- 积分
- 0
- 注册时间
- 2008-12-16
- 仿真币
-
- 最后登录
- 1970-1-1
|
Private Sub Command1_Click()
Dim a
a = Shell("c:\Program Files\ANSYS Inc\v100\ANSYS\bin\intel\ansys100.exe -b -i F:\vbansys\1.txt -o f:\ansys\output.txt", vbMaximizedFocus)
End Sub
1.txt文件
/prep7
et,1,beam3
mp,ex,1,2e11
r,1,0.1778,0.0923
et,2,link10
mp,ex,2,2.1e11
r,2,0.01
n,1,-80.699,-26.891,0
n,2,-77.720,-24.881,0,
n,3,-74.726,-22.881,0,
n,4,-71.687,-20.945,0,
n,5,-68.603,-19.083,0,
n,6,-65.475,-17.295,0,
n,7,-62.304,-15.584,0,
n,8,-59.091,-13.953,0,
n,9,-55.839,-12.403,0,
n,10,-52.548,-10.937,0,
n,11,-49.220,-9.556,0,
n,12,-45.857,-8.263,0,
n,13,-42.461,-7.059,0,
n,14,-39.034,-5.945,0,
n,15,-35.579,-4.924,0,
n,16,-32.098,-3.996,0,
n,17,-28.593,-3.162,0,
n,18,-25.066,-2.425,0,
n,19,-21.520,-1.784,0,
n,20,-17.959,-1.240,0,
n,21,-14.383,-0.794,0,
n,22,-10.797,-0.447,0,
n,23,-7.203,-0.199,0,
n,24,-3.603,-0.050,0,
n,25,-0.0,-0.0,0,
type,1
mat,1
real,1
e,1,2
e,2,3
e,3,4
e,4,5
e,5,6
e,6,7
e,7,8
e,8,9
e,9,10
e,10,11
e,11,12
e,12,13
e,13,14
e,14,15
e,15,16
e,16,17
e,17,18
e,18,19
e,19,20
e,20,21
e,21,22
e,22,23
e,23,24
e,24,25
mp,dens,1, 8269
d,1,ux
d,1,uy
n,26,-80.699,-4.924
n,27,-80.699,9
d,26,all
d,27,all
type,2
mat,2
real,2
e,26,5
e,26,8
e,26,11
e,26,14
e,27,17
e,27,20
e,27,23
/solu
acel,,9.81
solve
/post1
plnsol,u,sum,2
/SHOW,JPEG
JPEG,QUAL,75,
JPEG,ORIENT,HORIZ
JPEG,COLOR,2
JPEG,TMOD,1
/GFILE,600,
esel,mat,2
PRESOL,SMISC, 1
esel,all
esel,mat,1
nsel,r,node,,5,23,3
prnsol,u,y
output.txt中文件
ANSYS Mechanical U
*-------------------------------------------------------------*
| |
| W E L C O M E T O T H E A N S Y S P R O G R A M |
| |
*-------------------------------------------------------------*
***************************************************************
* ANSYS 10.0 LEGAL NOTICES *
***************************************************************
* *
* Copyright 2005 SAS IP, Inc. All rights reserved. *
* Unpublished rights reserved under the Copyright Laws of *
* the United States. *
* *
* ANSYS, Inc. is a UL registered ISO 9001: 2000 Company *
* *
* See the ANSYS, Inc. online documentation or the ANSYS, Inc. *
* documentation CD for the complete Legal Notice. *
* *
***************************************************************
* *
* DISCLAIMER NOTICE *
* *
* Information in this Information System is subject to *
* change without notice. Complying with all applicable *
* copyright laws is the responsibility of the user. No part *
* of this system may be reproduced or transmitted in any *
* form or by any means, electronic or mechanical, without *
* prior written permission of ANSYS, Inc. *
* *
* This document has been reviewed and approved in accordance *
* with ANSYS, Inc. Documentation Review and Approval *
* Procedures. *
* *
* This ANSYS, Inc. software product and program *
* documentation are furnished by ANSYS, Inc. under an ANSYS *
