ME670 Homework #4 x y z F 0.6" 6" y z 18" 18" 18" 18" 1 4 6 8 10 2 3 5 7 9 1 2 3 4 (1) Run the NASTRAN job as illustrated in the laboratory manual. (2) Remove the boundary condition of rotation into the y axis and re-run the NASTRAN job as illustrated in the laboratory manual. (3) Increase the number of elements to 8 by making each element to have a dimension of 9”x6”. Run Nastran and report the results. x y z F 0.6" 6" y z 1 2 3 4 5 6 7 8 3 4 1 2 5 6 7 8 9 10 11 12 13 14 15 16 17 18 (4) Increase the number of element to 8 by making each element to have a dimension of 18”x3”. Run Nastran and report the results. z x y z F 0.6" 6" y z 1 2 3 4 5 6 7 8 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 (5) Use the closed form solution to find all stresses and displacements. Compare to the 4 solutions listed above.
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ME670 Homework #4
x
y
z F
0.6"
6"y
z
18" 18" 18" 18"1 4 6 8 10
2 3 5 7 9
1 2 3 4
(1) Run the NASTRAN job as illustrated in the laboratory manual.
(2) Remove the boundary condition of rotation into the y axis and re-run the
NASTRAN job as illustrated in the laboratory manual.
(3) Increase the number of elements to 8 by making each element to have a dimension of 9”x6”. Run Nastran and report the results.
x
y
z F
0.6"
6"y
z
1 2 3 4 5 6 7 8
3
41
2 5
6
7
8
9
10
11
12
13
14
15
16
17
18
(4) Increase the number of element to 8 by making each element to have a dimension
of 18”x3”. Run Nastran and report the results.
z
x
y
z F
0.6"
6"y
z
1 2 3 4
5 6 7 8
1
2
3 4
5
6
7
8
9
10
11
12
13
14
15
(5) Use the closed form solution to find all stresses and displacements. Compare to
the 4 solutions listed above.
cquad4.bdf 2/8/2007
$ EXECUTIVE CONTROL SECTIONID Dr. S. BawabSOL 24TIME 10CEND$ CASE CONTROL SECTIONTITLE=CANTILEVER BEAM USING QUAD4 ELEMENTSSET 1=7,8,9,10DISPL=ALLSTRESS=ALLSPC=100SUBCASE 1SUBTITLE=10 LB. LOAD CASELOAD=100SUBCASE 2SUBTITLE=20 LB. LOAD CASELOAD=200SUBCASE 3SUBTITLE=30 LB. LOAD CASELOAD=300SUBCASE 4SUBTITLE = PRESSURE LOADSPC = 200LOAD = 500SUBCOM 5SUBTITLE = COMBINATION LOADSSUBSEQ = 1.0, 1.0, 0.0, 0.0$ BULK DATA SECTIONBEGIN BULKGRID,1,,0.,0.,-3.GRID,2,,0.,0.,+3.GRID,3,,18.,0.,3.GRID,4,,18.,0.,-3.GRID,5,,36.,0.,3.GRID,6,,36.,0.,-3.GRID,7,,54.,0.,3.GRID,8,,54.,0.,-3.GRID,9,,72.,0.,3.GRID,10,,72.,0.,-3.SPC1,100,123456,1,2SPC1,100,5,3,THRU,10SPC1,200,123456,1,2SPC1,200,5,3,THRU,10PLOAD2, 500, 10., 4FORCE,100,9,,10.,0.,0.,-1.FORCE,200,9,,20.,0.,0.,-1.FORCE,300,9,,30.,0.,0.,-1.CQUAD4,1,100,1,4,3,2CQUAD4,2,100,4,6,5,3
1
cquad4.bdf 2/8/2007
CQUAD4,3,100,6,8,7,5CQUAD4,4,100,8,10,9,7PSHELL,100,10,.6,10MAT1,10,3.+7,,0.33,.00073575ENDDATA
2
cquad4.f06 2/8/2007
1
THIS PROGRAM IS CONFIDENTIAL AND A TRADE SECRET OF MSC.SOFTWARE CORPORATION. THE RECEIPT ORPOSSESSION OF THIS PROGRAM DOES NOT CONVEY ANY RIGHTS TO REPRODUCE OR DISCLOSE ITS CONTENTS, OR TOMANUFACTURE, USE, OR SELL ANYTHING HEREIN, IN WHOLE OR IN PART, WITHOUT THE SPECIFIC WRITTEN CONSENT
OF MSC.SOFTWARE CORPORATION.
* * * * * * * * * * * * * * * * * * * ** * * * * * * * * * * * * * * * * * * ** * * ** * MSC.SOFTWARE * ** * CORP * ** * * ** * M S C . N a s t r a n * ** * * ** * * ** * * ** * Version 2005.1.0 * ** * 2005R2 * ** * * ** * * ** * JUN 17, 2005 * ** * * ** * Sun Microsystems Computer Co. * ** * MODEL UltraSPARC/1062 (acadia) * ** * SunOS 5.8 * ** * COMPILED FOR v9a(64-bit) * ** * * ** * * * * * * * * * * * * * * * * * * ** * * * * * * * * * * * * * * * * * * *
1News file - (6/03/05):
Thank you for choosing MSC.Nastran, the industry standard in FEA, and Welcometo MSC.Nastran 2005 r2.
You can find version-specific online documentation, and online technical supportat:
http://www.mscsoftware.com/support/prod_support/nastran/
Also at the technical support location is a searchable list of technicalapplication notes and the current error/avoidance list. Please don't hesitateto contact your nearest technical support representative if you requireassistance.
http://www.mscsoftware.com/about/locate/
The arbitrary beam cross section, explicit nonlinear (SOL 700), and the newnonlinear (SOL 400) solution sequences, are regarded as pre-release capabilitiesand are still undergoing testing and verification. These capabilities shouldnot be employed in any analysis except for the purpose of testing and verifyingthe functionality and working of the capabilities themselves.
MSC.Nastran 2005 r2 is mainly focused on improving quality, accuracy andease-of-use, but also introduces new capabilities, some of which were madeavailable as pre-release functionality in MSC.Nastran 2005 r1. In addition,
1
cquad4.f06 2/8/2007
significant advancements have been made regarding performance and scalability ofthe program. Some of the new features and enhancements are listed below.
Nonlinear- MSC.Nastran Implicit Nonlinear (SOL 600) - We have addressed many knownissues, improved memory usage, improved output options, added beam, bar, andshell offsets, and thermal contact
- MSC.Nastran Explicit Nonlinear (SOL 700) pre-release - you can nowexecute LS-Dyna from inside MSC.Nastran to perform crash and impactanalyses
Numeric Enhancements- Multi-level DMP - an enhanced Lanczos modal extraction methodology thatimproves scalability and efficiently handles large normal modes analyses withvery frequency ranges
- MDACMS enhanced robustness, improved handling of large masses, and improvedperformance
- Distributed memory parallel MPYAD
Elements- CFAST - a new fastener element based on user defined stiffness values.- Arbitrary beam cross section pre-release capability - you can specify crosssection shapes using POINT entries, and optimize them in SOL 200
- Enhanced nonstructural mass element summary printout - ELSUM1- spatially dependent heat transfer coefficient- Heat transfer coefficient as a function of two variables- Thermal analysis flux output
Optimization- MSC.Nastran Topology Optimization - this addition to the existing SOL 200optimization solution sequence allows optimization analyses to be performedthat require many design variables
Further Enhancements- Larger XDB database support- MATMOD option 16 - we have removed many previous limitations with thismatrix output capability
- K6ROT stiffness removed for membrane elements1 FEBRUARY 8, 2007 MSC.NASTRAN 6/17/05 PAGE 1
0 N A S T R A N F I L E A N D S Y S T E M P A R A M E T E R E C H O0
NASTRAN OP2NEW=0 $ MSC.NASTRAN .LCL FILENASTRAN BUFFSIZE=8193 $(/AFS/LIONS/SUN4X_58/DEP/CAE/MSC2005/CONF/NAST20051RC[3])$ EXECUTIVE CONTROL SECTION
1 FEBRUARY 8, 2007 MSC.NASTRAN 6/17/05 PAGE 2
0 N A S T R A N E X E C U T I V E C O N T R O L E C H O0
ID DR. S. BAWABSOL 24
*** USER WARNING MESSAGE 814 (XCSSUB)SOLUTION SEQUENCE 24 HAS BEEN REPLACED.USER INFORMATION: ALTERNATE SOLUTION SEQUENCE 1 WILL BE EXECUTED.TIME 10CEND
2
cquad4.f06 2/8/2007
1 CANTILEVER BEAM USING QUAD4 ELEMENTS FEBRUARY 8, 2007 MSC.NASTRAN 6/17/05 PAGE 3
00 C A S E C O N T R O L E C H O
COMMANDCOUNT1 $ CASE CONTROL SECTION2 TITLE=CANTILEVER BEAM USING QUAD4 ELEMENTS3 SET 1=7,8,9,104 DISPL=ALL5 STRESS=ALL6 SPC=1007 SUBCASE 18 SUBTITLE=10 LB. LOAD CASE9 LOAD=10010 SUBCASE 211 SUBTITLE=20 LB. LOAD CASE12 LOAD=20013 SUBCASE 314 SUBTITLE=30 LB. LOAD CASE15 LOAD=30016 SUBCASE 417 SUBTITLE = PRESSURE LOAD18 SPC = 20019 LOAD = 50020 SUBCOM 521 SUBTITLE = COMBINATION LOADS22 SUBSEQ = 1.0, 1.0, 0.0, 0.023 $ BULK DATA SECTION24 BEGIN BULK
*** USER WARNING MESSAGE 4699 (FREFLD)THE FREE FIELD BULK DATA ENTRY BELOW HAS A REAL FIELD WITH MORE THAN 8 CHARACTERS. SOME PRECISION MAY BE LOST.MAT1,10,3.+7,,0.33,.00073575
0 INPUT BULK DATA ENTRY COUNT = 251 CANTILEVER BEAM USING QUAD4 ELEMENTS FEBRUARY 8, 2007 MSC.NASTRAN 6/17/05 PAGE 4
00 S O R T E D B U L K D A T A E C H O
ENTRYCOUNT . 1 .. 2 .. 3 .. 4 .. 5 .. 6 .. 7 .. 8 .. 9 .. 10 .
