一起学习板屈曲分析

上传人:xzh****18 文档编号:34308373 上传时间:2018-02-23 格式:DOC 页数:15 大小:63KB
返回 下载 相关 举报
一起学习板屈曲分析_第1页
第1页 / 共15页
一起学习板屈曲分析_第2页
第2页 / 共15页
一起学习板屈曲分析_第3页
第3页 / 共15页
一起学习板屈曲分析_第4页
第4页 / 共15页
一起学习板屈曲分析_第5页
第5页 / 共15页
点击查看更多>>
资源描述

《一起学习板屈曲分析》由会员分享,可在线阅读,更多相关《一起学习板屈曲分析(15页珍藏版)》请在金锄头文库上搜索。

1、一起学习板屈曲分析simwe 会员名:LXCAD一,材料为铁,适合做模板分析,动态显性,物质的非线形指南 10.5 blast loading on a stiffened plate*Amplitude, name=Blast, smooth=0.250., 0., 0.001, 700000., 0.01, 700000., 0.02, 0.0.05, 0.* * MATERIALS*材料明确为铁 *Material, name=Steel*Density7800.,*Elastic2.1e+11, 0.3* Plastic 关键字规定使用 Misess 屈服准则*Plastic3e+08

2、, 0.3.5e+08, 0.0253.75e+08, 0.13.94e+08, 0.24e+08, 0.35* * BOUNDARY CONDITIONS* * Name: Fix edges Type: Symmetry/Antisymmetry/Encastre*BoundaryEdge, ENCASTRE* -* * STEP: Blast* *Step, name=BlastApply blast loading*显性动态分析*Dynamic, Explicit, 0.05*Bulk Viscosity!修改屈曲粘性参数,均使用缺省值0.06, 1.2* * LOADS* * Nam

3、e: Pressure load Type: Pressure*Dsload, amplitude=Blast_PickedSurf6, P, 1.* 二,箱型结构使用动态求特征值例子手册 2.2.4 中,Eigenvalue analysis of a structure using the parallel Lanczos eigensolver*PARAMETER* modal input parametersnumModes = 200lowFreq = 0.0highFreq = 133.0*SHELL GENERAL SECTION, ELSET=ALL, MATERIAL=STE

4、EL0.01*MATERIAL, NAME=STEEL*ELASTIC200.E9, 0.3*DENSITY7800.0* Step definition*STEPFrequency extraction*FREQUENCY, NUMBER INTERVAL=4,*BOUNDARYBOTLEFT, ENCASTREBOTRIGHT, ENCASTRE*output, field, freq=0*END STEP三,静力分析(屈曲崩塌分析 关键字*STATIC,STABILIZE 的使用)例字手册 1.2.5 Unstable static problem: reinforced plate u

5、nder compressive loads*ELEMENT,TYPE=SPRING1,ELSET=EPONT50000,34050001,2881*弹簧可模拟拉条*SPRING,ELSET=EPONT3,5.3E+08,*BEAM SECTION,MATERIAL=ACIER,SECTION=RECT,ELSET=E00000011.500000E-02, 1.500000E-020.000000E+00, 6.557236E-03,-9.999785E-01*MATERIAL,NAME=ACIER *ELASTIC2.100E+11, 3.000E-01*PLASTIC235.259E+0

6、6,0.0471.9E+06,0.18837*DENSITY7.850E+03, *BEAM SECTION,MATERIAL=ACIER,SECTION=RECT,ELSET=E00000021.500000E-02, 1.500000E-020.000000E+00, 8.695324E-03,-9.999622E-01*SHELL SECTION,ELSET=E0000003,MATERIAL=ACIER 7.000E-03, 3*SHELL SECTION,ELSET=E0000004,MATERIAL=ACIER 1.000E-02, 3*SHELL SECTION,ELSET=TO

7、LE,MATERIAL=ACIER 5.000E-03, 3*SHELL SECTION,ELSET=E0000006,MATERIAL=ACIER 6.000E-03, 3*SHELL SECTION,ELSET=E0000007,MATERIAL=ACIER 7.000E-03, 3*SHELL SECTION,ELSET=E0000008,MATERIAL=ACIER 1.000E-02, 3*SHELL SECTION,ELSET=E0000009,MATERIAL=ACIER 1.000E-02, 3*SHELL SECTION,ELSET=E0000010,MATERIAL=ACI

