGRID LINES= YESXTITLE= TIME (SEC)YTITLE= VERTICAL DISPLACEMENT OF POINT 1XYPLOT DISP/1(T2)YTITLE= VERTICAL DISPLACEMENT OF POINT 2XYPLOT DISP/2(T2)YTITLE= VERTICAL DISPLACEMENT OF POINT 3XYPLOT DISP/3(T2)
YTITLE= VERTICAL DISPLACEMENT OF POINT 4XYPLOT DISP/4(T2)YTITLE= VERTICAL DISPLACEMENT OF POINT 5XYPLOT DISP/5(T2)YTITLE= NONLINEAR FORCES AT POINT 1XYPLOT NONLINEAR/1(T2)YTITLE= NONLINEAR FORCES AT POINT 2XYPLOT NONLINEAR/2(T2)$BEGIN BULKPARAM,POST,-1$$ CARRIAGE POINTS$GRID, 1, , 0., 0., 0.GRID, 2, , 120., 0., 0.GRID, 5, , 60., 0., 0.$
$WHEEL POINTS$GRID, 3, , 0., -10., 0.GRID, 4, , 120., -10., 0.$$ CAR CARRIAGE$CBAR, 5, 11, 1, 5, 0., 1., 0.CBAR, 6, 11, 5, 2, 0., 1., 0.PBAR, 11, 12, 10., 10., 10.MAT1, 12, 3.0E+7, , .33$
$$ CONSTRAINTS TO ELIMINATE RIGID-BODY MODES$SPC1, 100, 1345, 1, 2, 5SPC1, 100, 13456, 3, 4$$ SYSTEM WILL HAVE A NATURAL FREQUENCY OF 1 HZ $ WITH CRITICAL DAMPING OF 1 PERCENT$CONM2, 10, 1, ,2.5CONM2, 15, 2, ,2.5CONM2, 20, 5, ,5.$CELAS2, 30, 197.4, 1, 2, 3, 2CELAS2, 40, 197.4, 2, 2, 4, 2$CDAMP2, 50, 1.88, 1, 2, 3, 2CDAMP2, 60, 1.88, 2, 2, 4, 2$$ DEFINE EXTRA POINTS TO HOLD DIFFERENCES$ BETWEEN WHEELS AND CARRIAGE$EPOINT, 101, 102$$ USE TRANSFER FUNCTIONS TO TRACK DIFFERENCES $ 101= V1 - V3$ 102= V2 - V4$TF, 100, 101, 0, 1., 0., 0., , 1, 2, -1., 0., 0., , 3, 2, 1., 0., 0.$TF, 100, 102, 0, 1., 0., 0., , 2, 2, -1., 0., 0., , 4, 2, 1., 0., 0.$$ ADD NONLINEAR PORTION OF SPRINGS$
NOLIN1, 100, 1, 2, 197.4, 101, 0, 111NOLIN1, 100, 2, 2, 197.4, 102, 0, 111TABLED2, 111, -2.0,, -1., 1., 0., 0., 1., 0.,ENDT$$ ADD NONLINEAR PORTION OF DAMPERS$NOLIN4, 100, 1, 2, -0.3, 101, 10, 2.NOLIN4, 100, 2, 2, -0.3, 102, 10, 2.$$ MOVE WHEELS OVER BUMP$TLOAD2, 100, 222, 333, D, 0., 0.5, 1., -90.SPCD, 222, 3, 2, 4.SPCD, 222, 4, 2, 4.SPC1,100,2,3,4
DELAY, 333, 4, 2, 1.2$$ INTEGRATION INFORMATIONTSTEP, 100, 200, .05, 1$ENDDATA
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  NONLIN    1        1(  4)      0.000000E+00   1.000002E+01   0.000000E+00   0.000000E+00   2.975151E+02   6.000001E-01                                          0.000000E+00   1.000002E+01   0.000000E+00   0.000000E+00   2.975151E+02   6.000001E-010       1  NONLIN    2        2(  4)      0.000000E+00   1.000002E+01   0.000000E+00   0.000000E+00   4.661460E+02   1.749999E+00                                          0.000000E+00   1.000002E+01   0.000000E+00   0.000000E+00   4.661460E+02   1.749999E+00                                                        .                                                        .                                                        .                                                        .                                                        .
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      3        1(  4)      0.000000E+00   1.000002E+01  -2.836541E+00   2.199999E+00   5.942877E+00   4.500000E-01                                          0.000000E+00   1.000002E+01  -2.836541E+00   2.199999E+00   5.942877E+00   4.500000E-010       1  DISP      4        2(  4)      0.000000E+00   1.000002E+01  -2.671688E+00   1.999999E+00   7.464219E+00   1.600000E+00                                          0.000000E+00   1.000002E+01  -2.671688E+00   1.999999E+00   7.464219E+00   1.600000E+000       1  DISP      5        3(  4)      0.000000E+00   1.000002E+01   0.000000E+00   0.000000E+00   4.000000E+00   2.500000E-01                                          0.000000E+00   1.000002E+01   0.000000E+00   0.000000E+00   4.000000E+00   2.500000E-010       1  DISP      6        4(  4)      0.000000E+00   1.000002E+01   0.000000E+00   0.000000E+00   4.000000E+00   1.450000E+00                                          0.000000E+00   1.000002E+01   0.000000E+00   0.000000E+00   4.000000E+00   1.450000E+000       1  DISP      7        5(  4)      0.000000E+00   1.000002E+01  -2.150819E+00   2.149999E+00   3.963917E+00   1.600000E+00                                          0.000000E+00   1.000002E+01  -2.150819E+00   2.149999E+00   3.963917E+00   1.600000E+00

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title: Презентация на тему: MSC.Nastran 102 2001 - 18

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Large Geometry Changes
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SOL 103TIME 600CENDTITLE = Normal Modes ExampleSUBCASE 1   METHOD = 1   SPC = 1   VECTOR=ALLBEGIN BULKPARAM    WTMASS  .00259PARAM   COUPMASS   1EIGRL    1                       3       0PBARL    1       1               I                                      +    A+      A 2.      1.      1.      .1      .1      .1CBAR     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       7       8       0.      1.      0.CBAR     8       1       8       9       0.      1.      0.CBAR     9       1       9       10      0.      1.      0.CBAR     10      1       10      11      0.      1.      0.MAT1     1       1.+7            .3      .101GRID     1               0.      0.      0.              345GRID     2               10.     0.      0.              345GRID     3               20.     0.      0.              345GRID     4               30.     0.      0.              345GRID     5               39.9999 0.      0.              345GRID     6               49.9999 0.      0.              345GRID     7               60.     0.      0.              345GRID     8               70.     0.      0.              345GRID     9               80.     0.      0.              345GRID     10              90.     0.      0.              345GRID     11              100.    0.      0.              345SPC1     1       1234    1SPC1     1       234     11ENDDATA
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 ................    3
                                     NUMBER OF SOLVES REQUIRED ............    4
1    NORMAL MODES EXAMPLE                                                     APRIL   8, 1998  MSC.Nastran  4/ 6/98   PAGE     5                                                                                0                                                                                SUBCASE 1                                                         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        2.239398E+04        1.496462E+02        2.381693E+01        1.000000E+00        2.239398E+04        2         2        3.549898E+05        5.958102E+02        9.482614E+01        1.000000E+00        3.549898E+05        3         3        1.771818E+06        1.331096E+03        2.118506E+02        1.000000E+00        1.771818E+06