1- CQUAD4 1 100 1 4 3 22- CQUAD4 2 100 4 6 5 33- CQUAD4 3 100 6 8 7 54- CQUAD4 4 100 8 10 9 75- FORCE 100 9 10. 0. 0. -1.6- FORCE 200 9 20. 0. 0. -1.7- FORCE 300 9 30. 0. 0. -1.8- GRID 1 0. 0. -3.9- GRID 2 0. 0. +3.10- GRID 3 18. 0. 3.11- GRID 4 18. 0. -3.12- GRID 5 36. 0. 3.13- GRID 6 36. 0. -3.14- GRID 7 54. 0. 3.15- GRID 8 54. 0. -3.16- GRID 9 72. 0. 3.17- GRID 10 72. 0. -3.18- MAT1 10 3.+7 0.33 7.358-419- PLOAD2 500 10. 420- PSHELL 100 10 .6 10
3
cquad4.f06 2/8/2007
21- SPC1 100 5 3 THRU 1022- SPC1 100 123456 1 223- SPC1 200 5 3 THRU 1024- SPC1 200 123456 1 2
ENDDATA0 TOTAL COUNT= 25
M O D E L S U M M A R Y
NUMBER OF GRID POINTS = 10
NUMBER OF CQUAD4 ELEMENTS = 4
*** SYSTEM INFORMATION MESSAGE 6916 (DFMSYN)DECOMP ORDERING METHOD CHOSEN: BEND, ORDERING METHOD USED: BEND
*** USER INFORMATION MESSAGE 5293 (SSG3A)FOR DATA BLOCK KLLLOAD SEQ. NO. EPSILON EXTERNAL WORK EPSILONS LARGER THAN 0.001 ARE FLAGGED WITH ASTERISKS
1 4.9098616E-12 1.7226920E-022 4.9098616E-12 6.8907678E-023 2.3782807E-12 1.5504228E-01
*** SYSTEM INFORMATION MESSAGE 6916 (DFMSYN)DECOMP ORDERING METHOD CHOSEN: BEND, ORDERING METHOD USED: BEND
*** USER INFORMATION MESSAGE 5293 (SSG3A)FOR DATA BLOCK KLLLOAD SEQ. NO. EPSILON EXTERNAL WORK EPSILONS LARGER THAN 0.001 ARE FLAGGED WITH ASTERISKS
4 5.9233135E-12 1.4648111E+041 CANTILEVER BEAM USING QUAD4 ELEMENTS FEBRUARY 8, 2007 MSC.NASTRAN 6/17/05 PAGE 5
10 LB. LOAD CASE0 SUBCASE 1
D I S P L A C E M E N T V E C T O R
POINT ID. TYPE T1 T2 T3 R1 R2 R31 G 0.0 0.0 0.0 0.0 0.0 0.02 G 0.0 0.0 0.0 0.0 0.0 0.03 G 9.599009E-05 0.0 -2.923512E-04 0.0 0.0 0.04 G -9.599575E-05 0.0 -2.923569E-04 0.0 0.0 0.05 G 1.634695E-04 0.0 -1.075013E-03 0.0 0.0 0.06 G -1.634582E-04 0.0 -1.074990E-03 0.0 0.0 0.07 G 2.034862E-04 0.0 -2.180098E-03 0.0 0.0 0.08 G -2.035372E-04 0.0 -2.180184E-03 0.0 0.0 0.09 G 2.168796E-04 0.0 -3.445384E-03 0.0 0.0 0.010 G -2.166982E-04 0.0 -3.445063E-03 0.0 0.0 0.0
1 CANTILEVER BEAM USING QUAD4 ELEMENTS FEBRUARY 8, 2007 MSC.NASTRAN 6/17/05 PAGE 620 LB. LOAD CASE
0 SUBCASE 2
D I S P L A C E M E N T V E C T O R
POINT ID. TYPE T1 T2 T3 R1 R2 R31 G 0.0 0.0 0.0 0.0 0.0 0.02 G 0.0 0.0 0.0 0.0 0.0 0.03 G 1.919802E-04 0.0 -5.847024E-04 0.0 0.0 0.04 G -1.919915E-04 0.0 -5.847138E-04 0.0 0.0 0.05 G 3.269390E-04 0.0 -2.150026E-03 0.0 0.0 0.06 G -3.269163E-04 0.0 -2.149980E-03 0.0 0.0 0.07 G 4.069724E-04 0.0 -4.360196E-03 0.0 0.0 0.08 G -4.070745E-04 0.0 -4.360368E-03 0.0 0.0 0.0
4
cquad4.f06 2/8/2007
9 G 4.337593E-04 0.0 -6.890768E-03 0.0 0.0 0.010 G -4.333964E-04 0.0 -6.890127E-03 0.0 0.0 0.0
1 CANTILEVER BEAM USING QUAD4 ELEMENTS FEBRUARY 8, 2007 MSC.NASTRAN 6/17/05 PAGE 730 LB. LOAD CASE
0 SUBCASE 3
D I S P L A C E M E N T V E C T O R
POINT ID. TYPE T1 T2 T3 R1 R2 R31 G 0.0 0.0 0.0 0.0 0.0 0.02 G 0.0 0.0 0.0 0.0 0.0 0.03 G 2.879702E-04 0.0 -8.770536E-04 0.0 0.0 0.04 G -2.879873E-04 0.0 -8.770708E-04 0.0 0.0 0.05 G 4.904084E-04 0.0 -3.225039E-03 0.0 0.0 0.06 G -4.903745E-04 0.0 -3.224970E-03 0.0 0.0 0.07 G 6.104586E-04 0.0 -6.540294E-03 0.0 0.0 0.08 G -6.106117E-04 0.0 -6.540551E-03 0.0 0.0 0.09 G 6.506389E-04 0.0 -1.033615E-02 0.0 0.0 0.010 G -6.500946E-04 0.0 -1.033519E-02 0.0 0.0 0.0
1 CANTILEVER BEAM USING QUAD4 ELEMENTS FEBRUARY 8, 2007 MSC.NASTRAN 6/17/05 PAGE 8PRESSURE LOAD
0 SUBCASE 4
D I S P L A C E M E N T V E C T O R
POINT ID. TYPE T1 T2 T3 R1 R2 R31 G 0.0 0.0 0.0 0.0 0.0 0.02 G 0.0 0.0 0.0 0.0 0.0 0.03 G 0.0 -2.924907E+00 0.0 -2.043789E-02 0.0 -3.089499E-014 G 0.0 -2.924907E+00 0.0 2.043789E-02 0.0 -3.089499E-015 G 0.0 -1.061024E+01 0.0 -7.348453E-03 0.0 -5.289359E-016 G 0.0 -1.061024E+01 0.0 7.348453E-03 0.0 -5.289359E-017 G 0.0 -2.123939E+01 0.0 -3.628299E-03 0.0 -6.360417E-018 G 0.0 -2.123939E+01 0.0 3.628299E-03 0.0 -6.360417E-019 G 0.0 -3.301287E+01 0.0 -4.133505E-04 0.0 -6.641026E-0110 G 0.0 -3.301287E+01 0.0 4.133505E-04 0.0 -6.641026E-01
1 CANTILEVER BEAM USING QUAD4 ELEMENTS FEBRUARY 8, 2007 MSC.NASTRAN 6/17/05 PAGE 9COMBINATION LOADS
0 SUBCOM 5
D I S P L A C E M E N T V E C T O R
POINT ID. TYPE T1 T2 T3 R1 R2 R31 G 0.0 0.0 0.0 0.0 0.0 0.02 G 0.0 0.0 0.0 0.0 0.0 0.03 G 2.879703E-04 0.0 -8.770535E-04 0.0 0.0 0.04 G -2.879873E-04 0.0 -8.770707E-04 0.0 0.0 0.05 G 4.904085E-04 0.0 -3.225039E-03 0.0 0.0 0.06 G -4.903745E-04 0.0 -3.224970E-03 0.0 0.0 0.07 G 6.104586E-04 0.0 -6.540294E-03 0.0 0.0 0.08 G -6.106117E-04 0.0 -6.540551E-03 0.0 0.0 0.09 G 6.506389E-04 0.0 -1.033615E-02 0.0 0.0 0.010 G -6.500946E-04 0.0 -1.033519E-02 0.0 0.0 0.0
1 CANTILEVER BEAM USING QUAD4 ELEMENTS FEBRUARY 8, 2007 MSC.NASTRAN 6/17/05 PAGE 1010 LB. LOAD CASE
0 SUBCASE 1
S T R E S S E S I N Q U A D R I L A T E R A L E L E M E N T S ( Q U A D 4 )ELEMENT FIBER STRESSES IN ELEMENT COORD SYSTEM PRINCIPAL STRESSES (ZERO SHEAR)ID. DISTANCE NORMAL-X NORMAL-Y SHEAR-XY ANGLE MAJOR MINOR VON MISES
5
cquad4.f06 2/8/2007
0 1 -3.000000E-01 -1.421085E-12 1.431791E-02 -2.741416E+00 -45.0748 2.748584E+00 -2.734266E+00 4.748293E+003.000000E-01 -1.421085E-12 1.431791E-02 -2.741416E+00 -45.0748 2.748584E+00 -2.734266E+00 4.748293E+00
0 2 -3.000000E-01 -9.473903E-13 -4.295427E-02 -2.679970E+00 -44.7704 2.658578E+00 -2.701533E+00 4.642042E+003.000000E-01 -9.473903E-13 -4.295427E-02 -2.679970E+00 -44.7704 2.658578E+00 -2.701533E+00 4.642042E+00
0 3 -3.000000E-01 -1.326346E-12 1.575008E-01 -2.639553E+00 -45.8545 2.719478E+00 -2.561977E+00 4.574552E+003.000000E-01 -1.326346E-12 1.575008E-01 -2.639553E+00 -45.8545 2.719478E+00 -2.561977E+00 4.574552E+00
0 4 -3.000000E-01 0.0 -5.870547E-01 -2.619508E+00 -41.8032 2.342375E+00 -2.929430E+00 4.574943E+003.000000E-01 0.0 -5.870547E-01 -2.619508E+00 -41.8032 2.342375E+00 -2.929430E+00 4.574943E+00
1 CANTILEVER BEAM USING QUAD4 ELEMENTS FEBRUARY 8, 2007 MSC.NASTRAN 6/17/05 PAGE 1120 LB. LOAD CASE
0 SUBCASE 2
S T R E S S E S I N Q U A D R I L A T E R A L E L E M E N T S ( Q U A D 4 )ELEMENT FIBER STRESSES IN ELEMENT COORD SYSTEM PRINCIPAL STRESSES (ZERO SHEAR)ID. DISTANCE NORMAL-X NORMAL-Y SHEAR-XY ANGLE MAJOR MINOR VON MISES
0 1 -3.000000E-01 -2.842171E-12 2.863582E-02 -5.482832E+00 -45.0748 5.497169E+00 -5.468533E+00 9.496587E+003.000000E-01 -2.842171E-12 2.863582E-02 -5.482832E+00 -45.0748 5.497169E+00 -5.468533E+00 9.496587E+00