* software license agreement that contains provisions *
* concerning non-disclosure, copying, length and nature of *
* use, warranties, disclaimers and remedies, and other *
* provisions. The Program and Documentation may be used or *
* copied only in accordance with the terms of that license *
* agreement. *
* *
* *
* THIS SOFTWARE CONTAINS CONFIDENTIAL INFORMATION AND TRADE *
* SECRETS OF SAS IP, INC. USE, DISCLOSURE, OR REPRODUCTION *
* IS PROHIBITED WITHOUT THE PRIOR EXPRESS WRITTEN PERMISSION *
* OF SAS IP, INC. *
* *
* ANSYS, Inc. may have patents, patent applications, *
* trademarks, copyrights, or other intellectual property *
* rights covering subject matter in this documentation and *
* product. Except as expressly provided in any written *
* license agreement from ANSYS, Inc., the furnishing of any *
* product does not give you any license to these patents, *
* trademarks, copyrights, or other intellectual property. *
* *
***************************************************************
* *
* Warning: This computer program is protected by copyright *
* law and international treaties. Unauthorized reproduction *
* or distribution of this program, or any portion of it, may *
* result in severe civil and criminal penalties, and will be *
* prosecuted to the maximum extent possible under the law. *
* *
***************************************************************
* *
* U.S. GOVERNMENT RIGHTS *
* *
* Use, duplication, or disclosure by the U.S. Government is *
* subject to restrictions set forth in the ANSYS, Inc. *
* license agreement and as provided in DFARS 227.7202-1(a) *
* and 227.7202-3(a)(1995), DFARS 252.227-7013(c)(1)(ii) (OCT *
* 1988), FAR 12.212(a)(1995), FAR 52.227-19, or FAR52.227-14 *
* (ALT III), as applicable. ANSYS, Inc. *
* *
***************************************************************
Completing ANSYS Load Process.
***** ANSYS COMMAND LINE ARGUMENTS *****
BATCH MODE REQUESTED = LIST
00265621 VERSION=INTEL NT RELEASE= 10.0 UP20050718
CURRENT JOBNAME=file 17:22:15 SEP 16, 2010 CP= 0.594
1 /prep7
2 et,1,beam3
3 mp,ex,1,2e11
4 r,1,0.1778,0.0923
5 et,2,link10
6 mp,ex,2,2.1e11
7 r,2,0.01
8 n,1,-80.699,-26.891,0
9 n,2,-77.720,-24.881,0,
10 n,3,-74.726,-22.881,0,
11 n,4,-71.687,-20.945,0,
12 n,5,-68.603,-19.083,0,
13 n,6,-65.475,-17.295,0,
14 n,7,-62.304,-15.584,0,
15 n,8,-59.091,-13.953,0,
16 n,9,-55.839,-12.403,0,
17 n,10,-52.548,-10.937,0,
18 n,11,-49.220,-9.556,0,
19 n,12,-45.857,-8.263,0,
20 n,13,-42.461,-7.059,0,
21 n,14,-39.034,-5.945,0,
22 n,15,-35.579,-4.924,0,
23 n,16,-32.098,-3.996,0,
24 n,17,-28.593,-3.162,0,
25 n,18,-25.066,-2.425,0,
26 n,19,-21.520,-1.784,0,
27 n,20,-17.959,-1.240,0,
28 n,21,-14.383,-0.794,0,
29 n,22,-10.797,-0.447,0,
30 n,23,-7.203,-0.199,0,
31 n,24,-3.603,-0.050,0,
32 n,25,-0.0,-0.0,0,
33 type,1
34 mat,1
35 real,1
36 e,1,2
37 e,2,3
38 e,3,4
39 e,4,5
40 e,5,6