SOL 106TIME 600CEND$TITLE = Normal Modes with Differential StiffnessMETHOD = 10SUBCASE 1   NLPARM = 1   SPC = 1   LOAD = 1   DISPLACEMENT=ALL$BEGIN BULKPARAM   COUPMASS 1PARAM    WTMASS  .00259PARAM    LGDISP  1NLPARM   1       5               AUTO    5       25      PW      NO     +      A+      A         .001    1.-7PARAM,NMLOOP,5$EIGRL,10,,,3PBARL    1       1               I                                      +      B+      B 2.      1.      1.      .1      .1      .1CBAR     1       1       1       2       0.      1.      0.CBAR     2       1       2       3       0.      1.      0.CBAR     3       1       3       4       0.      1.      0.CBAR     4       1       4       5       0.      1.      0.CBAR     5       1       5       6       0.      1.      0.CBAR     6       1       6       7       0.      1.      0.CBAR     7       1       7       8       0.      1.      0.CBAR     8       1       8       9       0.      1.      0.CBAR     9       1       9       10      0.      1.      0.CBAR     10      1       10      11      0.      1.      0.$
$MAT1     1       1.+7            .3      .101GRID     1               0.      0.      0.              345GRID     2               10.     0.      0.              345GRID     3               20.     0.      0.              345GRID     4               30.     0.      0.              345GRID     5               39.9999 0.      0.              345GRID     6               49.9999 0.      0.              345GRID     7               60.     0.      0.              345GRID     8               70.     0.      0.              345GRID     9               80.     0.      0.              345GRID     10              90.     0.      0.              345GRID     11              100.    0.      0.              345LOAD     2       1.      1.      1SPC1     1       1234    1SPC1     1       234     11FORCE    1       11      0       500.    1.      0.      0.ENDDATA
 R E A L   E I G E N V A L U E S   MODE    EXTRACTION      EIGENVALUE            RADIANS             CYCLES            GENERALIZED         GENERALIZED    NO.       ORDER                                                                       MASS              STIFFNESS        1         1        2.735837E+04        1.654037E+02        2.632481E+01        1.000000E+00        2.735837E+04        2         2        3.748482E+05        6.122484E+02        9.744236E+01        1.000000E+00        3.748482E+05        3         3        1.816508E+06        1.347779E+03        2.145057E+02        1.000000E+00        1.816508E+06
SOL 103DIAG 8CEND$TITLE = Normal Modes with Differential Stiffness$SPC = 1DISPLACEMENT=ALL$SUBCASE 1LOAD = 2$SUBCASE 2METHOD = 10STATSUB = 1$BEGIN BULKPARAM   COUPMASS 1PARAM    WTMASS  .00259$EIGRL,10,,,3PBARL    1       1               I                                      +      B+      B 2.      1.      1.      .1      .1      .1CBAR     1       1       1       2       0.      1.      0.CBAR     2       1       2       3       0.      1.      0.CBAR     3       1       3       4       0.      1.      0.CBAR     4       1       4       5       0.      1.      0.CBAR     5       1       5       6       0.      1.      0.CBAR     6       1       6       7       0.      1.      0.CBAR     7       1       7       8       0.      1.      0.CBAR     8       1       8       9       0.      1.      0.CBAR     9       1       9       10      0.      1.      0.CBAR     10      1       10      11      0.      1.      0.$
$MAT1     1       1.+7            .3      .101GRID     1               0.      0.      0.              345GRID     2               10.     0.      0.              345GRID     3               20.     0.      0.              345GRID     4               30.     0.      0.              345GRID     5               39.9999 0.      0.              345GRID     6               49.9999 0.      0.              345GRID     7               60.     0.      0.              345GRID     8               70.     0.      0.              345GRID     9               80.     0.      0.              345GRID     10              90.     0.      0.              345GRID     11              100.    0.      0.              345LOAD     2       1.      1.      1SPC1     1       1234    1SPC1     1       234     11FORCE    1       11      0       500.    1.      0.      0.ENDDATA
1    NORMAL MODES WITH DIFFERENTIAL STIFFNESS                                 APRIL   9, 1998  MSC.Nastran  4/ 6/98   PAGE     9                                                                                0                                                                                SUBCASE 2                                                         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        2.735837E+04        1.654037E+02        2.632481E+01        1.000000E+00        2.735837E+04        2         2        3.748482E+05        6.122484E+02        9.744236E+01        1.000000E+00        3.748482E+05        3         3        1.816508E+06        1.347779E+03        2.145057E+02        1.000000E+00        1.816508E+06


title: Презентация на тему: MSC.Nastran 101 2006 - 1

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MSC Confidential
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title: Презентация на тему: MSC.Nastran 102 2001 - 16

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$$ file - fs1.dat   $ $ all 7 s.e. brought in using begin super$ duplicate boundary grids id$ each s.e. contains its own property description with the same id$ condensed subcase setup$$ -------------------------------------------------------$id allsep1 dat SOL 101 TIME 15CENDTITLE = S.E. SAMPLE PROBLEM 1 SUBTITLE = S.E. STATICS - RUN 1 - MULTIPLE LOADSDISP = ALLstress = alloload = allSET 999 = 0,1,2,3,4,5,6,7SUPER = 999  $ ALL CASE CONTROL IS FOR ALL SUPERELEMENTSPARAM,GRDPNT,1SUBCASE 101LABEL = PRESSURE LOADLOAD = 101$SUBCASE 201LABEL = 2# NORMAL LOADSLOAD = 201$SUBCASE 301LABEL = OPPOSING LOADSLOAD = 301$
seplot 5ptitle = superelement 5find scale, origin 1, set 1plot static deformation set 1 origin 1 label both$seplot 6ptitle = superelement 6find scale, origin 1, set 1plot static deformation set 1 origin 1 label both$seplot 7ptitle = superelement 7find scale, origin 1, set 1plot static deformation set 1 origin 1 label both
$seplot 0ptitle = superelement 0find scale, origin 1, set 1plot static deformation set 1 origin 1 label both$seupplot 0ptitle = full structureaxes x,mz,yfind scale, origin 1, set 1plot static deformation set 1 origin 1$
$$    plot.blk$output(plot)$set 1 = allaxes z,x,yview 0.,0.,0.seupplot 0ptitle = full structurefind scale, origin 1, set 1plot set 1 origin 1 label both$$  deform plots$seplot 1ptitle = superelement 1find scale, origin 1, set 1plot static deformation set 1 origin 1 label both$seplot 2ptitle = superelement 2find scale, origin 1, set 1plot static deformation set 1 origin 1 label both$seplot 3ptitle = superelement 3find scale, origin 1, set 1plot static deformation set 1 origin 1 label both$seplot 4ptitle = superelement 4find scale, origin 1, set 1plot static deformation set 1 origin 1 label both$
GRID    33              -5.2    6.      0.                                      GRID    34              -4.4    6.      0.                                      GRID    37              -2.     6.      0.                                      GRID    38              -1.2    6.      0.                                      GRID    45              -5.2    6.8     0.                                      GRID    46              -4.4    6.8     0.                                      GRID    47              -3.6    6.8     0.                                      GRID    48              -2.8    6.8     0.                                      GRID    49              -2.     6.8     0.                                      GRID    50              -1.2    6.8     0.                                      GRID    57              -5.2    7.6     0.                                      GRID    58              -4.4    7.6     0.                                      GRID    59              -3.6    7.6     0.                                      GRID    60              -2.8    7.6     0.                                      GRID    61              -2.     7.6     0.                                      GRID    62              -1.2    7.6     0.                                      GRID    69              -5.2    8.4     0.
GRID    70              -4.4    8.4     0.                                      GRID    71              -3.6    8.4     0.                                      GRID    72              -2.8    8.4     0.                                      GRID    73              -2.     8.4     0.                                      GRID    74              -1.2    8.4     0.                                      GRID    81              -5.2    9.2     0.                                      GRID    82              -4.4    9.2     0.                                      GRID    83              -3.6    9.2     0.                                      GRID    84              -2.8    9.2     0.                                      GRID    85              -2.     9.2     0.                                      GRID    86              -1.2    9.2     0.                                      GRID    93              -5.2    10.     0.                                      GRID    94              -4.4    10.     0.                                      GRID    95              -3.6    10.     0.                                      GRID    96              -2.8    10.     0.                                      GRID    97              -2.     10.     0.                                      GRID    98              -1.2    10.     0.

$$     se1.blk$                                                                               CQUAD4  18      1       33      34      46      45                              CQUAD4  19      1       34      35      47      46                              CQUAD4  20      1       35      36      48      47                              CQUAD4  21      1       36      37      49      48                              CQUAD4  22      1       37      38      50      49                              CQUAD4  23      1       45      46      58      57                              CQUAD4  24      1       46      47      59      58                              CQUAD4  25      1       47      48      60      59                              CQUAD4  26      1       48      49      61      60                              CQUAD4  27      1       49      50      62      61                              CQUAD4  28      1       57      58      70      69                              CQUAD4  29      1       58      59      71      70                              CQUAD4  30      1       59      60      72      71                              CQUAD4  31      1       60      61      73      72                              CQUAD4  32      1       61      62      74      73                              CQUAD4  33      1       69      70      82      81                              CQUAD4  34      1       70      71      83      82                              CQUAD4  35      1       71      72      84      83                              CQUAD4  36      1       72      73      85      84                              CQUAD4  37      1       73      74      86      85                              CQUAD4  38      1       81      82      94      93                              CQUAD4  39      1       82      83      95      94                              CQUAD4  40      1       83      84      96      95                              CQUAD4  41      1       84      85      97      96                              CQUAD4  42      1       85      86      98      97                              $GRDSET                                                  6                       $6                       $     boundary grids$GRID    35              -3.6    6.      0.                                      GRID    36              -2.8    6.      0.                                      $
$                                                                               $    se2.blk$CQUAD4  43      1       39      40      52      51                              CQUAD4  44      1       40      41      53      52                              CQUAD4  45      1       41      42      54      53                              CQUAD4  46      1       42      43      55      54                              CQUAD4  47      1       43      44      56      55                              CQUAD4  48      1       51      52      64      63                              CQUAD4  49      1       52      53      65      64                              CQUAD4  50      1       53      54      66      65                              CQUAD4  51      1       54      55      67      66                              CQUAD4  52      1       55      56      68      67                              CQUAD4  53      1       63      64      76      75                              CQUAD4  54      1       64      65      77      76                              CQUAD4  55      1       65      66      78      77                              CQUAD4  56      1       66      67      79      78                              CQUAD4  57      1       67      68      80      79                              CQUAD4  58      1       75      76      88      87                              CQUAD4  59      1       76      77      89      88                              CQUAD4  60      1       77      78      90      89                              CQUAD4  61      1       78      79      91      90                              CQUAD4  62      1       79      80      92      91                              CQUAD4  63      1       87      88      100     99                              CQUAD4  64      1       88      89      101     100                             CQUAD4  65      1       89      90      102     101                             CQUAD4  66      1       90      91      103     102                             CQUAD4  67      1       91      92      104     103                             $GRDSET                                                  6                       $$     boundary grids$GRID    41              2.8     6.      0.                                      GRID    42              3.6     6.      0.                                      $
$GRID    39              1.2     6.      0.                                      GRID    40              2.      6.      0.                                      GRID    43              4.4     6.      0.                                      GRID    44              5.2     6.      0.                                      $GRID    51              1.2     6.8     0.                                      GRID    52              2.      6.8     0.                                      GRID    53              2.8     6.8     0.                                      GRID    54              3.6     6.8     0.                                      GRID    55              4.4     6.8     0.                                      GRID    56              5.2     6.8     0.                                      GRID    63              1.2     7.6     0.                                      GRID    64              2.      7.6     0.                                      GRID    65              2.8     7.6     0.                                      GRID    66              3.6     7.6     0.                                      GRID    67              4.4     7.6     0.                                      GRID    68              5.2     7.6     0.                                      GRID    75              1.2     8.4     0.
GRID    76              2.      8.4     0.                                      GRID    77              2.8     8.4     0.                                      GRID    78              3.6     8.4     0.                                      GRID    79              4.4     8.4     0.                                      GRID    80              5.2     8.4     0.                                      GRID    87              1.2     9.2     0.                                      GRID    88              2.      9.2     0.                                      GRID    89              2.8     9.2     0.                                      GRID    90              3.6     9.2     0.                                      GRID    91              4.4     9.2     0.                                      GRID    92              5.2     9.2     0.                                      GRID    99              1.2     10.     0.                                      GRID    100             2.      10.     0.                                      GRID    101             2.8     10.     0.                                      GRID    102             3.6     10.     0.                                      GRID    103             4.4     10.     0.                                      GRID    104             5.2     10.     0.                                      $