0 2 -3.000000E-01 -1.894781E-12 -8.590853E-02 -5.359939E+00 -44.7704 5.317157E+00 -5.403066E+00 9.284084E+003.000000E-01 -1.894781E-12 -8.590853E-02 -5.359939E+00 -44.7704 5.317157E+00 -5.403066E+00 9.284084E+00
0 3 -3.000000E-01 -2.652693E-12 3.150015E-01 -5.279106E+00 -45.8545 5.438956E+00 -5.123954E+00 9.149104E+003.000000E-01 -2.652693E-12 3.150015E-01 -5.279106E+00 -45.8545 5.438956E+00 -5.123954E+00 9.149104E+00
0 4 -3.000000E-01 0.0 -1.174109E+00 -5.239016E+00 -41.8032 4.684750E+00 -5.858859E+00 9.149885E+003.000000E-01 0.0 -1.174109E+00 -5.239016E+00 -41.8032 4.684750E+00 -5.858859E+00 9.149885E+00
1 CANTILEVER BEAM USING QUAD4 ELEMENTS FEBRUARY 8, 2007 MSC.NASTRAN 6/17/05 PAGE 1230 LB. LOAD CASE
0 SUBCASE 3
S T R E S S E S I N Q U A D R I L A T E R A L E L E M E N T S ( Q U A D 4 )ELEMENT FIBER STRESSES IN ELEMENT COORD SYSTEM PRINCIPAL STRESSES (ZERO SHEAR)ID. DISTANCE NORMAL-X NORMAL-Y SHEAR-XY ANGLE MAJOR MINOR VON MISES
0 1 -3.000000E-01 -4.547474E-12 4.295373E-02 -8.224248E+00 -45.0748 8.245752E+00 -8.202799E+00 1.424488E+013.000000E-01 -4.547474E-12 4.295373E-02 -8.224248E+00 -45.0748 8.245752E+00 -8.202799E+00 1.424488E+01
0 2 -3.000000E-01 -3.410605E-12 -1.288628E-01 -8.039908E+00 -44.7704 7.975735E+00 -8.104598E+00 1.392613E+013.000000E-01 -3.410605E-12 -1.288628E-01 -8.039908E+00 -44.7704 7.975735E+00 -8.104598E+00 1.392613E+01
0 3 -3.000000E-01 -1.515824E-12 4.725023E-01 -7.918659E+00 -45.8545 8.158434E+00 -7.685931E+00 1.372366E+013.000000E-01 -1.515824E-12 4.725023E-01 -7.918659E+00 -45.8545 8.158434E+00 -7.685931E+00 1.372366E+01
0 4 -3.000000E-01 -4.547474E-12 -1.761164E+00 -7.858524E+00 -41.8032 7.027124E+00 -8.788289E+00 1.372483E+013.000000E-01 -4.547474E-12 -1.761164E+00 -7.858524E+00 -41.8032 7.027124E+00 -8.788289E+00 1.372483E+01
1 CANTILEVER BEAM USING QUAD4 ELEMENTS FEBRUARY 8, 2007 MSC.NASTRAN 6/17/05 PAGE 13PRESSURE LOAD
0 SUBCASE 4
S T R E S S E S I N Q U A D R I L A T E R A L E L E M E N T S ( Q U A D 4 )ELEMENT FIBER STRESSES IN ELEMENT COORD SYSTEM PRINCIPAL STRESSES (ZERO SHEAR)ID. DISTANCE NORMAL-X NORMAL-Y SHEAR-XY ANGLE MAJOR MINOR VON MISES
0 1 -3.000000E-01 1.620000E+05 2.280317E+04 -7.200166E-09 0.0000 1.620000E+05 2.280317E+04 1.518877E+053.000000E-01 -1.620000E+05 -2.280317E+04 7.200166E-09 90.0000 -2.280317E+04 -1.620000E+05 1.518877E+05
0 2 -3.000000E-01 1.080000E+05 -6.039510E+03 2.955858E-09 0.0000 1.080000E+05 -6.039510E+03 1.111429E+053.000000E-01 -1.080000E+05 6.039510E+03 -2.955858E-09 -90.0000 6.039510E+03 -1.080000E+05 1.111429E+05
0 3 -3.000000E-01 5.400000E+04 1.354871E+03 -1.018634E-08 0.0000 5.400000E+04 1.354871E+03 5.333547E+043.000000E-01 -5.400000E+04 -1.354871E+03 1.018634E-08 90.0000 -1.354871E+03 -5.400000E+04 5.333547E+04
0 4 -3.000000E-01 1.350000E+04 -1.607474E+03 -1.249039E-08 0.0000 1.350000E+04 -1.607474E+03 1.437132E+043.000000E-01 -1.350000E+04 1.607474E+03 1.249039E-08 90.0000 1.607474E+03 -1.350000E+04 1.437132E+04
1 CANTILEVER BEAM USING QUAD4 ELEMENTS FEBRUARY 8, 2007 MSC.NASTRAN 6/17/05 PAGE 14COMBINATION LOADS
0 SUBCOM 5
S T R E S S E S I N Q U A D R I L A T E R A L E L E M E N T S ( Q U A D 4 )ELEMENT FIBER STRESSES IN ELEMENT COORD SYSTEM PRINCIPAL STRESSES (ZERO SHEAR)ID. DISTANCE NORMAL-X NORMAL-Y SHEAR-XY ANGLE MAJOR MINOR VON MISES
6
cquad4.f06 2/8/2007
0 1 -3.000000E-01 -4.547474E-12 4.295373E-02 -8.224248E+00 -45.0748 8.245752E+00 -8.202799E+00 1.424488E+013.000000E-01 -4.547474E-12 4.295373E-02 -8.224248E+00 -45.0748 8.245752E+00 -8.202799E+00 1.424488E+01
0 2 -3.000000E-01 -3.410605E-12 -1.288628E-01 -8.039908E+00 -44.7704 7.975735E+00 -8.104598E+00 1.392613E+013.000000E-01 -3.410605E-12 -1.288628E-01 -8.039908E+00 -44.7704 7.975735E+00 -8.104598E+00 1.392613E+01
0 3 -3.000000E-01 -3.031649E-12 4.725023E-01 -7.918659E+00 -45.8545 8.158434E+00 -7.685931E+00 1.372366E+013.000000E-01 -3.031649E-12 4.725023E-01 -7.918659E+00 -45.8545 8.158434E+00 -7.685931E+00 1.372366E+01
0 4 -3.000000E-01 -7.579122E-13 -1.761164E+00 -7.858524E+00 -41.8032 7.027124E+00 -8.788289E+00 1.372483E+013.000000E-01 -7.579122E-13 -1.761164E+00 -7.858524E+00 -41.8032 7.027124E+00 -8.788289E+00 1.372483E+01
1 CANTILEVER BEAM USING QUAD4 ELEMENTS FEBRUARY 8, 2007 MSC.NASTRAN 6/17/05 PAGE 15
0
No PARAM values were set in the Control File.
1 * * * END OF JOB * * *
7
cquad4_no5.bdf 2/7/2007
$ EXECUTIVE CONTROL SECTIONID Dr. S. BawabSOL 24TIME 10CEND$ CASE CONTROL SECTIONTITLE=CANTILEVER BEAM USING QUAD4 ELEMENTSSET 1=7,8,9,10DISPL=ALLSTRESS=ALLSPC=100SUBCASE 1SUBTITLE=10 LB. LOAD CASELOAD=100SUBCASE 2SUBTITLE=20 LB. LOAD CASELOAD=200SUBCASE 3SUBTITLE=30 LB. LOAD CASELOAD=300SUBCASE 4SUBTITLE = PRESSURE LOADSPC = 200LOAD = 500SUBCOM 5SUBTITLE = COMBINATION LOADSSUBSEQ = 1.0, 1.0, 0.0, 0.0$ BULK DATA SECTIONBEGIN BULKGRID,1,,0.,0.,-3.GRID,2,,0.,0.,+3.GRID,3,,18.,0.,3.GRID,4,,18.,0.,-3.GRID,5,,36.,0.,3.GRID,6,,36.,0.,-3.GRID,7,,54.,0.,3.GRID,8,,54.,0.,-3.GRID,9,,72.,0.,3.GRID,10,,72.,0.,-3.SPC1,100,123456,1,2SPC1,200,123456,1,2SPC1,200,5,3,THRU,10PLOAD2, 500, 10., 4FORCE,100,9,,10.,0.,0.,-1.FORCE,200,9,,20.,0.,0.,-1.FORCE,300,9,,30.,0.,0.,-1.CQUAD4,1,100,1,4,3,2CQUAD4,2,100,4,6,5,3CQUAD4,3,100,6,8,7,5
1
cquad4_no5.bdf 2/7/2007
CQUAD4,4,100,8,10,9,7PSHELL,100,10,.6,10MAT1,10,3.+7,,0.33,.00073575ENDDATA
2
cquad4_no5.f06 2/7/2007
1
THIS PROGRAM IS CONFIDENTIAL AND A TRADE SECRET OF MSC.SOFTWARE CORPORATION. THE RECEIPT ORPOSSESSION OF THIS PROGRAM DOES NOT CONVEY ANY RIGHTS TO REPRODUCE OR DISCLOSE ITS CONTENTS, OR TOMANUFACTURE, USE, OR SELL ANYTHING HEREIN, IN WHOLE OR IN PART, WITHOUT THE SPECIFIC WRITTEN CONSENT
OF MSC.SOFTWARE CORPORATION.
* * * * * * * * * * * * * * * * * * * ** * * * * * * * * * * * * * * * * * * ** * * ** * MSC.SOFTWARE * ** * CORP * ** * * ** * M S C . N a s t r a n * ** * * ** * * ** * * ** * Version 2005.1.0 * ** * 2005R2 * ** * * ** * * ** * JUN 17, 2005 * ** * * ** * Sun Microsystems Computer Co. * ** * MODEL UltraSPARC/1062 (acadia) * ** * SunOS 5.8 * ** * COMPILED FOR v9a(64-bit) * ** * * ** * * * * * * * * * * * * * * * * * * ** * * * * * * * * * * * * * * * * * * *
1News file - (6/03/05):
Thank you for choosing MSC.Nastran, the industry standard in FEA, and Welcometo MSC.Nastran 2005 r2.