41 e,6,7
42 e,7,8
43 e,8,9
44 e,9,10
45 e,10,11
46 e,11,12
47 e,12,13
48 e,13,14
49 e,14,15
50 e,15,16
51 e,16,17
52 e,17,18
53 e,18,19
54 e,19,20
55 e,20,21
56 e,21,22
57 e,22,23
58 e,23,24
59 e,24,25
60 mp,dens,1, 8269
61 d,1,ux
62 d,1,uy
63 n,26,-80.699,-4.924
64 n,27,-80.699,9
65 d,26,all
66 d,27,all
67 type,2
68 mat,2
69 real,2
70 e,26,5
71 e,26,8
72 e,26,11
73 e,26,14
74 e,27,17
75 e,27,20
76 e,27,23
77 /solu
78 acel,,9.81
79 solve
80 /post1
81 plnsol,u,sum,2
82 /SHOW,JPEG
83 JPEG,QUAL,75,
84 JPEG,ORIENT,HORIZ
85 JPEG,COLOR,2
86 JPEG,TMOD,1
87 /GFILE,600,
88 esel,mat,2
89 PRESOL,SMISC, 1
90 esel,all
91 esel,mat,1
92 nsel,r,node,,5,23,3
93 prnsol,u,y
94
95
RUN SETUP PROCEDURE FROM FILE= C:\Program Files\Ansys Inc\v100\ANSYS\apdl\start100.ans
/INPUT FILE= C:\Program Files\Ansys Inc\v100\ANSYS\apdl\start100.ans LINE= 0
1
***** ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 10.0 *****
ANSYS Mechanical U
00265621 VERSION=INTEL NT 17:22:15 SEP 16, 2010 CP= 0.594
***** ANSYS ANALYSIS DEFINITION (PREP7) *****
ELEMENT TYPE 1 IS BEAM3 2-D ELASTIC BEAM
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0
CURRENT NODAL DOF SET IS UX UY ROTZ
TWO-DIMENSIONAL MODEL
MATERIAL 1 EX = 0.2000000E+12
REAL CONSTANT SET 1 ITEMS 1 TO 6
0.17780 0.92300E-01 0.0000 0.0000 0.0000 0.0000
ELEMENT TYPE 2 IS LINK10 TENSION-ONLY SPAR
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0
CURRENT NODAL DOF SET IS UX UY UZ ROTZ
THREE-DIMENSIONAL MODEL
MATERIAL 2 EX = 0.2100000E+12
REAL CONSTANT SET 2 ITEMS 1 TO 6
0.10000E-01 0.0000 0.0000 0.0000 0.0000 0.0000
NODE 1 KCS= 0 X,Y,Z= -80.699 -26.891 0.0000
NODE 2 KCS= 0 X,Y,Z= -77.720 -24.881 0.0000
NODE 3 KCS= 0 X,Y,Z= -74.726 -22.881 0.0000
NODE 4 KCS= 0 X,Y,Z= -71.687 -20.945 0.0000
NODE 5 KCS= 0 X,Y,Z= -68.603 -19.083 0.0000
NODE 6 KCS= 0 X,Y,Z= -65.475 -17.295 0.0000
NODE 7 KCS= 0 X,Y,Z= -62.304 -15.584 0.0000
NODE 8 KCS= 0 X,Y,Z= -59.091 -13.953 0.0000
NODE 9 KCS= 0 X,Y,Z= -55.839 -12.403 0.0000
NODE 10 KCS= 0 X,Y,Z= -52.548 -10.937 0.0000
NODE 11 KCS= 0 X,Y,Z= -49.220 -9.5560 0.0000
NODE 12 KCS= 0 X,Y,Z= -45.857 -8.2630 0.0000
NODE 13 KCS= 0 X,Y,Z= -42.461 -7.0590 0.0000
NODE 14 KCS= 0 X,Y,Z= -39.034 -5.9450 0.0000
NODE 15 KCS= 0 X,Y,Z= -35.579 -4.9240 0.0000
NODE 16 KCS= 0 X,Y,Z= -32.098 -3.9960 0.0000
NODE 17 KCS= 0 X,Y,Z= -28.593 -3.1620 0.0000
NODE 18 KCS= 0 X,Y,Z= -25.066 -2.4250 0.0000
NODE 19 KCS= 0 X,Y,Z= -21.520 -1.7840 0.0000
NODE 20 KCS= 0 X,Y,Z= -17.959 -1.2400 0.0000
NODE 21 KCS= 0 X,Y,Z= -14.383 -0.79400 0.0000
NODE 22 KCS= 0 X,Y,Z= -10.797 -0.44700 0.0000
NODE 23 KCS= 0 X,Y,Z= -7.2030 -0.19900 0.0000
NODE 24 KCS= 0 X,Y,Z= -3.6030 -0.50000E-01 0.0000
NODE 25 KCS= 0 X,Y,Z= 0.0000 0.0000 0.0000
ELEMENT TYPE SET TO 1
MATERIAL NUMBER SET TO 1
REAL CONSTANT NUMBER= 1
ELEMENT 1 1 2
ELEMENT 2 2 3
ELEMENT 3 3 4
ELEMENT 4 4 5
ELEMENT 5 5 6
ELEMENT 6 6 7