$$     se3.blk$                                                                               CQUAD4  14      1       19      20      30      29                              CQUAD4  15      1       29      30      36      35                              $GRDSET                                                  6                       $$     boundary grids$GRID    19              -3.6    4.4     0.                                      GRID    20              -2.8    4.4     0.                                      GRID    35              -3.6    6.      0.                                      GRID    36              -2.8    6.      0.                                      $GRID    29              -3.6    5.2     0.                                      GRID    30              -2.8    5.2     0.                                      $
$$      se4.blk$                                                                               CQUAD4  16      1       27      28      32      31                              CQUAD4  17      1       31      32      42      41                              $GRDSET                                                  6                       $$       boundary grids$GRID    27              2.8     4.4     0.                                      GRID    28              3.6     4.4     0.                                      GRID    41              2.8     6.      0.                                      GRID    42              3.6     6.      0.                                      $GRID    31              2.8     5.2     0.                                      GRID    32              3.6     5.2     0.                                      $

$                                                                               $      se5.blk$CQUAD4  6       1       9       10      20      19                              CQUAD4  7       1       10      11      21      20                              CQUAD4  8       1       11      12      22      21                              CQUAD4  9       1       12      13      23      22                              $GRDSET                                                  6                       $$      boundary grids$GRID    19              -3.6    4.4     0.                                      GRID    20              -2.8    4.4     0.                                      GRID    13              -.4     3.6     0.                                      GRID    23              -.4     4.4     0.                                      $GRID    9               -3.6    3.6     0.                                      GRID    10              -2.8    3.6     0.                                      GRID    11              -2.     3.6     0.                                      GRID    12              -1.2    3.6     0.                                      GRID    21              -2.     4.4     0.                                      GRID    22              -1.2    4.4     0.                                      $
$                                                                               $       se6.blk$CQUAD4  10      1       14      15      25      24                              CQUAD4  11      1       15      16      26      25                              CQUAD4  12      1       16      17      27      26                              CQUAD4  13      1       17      18      28      27                              $GRDSET                                                  6                       $$    boundary grids$GRID    27              2.8     4.4     0.                                      GRID    28              3.6     4.4     0.                                      GRID    14              .4      3.6     0.                                      GRID    24              .4      4.4     0.                                      $GRID    15              1.2     3.6     0.                                      GRID    16              2.      3.6     0.                                      GRID    17              2.8     3.6     0.                                      GRID    18              3.6     3.6     0.                                      $GRID    25              1.2     4.4     0.                                      GRID    26              2.      4.4     0.                                      $
$                                                                               $     se7.blk$CQUAD4  1       1       1       2       4       3                               CQUAD4  2       1       3       4       6       5                               CQUAD4  3       1       5       6       8       7                               CQUAD4  4       1       7       8       14      13                              $GRDSET                                                  6                       $GRID    1               -.4     0.      0.              123456                  GRID    2               .4      0.      0.              123456                  GRID    3               -.4     0.9     0.                                      GRID    4               .4      0.9     0.                                      GRID    5               -.4     1.8     0.                                      GRID    6               .4      1.8     0.                                      GRID    7               -.4     2.7     0.                                      GRID    8               .4      2.7     0.                                      $$       boundary grids$GRID    13              -.4     3.6     0.                                      GRID    14              .4      3.6     0.                                      $
$$   prop1.blk$MAT1,1,30.+6,,.3,.283PARAM,WTMASS,.00259PARAM,AUTOSPC,YESPSHELL,1,1,.05,1,,1$
$$ file - loadse1.blk$ loads on s.e. 1$$ LOAD CASE 1 - PRESSURE LOAD$PLOAD2,101,-1.,18,THRU,42$$ LOAD CASE 2 - 2 POINT LOADS AT CORNERS$FORCE,201,93,,2.,0.,0.,1.$$ LOAD CASE 3 - OPPOSING POINT LOADS AT CORNERS$FORCE,301,93,,2.,0.,0.,1.$

$$ file - loadse2.blk$ loads on s.e. 2 $$ LOAD CASE 1 - PRESSURE LOAD$PLOAD2,101,-1.,43,THRU,67$$ LOAD CASE 2 - 2 POINT LOADS AT CORNERS$FORCE,201,104,,2.,0.,0.,1.$$ LOAD CASE 3 - OPPOSING POINT LOADS AT CORNERS$FORCE,301,104,,2.,0.,0.,-1.$
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o
o
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$$   sesp1.dat$SOL 103CENDTITLE = SAMPLE PROBLEM FOR CMS USING PARTSSPC = 1DISP = ALLPARAM,GRDPNT,0PARAM,USETPRT,0$SUBCASE 1LABEL = CMS FOR PART 1SUPER = 1METHOD=1 $ $SUBCASE 2LABEL = CMS FOR PART 2SUPER = 2METHOD = 2$SUBCASE 100LABEL = SYSTEM MODESSUPER = 0METHOD = 100$BEGIN BULK$grid,3,,20.conm2,13,3,,1.0$EIGRL,100,,,4senqset,1,2senqset,2,1
BEGIN SUPER = 1$EIGRL,1,,,2grid,3,,20.grid,4,,30.grid,5,,40.$CELAS2,3,1.,3,1,4,1CELAS2,4,1.,4,1,5,1CONM2,14,4,,1.
CONM2,15,5,,1.$BEGIN SUPER = 2$EIGRL,2,,,1grid,1,,0.grid,2,,10.grid,3,,20.$CELAS2,1,1.,1,1,2,1CELAS2,2,1.,2,1,3,1CONM2,11,1,,1.CONM2,12,2,,1.SPC1,1,123456,1$ENDDATA
OUTPUT FROM SPRING MODEL CMS RUN
1    SAMPLE PROBLEM FOR CMS USING PARTS                                         MAY  12, 1998  MSC.Nastran  7/17/97   PAGE    25                                                                                SUPERELEMENT 1              0                                                                                SUBCASE 1              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   (REIGL MODULE)
                                     BLOCK SIZE USED ......................    1
                                     NUMBER OF DECOMPOSITIONS .............    1
                                     NUMBER OF ROOTS FOUND ................    2
                                     NUMBER OF SOLVES REQUIRED ............    3
1    SAMPLE PROBLEM FOR CMS USING PARTS                                         MAY  12, 1998  MSC.Nastran  7/17/97   PAGE    26                                                                                SUPERELEMENT 1              0                                                                                SUBCASE 1                                                             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        3.819660E-01        6.180340E-01        9.836316E-02        1.000000E+00        3.819660E-01        2         2        2.618034E+00        1.618034E+00        2.575181E-01        1.000000E+00        2.618034E+00

OUTPUT FROM SPRING MODEL CMS RUN
1    SAMPLE PROBLEM FOR CMS USING PARTS                                         MAY  12, 1998  MSC.Nastran  7/17/97   PAGE    38                                                                                SUPERELEMENT 2              0                                                                                SUBCASE 2              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   (REIGL MODULE)
                                     BLOCK SIZE USED ......................    1
                                     NUMBER OF DECOMPOSITIONS .............    1
                                     NUMBER OF ROOTS FOUND ................    1
                                     NUMBER OF SOLVES REQUIRED ............    2
1    SAMPLE PROBLEM FOR CMS USING PARTS                                         MAY  12, 1998  MSC.Nastran  7/17/97   PAGE    39                                                                                SUPERELEMENT 2              0                                                                                SUBCASE 2                                                             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        2.000000E+00        1.414214E+00        2.250791E-01        1.000000E+00        2.000000E+00