You can find version-specific online documentation, and online technical supportat:
http://www.mscsoftware.com/support/prod_support/nastran/
Also at the technical support location is a searchable list of technicalapplication notes and the current error/avoidance list. Please don't hesitateto contact your nearest technical support representative if you requireassistance.
http://www.mscsoftware.com/about/locate/
The arbitrary beam cross section, explicit nonlinear (SOL 700), and the newnonlinear (SOL 400) solution sequences, are regarded as pre-release capabilitiesand are still undergoing testing and verification. These capabilities shouldnot be employed in any analysis except for the purpose of testing and verifyingthe functionality and working of the capabilities themselves.
MSC.Nastran 2005 r2 is mainly focused on improving quality, accuracy andease-of-use, but also introduces new capabilities, some of which were madeavailable as pre-release functionality in MSC.Nastran 2005 r1. In addition,
1
cquad4_no5.f06 2/7/2007
significant advancements have been made regarding performance and scalability ofthe program. Some of the new features and enhancements are listed below.
Nonlinear- MSC.Nastran Implicit Nonlinear (SOL 600) - We have addressed many knownissues, improved memory usage, improved output options, added beam, bar, andshell offsets, and thermal contact
- MSC.Nastran Explicit Nonlinear (SOL 700) pre-release - you can nowexecute LS-Dyna from inside MSC.Nastran to perform crash and impactanalyses
Numeric Enhancements- Multi-level DMP - an enhanced Lanczos modal extraction methodology thatimproves scalability and efficiently handles large normal modes analyses withvery frequency ranges
- MDACMS enhanced robustness, improved handling of large masses, and improvedperformance
- Distributed memory parallel MPYAD
Elements- CFAST - a new fastener element based on user defined stiffness values.- Arbitrary beam cross section pre-release capability - you can specify crosssection shapes using POINT entries, and optimize them in SOL 200
- Enhanced nonstructural mass element summary printout - ELSUM1- spatially dependent heat transfer coefficient- Heat transfer coefficient as a function of two variables- Thermal analysis flux output
Optimization- MSC.Nastran Topology Optimization - this addition to the existing SOL 200optimization solution sequence allows optimization analyses to be performedthat require many design variables
Further Enhancements- Larger XDB database support- MATMOD option 16 - we have removed many previous limitations with thismatrix output capability
- K6ROT stiffness removed for membrane elements1 FEBRUARY 7, 2007 MSC.NASTRAN 6/17/05 PAGE 1
0 N A S T R A N F I L E A N D S Y S T E M P A R A M E T E R E C H O0
NASTRAN OP2NEW=0 $ MSC.NASTRAN .LCL FILENASTRAN BUFFSIZE=8193 $(/AFS/LIONS/SUN4X_58/DEP/CAE/MSC2005/CONF/NAST20051RC[3])$ EXECUTIVE CONTROL SECTION
1 FEBRUARY 7, 2007 MSC.NASTRAN 6/17/05 PAGE 2
0 N A S T R A N E X E C U T I V E C O N T R O L E C H O0
ID DR. S. BAWABSOL 24
*** USER WARNING MESSAGE 814 (XCSSUB)SOLUTION SEQUENCE 24 HAS BEEN REPLACED.USER INFORMATION: ALTERNATE SOLUTION SEQUENCE 1 WILL BE EXECUTED.TIME 10CEND
2
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1 CANTILEVER BEAM USING QUAD4 ELEMENTS FEBRUARY 7, 2007 MSC.NASTRAN 6/17/05 PAGE 3
00 C A S E C O N T R O L E C H O
COMMANDCOUNT1 $ CASE CONTROL SECTION2 TITLE=CANTILEVER BEAM USING QUAD4 ELEMENTS3 SET 1=7,8,9,104 DISPL=ALL5 STRESS=ALL6 SPC=1007 SUBCASE 18 SUBTITLE=10 LB. LOAD CASE9 LOAD=10010 SUBCASE 211 SUBTITLE=20 LB. LOAD CASE12 LOAD=20013 SUBCASE 314 SUBTITLE=30 LB. LOAD CASE15 LOAD=30016 SUBCASE 417 SUBTITLE = PRESSURE LOAD18 SPC = 20019 LOAD = 50020 SUBCOM 521 SUBTITLE = COMBINATION LOADS22 SUBSEQ = 1.0, 1.0, 0.0, 0.023 $ BULK DATA SECTION24 BEGIN BULK
*** USER WARNING MESSAGE 4699 (FREFLD)THE FREE FIELD BULK DATA ENTRY BELOW HAS A REAL FIELD WITH MORE THAN 8 CHARACTERS. SOME PRECISION MAY BE LOST.MAT1,10,3.+7,,0.33,.00073575
0 INPUT BULK DATA ENTRY COUNT = 241 CANTILEVER BEAM USING QUAD4 ELEMENTS FEBRUARY 7, 2007 MSC.NASTRAN 6/17/05 PAGE 4
00 S O R T E D B U L K D A T A E C H O
ENTRYCOUNT . 1 .. 2 .. 3 .. 4 .. 5 .. 6 .. 7 .. 8 .. 9 .. 10 .
1- CQUAD4 1 100 1 4 3 22- CQUAD4 2 100 4 6 5 33- CQUAD4 3 100 6 8 7 54- CQUAD4 4 100 8 10 9 75- FORCE 100 9 10. 0. 0. -1.6- FORCE 200 9 20. 0. 0. -1.7- FORCE 300 9 30. 0. 0. -1.8- GRID 1 0. 0. -3.9- GRID 2 0. 0. +3.10- GRID 3 18. 0. 3.11- GRID 4 18. 0. -3.12- GRID 5 36. 0. 3.13- GRID 6 36. 0. -3.14- GRID 7 54. 0. 3.15- GRID 8 54. 0. -3.16- GRID 9 72. 0. 3.17- GRID 10 72. 0. -3.18- MAT1 10 3.+7 0.33 7.358-419- PLOAD2 500 10. 420- PSHELL 100 10 .6 10
3
cquad4_no5.f06 2/7/2007
21- SPC1 100 123456 1 222- SPC1 200 5 3 THRU 1023- SPC1 200 123456 1 2
ENDDATA0 TOTAL COUNT= 24
M O D E L S U M M A R Y
NUMBER OF GRID POINTS = 10
NUMBER OF CQUAD4 ELEMENTS = 4
*** SYSTEM INFORMATION MESSAGE 6916 (DFMSYN)DECOMP ORDERING METHOD CHOSEN: BEND, ORDERING METHOD USED: BEND
*** USER INFORMATION MESSAGE 5293 (SSG3A)FOR DATA BLOCK KLLLOAD SEQ. NO. EPSILON EXTERNAL WORK EPSILONS LARGER THAN 0.001 ARE FLAGGED WITH ASTERISKS
1 3.4827018E-12 1.8970942E-022 3.4827018E-12 7.5883768E-023 2.9092000E-12 1.7073847E-01
*** SYSTEM INFORMATION MESSAGE 6916 (DFMSYN)DECOMP ORDERING METHOD CHOSEN: BEND, ORDERING METHOD USED: BEND
*** USER INFORMATION MESSAGE 5293 (SSG3A)FOR DATA BLOCK KLLLOAD SEQ. NO. EPSILON EXTERNAL WORK EPSILONS LARGER THAN 0.001 ARE FLAGGED WITH ASTERISKS
4 5.9233135E-12 1.4648111E+041 CANTILEVER BEAM USING QUAD4 ELEMENTS FEBRUARY 7, 2007 MSC.NASTRAN 6/17/05 PAGE 5
10 LB. LOAD CASE0 SUBCASE 1
D I S P L A C E M E N T V E C T O R
POINT ID. TYPE T1 T2 T3 R1 R2 R31 G 0.0 0.0 0.0 0.0 0.0 0.02 G 0.0 0.0 0.0 0.0 0.0 0.03 G 1.048975E-04 0.0 -3.191291E-04 0.0 3.384098E-05 0.04 G -1.049032E-04 0.0 -3.191349E-04 0.0 3.384066E-05 0.05 G 1.798300E-04 0.0 -1.177746E-03 0.0 5.881517E-05 0.06 G -1.798186E-04 0.0 -1.177723E-03 0.0 5.881629E-05 0.07 G 2.247532E-04 0.0 -2.395930E-03 0.0 7.380258E-05 0.08 G -2.248042E-04 0.0 -2.396016E-03 0.0 7.379845E-05 0.09 G 2.398542E-04 0.0 -3.794188E-03 0.0 7.880109E-05 0.010 G -2.396728E-04 0.0 -3.793868E-03 0.0 7.878980E-05 0.0
1 CANTILEVER BEAM USING QUAD4 ELEMENTS FEBRUARY 7, 2007 MSC.NASTRAN 6/17/05 PAGE 620 LB. LOAD CASE
0 SUBCASE 2
D I S P L A C E M E N T V E C T O R
POINT ID. TYPE T1 T2 T3 R1 R2 R31 G 0.0 0.0 0.0 0.0 0.0 0.02 G 0.0 0.0 0.0 0.0 0.0 0.03 G 2.097951E-04 0.0 -6.382582E-04 0.0 6.768197E-05 0.04 G -2.098064E-04 0.0 -6.382697E-04 0.0 6.768133E-05 0.05 G 3.596600E-04 0.0 -2.355493E-03 0.0 1.176303E-04 0.06 G -3.596373E-04 0.0 -2.355447E-03 0.0 1.176326E-04 0.07 G 4.495063E-04 0.0 -4.791860E-03 0.0 1.476052E-04 0.08 G -4.496084E-04 0.0 -4.792031E-03 0.0 1.475969E-04 0.09 G 4.797084E-04 0.0 -7.588377E-03 0.0 1.576022E-04 0.0
4
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10 G -4.793455E-04 0.0 -7.587736E-03 0.0 1.575796E-04 0.01 CANTILEVER BEAM USING QUAD4 ELEMENTS FEBRUARY 7, 2007 MSC.NASTRAN 6/17/05 PAGE 7
30 LB. LOAD CASE0 SUBCASE 3
D I S P L A C E M E N T V E C T O R
POINT ID. TYPE T1 T2 T3 R1 R2 R31 G 0.0 0.0 0.0 0.0 0.0 0.02 G 0.0 0.0 0.0 0.0 0.0 0.03 G 3.146926E-04 0.0 -9.573874E-04 0.0 1.015229E-04 0.04 G -3.147096E-04 0.0 -9.574046E-04 0.0 1.015220E-04 0.05 G 5.394900E-04 0.0 -3.533239E-03 0.0 1.764455E-04 0.06 G -5.394560E-04 0.0 -3.533170E-03 0.0 1.764489E-04 0.07 G 6.742595E-04 0.0 -7.187789E-03 0.0 2.214078E-04 0.08 G -6.744126E-04 0.0 -7.188047E-03 0.0 2.213954E-04 0.09 G 7.195626E-04 0.0 -1.138256E-02 0.0 2.364033E-04 0.010 G -7.190183E-04 0.0 -1.138160E-02 0.0 2.363694E-04 0.0