ELEMENT 7 7 8
ELEMENT 8 8 9
ELEMENT 9 9 10
ELEMENT 10 10 11
ELEMENT 11 11 12
ELEMENT 12 12 13
ELEMENT 13 13 14
ELEMENT 14 14 15
ELEMENT 15 15 16
ELEMENT 16 16 17
ELEMENT 17 17 18
ELEMENT 18 18 19
ELEMENT 19 19 20
ELEMENT 20 20 21
ELEMENT 21 21 22
ELEMENT 22 22 23
ELEMENT 23 23 24
ELEMENT 24 24 25
MATERIAL 1 DENS = 8269.000
SPECIFIED CONSTRAINT UX FOR SELECTED NODES 1 TO 1 BY 1
REAL= 0.00000000 IMAG= 0.00000000
SPECIFIED CONSTRAINT UY FOR SELECTED NODES 1 TO 1 BY 1
REAL= 0.00000000 IMAG= 0.00000000
NODE 26 KCS= 0 X,Y,Z= -80.699 -4.9240 0.0000
NODE 27 KCS= 0 X,Y,Z= -80.699 9.0000 0.0000
SPECIFIED CONSTRAINT UX FOR SELECTED NODES 26 TO 26 BY 1
REAL= 0.00000000 IMAG= 0.00000000
ADDITIONAL DOFS= UY UZ ROTZ
SPECIFIED CONSTRAINT UX FOR SELECTED NODES 27 TO 27 BY 1
REAL= 0.00000000 IMAG= 0.00000000
ADDITIONAL DOFS= UY UZ ROTZ
ELEMENT TYPE SET TO 2
MATERIAL NUMBER SET TO 2
REAL CONSTANT NUMBER= 2
ELEMENT 25 26 5
ELEMENT 26 26 8
ELEMENT 27 26 11
ELEMENT 28 26 14
ELEMENT 29 27 17
ELEMENT 30 27 20
ELEMENT 31 27 23
***** ROUTINE COMPLETED ***** CP = 0.594
***** ANSYS SOLUTION ROUTINE *****
ACEL= 0.0000 9.8100 0.0000
***** ANSYS SOLVE COMMAND *****
*** NOTE *** CP = 0.609 TIME= 17:22:15
There is no title defined for this analysis.
1
***** ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 10.0 *****
ANSYS Mechanical U
00265621 VERSION=INTEL NT 17:22:15 SEP 16, 2010 CP= 0.609
S O L U T I O N O P T I O N S
PROBLEM DIMENSIONALITY. . . . . . . . . . . . .3-D
DEGREES OF FREEDOM. . . . . . UX UY UZ ROTZ
ANALYSIS TYPE . . . . . . . . . . . . . . . . .STATIC (STEADY-STATE)
NEWTON-RAPHSON OPTION . . . . . . . . . . . . .PROGRAM CHOSEN
GLOBALLY ASSEMBLED MATRIX . . . . . . . . . . .SYMMETRIC
*** WARNING *** CP = 0.609 TIME= 17:22:15
Zero thickness element 1 may result in wrong thermal or bending stress.
Check real constant table 1.
*** WARNING *** CP = 0.609 TIME= 17:22:15
Element 1 ( BEAM3 ) uses material 1 for which GXY, PRXY and NUXY are
all undefined. A default value of EX/2.6 will be used. Input MP,GXY,
1,EX/2.6 (EX = parameter value of Young's modulus) to eliminate this
warning.
*** NOTE *** CP = 0.609 TIME= 17:22:15
Present time 0 is less than or equal to the previous time.
Time will default to 1.
*** NOTE *** CP = 0.609 TIME= 17:22:15
The step data was checked and warning messages were found.
Please review output or errors file ( F:\vbansys\file.err ) for these
warning messages.
*** NOTE *** CP = 0.609 TIME= 17:22:15
Nonlinear analysis, NROPT set to the INITial stiffness Newton-Raphson
solution procedure for ALL DOFs.
SOLCONTROL,ON uses sparse matrix direct solver
*** WARNING *** CP = 0.609 TIME= 17:22:15
The program chosen initial timestep/load-factor is arbitrary. It is
necessary for the user to supply a suitable initial
timestep/load-factor through the NSUB or DELTIM command for
convergence and overall efficiency.