1    SAMPLE PROBLEM FOR CMS USING PARTS                                         MAY  12, 1998  MSC.Nastran  7/17/97   PAGE    48                                                                                SUPERELEMENT 0              0                                                                                SUBCASE 100                                                           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        1.206148E-01        3.472964E-01        5.527393E-02        1.000000E+00        1.206148E-01        2         2        1.000000E+00        1.000000E+00        1.591549E-01        1.000000E+00        1.000000E+00        3         3        2.347296E+00        1.532089E+00        2.438395E-01        1.000000E+00        2.347296E+00        4         4        3.532089E+00        1.879385E+00        2.991135E-01        1.000000E+00        3.532089E+001    SAMPLE PROBLEM FOR CMS USING PARTS                                         MAY  12, 1998  MSC.Nastran  7/17/97   PAGE    49                                                                                SUPERELEMENT 0              0                                                                                SUBCASE 100            1    SAMPLE PROBLEM FOR CMS USING PARTS                                         MAY  12, 1998  MSC.Nastran  7/17/97   PAGE    50                                                                                SUPERELEMENT 0              0                                                                                SUBCASE 100            0***USER INFORMATION MESSAGE---DATA RECOVERY FOR SUPERELEMENT       0 IS NOW INITIATED.1    SAMPLE PROBLEM FOR CMS USING PARTS                                         MAY  12, 1998  MSC.Nastran  7/17/97   PAGE    51                                                                                SUPERELEMENT 0              0     SYSTEM MODES                                                                                SUBCASE 100                  EIGENVALUE =  1.206148E-01          CYCLES =  5.527393E-02         R E A L   E I G E N V E C T O R   N O .          1       POINT ID.   TYPE          T1             T2             T3             R1             R2             R3             3      G     -4.285251E-01    .0             .0             .0             .0             .0
1    SAMPLE PROBLEM FOR CMS USING PARTS                                         MAY  12, 1998  MSC.Nastran  7/17/97   PAGE    52                                                                                SUPERELEMENT 0              0     SYSTEM MODES                                                                                SUBCASE 100                  EIGENVALUE =  1.000000E+00          CYCLES =  1.591549E-01         R E A L   E I G E N V E C T O R   N O .          2       POINT ID.   TYPE          T1             T2             T3             R1             R2             R3             3      G     -5.773503E-01    .0             .0             .0             .0             .01    SAMPLE PROBLEM FOR CMS USING PARTS                                         MAY  12, 1998  MSC.Nastran  7/17/97   PAGE    53                                                                                SUPERELEMENT 0              0     SYSTEM MODES                                                                                SUBCASE 100                  EIGENVALUE =  2.347296E+00          CYCLES =  2.438395E-01         R E A L   E I G E N V E C T O R   N O .          3       POINT ID.   TYPE          T1             T2             T3             R1             R2             R3             3      G      2.280134E-01    .0             .0             .0             .0             .01    SAMPLE PROBLEM FOR CMS USING PARTS                                         MAY  12, 1998  MSC.Nastran  7/17/97   PAGE    54                                                                                SUPERELEMENT 0              0     SYSTEM MODES                                                                                SUBCASE 100                  EIGENVALUE =  3.532089E+00          CYCLES =  2.991135E-01         R E A L   E I G E N V E C T O R   N O .          4       POINT ID.   TYPE          T1             T2             T3             R1             R2             R3             3      G     -6.565385E-01    .0             .0             .0             .0             .01    SAMPLE PROBLEM FOR CMS USING PARTS                                         MAY  12, 1998  MSC.Nastran  7/17/97   PAGE    55                                                                                SUPERELEMENT 0              0                                                                                SUBCASE 100            1    SAMPLE PROBLEM FOR CMS USING PARTS                                         MAY  12, 1998  MSC.Nastran  7/17/97   PAGE    56                                                                                SUPERELEMENT 1              0                                                                                SUBCASE 100            0***USER INFORMATION MESSAGE---DATA RECOVERY FOR SUPERELEMENT       1 IS NOW INITIATED.1    SAMPLE PROBLEM FOR CMS USING PARTS                                         MAY  12, 1998  MSC.Nastran  7/17/97   PAGE    57                                                                                SUPERELEMENT 1              0     CMS FOR PART 1                                                                                SUBCASE 1                    EIGENVALUE =  1.206148E-01          CYCLES =  5.527393E-02         R E A L   E I G E N V E C T O R   N O .          1       POINT ID.   TYPE          T1             T2             T3             R1             R2             R3             3      G     -4.285251E-01    .0             .0             .0             .0             .0             4      G     -5.773503E-01    .0             .0             .0             .0             .0             5      G     -6.565385E-01    .0             .0             .0             .0             .0
OUTPUT FROM SPRING MODEL CMS RUN  (Cont.)
1    SAMPLE PROBLEM FOR CMS USING PARTS                                         MAY  12, 1998  MSC.Nastran  7/17/97   PAGE    58                                                                                SUPERELEMENT 1              0     CMS FOR PART 1                                                                                SUBCASE 1                    EIGENVALUE =  1.000000E+00          CYCLES =  1.591549E-01         R E A L   E I G E N V E C T O R   N O .          2       POINT ID.   TYPE          T1             T2             T3             R1             R2             R3             3      G     -5.773503E-01    .0             .0             .0             .0             .0             4      G      8.187895E-16    .0             .0             .0             .0             .0             5      G      5.773503E-01    .0             .0             .0             .0             .01    SAMPLE PROBLEM FOR CMS USING PARTS                                         MAY  12, 1998  MSC.Nastran  7/17/97   PAGE    59                                                                                SUPERELEMENT 1              0     CMS FOR PART 1                                                                                SUBCASE 1                    EIGENVALUE =  2.347296E+00          CYCLES =  2.438395E-01         R E A L   E I G E N V E C T O R   N O .          3       POINT ID.   TYPE          T1             T2             T3             R1             R2             R3             3      G      2.280134E-01    .0             .0             .0             .0             .0             4      G      5.773503E-01    .0             .0             .0             .0             .0             5      G     -4.285251E-01    .0             .0             .0             .0             .01    SAMPLE PROBLEM FOR CMS USING PARTS                                         MAY  12, 1998  MSC.Nastran  7/17/97   PAGE    60                                                                                SUPERELEMENT 1              0     CMS FOR PART 1                                                                                SUBCASE 1                    EIGENVALUE =  3.532089E+00          CYCLES =  2.991135E-01         R E A L   E I G E N V E C T O R   N O .          4       POINT ID.   TYPE          T1             T2             T3             R1             R2             R3             3      G     -6.565385E-01    .0             .0             .0             .0             .0             4      G      5.773503E-01    .0             .0             .0             .0             .0             5      G     -2.280134E-01    .0             .0             .0             .0             .01    SAMPLE PROBLEM FOR CMS USING PARTS                                         MAY  12, 1998  MSC.Nastran  7/17/97   PAGE    61                                                                                SUPERELEMENT 1              0                                                                                SUBCASE 100            1    SAMPLE PROBLEM FOR CMS USING PARTS                                         MAY  12, 1998  MSC.Nastran  7/17/97   PAGE    62                                                                                SUPERELEMENT 2              0                                                                                SUBCASE 100            0***USER INFORMATION MESSAGE---DATA RECOVERY FOR SUPERELEMENT       2 IS NOW INITIATED.
1    SAMPLE PROBLEM FOR CMS USING PARTS                                         MAY  12, 1998  MSC.Nastran  7/17/97   PAGE    63                                                                                SUPERELEMENT 2              0     CMS FOR PART 2                                                                                SUBCASE 2                    EIGENVALUE =  1.206148E-01          CYCLES =  5.527393E-02         R E A L   E I G E N V E C T O R   N O .          1       POINT ID.   TYPE          T1             T2             T3             R1             R2             R3             1      G       .0             .0             .0             .0             .0             .0             2      G     -2.280134E-01    .0             .0             .0             .0             .0             3      G     -4.285251E-01    .0             .0             .0             .0             .01    SAMPLE PROBLEM FOR CMS USING PARTS                                         MAY  12, 1998  MSC.Nastran  7/17/97   PAGE    64                                                                                SUPERELEMENT 2              0     CMS FOR PART 2                                                                                SUBCASE 2                    EIGENVALUE =  1.000000E+00          CYCLES =  1.591549E-01         R E A L   E I G E N V E C T O R   N O .          2       POINT ID.   TYPE          T1             T2             T3             R1             R2             R3             1      G       .0             .0             .0             .0             .0             .0             2      G     -5.773503E-01    .0             .0             .0             .0             .0             3      G     -5.773503E-01    .0             .0             .0             .0             .01    SAMPLE PROBLEM FOR CMS USING PARTS                                         MAY  12, 1998  MSC.Nastran  7/17/97   PAGE    65                                                                                SUPERELEMENT 2              0     CMS FOR PART 2                                                                                SUBCASE 2                    EIGENVALUE =  2.347296E+00          CYCLES =  2.438395E-01         R E A L   E I G E N V E C T O R   N O .          3       POINT ID.   TYPE          T1             T2             T3             R1             R2             R3             1      G       .0             .0             .0             .0             .0             .0             2      G     -6.565385E-01    .0             .0             .0             .0             .0             3      G      2.280134E-01    .0             .0             .0             .0             .01    SAMPLE PROBLEM FOR CMS USING PARTS                                         MAY  12, 1998  MSC.Nastran  7/17/97   PAGE    66                                                                                SUPERELEMENT 2              0     CMS FOR PART 2                                                                                SUBCASE 2                    EIGENVALUE =  3.532089E+00          CYCLES =  2.991135E-01         R E A L   E I G E N V E C T O R   N O .          4       POINT ID.   TYPE          T1             T2             T3             R1             R2             R3             1      G       .0             .0             .0             .0             .0             .0             2      G      4.285251E-01    .0             .0             .0             .0             .0             3      G     -6.565385E-01    .0             .0             .0             .0             .01    SAMPLE PROBLEM FOR CMS USING PARTS                                         MAY  12, 1998  MSC.Nastran  7/17/97   PAGE    67

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Second Level
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MSC Corporate Overview Speaker Notes


title: Презентация на тему: MSC.Nastran 101 2006 - 0


title: Презентация на тему: MSC.Mvision Workshops 12

text:
Now, write all the data from this databank to an Mvision Define/Input File as well as a Schema/Express File.
a.	In the Browser Menu, select File/Builder Functions/Write Databank.
b.	In Choose a File Type to Write:, select Mvision Define/Input File.
c.	In Enter a Define/Schema File Name:, select ex12_out.def.
d.	In Enter a Input/Data File Name:, select ex12_out.inp.
e.	In Choose Data to Write:, select Entire Databank.
f.	OK.