1 CANTILEVER BEAM USING QUAD4 ELEMENTS FEBRUARY 7, 2007 MSC.NASTRAN 6/17/05 PAGE 8PRESSURE LOAD
0 SUBCASE 4
D I S P L A C E M E N T V E C T O R
POINT ID. TYPE T1 T2 T3 R1 R2 R31 G 0.0 0.0 0.0 0.0 0.0 0.02 G 0.0 0.0 0.0 0.0 0.0 0.03 G 0.0 -2.924907E+00 0.0 -2.043789E-02 0.0 -3.089499E-014 G 0.0 -2.924907E+00 0.0 2.043789E-02 0.0 -3.089499E-015 G 0.0 -1.061024E+01 0.0 -7.348453E-03 0.0 -5.289359E-016 G 0.0 -1.061024E+01 0.0 7.348453E-03 0.0 -5.289359E-017 G 0.0 -2.123939E+01 0.0 -3.628299E-03 0.0 -6.360417E-018 G 0.0 -2.123939E+01 0.0 3.628299E-03 0.0 -6.360417E-019 G 0.0 -3.301287E+01 0.0 -4.133505E-04 0.0 -6.641026E-0110 G 0.0 -3.301287E+01 0.0 4.133505E-04 0.0 -6.641026E-01
1 CANTILEVER BEAM USING QUAD4 ELEMENTS FEBRUARY 7, 2007 MSC.NASTRAN 6/17/05 PAGE 9COMBINATION LOADS
0 SUBCOM 5
D I S P L A C E M E N T V E C T O R
POINT ID. TYPE T1 T2 T3 R1 R2 R31 G 0.0 0.0 0.0 0.0 0.0 0.02 G 0.0 0.0 0.0 0.0 0.0 0.03 G 3.146926E-04 0.0 -9.573874E-04 0.0 1.015229E-04 0.04 G -3.147096E-04 0.0 -9.574046E-04 0.0 1.015220E-04 0.05 G 5.394900E-04 0.0 -3.533239E-03 0.0 1.764455E-04 0.06 G -5.394559E-04 0.0 -3.533170E-03 0.0 1.764489E-04 0.07 G 6.742595E-04 0.0 -7.187789E-03 0.0 2.214078E-04 0.08 G -6.744126E-04 0.0 -7.188047E-03 0.0 2.213954E-04 0.09 G 7.195626E-04 0.0 -1.138256E-02 0.0 2.364033E-04 0.010 G -7.190183E-04 0.0 -1.138160E-02 0.0 2.363694E-04 0.0
1 CANTILEVER BEAM USING QUAD4 ELEMENTS FEBRUARY 7, 2007 MSC.NASTRAN 6/17/05 PAGE 1010 LB. LOAD CASE
0 SUBCASE 1
S T R E S S E S I N Q U A D R I L A T E R A L E L E M E N T S ( Q U A D 4 )ELEMENT FIBER STRESSES IN ELEMENT COORD SYSTEM PRINCIPAL STRESSES (ZERO SHEAR)ID. DISTANCE NORMAL-X NORMAL-Y SHEAR-XY ANGLE MAJOR MINOR VON MISES
0 1 -3.000000E-01 -1.610563E-12 1.431786E-02 -2.776230E+00 -45.0739 2.783398E+00 -2.769080E+00 4.808593E+00
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3.000000E-01 -1.610563E-12 1.431786E-02 -2.776230E+00 -45.0739 2.783398E+00 -2.769080E+00 4.808593E+000 2 -3.000000E-01 -1.326346E-12 -4.295445E-02 -2.774961E+00 -44.7783 2.753567E+00 -2.796521E+00 4.806565E+00
3.000000E-01 -1.326346E-12 -4.295445E-02 -2.774961E+00 -44.7783 2.753567E+00 -2.796521E+00 4.806565E+000 3 -3.000000E-01 -3.789561E-13 1.575023E-01 -2.774961E+00 -45.8128 2.854829E+00 -2.697327E+00 4.808953E+00
3.000000E-01 -3.789561E-13 1.575023E-01 -2.774961E+00 -45.8128 2.854829E+00 -2.697327E+00 4.808953E+000 4 -3.000000E-01 -7.579122E-13 -5.870561E-01 -2.774961E+00 -41.9809 2.496914E+00 -3.083970E+00 4.842093E+00
3.000000E-01 -7.579122E-13 -5.870561E-01 -2.774961E+00 -41.9809 2.496914E+00 -3.083970E+00 4.842093E+001 CANTILEVER BEAM USING QUAD4 ELEMENTS FEBRUARY 7, 2007 MSC.NASTRAN 6/17/05 PAGE 11
20 LB. LOAD CASE0 SUBCASE 2
S T R E S S E S I N Q U A D R I L A T E R A L E L E M E N T S ( Q U A D 4 )ELEMENT FIBER STRESSES IN ELEMENT COORD SYSTEM PRINCIPAL STRESSES (ZERO SHEAR)ID. DISTANCE NORMAL-X NORMAL-Y SHEAR-XY ANGLE MAJOR MINOR VON MISES
0 1 -3.000000E-01 -3.221127E-12 2.863573E-02 -5.552460E+00 -45.0739 5.566797E+00 -5.538161E+00 9.617186E+003.000000E-01 -3.221127E-12 2.863573E-02 -5.552460E+00 -45.0739 5.566797E+00 -5.538161E+00 9.617186E+00
0 2 -3.000000E-01 -2.652693E-12 -8.590890E-02 -5.549922E+00 -44.7783 5.507133E+00 -5.593042E+00 9.613130E+003.000000E-01 -2.652693E-12 -8.590890E-02 -5.549922E+00 -44.7783 5.507133E+00 -5.593042E+00 9.613130E+00
0 3 -3.000000E-01 -7.579122E-13 3.150046E-01 -5.549922E+00 -45.8128 5.709659E+00 -5.394654E+00 9.617907E+003.000000E-01 -7.579122E-13 3.150046E-01 -5.549922E+00 -45.8128 5.709659E+00 -5.394654E+00 9.617907E+00
0 4 -3.000000E-01 -1.515824E-12 -1.174112E+00 -5.549922E+00 -41.9809 4.993828E+00 -6.167940E+00 9.684185E+003.000000E-01 -1.515824E-12 -1.174112E+00 -5.549922E+00 -41.9809 4.993828E+00 -6.167940E+00 9.684185E+00
1 CANTILEVER BEAM USING QUAD4 ELEMENTS FEBRUARY 7, 2007 MSC.NASTRAN 6/17/05 PAGE 1230 LB. LOAD CASE
0 SUBCASE 3
S T R E S S E S I N Q U A D R I L A T E R A L E L E M E N T S ( Q U A D 4 )ELEMENT FIBER STRESSES IN ELEMENT COORD SYSTEM PRINCIPAL STRESSES (ZERO SHEAR)ID. DISTANCE NORMAL-X NORMAL-Y SHEAR-XY ANGLE MAJOR MINOR VON MISES
0 1 -3.000000E-01 -4.547474E-12 4.295360E-02 -8.328691E+00 -45.0739 8.350195E+00 -8.307241E+00 1.442578E+013.000000E-01 -4.547474E-12 4.295360E-02 -8.328691E+00 -45.0739 8.350195E+00 -8.307241E+00 1.442578E+01
0 2 -3.000000E-01 -3.789561E-12 -1.288633E-01 -8.324883E+00 -44.7783 8.260699E+00 -8.389563E+00 1.441969E+013.000000E-01 -3.789561E-12 -1.288633E-01 -8.324883E+00 -44.7783 8.260699E+00 -8.389563E+00 1.441969E+01
0 3 -3.000000E-01 -1.515824E-12 4.725069E-01 -8.324883E+00 -45.8128 8.564488E+00 -8.091981E+00 1.442686E+013.000000E-01 -1.515824E-12 4.725069E-01 -8.324883E+00 -45.8128 8.564488E+00 -8.091981E+00 1.442686E+01
0 4 -3.000000E-01 -1.515824E-12 -1.761168E+00 -8.324883E+00 -41.9809 7.490742E+00 -9.251910E+00 1.452628E+013.000000E-01 -1.515824E-12 -1.761168E+00 -8.324883E+00 -41.9809 7.490742E+00 -9.251910E+00 1.452628E+01
1 CANTILEVER BEAM USING QUAD4 ELEMENTS FEBRUARY 7, 2007 MSC.NASTRAN 6/17/05 PAGE 13PRESSURE LOAD
0 SUBCASE 4
S T R E S S E S I N Q U A D R I L A T E R A L E L E M E N T S ( Q U A D 4 )ELEMENT FIBER STRESSES IN ELEMENT COORD SYSTEM PRINCIPAL STRESSES (ZERO SHEAR)ID. DISTANCE NORMAL-X NORMAL-Y SHEAR-XY ANGLE MAJOR MINOR VON MISES
0 1 -3.000000E-01 1.620000E+05 2.280317E+04 -7.200166E-09 0.0000 1.620000E+05 2.280317E+04 1.518877E+053.000000E-01 -1.620000E+05 -2.280317E+04 7.200166E-09 90.0000 -2.280317E+04 -1.620000E+05 1.518877E+05
0 2 -3.000000E-01 1.080000E+05 -6.039510E+03 2.955858E-09 0.0000 1.080000E+05 -6.039510E+03 1.111429E+053.000000E-01 -1.080000E+05 6.039510E+03 -2.955858E-09 -90.0000 6.039510E+03 -1.080000E+05 1.111429E+05
0 3 -3.000000E-01 5.400000E+04 1.354871E+03 -1.018634E-08 0.0000 5.400000E+04 1.354871E+03 5.333547E+043.000000E-01 -5.400000E+04 -1.354871E+03 1.018634E-08 90.0000 -1.354871E+03 -5.400000E+04 5.333547E+04
0 4 -3.000000E-01 1.350000E+04 -1.607474E+03 -1.249039E-08 0.0000 1.350000E+04 -1.607474E+03 1.437132E+043.000000E-01 -1.350000E+04 1.607474E+03 1.249039E-08 90.0000 1.607474E+03 -1.350000E+04 1.437132E+04
1 CANTILEVER BEAM USING QUAD4 ELEMENTS FEBRUARY 7, 2007 MSC.NASTRAN 6/17/05 PAGE 14COMBINATION LOADS
0 SUBCOM 5
S T R E S S E S I N Q U A D R I L A T E R A L E L E M E N T S ( Q U A D 4 )ELEMENT FIBER STRESSES IN ELEMENT COORD SYSTEM PRINCIPAL STRESSES (ZERO SHEAR)ID. DISTANCE NORMAL-X NORMAL-Y SHEAR-XY ANGLE MAJOR MINOR VON MISES
0 1 -3.000000E-01 -4.736951E-12 4.295360E-02 -8.328691E+00 -45.0739 8.350195E+00 -8.307241E+00 1.442578E+01
6
cquad4_no5.f06 2/7/2007
3.000000E-01 -4.736951E-12 4.295360E-02 -8.328691E+00 -45.0739 8.350195E+00 -8.307241E+00 1.442578E+010 2 -3.000000E-01 -3.789561E-12 -1.288633E-01 -8.324883E+00 -44.7783 8.260699E+00 -8.389563E+00 1.441969E+01
3.000000E-01 -3.789561E-12 -1.288633E-01 -8.324883E+00 -44.7783 8.260699E+00 -8.389563E+00 1.441969E+010 3 -3.000000E-01 -1.515824E-12 4.725069E-01 -8.324883E+00 -45.8128 8.564488E+00 -8.091981E+00 1.442686E+01
3.000000E-01 -1.515824E-12 4.725069E-01 -8.324883E+00 -45.8128 8.564488E+00 -8.091981E+00 1.442686E+010 4 -3.000000E-01 -3.031649E-12 -1.761168E+00 -8.324883E+00 -41.9809 7.490742E+00 -9.251910E+00 1.452628E+01
3.000000E-01 -3.031649E-12 -1.761168E+00 -8.324883E+00 -41.9809 7.490742E+00 -9.251910E+00 1.452628E+011 CANTILEVER BEAM USING QUAD4 ELEMENTS FEBRUARY 7, 2007 MSC.NASTRAN 6/17/05 PAGE 15
0
No PARAM values were set in the Control File.