8、ER 1.000E-02, 3*NSET,NSET=NM1329, *ELSET,ELSET=HILOIRE E0000004,E0000009,E0000010*ELSET,ELSET=BARROTS E0000003,E0000007,E0000008*ELSET,ELSET=TOT TOLE,HILOIRE,BARROTS,E0000001,E0000002,E0000006*MPCBEAM,COTE1,NM1*BOUNDARYNM1,3,3NM1,4,4NM1,6,6COTE2,1,1COTE2,3,3COTE2,4,4COTE2,6,68896,2,2COTE3,2,2COTE3,4

9、,4COTE3,6,6COTE4,2,2COTE4,4,4COTE4,6,6*RESTART,WRITE,F=30* *STEP,NLGEOM,INC=1GRAVITY LOAD*STATIC1.,1.*DLOADTOT,GRAV,9.81,0,0,-1.*NODE FILE,NSET=NM1,FREQ=1U,CF*EL FILE,ELSET=HILOIRE,FREQ=200S,E,PE *ENERGY FILE *OUTPUT,FIELD,FREQ=30*NODE OUTPUTU,*OUTPUT,HISTORY*NODE OUTPUT,NSET=NM1U,CF*ENERGY OUTPUT,V

10、ARIABLE=ALL*EL PRINT,FREQ=0*NODE PRINT,FREQ=0*END STEP*STEP,NLGEOM,INC=1000BUCKLING LOAD*STATIC,STABILIZE0.1,1.,*CLOADNM1,1,646.E+04*END STEP四,静力分析,焊点与接触的使用例子 1.2.3 Buckling of a column with spot welds*SHELL SECTION,ELSET=WPIL,MATERIAL=STEEL,SECTION INTEGRA=GAUSS0.002,*SHELL SECTION,ELSET=BPIL,MATER

11、IAL=STEEL,SECTION INTEGRA=GAUSS0.003,*MATERIAL,NAME=STEEL*DENSITY7850.,*ELASTIC206.8E9,0.3*PLASTIC170.0E6, 0.0000000E+00180.0E6, 1.7205942E-03190.0E6, 3.8296832E-03200.0E6, 6.3897874E-03210.0E6, 9.4694765E-03220.0E6, 1.3143660E-02230.0E6, 1.7493792E-02240.0E6, 2.2608092E-02250.0E6, 2.8581845E-02260.

12、0E6, 3.5517555E-02270.0E6, 4.3525275E-02280.0E6, 5.2722659E-02290.0E6, 6.3235357E-02300.0E6, 7.5197279E-02310.0E6, 8.8750519E-02320.0E6, 0.1040458330.0E6, 0.1212430340.0E6, 0.1405106350.0E6, 0.1620263360.0E6, 0.1859779370.0E6, 0.2125620380.0E6, 0.2419857390.0E6, 0.2744660400.0E6, 0.3102303410.0E6, 0

13、.3495160420.0E6, 0.3925720430.0E6, 0.4396578440.0E6, 0.4910434450.0E6, 0.5470111460.0E6, 0.6078544470.0E6, 0.6738777480.0E6, 0.7453985490.0E6, 0.8227461500.0E6, 0.9062610510.0E6, 0.9962980*NSET,NSET=BASE,GEN101,129,1200,214,1*BOUNDARYBASE,ENCASTRE*SURFACE,TYPE=ELEMENT,NAME=BPILBPIL1, *SURFACE,TYPE=E

14、LEMENT,NAME=WPILWPIL1, *RIGID BODY,ELSET=ROOF,REF=60000*NSET,NSET=WELDREFNODES,GEN5203,45203,100005211,45211,10000*ELEMENT, TYPE=CONN3D2, ELSET=FASTCONN1000000,5203,1052031000001,15203,10152031000002,25203,10252031000003,35203,10352031000004,45203,10452032000000,5211,1052112000001,15211,10152112000002,25211,10252112000003,35211,10352112000004,45211,1045211*ORIENTATION, NAME=GLOBAL1.,0.,0.,0.,1.,0.*CONNECTOR SECTION, ELSET=FASTCONN, BEHAVIOR=BEHV,ELIM

展开阅读全文
相关资源
相关搜索

当前位置:首页 > 办公文档 > 其它办公文档

电脑版 |金锄头文库版权所有
经营许可证:蜀ICP备13022795号 | 川公网安备 51140202000112号