L O A D S T E P O P T I O N S
LOAD STEP NUMBER. . . . . . . . . . . . . . . . 1
TIME AT END OF THE LOAD STEP. . . . . . . . . . 1.0000
AUTOMATIC TIME STEPPING . . . . . . . . . . . . ON
INITIAL NUMBER OF SUBSTEPS . . . . . . . . . 1
MAXIMUM NUMBER OF SUBSTEPS . . . . . . . . . 1000
MINIMUM NUMBER OF SUBSTEPS . . . . . . . . . 1
START WITH TIME STEP FROM PREVIOUS SUBSTEP . YES
MAXIMUM NUMBER OF EQUILIBRIUM ITERATIONS. . . . 15
STEP CHANGE BOUNDARY CONDITIONS . . . . . . . . NO
TERMINATE ANALYSIS IF NOT CONVERGED . . . . . .YES (EXIT)
CONVERGENCE CONTROLS. . . . . . . . . . . . . .USE DEFAULTS
INERTIA LOADS X Y Z
ACEL . . . . . . . . . . . . 0.0000 9.8100 0.0000
PRINT OUTPUT CONTROLS . . . . . . . . . . . . .NO PRINTOUT
DATABASE OUTPUT CONTROLS. . . . . . . . . . . .ALL DATA WRITTEN
FOR THE LAST SUBSTEP
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file.mntr
MAXIMUM NUMBER OF EQUILIBRIUM ITERATIONS HAS BEEN MODIFIED
TO BE, NEQIT = 22, BY SOLUTION CONTROL LOGIC.
**** CENTER OF MASS, MASS, AND MASS MOMENTS OF INERTIA ****
CALCULATIONS ASSUME ELEMENT MASS AT ELEMENT CENTROID
TOTAL MASS = 0.12712E+06
MOM. OF INERTIA MOM. OF INERTIA
CENTER OF MASS ABOUT ORIGIN ABOUT CENTER OF MASS
XC = -41.733 IXX = 0.1913E+08 IXX = 0.8334E+07
YC = -9.2166 IYY = 0.2911E+09 IYY = 0.6967E+08
ZC = 0.0000 IZZ = 0.3102E+09 IZZ = 0.7800E+08
IXY = -0.7215E+08 IXY = -0.2326E+08
IYZ = 0.000 IYZ = 0.000
IZX = 0.000 IZX = 0.000
*** MASS SUMMARY BY ELEMENT TYPE ***
TYPE MASS
1 127116.
Range of element maximum matrix coefficients in global coordinates
Maximum= 2.054717881E+10 at element 1.
Minimum= 27914465.7 at element 31.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 24 BEAM3 0.000 0.000000
2 7 LINK10 0.000 0.000000
Time at end of element matrix formulation CP= 0.6875.
ALL CURRENT ANSYS DATA WRITTEN TO FILE NAME= file.rdb
FOR POSSIBLE RESUME FROM THIS POINT
FORCE CONVERGENCE VALUE = 0.2505E+06 CRITERION= 1278.
MOMENT CONVERGENCE VALUE = 0.2024E+05 CRITERION= 103.2
SPARSE MATRIX DIRECT SOLVER.
Number of equations = 73, Maximum wavefront = 6
Memory available for solver = 38.17 MB
Memory required for in-core = 0.02 MB
Optimal memory required for out-of-core = 0.02 MB
Minimum memory required for out-of-core = 0.02 MB
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.8449E-01
FORCE CONVERGENCE VALUE = 0.2806E-06 CRITERION= 0.1126E+05 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.3301E-06 CRITERION= 105.3 <<< CONVERGED
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1
*** ELEMENT RESULT CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 24 BEAM3 0.000 0.000000
2 7 LINK10 0.000 0.000000
*** NODAL LOAD CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 24 BEAM3 0.000 0.000000
2 7 LINK10 0.000 0.000000
*** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 1
*** TIME = 1.00000 TIME INC = 1.00000
*** ANSYS BINARY FILE STATISTICS
BUFFER SIZE USED= 16384
0.063 MB WRITTEN ON ELEMENT MATRIX FILE: file.emat
0.063 MB WRITTEN ON ELEMENT SAVED DATA FILE: file.esav
0.063 MB WRITTEN ON ASSEMBLED MATRIX FILE: file.full
0.063 MB WRITTEN ON RESULTS FILE: file.rst
FINISH SOLUTION PROCESSING
***** ROUTINE COMPLETED ***** CP = 0.734
1
***** ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 10.0 *****
ANSYS Mechanical U
00265621 VERSION=INTEL NT 17:22:16 SEP 16, 2010 CP= 0.734
***** ANSYS RESULTS INTERPRETATION (POST1) *****
*** NOTE *** CP = 0.734 TIME= 17:22:16
Reading results into the database (SET command) will update the current
displacement and force boundary conditions in the database with the
values from the results file for that load set. Note that any
subsequent solutions will use these values unless action is taken to
either SAVE the current values or not overwrite them (/EXIT,NOSAVE).