1 * * * END OF JOB * * *
7
cquad4_3.bdf 2/19/2007
$ EXECUTIVE CONTROL SECTIONID Dr. S. BawabSOL 24TIME 10CEND$ CASE CONTROL SECTIONTITLE=CANTILEVER BEAM USING 8 QUAD4 ELEMENTSDISPL=ALLSTRESS=ALLSPC=100SUBCASE 1SUBTITLE=10 LB. LOAD CASELOAD=100$ BULK DATA SECTIONBEGIN BULKGRID,1,,0.,0.,-3.GRID,2,,0.,0.,+3.GRID,3,,9.,0.,3.GRID,4,,9.,0.,-3.GRID,5,,18.,0.,3.GRID,6,,18.,0.,-3.GRID,7,,27.,0.,3.GRID,8,,27.,0.,-3.GRID,9,,36.,0.,3.GRID,10,,36.,0.,-3.GRID,11,,45.,0.,3.GRID,12,,45.,0.,-3.GRID,13,,54.,0.,3.GRID,14,,54.,0.,-3.GRID,15,,63.,0.,3.GRID,16,,63.,0.,-3.GRID,17,,72.,0.,3.GRID,18,,72.,0.,-3.SPC1,100,123456,1,2FORCE,100,17,,10.,0.,0.,-1.CQUAD4,1,100,1,4,3,2CQUAD4,2,100,4,6,5,3CQUAD4,3,100,6,8,7,5CQUAD4,4,100,8,10,9,7CQUAD4,5,100,10,12,11,9CQUAD4,6,100,12,14,13,11CQUAD4,7,100,14,16,15,13CQUAD4,8,100,16,18,17,15PSHELL,100,10,.6,10MAT1,10,3.+7,,0.33,.0007358ENDDATA
1
cquad4_3.f06 2/19/2007
1
THIS PROGRAM IS CONFIDENTIAL AND A TRADE SECRET OF MSC.SOFTWARE CORPORATION. THE RECEIPT ORPOSSESSION OF THIS PROGRAM DOES NOT CONVEY ANY RIGHTS TO REPRODUCE OR DISCLOSE ITS CONTENTS, OR TOMANUFACTURE, USE, OR SELL ANYTHING HEREIN, IN WHOLE OR IN PART, WITHOUT THE SPECIFIC WRITTEN CONSENT
OF MSC.SOFTWARE CORPORATION.
* * * * * * * * * * * * * * * * * * * ** * * * * * * * * * * * * * * * * * * ** * * ** * MSC.SOFTWARE * ** * CORP * ** * * ** * M S C . N a s t r a n * ** * * ** * * ** * * ** * Version 2005.1.0 * ** * 2005R2 * ** * * ** * * ** * JUN 17, 2005 * ** * * ** * Sun Microsystems Computer Co. * ** * MODEL UltraSPARC/1062 (acadia) * ** * SunOS 5.8 * ** * COMPILED FOR v9a(64-bit) * ** * * ** * * * * * * * * * * * * * * * * * * ** * * * * * * * * * * * * * * * * * * *
1News file - (6/03/05):
Thank you for choosing MSC.Nastran, the industry standard in FEA, and Welcometo MSC.Nastran 2005 r2.
You can find version-specific online documentation, and online technical supportat:
http://www.mscsoftware.com/support/prod_support/nastran/
Also at the technical support location is a searchable list of technicalapplication notes and the current error/avoidance list. Please don't hesitateto contact your nearest technical support representative if you requireassistance.
http://www.mscsoftware.com/about/locate/
The arbitrary beam cross section, explicit nonlinear (SOL 700), and the newnonlinear (SOL 400) solution sequences, are regarded as pre-release capabilitiesand are still undergoing testing and verification. These capabilities shouldnot be employed in any analysis except for the purpose of testing and verifyingthe functionality and working of the capabilities themselves.
MSC.Nastran 2005 r2 is mainly focused on improving quality, accuracy andease-of-use, but also introduces new capabilities, some of which were madeavailable as pre-release functionality in MSC.Nastran 2005 r1. In addition,
1
cquad4_3.f06 2/19/2007
significant advancements have been made regarding performance and scalability ofthe program. Some of the new features and enhancements are listed below.
Nonlinear- MSC.Nastran Implicit Nonlinear (SOL 600) - We have addressed many knownissues, improved memory usage, improved output options, added beam, bar, andshell offsets, and thermal contact
- MSC.Nastran Explicit Nonlinear (SOL 700) pre-release - you can nowexecute LS-Dyna from inside MSC.Nastran to perform crash and impactanalyses
Numeric Enhancements- Multi-level DMP - an enhanced Lanczos modal extraction methodology thatimproves scalability and efficiently handles large normal modes analyses withvery frequency ranges
- MDACMS enhanced robustness, improved handling of large masses, and improvedperformance
- Distributed memory parallel MPYAD
Elements- CFAST - a new fastener element based on user defined stiffness values.- Arbitrary beam cross section pre-release capability - you can specify crosssection shapes using POINT entries, and optimize them in SOL 200
- Enhanced nonstructural mass element summary printout - ELSUM1- spatially dependent heat transfer coefficient- Heat transfer coefficient as a function of two variables- Thermal analysis flux output
Optimization- MSC.Nastran Topology Optimization - this addition to the existing SOL 200optimization solution sequence allows optimization analyses to be performedthat require many design variables
Further Enhancements- Larger XDB database support- MATMOD option 16 - we have removed many previous limitations with thismatrix output capability
- K6ROT stiffness removed for membrane elements1 FEBRUARY 19, 2007 MSC.NASTRAN 6/17/05 PAGE 1
0 N A S T R A N F I L E A N D S Y S T E M P A R A M E T E R E C H O0
NASTRAN OP2NEW=0 $ MSC.NASTRAN .LCL FILENASTRAN BUFFSIZE=8193 $(/AFS/LIONS/SUN4X_58/DEP/CAE/MSC2005/CONF/NAST20051RC[3])$ EXECUTIVE CONTROL SECTION
1 FEBRUARY 19, 2007 MSC.NASTRAN 6/17/05 PAGE 2
0 N A S T R A N E X E C U T I V E C O N T R O L E C H O0
ID DR. S. BAWABSOL 24
*** USER WARNING MESSAGE 814 (XCSSUB)SOLUTION SEQUENCE 24 HAS BEEN REPLACED.USER INFORMATION: ALTERNATE SOLUTION SEQUENCE 1 WILL BE EXECUTED.TIME 10CEND
2
cquad4_3.f06 2/19/2007
1 CANTILEVER BEAM USING 8 QUAD4 ELEMENTS FEBRUARY 19, 2007 MSC.NASTRAN 6/17/05 PAGE 3
00 C A S E C O N T R O L E C H O
COMMANDCOUNT1 $ CASE CONTROL SECTION2 TITLE=CANTILEVER BEAM USING 8 QUAD4 ELEMENTS3 DISPL=ALL4 STRESS=ALL5 SPC=1006 SUBCASE 17 SUBTITLE=10 LB. LOAD CASE8 LOAD=1009 $ BULK DATA SECTION10 BEGIN BULK
0 INPUT BULK DATA ENTRY COUNT = 311 CANTILEVER BEAM USING 8 QUAD4 ELEMENTS FEBRUARY 19, 2007 MSC.NASTRAN 6/17/05 PAGE 4
00 S O R T E D B U L K D A T A E C H O
ENTRYCOUNT . 1 .. 2 .. 3 .. 4 .. 5 .. 6 .. 7 .. 8 .. 9 .. 10 .