Clean up any search selections, save the newly created databank and exit the Data Viewer and MSC.Mvision.
a.	In the Data Viewer Menu, select File/Close Data Viewer.
b.	In Select a Category Button:, select List All Materials.
c.	In the Browser Menu, select File/Builder Functions/Save Databank.
d.	In the Browser Menu, select File/Exit MVISION.

This ends this exercise
CLICK TO EDIT MASTER TITLE STYLE
MVI320, Workshop 12, August 2001
HEIRARCHY is MATERIAL, SPECIMEN, ENVIRONMENT, SOURCE.
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Again, you get the standard Information Dialog window indicating the translation status.
The Express files just written can be read into another database using File/Builder Functions/Read Data
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Clean up any search selections, save the newly created databank and exit the Data Viewer and MSC.Mvision.
a.	In the Data Viewer Menu, select File/Close Data Viewer.
b.	In Select a Category Button:, select List All Materials.
c.	In the Browser Menu, select File/Builder Functions/Save Databank.
d.	In the Browser Menu, select File/Exit MVISION.

This ends this exercise
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f
b
c
d
Clean up any search selections, save the newly created databank and exit the Data Viewer and MSC.Mvision.
a.	In the Data Viewer Menu, select File/Close Data Viewer.
b.	In Select a Category Button:, select List All Materials.
c.	In the Browser Menu, select File/Builder Functions/Save Databank.
d.	In the Browser Menu, select File/Exit MVISION.

This ends this exercise
e
f
b
c
d
Clean up any search selections, save the newly created databank and exit the Data Viewer and MSC.Mvision.
a.	In the Data Viewer Menu, select File/Close Data Viewer.
b.	In Select a Category Button:, select List All Materials.
c.	In the Browser Menu, select File/Builder Functions/Save Databank.
d.	In the Browser Menu, select File/Exit MVISION.

This ends this exercise
e
f
b
c
d
Clean up any search selections, save the newly created databank and exit the Data Viewer and MSC.Mvision.
a.	In the Data Viewer Menu, select File/Close Data Viewer.
b.	In Select a Category Button:, select List All Materials.
c.	In the Browser Menu, select File/Builder Functions/Save Databank.
d.	In the Browser Menu, select File/Exit MVISION.

This ends this exercise
e
f
b
c
d
Clean up any search selections, save the newly created databank and exit the Data Viewer and MSC.Mvision.
a.	In the Data Viewer Menu, select File/Close Data Viewer.
b.	In Select a Category Button:, select List All Materials.
c.	In the Browser Menu, select File/Builder Functions/Save Databank.
d.	In the Browser Menu, select File/Exit MVISION.

This ends this exercise
k
l
h
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j
Clean up any search selections, save the newly created databank and exit the Data Viewer and MSC.Mvision.
a.	In the Data Viewer Menu, select File/Close Data Viewer.
b.	In Select a Category Button:, select List All Materials.
c.	In the Browser Menu, select File/Builder Functions/Save Databank.
d.	In the Browser Menu, select File/Exit MVISION.

This ends this exercise
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title: Презентация на тему: MSC.Nastran 102 2001 - 19

text:
$
$    beginning of optim1.blk
$
$ data for design sensitivity
$
$ define design variables
$
desvar,1,frntdamp,1.,.1,10.
desvar,2,reardamp,1.,.2,20.
desvar,3,frntstif,1.,.4,2.
desvar,4,rearstif,1.,.5,2.5
$
$ relation between properties and variables
$
dvprel1,101,pvisc,2001,3,1.,,,,+dv101
+dv101,1,10.
dvprel1,102,pvisc,2002,3,1.,,,,+dv102
+dv102,2,5.
dvprel1,103,prod,1001,4,4.,,,,+dv103
+dv103,3,10.
dvprel1,104,prod,1002,4,4.,,,,+dv104
+dv104,4,8.
$
$
$  select displacement Y at tire and driver seat as
$  response quantities
$
$ maximum tire displacement be < +/-0.5 inches
$
dconstr,101,200,-.5,.5
dresp1,200,disp,frdisp,,,2,,358
$
$ define driver's seat disp as a response
$
$
$ require that maximum driver displacement be < +/- 0.25 inches
$ between .5 and 25 hz
$
dconstr,102,201,-.25,.25,0.5,25.0
dresp1,201,driver,frdisp,,,2,,471
$
$ combine constraints into set 100
$
dconadd,100,101,102
$
$ define objective = minimize srss of response
$
dresp1,300,rss,frdisp,,,2,rss,471
$
$ end of optimization input
$
$ end of                optim1.blk
$