/SHOW SWITCH PLOTS TO JPEG - RASTER MODE.
JPEG quality setting = 75
JPEG orientation is horizontal
JPEG pixels are in color
JPEG characters are bitmaps
GRAPHICS FILE PIXEL RESOLUTION = 600
ESEL FOR LABEL= MAT FROM 2 TO 2 BY 1
7 ELEMENTS (OF 31 DEFINED) SELECTED BY ESEL COMMAND.
PRINT SUMMABLE MISCELLANEOUS ELEMENT SOLUTION PER ELEMENT
1
***** ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 10.0 *****
ANSYS Mechanical U
00265621 VERSION=INTEL NT 17:22:16 SEP 16, 2010 CP= 0.734
***** POST1 ELEMENT SUMMABLE MISCELLANEOUS RECORD LISTING *****
LOAD STEP= 1 SUBSTEP= 1
TIME= 1.0000 LOAD CASE= 0
ELEM SMIS1
25 25364.
26 11611.
27 37305.
28 84912.
29 0.33551E+06
30 0.44652E+06
31 0.49910E+06
MINIMUM VALUES
ELEM 26
VALUE 11611.
MAXIMUM VALUES
ELEM 31
VALUE 0.49910E+06
ALL SELECT FOR ITEM=ELEM COMPONENT=
IN RANGE 1 TO 31 STEP 1
31 ELEMENTS (OF 31 DEFINED) SELECTED BY ESEL COMMAND.
ESEL FOR LABEL= MAT FROM 1 TO 1 BY 1
24 ELEMENTS (OF 31 DEFINED) SELECTED BY ESEL COMMAND.
RESELECT FOR ITEM=NODE COMPONENT=
IN RANGE 5 TO 23 STEP 3
7 NODES (OF 27 DEFINED) SELECTED BY NSEL COMMAND.
PRINT U NODAL SOLUTION PER NODE
1
***** ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 10.0 *****
ANSYS Mechanical U
00265621 VERSION=INTEL NT 17:22:16 SEP 16, 2010 CP= 0.734
***** POST1 NODAL DEGREE OF FREEDOM LISTING *****
LOAD STEP= 1 SUBSTEP= 1
TIME= 1.0000 LOAD CASE= 0
THE FOLLOWING DEGREE OF FREEDOM RESULTS ARE IN THE GLOBAL COORDINATE SYSTEM
NODE UY
5 -0.63425E-03
8 -0.14940E-02
11 -0.37722E-02
14 -0.92112E-02
17 -0.20455E-01
20 -0.39926E-01
23 -0.65804E-01
MAXIMUM ABSOLUTE VALUES
NODE 23
VALUE -0.65804E-01
***** END OF INPUT ENCOUNTERED *****
NUMBER OF WARNING MESSAGES ENCOUNTERED= 3
NUMBER OF ERROR MESSAGES ENCOUNTERED= 0
***** PROBLEM TERMINATED BY INDICATED ERROR(S) OR BY END OF INPUT DATA *****
*---------------------------------------------------------------------------*
| |
| ANSYS RUN COMPLETED |
| |
|---------------------------------------------------------------------------|
| |
| Release 10.0 UP20050718 INTEL NT |
| |
|---------------------------------------------------------------------------|
| |
| Maximum Scratch Memory Used = 67008344 Words 255.617 MB |
| |
|---------------------------------------------------------------------------|
| |
| CP Time (sec) = 0.750 Time = 17:22:16 |
| Elapsed Time (sec) = 2.000 Date = 09/16/2010 |
| |
*---------------------------------------------------------------------------*
请求高手指点 |
|
IP卡
狗仔卡
发表于 2010-9-16 17:34:41
提升卡
沉默卡
喧嚣卡
变色卡
抢沙发
千斤顶
显身卡
发表于 2010-12-25 22:21:42