1- CQUAD4 1 100 1 4 3 22- CQUAD4 2 100 4 6 5 33- CQUAD4 3 100 6 8 7 54- CQUAD4 4 100 8 10 9 75- CQUAD4 5 100 10 12 11 96- CQUAD4 6 100 12 14 13 117- CQUAD4 7 100 14 16 15 138- CQUAD4 8 100 16 18 17 159- FORCE 100 17 10. 0. 0. -1.10- GRID 1 0. 0. -3.11- GRID 2 0. 0. +3.12- GRID 3 9. 0. 3.13- GRID 4 9. 0. -3.14- GRID 5 18. 0. 3.15- GRID 6 18. 0. -3.16- GRID 7 27. 0. 3.17- GRID 8 27. 0. -3.18- GRID 9 36. 0. 3.19- GRID 10 36. 0. -3.20- GRID 11 45. 0. 3.21- GRID 12 45. 0. -3.22- GRID 13 54. 0. 3.23- GRID 14 54. 0. -3.24- GRID 15 63. 0. 3.25- GRID 16 63. 0. -3.26- GRID 17 72. 0. 3.27- GRID 18 72. 0. -3.28- MAT1 10 3.+7 0.33 .000735829- PSHELL 100 10 .6 1030- SPC1 100 123456 1 2
ENDDATA0 TOTAL COUNT= 31
M O D E L S U M M A R Y
NUMBER OF GRID POINTS = 18
3
cquad4_3.f06 2/19/2007
NUMBER OF CQUAD4 ELEMENTS = 8
*** SYSTEM INFORMATION MESSAGE 6916 (DFMSYN)DECOMP ORDERING METHOD CHOSEN: BEND, ORDERING METHOD USED: BEND
*** USER INFORMATION MESSAGE 5293 (SSG3A)FOR DATA BLOCK KLLLOAD SEQ. NO. EPSILON EXTERNAL WORK EPSILONS LARGER THAN 0.001 ARE FLAGGED WITH ASTERISKS
1 2.2382771E-12 1.9210428E-021 CANTILEVER BEAM USING 8 QUAD4 ELEMENTS FEBRUARY 19, 2007 MSC.NASTRAN 6/17/05 PAGE 5
10 LB. LOAD CASE0 SUBCASE 1
D I S P L A C E M E N T V E C T O R
POINT ID. TYPE T1 T2 T3 R1 R2 R31 G 0.0 0.0 0.0 0.0 0.0 0.02 G 0.0 0.0 0.0 0.0 0.0 0.03 G 5.623600E-05 0.0 -8.657027E-05 0.0 1.855603E-05 0.04 G -5.623603E-05 0.0 -8.657033E-05 0.0 1.855602E-05 0.05 G 1.049737E-04 0.0 -3.306010E-04 0.0 3.480190E-05 0.06 G -1.049736E-04 0.0 -3.306008E-04 0.0 3.480192E-05 0.07 G 1.462130E-04 0.0 -7.095968E-04 0.0 4.854846E-05 0.08 G -1.462133E-04 0.0 -7.095977E-04 0.0 4.854838E-05 0.09 G 1.799551E-04 0.0 -1.201067E-03 0.0 5.979541E-05 0.010 G -1.799541E-04 0.0 -1.201063E-03 0.0 5.979573E-05 0.011 G 2.061962E-04 0.0 -1.782504E-03 0.0 6.854394E-05 0.012 G -2.061997E-04 0.0 -1.782516E-03 0.0 6.854275E-05 0.013 G 2.249498E-04 0.0 -2.431461E-03 0.0 7.478955E-05 0.014 G -2.249366E-04 0.0 -2.431415E-03 0.0 7.479398E-05 0.015 G 2.361658E-04 0.0 -3.125268E-03 0.0 7.854908E-05 0.016 G -2.362149E-04 0.0 -3.125440E-03 0.0 7.853254E-05 0.017 G 2.400310E-04 0.0 -3.842086E-03 0.0 7.981309E-05 0.018 G -2.398477E-04 0.0 -3.841444E-03 0.0 7.976790E-05 0.0
1 CANTILEVER BEAM USING 8 QUAD4 ELEMENTS FEBRUARY 19, 2007 MSC.NASTRAN 6/17/05 PAGE 610 LB. LOAD CASE
0 SUBCASE 1
S T R E S S E S I N Q U A D R I L A T E R A L E L E M E N T S ( Q U A D 4 )ELEMENT FIBER STRESSES IN ELEMENT COORD SYSTEM PRINCIPAL STRESSES (ZERO SHEAR)ID. DISTANCE NORMAL-X NORMAL-Y SHEAR-XY ANGLE MAJOR MINOR VON MISES
0 1 -3.000000E-01 -4.500104E-12 1.475584E-04 -2.777287E+00 -45.0008 2.777360E+00 -2.777213E+00 4.810401E+003.000000E-01 -4.500104E-12 1.475584E-04 -2.777287E+00 -45.0008 2.777360E+00 -2.777213E+00 4.810401E+00
0 2 -3.000000E-01 -4.357995E-12 -4.427104E-04 -2.777073E+00 -44.9977 2.776852E+00 -2.777294E+00 4.810031E+003.000000E-01 -4.357995E-12 -4.427104E-04 -2.777073E+00 -44.9977 2.776852E+00 -2.777294E+00 4.810031E+00
0 3 -3.000000E-01 -4.168517E-12 1.623381E-03 -2.777073E+00 -45.0084 2.777885E+00 -2.776261E+00 4.810032E+003.000000E-01 -4.168517E-12 1.623381E-03 -2.777073E+00 -45.0084 2.777885E+00 -2.776261E+00 4.810032E+00
0 4 -3.000000E-01 -3.979039E-12 -6.051181E-03 -2.777073E+00 -44.9688 2.774049E+00 -2.780100E+00 4.810035E+003.000000E-01 -3.979039E-12 -6.051181E-03 -2.777073E+00 -44.9688 2.774049E+00 -2.780100E+00 4.810035E+00
0 5 -3.000000E-01 -4.357995E-12 2.258271E-02 -2.777073E+00 -45.1165 2.788387E+00 -2.765805E+00 4.810084E+003.000000E-01 -4.357995E-12 2.258271E-02 -2.777073E+00 -45.1165 2.788387E+00 -2.765805E+00 4.810084E+00
0 6 -3.000000E-01 -3.221127E-12 -8.428474E-02 -2.777073E+00 -44.5653 2.735250E+00 -2.819535E+00 4.810770E+003.000000E-01 -3.221127E-12 -8.428474E-02 -2.777073E+00 -44.5653 2.735250E+00 -2.819535E+00 4.810770E+00
0 7 -3.000000E-01 -1.326346E-12 3.145753E-01 -2.777073E+00 -46.6208 2.938811E+00 -2.624236E+00 4.820307E+003.000000E-01 -1.326346E-12 3.145753E-01 -2.777073E+00 -46.6208 2.938811E+00 -2.624236E+00 4.820307E+00
0 8 -3.000000E-01 -1.515824E-12 -1.174027E+00 -2.777073E+00 -39.0323 2.251423E+00 -3.425450E+00 4.951236E+003.000000E-01 -1.515824E-12 -1.174027E+00 -2.777073E+00 -39.0323 2.251423E+00 -3.425450E+00 4.951236E+00
1 CANTILEVER BEAM USING 8 QUAD4 ELEMENTS FEBRUARY 19, 2007 MSC.NASTRAN 6/17/05 PAGE 7
0
4
cquad4_3.f06 2/19/2007
No PARAM values were set in the Control File.
1 * * * END OF JOB * * *
5
cquad4_4.bdf 2/20/2007
$ EXECUTIVE CONTROL SECTIONID Dr. S. BawabSOL 24TIME 10CEND$ CASE CONTROL SECTIONTITLE=CANTILEVER BEAM USING QUAD4 ELEMENTSDISPL=ALLSTRESS=ALLSPC=100SUBCASE 1SUBTITLE=10 LB. LOAD CASELOAD=100$ BULK DATA SECTIONBEGIN BULKGRID,1,,0.,0.,-3.GRID,2,,0.,0.,0.GRID,3,,0.,0.,3.GRID,4,,18.,0.,3.GRID,5,,18.,0.,0.GRID,6,,18.,0.,-3.GRID,7,,36.,0.,3.GRID,8,,36.,0.,0.GRID,9,,36.,0.,-3.GRID,10,,54.,0.,3.GRID,11,,54.,0.,0.GRID,12,,54.,0.,-3.GRID,13,,72.,0.,3.GRID,14,,72.,0.,0.GRID,15,,72.,0.,-3.SPC1,100,123456,1,2,3FORCE,100,13,,10.,0.,0.,-1.CQUAD4,1,100,2,5,4,3CQUAD4,2,100,5,8,7,4CQUAD4,3,100,8,11,10,7CQUAD4,4,100,11,14,13,10CQUAD4,5,100,1,6,5,2CQUAD4,6,100,6,9,8,5CQUAD4,7,100,9,12,11,8CQUAD4,8,100,12,15,14,11PSHELL,100,10,.6,10MAT1,10,3.+7,,0.33,.0007358ENDDATA
1
cquad4_4.f06 2/20/2007
1
THIS PROGRAM IS CONFIDENTIAL AND A TRADE SECRET OF MSC.SOFTWARE CORPORATION. THE RECEIPT ORPOSSESSION OF THIS PROGRAM DOES NOT CONVEY ANY RIGHTS TO REPRODUCE OR DISCLOSE ITS CONTENTS, OR TOMANUFACTURE, USE, OR SELL ANYTHING HEREIN, IN WHOLE OR IN PART, WITHOUT THE SPECIFIC WRITTEN CONSENT
OF MSC.SOFTWARE CORPORATION.
* * * * * * * * * * * * * * * * * * * ** * * * * * * * * * * * * * * * * * * ** * * ** * MSC.SOFTWARE * ** * CORP * ** * * ** * M S C . N a s t r a n * ** * * ** * * ** * * ** * Version 2005.1.0 * ** * 2005R2 * ** * * ** * * ** * JUN 17, 2005 * ** * * ** * Sun Microsystems Computer Co. * ** * MODEL UltraSPARC/1062 (acadia) * ** * SunOS 5.8 * ** * COMPILED FOR v9a(64-bit) * ** * * ** * * * * * * * * * * * * * * * * * * ** * * * * * * * * * * * * * * * * * * *
1News file - (6/03/05):
Thank you for choosing MSC.Nastran, the industry standard in FEA, and Welcometo MSC.Nastran 2005 r2.
You can find version-specific online documentation, and online technical supportat:
http://www.mscsoftware.com/support/prod_support/nastran/
Also at the technical support location is a searchable list of technicalapplication notes and the current error/avoidance list. Please don't hesitateto contact your nearest technical support representative if you requireassistance.
http://www.mscsoftware.com/about/locate/
The arbitrary beam cross section, explicit nonlinear (SOL 700), and the newnonlinear (SOL 400) solution sequences, are regarded as pre-release capabilitiesand are still undergoing testing and verification. These capabilities shouldnot be employed in any analysis except for the purpose of testing and verifyingthe functionality and working of the capabilities themselves.
MSC.Nastran 2005 r2 is mainly focused on improving quality, accuracy andease-of-use, but also introduces new capabilities, some of which were madeavailable as pre-release functionality in MSC.Nastran 2005 r1. In addition,
1
cquad4_4.f06 2/20/2007
significant advancements have been made regarding performance and scalability ofthe program. Some of the new features and enhancements are listed below.