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MSC Corporate Overview Speaker Notes
ID NAS102, WORKSHOP 15TIME 10SOL 200            $ OPTIMIZATIONCENDTITLE= SYMMETRIC THREE BAR TRUSS DESIGN OPTIMIZATION - VARIATION OF D200X1SUBTITLE= GOAL IS TO MIN WT WHILE KEEPING THE 1ST MODE BETWEEN 1500-1550 HZECHO= SORTSPC= 100DISP(PLOT) ALLDESOBJ(MIN)= 100   $ (DESIGN OBJECTIVE = DRESP ID)DESSUB= 200        $  DEFINE CONSTRAINT SET FOR BOTH SUBCASESSUBCASE 1  ANALYSIS= MODES  METHOD= 10BEGIN BULK$$----------------------------------------------------------------------$ ANALYSIS MODEL$----------------------------------------------------------------------$EIGRL, 10, , , 2PARAM, POST, -1$$ GRID DATA$       2        3        4      5       6       7      8       9       10GRID,   1,       ,      -10.0,    0.0,  0.0GRID,   2,       ,        0.0,    0.0,  0.0GRID,   3,       ,       10.0,    0.0,  0.0GRID,   4,       ,        0.0,  -10.0,  0.0$ SUPPORT DATASPC,    100,    1,      123456,  ,      2,      123456SPC,    100,    3,      123456,  ,      4,      3456$ ELEMENT DATACROD,   1,      11,     1,       4CROD,   2,      12,     2,       4CROD,   3,      13,     3,       4$ PROPERTY DATAPROD,   11,     1,      1.0PROD,   12,     1,      2.0PROD,   13,     1,      1.0MAT1,   1,      1.0E+7, ,       0.33,   0.1$PARAM, WTMASS, .00259
$$----------------------------------------------------------------------$ DESIGN MODEL$----------------------------------------------------------------------$$...DESIGN VARIABLE DEFINITION$$DESVAR,ID,     LABEL,  XINIT,  XLB,    XUB,    DELXV(OPTIONAL)DESVAR, 1,      A1,     1.0,    0.1,    100.0DESVAR, 2,      A2,     2.0,    0.1,    100.0DESVAR, 3,      A3,     1.0,    0.1,    100.0$$...IMPOSE X3=X1 (LEADS TO A3=A1)$$DLINK, ID,     DDVID,  CO,     CMULT,  IDV1,   C1,     IDV2,   C2,     +$+,     IDV3,   C3,     ...DLINK,  1,      3,      0.0,    1.0,    1       1.00$$...DEFINITION OF DESIGN VARIABLE TO ANALYSIS MODEL PARAMETER RELATIONS$$DVPREL1,ID,    TYPE,   PID,    FID,    PMIN,   PMAX,   CO,     ,       +$+,     DVID1,  COEF1,  DVID2,  COEF2,  ...DVPREL1, 10,    PROD,   11,     4,      ,       ,       ,       ,       +DP1+DP1,   1,      1.0DVPREL1, 20,    PROD,   12,     4,      ,       ,       ,       ,       +DP2+DP2,   2,      1.0DVPREL1, 30,    PROD,   13,     4,      ,       ,       ,       ,       +DP3+DP3,   3,      1.0$$...STRUCTURAL RESPONSE INDENTIFICATION$$DRESP1 ID      LABEL   RTYPE   PTYPE   REGION  ATTA    ATTB    ATT1    +$+      ATT2    ...DRESP1  100     W       WEIGHTDRESP1  210     MODE1   EIGN                    1$$...CONSTRAINTS$$DCONSTR,DCID,  RID,    LALLOW, UALLOWDCONSTR, 200,   210,    8.883E7, 9.485E7$$...OPTIMIZATION CONTROL$DOPTPRM, DESMAX, 30$ENDDATA
0                                                                                SUBCASE 1                                           ***************************************************************                                   S U M M A R Y   O F   D E S I G N    C Y C L E    H I S T O R Y                                   ***************************************************************
                                                      (HARD CONVERGENCE ACHIEVED)
                                                      (SOFT CONVERGENCE ACHIEVED)
                                       NUMBER OF FINITE ELEMENT ANALYSES COMPLETED          13                                       NUMBER OF OPTIMIZATIONS W.R.T. APPROXIMATE MODELS    12
                                              OBJECTIVE AND MAXIMUM CONSTRAINT HISTORY           ---------------------------------------------------------------------------------------------------------------                              OBJECTIVE FROM           OBJECTIVE FROM          FRACTIONAL ERROR          MAXIMUM VALUE               CYCLE              APPROXIMATE                 EXACT                    OF                       OF             NUMBER            OPTIMIZATION               ANALYSIS              APPROXIMATION             CONSTRAINT              ---------------------------------------------------------------------------------------------------------------
             INITIAL                                      4.828427E+00                                      1.922634E-01
                   1             4.624039E+00             4.623868E+00             3.712506E-05            -3.992662E-03
                   2             3.699272E+00             3.699094E+00             4.795320E-05            -3.992493E-03
                   3             2.958851E+00             2.959000E+00            -5.019763E-05            -4.089320E-03
                   4             2.366940E+00             2.367200E+00            -1.099836E-04            -4.089320E-03
                   5             1.892237E+00             1.892110E+00             6.722458E-05            -4.995593E-03
                   6             1.514333E+00             1.514324E+00             5.982807E-06            -4.559115E-03
                   7             1.210749E+00             1.210854E+00            -8.624274E-05            -5.078925E-03
                   8             9.690658E-01             9.690483E-01             1.808348E-05            -4.686642E-03
                   9             7.753531E-01             7.752386E-01             1.476971E-04            -4.686642E-03
                  10             6.202133E-01             6.201910E-01             3.604010E-05            -4.686726E-03
                  11             5.758922E-01             5.758651E-01             4.699106E-05            -3.288561E-04
                  12             5.758651E-01             5.758651E-01             0.000000E+00            -3.288561E-04           ---------------------------------------------------------------------------------------------------------------
1    SYMMETRIC THREE BAR TRUSS DESIGN OPTIMIZATION - VARIATION OF D200        APRIL  22, 1998  MSC.Nastran  4/20/98   PAGE    47      GOAL IS TO MIN WT WHILE KEEPING THE 1ST MODE BETWEEN 1500-1550                                                                0                                                                                SUBCASE 1                                                                     DESIGN VARIABLE HISTORY ----------------------------------------------------------------------------------------------------------------------------------  INTERNAL |   EXTERNAL   |             |                                                                                DV. ID. |    DV. ID.   |    LABEL    |   INITIAL    :      1       :      2       :      3       :      4       :      5       : ----------------------------------------------------------------------------------------------------------------------------------         1 |          1   |  A1         |   1.0000E+00 :   8.0000E-01 :   6.4000E-01 :   5.1190E-01 :   4.0952E-01 :   3.2703E-01 :         2 |          2   |  A2         |   2.0000E+00 :   2.3611E+00 :   1.8889E+00 :   1.5111E+00 :   1.2089E+00 :   9.6712E-01 :         3 |          3   |  A3         |   1.0000E+00 :   8.0000E-01 :   6.4000E-01 :   5.1190E-01 :   4.0952E-01 :   3.2703E-01 :
 ----------------------------------------------------------------------------------------------------------------------------------  INTERNAL |   EXTERNAL   |             |   DV. ID. |    DV. ID.   |    LABEL    |         6    :         7    :         8    :         9    :        10    :        11    : ----------------------------------------------------------------------------------------------------------------------------------         1 |          1   |  A1         |   2.6185E-01 :   2.0927E-01 :   1.6754E-01 :   1.3403E-01 :   1.0723E-01 :   1.0000E-01 :         2 |          2   |  A2         |   7.7369E-01 :   6.1895E-01 :   4.9516E-01 :   3.9613E-01 :   3.1690E-01 :   2.9302E-01 :         3 |          3   |  A3         |   2.6185E-01 :   2.0927E-01 :   1.6754E-01 :   1.3403E-01 :   1.0723E-01 :   1.0000E-01 :
 ----------------------------------------------------------------------------------------------------------------------------------  INTERNAL |   EXTERNAL   |             |   DV. ID. |    DV. ID.   |    LABEL    |        12    :        13    :        14    :        15    :        16    :        17    : ----------------------------------------------------------------------------------------------------------------------------------         1 |          1   |  A1         |   1.0000E-01 :         2 |          2   |  A2         |   2.9302E-01 :         3 |          3   |  A3         |   1.0000E-01 : *** USER INFORMATION MESSAGE 6464 (DOM12E)     RUN TERMINATED DUE TO HARD CONVERGENCE TO AN OPTIMUM AT CYCLE NUMBER =       12.

F = mr
w
2
q
 =
w
t
F
x
 = F cos(
w
t)
F
y
= F sin(
w
t)
q
$$  DATA RELATED TO FREQUENCY RESPONSE$DLOAD   1       1.      1.      11      1.      12RLOAD1  11      20                      111RLOAD1  12      30              40      111DPHASE  40      358     2       90.DAREA   20      358     1       3.DAREA   30      358     2       3.TABLED4 111     0.      1.      0.      100.        0.      39.478  ENDTFREQ1   1       .5      .5      100$ENDDATA
$$     springs.blk$CONM2   3001    1402            1.E8CONM2   3002    1825            1.E8CONM2   3003    1358            1.E8CONM2   3004    1869            1.E8$GRID    1402            159.870 11.0000 -14.3750        13456GRID    1358            20.6116 11.0000 -15.1000        13456    GRID    1825            20.6116 11.0000 -54.9000        13456GRID    1869            159.870 11.0000 -55.6250        13456 $CELAS2  1001    10000.  402     1       1402    1CROD    1002    1002    402     1402 CELAS2  1003    10000.  402     3       1402    3 CELAS2  1011    10000.  825     1       1825    1CROD    1012    1001    825     1825 CELAS2  1013    10000.  825     3       1825    3CELAS2  1021    10000.  358     1       1358    1CROD    1022    1001    358     1358CELAS2  1023    10000.  358     3       1358    3CELAS2  1031    10000.  869     1       1869    1CROD    1032    1002    869     1869CELAS2  1033    10000.  869     3       1869    3$$ properties for springs$PROD    1001    1000    1000.PROD    1002    1000    800.$ select material so that value of PROD is spring stiffness,$  therefore, E = l = 10.MAT1    1000    10.
$$ add dampers for shock absorbers$ frontcvisc   2011    2001    825     1825cvisc   2021    2001    358     1358$ backcvisc   2001    2002    402     1402cvisc   2031    2002    869     1869$ damper propertiespvisc   2001    10.     0. pvisc   2002     5.     0.$$  end of springs.blk$
$$    file    -      car.blk$$    MODEL COURTESY LAPCAD ENGINEERING$    CHULA VISTA, CALIFORNIA$GRID           1         79.0000 56.0000-2.00000                        GRID           2         157.000 40.1000-1.30000                        ..CQUAD4        29       2      22      19      12      21 0.00E+0 0.00E+0CQUAD4        30       2      21      20      11      22 0.00E+0 0.00E+0.. PSHELL         1       1   0.025       1PSHELL         2       1   0.200       1..MAT1           11.000E+73.759E+63.300E-12.600E-41.370E-57.000E+1.3$$    end of car.blk$
$
$    beginning of optim1.blk
$
$ data for design sensitivity
$
$ define design variables
$
desvar,1,frntdamp,1.,.1,10.
desvar,2,reardamp,1.,.2,20.
desvar,3,frntstif,1.,.4,2.
desvar,4,rearstif,1.,.5,2.5
$
$ relation between properties and variables
$
dvprel1,101,pvisc,2001,3,1.,,,,+dv101
+dv101,1,10.
dvprel1,102,pvisc,2002,3,1.,,,,+dv102
+dv102,2,5.
dvprel1,103,prod,1001,4,4.,,,,+dv103
+dv103,3,10.
dvprel1,104,prod,1002,4,4.,,,,+dv104
+dv104,4,8.
$
$
$  select displacement Y at tire and driver seat as
$  response quantities
$
$ maximum tire displacement be < +/-0.5 inches
$
dconstr,101,200,-.5,.5
dresp1,200,disp,frdisp,,,2,,358
$
$ define driver's seat disp as a response
$
$
$ require that maximum driver displacement be < +/- 0.25 inches
$ between .5 and 25 hz
$
dconstr,102,201,-.25,.25,0.5,25.0
dresp1,201,driver,frdisp,,,2,,471
$
$ combine constraints into set 100
$
dconadd,100,101,102
$
$ define objective = minimize srss of response
$
dresp1,300,rss,frdisp,,,2,rss,471
$
$ end of optimization input
$
$ end of                optim1.blk
$

$
$    beginning of optim1.blk
$
$ data for design sensitivity
$
$ define design variables
$
desvar,1,frntdamp,1.,.1,10.
desvar,2,reardamp,1.,.2,20.
desvar,3,frntstif,1.,.4,2.
desvar,4,rearstif,1.,.5,2.5
$
$ relation between properties and variables
$
dvprel1,101,pvisc,2001,3,1.,,,,+dv101
+dv101,1,10.
dvprel1,102,pvisc,2002,3,1.,,,,+dv102
+dv102,2,5.
dvprel1,103,prod,1001,4,4.,,,,+dv103
+dv103,3,10.
dvprel1,104,prod,1002,4,4.,,,,+dv104
+dv104,4,8.
$
$
$  select displacement Y at tire and driver seat as
$  response quantities
$
$ maximum tire displacement be < +/-0.5 inches
$
dconstr,101,200,-.5,.5
dresp1,200,disp,frdisp,,,2,,358
$
$ define driver's seat disp as a response
$
$
$ require that maximum driver displacement be < +/- 0.25 inches
$ between .5 and 25 hz
$
dconstr,102,201,-.25,.25,0.5,25.0
dresp1,201,driver,frdisp,,,2,,471
$
$ combine constraints into set 100
$
dconadd,100,101,102
$
$ define objective = minimize srss of response
$
dresp1,300,rss,frdisp,,,2,rss,471
$
$ end of optimization input
$
$ end of                optim1.blk
$