Nonlinear- MSC.Nastran Implicit Nonlinear (SOL 600) - We have addressed many knownissues, improved memory usage, improved output options, added beam, bar, andshell offsets, and thermal contact
- MSC.Nastran Explicit Nonlinear (SOL 700) pre-release - you can nowexecute LS-Dyna from inside MSC.Nastran to perform crash and impactanalyses
Numeric Enhancements- Multi-level DMP - an enhanced Lanczos modal extraction methodology thatimproves scalability and efficiently handles large normal modes analyses withvery frequency ranges
- MDACMS enhanced robustness, improved handling of large masses, and improvedperformance
- Distributed memory parallel MPYAD
Elements- CFAST - a new fastener element based on user defined stiffness values.- Arbitrary beam cross section pre-release capability - you can specify crosssection shapes using POINT entries, and optimize them in SOL 200
- Enhanced nonstructural mass element summary printout - ELSUM1- spatially dependent heat transfer coefficient- Heat transfer coefficient as a function of two variables- Thermal analysis flux output
Optimization- MSC.Nastran Topology Optimization - this addition to the existing SOL 200optimization solution sequence allows optimization analyses to be performedthat require many design variables
Further Enhancements- Larger XDB database support- MATMOD option 16 - we have removed many previous limitations with thismatrix output capability
- K6ROT stiffness removed for membrane elements1 FEBRUARY 20, 2007 MSC.NASTRAN 6/17/05 PAGE 1
0 N A S T R A N F I L E A N D S Y S T E M P A R A M E T E R E C H O0
NASTRAN OP2NEW=0 $ MSC.NASTRAN .LCL FILENASTRAN BUFFSIZE=8193 $(/AFS/LIONS/SUN4X_58/DEP/CAE/MSC2005/CONF/NAST20051RC[3])$ EXECUTIVE CONTROL SECTION
1 FEBRUARY 20, 2007 MSC.NASTRAN 6/17/05 PAGE 2
0 N A S T R A N E X E C U T I V E C O N T R O L E C H O0
ID DR. S. BAWABSOL 24
*** USER WARNING MESSAGE 814 (XCSSUB)SOLUTION SEQUENCE 24 HAS BEEN REPLACED.USER INFORMATION: ALTERNATE SOLUTION SEQUENCE 1 WILL BE EXECUTED.TIME 10CEND
2
cquad4_4.f06 2/20/2007
1 CANTILEVER BEAM USING QUAD4 ELEMENTS FEBRUARY 20, 2007 MSC.NASTRAN 6/17/05 PAGE 3
00 C A S E C O N T R O L E C H O
COMMANDCOUNT1 $ CASE CONTROL SECTION2 TITLE=CANTILEVER BEAM USING QUAD4 ELEMENTS3 DISPL=ALL4 STRESS=ALL5 SPC=1006 SUBCASE 17 SUBTITLE=10 LB. LOAD CASE8 LOAD=1009 $ BULK DATA SECTION10 BEGIN BULK
0 INPUT BULK DATA ENTRY COUNT = 281 CANTILEVER BEAM USING QUAD4 ELEMENTS FEBRUARY 20, 2007 MSC.NASTRAN 6/17/05 PAGE 4
00 S O R T E D B U L K D A T A E C H O
ENTRYCOUNT . 1 .. 2 .. 3 .. 4 .. 5 .. 6 .. 7 .. 8 .. 9 .. 10 .
1- CQUAD4 1 100 2 5 4 32- CQUAD4 2 100 5 8 7 43- CQUAD4 3 100 8 11 10 74- CQUAD4 4 100 11 14 13 105- CQUAD4 5 100 1 6 5 26- CQUAD4 6 100 6 9 8 57- CQUAD4 7 100 9 12 11 88- CQUAD4 8 100 12 15 14 119- FORCE 100 13 10. 0. 0. -1.10- GRID 1 0. 0. -3.11- GRID 2 0. 0. 0.12- GRID 3 0. 0. 3.13- GRID 4 18. 0. 3.14- GRID 5 18. 0. 0.15- GRID 6 18. 0. -3.16- GRID 7 36. 0. 3.17- GRID 8 36. 0. 0.18- GRID 9 36. 0. -3.19- GRID 10 54. 0. 3.20- GRID 11 54. 0. 0.21- GRID 12 54. 0. -3.22- GRID 13 72. 0. 3.23- GRID 14 72. 0. 0.24- GRID 15 72. 0. -3.25- MAT1 10 3.+7 0.33 .000735826- PSHELL 100 10 .6 1027- SPC1 100 123456 1 2 3
ENDDATA0 TOTAL COUNT= 28
M O D E L S U M M A R Y
NUMBER OF GRID POINTS = 15
NUMBER OF CQUAD4 ELEMENTS = 8
3
cquad4_4.f06 2/20/2007
*** SYSTEM INFORMATION MESSAGE 6916 (DFMSYN)DECOMP ORDERING METHOD CHOSEN: BEND, ORDERING METHOD USED: BEND
*** USER INFORMATION MESSAGE 5293 (SSG3A)FOR DATA BLOCK KLLLOAD SEQ. NO. EPSILON EXTERNAL WORK EPSILONS LARGER THAN 0.001 ARE FLAGGED WITH ASTERISKS
1 5.2144270E-13 1.8654190E-021 CANTILEVER BEAM USING QUAD4 ELEMENTS FEBRUARY 20, 2007 MSC.NASTRAN 6/17/05 PAGE 5
10 LB. LOAD CASE0 SUBCASE 1
D I S P L A C E M E N T V E C T O R
POINT ID. TYPE T1 T2 T3 R1 R2 R31 G 0.0 0.0 0.0 0.0 0.0 0.02 G 0.0 0.0 0.0 0.0 0.0 0.03 G 0.0 0.0 0.0 0.0 0.0 0.04 G 1.012401E-04 0.0 -3.098400E-04 0.0 3.282692E-05 0.05 G -3.519810E-09 0.0 -3.064713E-04 0.0 3.280673E-05 0.06 G -1.012438E-04 0.0 -3.098455E-04 0.0 3.282605E-05 0.07 G 1.771986E-04 0.0 -1.148615E-03 0.0 5.786220E-05 0.08 G 6.565085E-09 0.0 -1.147181E-03 0.0 5.789857E-05 0.09 G -1.771886E-04 0.0 -1.148592E-03 0.0 5.786383E-05 0.010 G 2.217550E-04 0.0 -2.349614E-03 0.0 7.282718E-05 0.011 G -2.281556E-08 0.0 -2.348846E-03 0.0 7.284190E-05 0.012 G -2.218111E-04 0.0 -2.349700E-03 0.0 7.282478E-05 0.013 G 2.372800E-04 0.0 -3.730838E-03 0.0 7.790202E-05 0.014 G 7.183759E-08 0.0 -3.730402E-03 0.0 7.790491E-05 0.015 G -2.370603E-04 0.0 -3.730518E-03 0.0 7.787807E-05 0.0
1 CANTILEVER BEAM USING QUAD4 ELEMENTS FEBRUARY 20, 2007 MSC.NASTRAN 6/17/05 PAGE 610 LB. LOAD CASE
0 SUBCASE 1
S T R E S S E S I N Q U A D R I L A T E R A L E L E M E N T S ( Q U A D 4 )ELEMENT FIBER STRESSES IN ELEMENT COORD SYSTEM PRINCIPAL STRESSES (ZERO SHEAR)ID. DISTANCE NORMAL-X NORMAL-Y SHEAR-XY ANGLE MAJOR MINOR VON MISES
0 1 -3.000000E-01 8.843602E+01 1.234005E+01 -2.772477E+00 -2.0838 8.853690E+01 1.223917E+01 8.309609E+013.000000E-01 8.843602E+01 1.234005E+01 -2.772477E+00 -2.0838 8.853690E+01 1.223917E+01 8.309609E+01
0 2 -3.000000E-01 6.215171E+01 -3.501347E+00 -2.779316E+00 -2.4198 6.226915E+01 -3.618794E+00 6.415514E+013.000000E-01 6.215171E+01 -3.501347E+00 -2.779316E+00 -2.4198 6.226915E+01 -3.618794E+00 6.415514E+01
0 3 -3.000000E-01 3.756313E+01 1.385617E+00 -2.770751E+00 -4.3543 3.777411E+01 1.174642E+00 3.720070E+013.000000E-01 3.756313E+01 1.385617E+00 -2.770751E+00 -4.3543 3.777411E+01 1.174642E+00 3.720070E+01
0 4 -3.000000E-01 1.237556E+01 -1.941755E+00 -2.776967E+00 -10.6011 1.289531E+01 -2.461504E+00 1.428601E+013.000000E-01 1.237556E+01 -1.941755E+00 -2.776967E+00 -10.6011 1.289531E+01 -2.461504E+00 1.428601E+01
0 5 -3.000000E-01 -8.843602E+01 -1.231288E+01 -2.780424E+00 -87.9110 -1.221146E+01 -8.853744E+01 8.310732E+013.000000E-01 -8.843602E+01 -1.231288E+01 -2.780424E+00 -87.9110 -1.221146E+01 -8.853744E+01 8.310732E+01
0 6 -3.000000E-01 -6.215171E+01 3.415766E+00 -2.770915E+00 -87.5844 3.532658E+00 -6.226860E+01 6.410797E+013.000000E-01 -6.215171E+01 3.415766E+00 -2.770915E+00 -87.5844 3.532658E+00 -6.226860E+01 6.410797E+01
0 7 -3.000000E-01 -3.756313E+01 -1.070353E+00 -2.779112E+00 -85.6699 -8.599231E-01 -3.777356E+01 3.735103E+013.000000E-01 -3.756313E+01 -1.070353E+00 -2.779112E+00 -85.6699 -8.599231E-01 -3.777356E+01 3.735103E+01
0 8 -3.000000E-01 -1.237556E+01 7.673735E-01 -2.772951E+00 -78.5609 1.328468E+00 -1.293666E+01 1.364947E+013.000000E-01 -1.237556E+01 7.673735E-01 -2.772951E+00 -78.5609 1.328468E+00 -1.293666E+01 1.364947E+01
1 CANTILEVER BEAM USING QUAD4 ELEMENTS FEBRUARY 20, 2007 MSC.NASTRAN 6/17/05 PAGE 7
0
No PARAM values were set in the Control File.
1 * * * END OF JOB * * *
4
cquad4_4.f06 2/20/2007
5
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