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title: Презентация на тему: MSC.Nastran 102 2001 - 02

text:
MSC.Nastran Quick Reference Guide:
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MSC.Nastran Quick Reference Guide:
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MSC.Nastran Quick Reference Guide:
MSC.Nastran Quick Reference Guide:


title: Презентация на тему: MSC.Nastran 102 2001 - 20

text:
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/
/
DMI     MXX            0       6       1       0              10      10DMI*    MXX                            1               1  9.62499976E-02*                      3  1.92499999E-02DMI*    MXX                            2               2  1.38867334E-01*                      4  2.67470982E-02               6 -1.37760025E-02*                      8  4.32037748E-03              10  3.94638191E-05..  (rest of MXX).DMI     PHIX           0       2       1       0              10       6 DMI*    PHIX                           1               1 -1.02694275E-17*         3.79799381E-02 -3.21330419E-17  3.09179097E-01  1.62494801E-17*         7.69559503E-01 -1.60461922E-17  1.34014440E+00 -4.83748987E-17*         1.95740056E+00DMI*    PHIX                           2               1  2.53673702E-01*        -3.71932167E-18  7.36189783E-01 -2.11487186E-17  1.14664245E+00*        -1.32509834E-17  1.44485378E+00 -5.04831637E-19  1.60163271E+00*         1.19194476E-17..  (rest of PHIX).ENDDATA
                                                                                MATRIX COR      (GINO NAME 101 ) IS A DB  PREC      6 COLUMN X      6 ROW SQUARE   MATRIX.COLUMN      1      ROWS      1 THRU      6     --------------------------------------------------ROW         1)    5.1380D-01  6.7188D-19  1.8822D-03 -1.6038D-17  8.3091D-03 -1.5467D-16COLUMN      2      ROWS      1 THRU      6     --------------------------------------------------ROW         1)   -1.0247D-17  6.1972D-01  3.1542D-18 -5.7035D-03 -1.0390D-17 -8.8287D-09COLUMN      3      ROWS      1 THRU      6     --------------------------------------------------ROW         1)   -1.5467D-02 -6.3725D-18  6.3014D-01 -2.7673D-17 -4.6145D-03  9.5503D-17COLUMN      4      ROWS      1 THRU      6     --------------------------------------------------ROW         1)    2.5192D-18  1.1390D-02  8.1214D-17  5.8007D-01 -1.0636D-16  7.5993D-03COLUMN      5      ROWS      1 THRU      6     --------------------------------------------------ROW         1)   -1.0452D-17  5.3899D-03 -2.1283D-17 -1.3447D-02  1.2668D-14  7.4474D-01COLUMN      6      ROWS      1 THRU      6     --------------------------------------------------ROW         1)   -3.2927D-03 -2.5409D-18  8.7221D-03 -2.3220D-16 -5.6143D-01  9.6348D-15THE NUMBER OF NON-ZERO TERMS IN THE DENSEST COLUMN =       6THE DENSITY OF THIS MATRIX IS 100.00 PERCENT.^^^CROSS-ORTHOGONALITY MATRIX

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title: Презентация на тему: MSC.Nastran 101 2006 - 6

text:
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MSC Confidential
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i
0.1
0.3
10.+7
1
MAT1
RHO
NU
G
E
MID
MAT1
10
9
8
7
6
5
4
3
2
1
0.15
1
1
0.1
1
2
PSHELL
NSM
TS/T
MID3
121/T3
MID2
T
MID1
PID
PSHELL
10
9
8
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6
5
4
3
2
1
PARAM,GRDPNT,0
125
16
SUPORT
C
ID
C
ID
C
ID
C
ID
SUPORT
10
3.2
0.1
1
EIGRL
NORM
SHFSCL
MAXSET
MSGLVL
ND
V2
V1
SID
EIGRL
10
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2
1


title: Презентация на тему: MSC.Nastran 102 2001 - 06

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title: Презентация на тему: MSC.Nastran 101 2006 - 8


title: Презентация на тему: MSC.Nastran 102 2001 - 05

text:
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title: Презентация на тему: MSC.Nastran 102 2001 - 03

text:
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,
*** 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 = 1.912348D+09, CYCLES = 6.959910D+03 NUMBER OF EIGENVALUES BELOW THIS VALUE = 10
TABLE OF SHIFTS:  (LNNRIGL)
SHIFT #        SHIFT VALUE         FREQUENCY, CYCLES     # EIGENVALUES BELOW    # NEW EIGENVALUES FOUND
     1.        9.4339576E+07          1.5458490E+03                 3                       10
     2.     		1.9123482E+09          6.9599097E+03                10                       0
1    NORMAL MODES EXAMPLE                                   APRIL 8, 1998  MSC.Nastran  4/6/98   PAGE 6

0                                                                                SUBCASE 1
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 ................    10
                         	NUMBER OF SOLVES REQUIRED ............    7
1    NORMAL MODES EXAMPLE                                   APRIL 8, 1998  MSC.Nastran  4/6/98   PAGE 7

0                                                                                SUBCASE 1

                                      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
  6      	6       2.328801E+08     1.526041E+04     2.428770E+03     1.000000E+00     2.328801E+08
  7      	7       6.845924E+08     2.616472E+04     4.164244E+03     1.000000E+00     6.845924E+08
  8      	8       9.602215E+08     3.098744E+04     4.931804E+03     1.000000E+00     9.602215E+08
  9      	9       1.365611E+09     3.695418E+04     5.881439E+03     1.000000E+00     1.365611E+09
 10           10       1.855386E+09     4.307420E+04     6.855471E+03     1.000000E+00	1.855386E+09
1    NORMAL MODES EXAMPLE                             APRIL 8, 1998  MSC.Nastran  4/6/98   PAGE    8
0                                                                                SUBCASE 1
1    NORMAL MODES EXAMPLE                             APRIL 8, 1998  MSC.Nastran  4/6/98   PAGE    9
      USING LANCZOS
0                                                                                SUBCASE 1
      EIGENVALUE =  7.056994E+05
          CYCLES =  1.336996E+02      R E A L   E I G E N V E C T O R   N O .          1

      POINT ID.  TYPE         T1             T2             T3             R1             R2       R3
            1     G        .0             .0             .0             .0             .0          .0
            2     G     -3.515604E-14  -2.083550E-14  -9.748799E-01  -1.090191E+00   4.011783E+00  .0
            3     G     -5.976152E-14  -6.029845E-14  -4.170314E+00  -1.593278E+00   8.679599E+00  .0

            4     G     -6.872012E-14  -1.060940E-13  -9.445755E+00  -1.531076E+00   1.230244E+01  .0
            5     G     -6.341396E-14  -1.494814E-13  -1.636251E+01  -1.362968E+00   1.522316E+01  .0
                                                       .
                                                       .
                                                       .
            54    G     -2.994638E-14  -1.751692E-13  -6.384793E+01   2.199729E-01   2.066229E+01  .0
            55    G     -2.713030E-14  -1.739597E-13  -7.419337E+01   1.691507E-01   2.070036E+01  .0
                                                       .
                                                       .
                                                       .
                                                       .
                                                       .
                                                       .
      EIGENVALUE =  1.878432E+07
          CYCLES =  6.897916E+02      R E A L   E I G E N V E C T O R   N O .          2

      POINT ID.   TYPE        T1            T2             T3              R1             R2       R3

	1      G      .0             .0             .0             .0             .0           .0
	2      G     2.689105E-14   2.049585E-14  -6.305859E+00   5.289161E+00   2.135918E+01  .0
	3      G     4.441315E-14   5.120965E-14  -1.933128E+01   1.932312E+01   2.758354E+01   0
	4      G     5.540902E-14   8.667080E-14  -3.398484E+01   3.400354E+01   2.819633E+01  .0
	5      G     6.112096E-14   1.273261E-13  -4.831832E+01   4.840071E+01   2.654789E+01  .0
	6      G     6.240562E-14   1.721406E-13  -6.144451E+01   6.153912E+01   2.363943E+01  .0
	7      G     5.830800E-14   2.121037E-13  -7.283444E+01   7.294494E+01   1.992698E+01  .0
                                                       .
                                                       .
                                                       .
	53      G   -8.359115E-14   2.867785E-13   8.914771E+01   8.923321E+01  -1.121007E+01  .0
	54      G   -8.422337E-14   3.180499E-13   9.390352E+01   9.367941E+01  -7.136850E+00  .0
	55      G   -8.453551E-14   3.525693E-13   9.704356E+01   9.580685E+01  -5.385391E+00  .0


title: Презентация на тему: MSC.Nastran 102 2001 - 00

text:
MSC.Nastran 2001

Slide Title
Body Text
Second Level
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Fifth Level
Body Text
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MSC Corporate Overview Speaker Notes
Corporate
MSC.Software Corporation
815 Colorado Boulevard
Los Angeles, CA 90041-1777
Telephone: (323) 258-9111 or (800) 336-4858
FAX: (323) 259-3638
Europe
MSC.Software Corporation
Innsbrucker Ring 15
Postfach 80 12 40
81612 MUNCHEN, GERMANY
Telephone: (49) (89) 43 19 87 0
Fax: (49) (89) 43 61 71 6
Asia Pacific
MSC.Software Corporation
Entsuji-Gadelius Building
2-39, Akasaka 5-chome
Minato-ku, TOKYO 107-0052, JAPAN
Telephone: (81) (3) 3505 0266
Fax: (81) (3) 3505 0914
Worldwide Web
www.mscsoftware.com

Disclaimer
MSC.Software Corporation reserves the right to make changes in specifications and other information contained in this document without prior notice.
The concepts, methods, and examples presented in this text are for illustrative and educational purposes only, and are not intended to be exhaustive or to apply to any particular engineering problem or design. MSC.Software Corporation assumes no liability or responsibility to any person or company for direct or indirect damages resulting from the use of any information contained herein.
User Documentation: Copyright ©  2001 MSC.Software Corporation. Printed in U.S.A. All Rights Reserved.
This notice shall be marked on any reproduction of this documentation, in whole or in part. Any reproduction or distribution of this document, in whole or in part, without the prior written consent of MSC.Software Corporation is prohibited.
MSC and MSC. are registered trademarks and service marks of MSC.Software Corporation. NASTRAN is a registered trademark of the National Aeronautics and Space Administration. MSC.Nastran is an enhanced proprietary version developed and maintained by MSC.Software Corporation. MSC.Patran is a trademark of MSC.Software Corporation.
All other trademarks are the property of their respective owners.
NA*V2001*Z*Z*Z*SM-NAS102-NT1


title: Презентация на тему: MSC.Nastran 102 2001 - 09

text:
Slide Title
Body Text
Second Level
Third Level
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Body Text
Second Level
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MSC Corporate Overview Speaker Notes


title: Презентация на тему: MSC.Nastran 101 2006 - 3

text:
TEMPD
TITLE = GARAGE ROOF FRAME
SUBTITLE = WOOD AND STEEL MEMBERS
SUBCASE 1
   SUBTITLE=TRUSS_LBCS
   LOAD = 1
   DISPLACEMENT = ALL
   SPCFORCES = ALL
   STRESS = ALL
   SPC = 10
SUBCASE 20
   SUBTITLE = THERMAL LOAD
   TEMP(INIT) = 20
   TEMP(LOAD) = 26
   DISPLACEMENT = ALL
   SPCFORCES = ALL
   STRESS = ALL
   SPC = 10
SUBCASE 30
   SUBTITLE = GRAVITY LOAD
   LOAD = 30
   DISPLACEMENT = ALL
   SPCFORCES = ALL
   STRESS = ALL
   SPC = 10
BEGIN BULK
TEMPD,20,70.
TEMPD,26,100.
GRAV,30,,386.0886,0.,-1.,0.
$ The rest of the input file is
$ unchanged from workshop 2
Click to edit Master title style
Click to edit Master text styles
Second level
Third level
Fourth level
Fifth level
MSC Confidential
Body Text
Second Level
Third Level
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MSC Corporate Overview Speaker Notes
386.4 in/sec2
386.4 in/sec2
24000 psi
1900 psi
24000 psi
1900 psi
24000 psi
72 deg.F
72 deg.F
0.32
TEMP(INIT)
TEMP(LOAD)
TEMPD
TITLE = GARAGE ROOF FRAME
SUBTITLE = WOOD AND STEEL MEMBERS
SUBCASE 1
   SUBTITLE=TRUSS_LBCS
   LOAD = 1
   DISPLACEMENT = ALL
   SPCFORCES = ALL
   STRESS = ALL
   SPC = 10
SUBCASE 20
   SUBTITLE = THERMAL LOAD
   TEMP(INIT) = 20
   TEMP(LOAD) = 26
   DISPLACEMENT = ALL
   SPCFORCES = ALL
   STRESS = ALL
   SPC = 10
SUBCASE 30
   SUBTITLE = GRAVITY LOAD
   LOAD = 30
   DISPLACEMENT = ALL
   SPCFORCES = ALL
   STRESS = ALL
   SPC = 10
BEGIN BULK
TEMPD,20,70.
TEMPD,26,100.
GRAV,30,,386.0886,0.,-1.,0.
$ The rest of the input file is
$ unchanged from workshop 2


title: Презентация на тему: MSC.Nastran 101 2006 - 7

text:
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MSC Confidential
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SUBCASE 2

METHOD = N
STATSUB = i
SUBCASE 1LOAD = M
10
3.2
0.1
1
EIGRL
NORM
SHFSCL
MAXSET
MSGLVL
ND
V2
V1
SID
EIGRL
10
9
8
7
6
5
4
3
2
1

7
7
7
2
2
2
1
1
x
y
K5 = 100. , K6 = 120
100


title: Презентация на тему: MSC.Nastran 102 2001 - 04

text:
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2
5
 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        43        7.057454E+05        8.400865E+02        1.337039E+02        1.000000E+00        7.057454E+05        2        45        1.880877E+07        4.336908E+03        6.902404E+02        1.000000E+00        1.880877E+07        3        44        2.818009E+07        5.308492E+03        8.448727E+02        1.000000E+00        2.818009E+07        4        42        1.956108E+08        1.398609E+04        2.225956E+03        1.000000E+00        1.956108E+08        5        41        2.367820E+08        1.538772E+04        2.449032E+03        1.000000E+00        2.367820E+08        6        40        7.114644E+08        2.667329E+04        4.245186E+03         .0                  .0        7        38        1.011468E+09        3.180359E+04        5.061698E+03         .0                  .0        8        39        1.399003E+09        3.740325E+04        5.952912E+03         .0                  .0        9        36        2.010170E+09        4.483492E+04        7.135699E+03         .0                  .0       10        37        2.030104E+09        4.505668E+04        7.170993E+03         .0                  .0       11        35        3.226556E+09        5.680278E+04        9.040443E+03         .0                  .0       12        34        3.629181E+09        6.024268E+04        9.587920E+03         .0                  .0       13        33        4.912542E+09        7.008953E+04        1.115509E+04         .0                  .0       14        32        6.537906E+09        8.085732E+04        1.286884E+04         .0                  .0       15        31        1.160219E+10        1.077134E+05        1.714313E+04         .0                  .0       16        30        1.399534E+10        1.183019E+05        1.882833E+04         .0                  .0       17        29        1.633258E+10        1.277990E+05        2.033984E+04         .0                  .0       18        28        2.118600E+10        1.455541E+05        2.316566E+04         .0                  .0       19        27        2.394404E+10        1.547386E+05        2.462741E+04         .0                  .0       20        26        2.859707E+10        1.691067E+05        2.691416E+04         .0                  .0       21        25        2.915433E+10        1.707464E+05        2.717513E+04         .0                  .0       22        24        3.734805E+10        1.932564E+05        3.075772E+04         .0                  .0       23        23        3.752350E+10        1.937098E+05        3.082988E+04         .0                  .0       24        22        4.883849E+10        2.209943E+05        3.517234E+04         .0                  .0       25        21        5.044853E+10        2.246075E+05        3.574739E+04         .0                  .0       26        20        5.823102E+10        2.413110E+05        3.840584E+04         .0                  .0       27        19        1.070747E+11        3.272227E+05        5.207910E+04         .0                  .0       28        18        1.194176E+11        3.455685E+05        5.499893E+04         .0                  .0       29        17        1.457577E+11        3.817823E+05        6.076254E+04         .0                  .0       30        16        1.852473E+11        4.304036E+05        6.850086E+04         .0                  .0       31        12        1.992662E+11        4.463924E+05        7.104556E+04         .0                  .0       32        13        2.096219E+11        4.578448E+05        7.286827E+04         .0                  .0       33        15        2.158487E+11        4.645952E+05        7.394262E+04         .0                  .0       34        14        2.167496E+11        4.655638E+05        7.409677E+04         .0                  .0       35        11        3.969222E+11        6.300176E+05        1.002704E+05         .0                  .0       36        10        4.039548E+11        6.355744E+05        1.011548E+05         .0                  .0       37         9        5.184081E+11        7.200056E+05        1.145925E+05         .0                  .0       38         8        3.900314E+12        1.974921E+06        3.143185E+05         .0                  .0       39         7        3.920771E+12        1.980094E+06        3.151417E+05         .0                  .0       40         6        5.156148E+12        2.270715E+06        3.613955E+05         .0                  .0       41         5        2.977769E+15        5.456894E+07        8.684916E+06         .0                  .0       42         4        3.462917E+15        5.884656E+07        9.365720E+06         .0                  .0       43         3        6.992731E+15        8.362255E+07        1.330894E+07         .0                  .0       44         2        1.321399E+16        1.149521E+08        1.829520E+07         .0                  .0       45         1        1.671511E+18        1.292869E+09        2.057665E+08         .0                  .0
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title: Презентация на тему: MSC.Nastran 101 2006 - App. A

text:
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Second level
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MSC Confidential
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Release Guide
Configuration and Operations Guide
Common Questions & Answers
Bibliography
Online Encyclopedia CD-ROM
Quick Reference Guide
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