1)  Ansys Workbech
Ansys Workbech
2)  Ansys
Ansys
1.
Damage Study of Light Hydraulic Support Turned-beam Based on ANSYS;
基于ANSYS的轻型液压支架翻转梁破坏研究
2.
Stress Finite Element Analysis of Coal Mine Derrick Structural Based on ANSYS;
基于ANSYS的立井井架力学有限元分析
3.
Model Analysis of Vertical Wire Electrical Discharge Machining with Rotation Wire Based on ANSYS;
基于ANSYS的立式回转电火花线切割机床线架的模态分析
3)  ANSYS
ANSYS有限元分析程序
1.
This research measures the residual stress of high frequency electric resistant welded pipe using the central-hole method and analyses the transient state of deformation and residual stress of the weld with ANSYS nonlinear finite element program.
研究在现有条件下利用盲孔法测量了高频焊管接头焊缝的残余应力,并且采用ANSYS有限元分析程序,分析管道焊缝在焊接过程中的焊接残余应力。
4)  ANSYS
ANSYS软件
1.
Study on Application of ANSYS Software in Stability Analysis of Tailing Dam;
ANSYS软件在尾矿坝稳定性分析中的应用研究
2.
Thinking about application of ANSYS in some geotechnical project problems;
ANSYS软件分析不同岩土工程问题的若干思考
3.
The Application of ANSYS to Filled Conduit Analysis;
应用ANSYS软件分析地下埋管工程
5)  ANSYS
ANSYS有限元分析软件
1.
To improve the structural design of plasma spraying gun and make the cooling system of the gun more proper,the three-dimensional fluid field and temperature field inside plasma spraying gun were calculated approximately based on ANSYS software,and then the distribution diagrams of three-dimensional fluid field and temperature field inside the gun were gotten.
为改善等离子枪体结构设计,使枪体冷却系统更加完善,用ANSYS有限元分析软件对等离子枪体内部的三维流场和温度场进行了模拟计算,得到了枪体内部的三维温度场与流场分布图。
6)  ANSYS
有限元分析软件ANSYS
1.
The involute spur gear model is built in SolidWorks-3D mechanic design software,then analyzes stress of gear tooth by the finite element software ANSYS,so obtain the contour of bending stress distribution of tooth root.
通过三维机械设计软件SolidWorks构建直齿圆柱齿轮实体模型,运用有限元分析软件ANSYS对齿根进行应力分析计算,得出齿根弯曲应力分布云图,通过与理论分析结果的比较,说明ANSYS在齿轮计算中的有效性。
参考词条
补充资料:ANSYS工字梁焊缝初应力例子

建立好模型
…..
/SOLU
!*
ANTYPE,0
/INPUT,'input','txt',
/INPUT,'output1','txt',
!*
ISFILE,READ,1,txt, ,0
SOLVE
=====================
!定义残余应力矩阵
I=1
fy=310e6
!定义单元中心坐标数组,初应力数组
*DIM,EleCenter,ARRAY,NumNode,3,1, , ,
*DIM,EleIS,ARRAY,NumNode,1,1, , ,
*DO,I, 1, NumNode,1
!得到单元中心坐标
*GET,EleCenter(I,1,1),ELEM,I,CENT,X
*GET,EleCenter(I,2,1),ELEM,I,CENT,Y
*GET,EleCenter(I,3,1),ELEM,I,CENT,Z
!焊缝位置在X=1.0 到1.05 之间
*IF,EleCenter(I,1,1),GT,1,THEN
*IF,EleCenter(I,1,1),LT,1.05,THEN
*IF,EleCenter(I,2,1),GT,0.5,THEN
!上翼缘初始应力
EleIS(I,1,1)=-20*fy*EleCenter(I,3,1)**2+0.3*fy
*endif
*IF,EleCenter(I,2,1),LT,0.0,THEN
!下翼缘初始应力
EleIS(I,1,1)=-20*fy*EleCenter(I,3,1)**2+0.3*fy
*endif
!腹板初始应力
*if,EleCenter(I,2,1),GE,0.0,THEN
*IF,ELECENTER(I,2,1),LE,0.5,THEN
EleIS(I,1,1)=4.076*fy*(EleCenter(I,2,1)-0.5)**2
EleIS(I,1,1)=EleIS(I,1,1)-0.719*fy
*IF,EleIS(I,1,1),LT,-0.3*fy,THEN
ELeIS(I,1,1)=-0.3*fy
*ENDIF


*ENDIF
*ENDIF
*ENDIF
*ENDIF
*ENDDO
===============
!输出应力数值
*CFOPEN,'1','txt',' '
*DO,I,1,3840
!*IF,EleIS(I,1,1),ne,0.,then
*VWRITE,'!'
(A)
*VWRITE,'! Stress for element',
(A,F)
*VWRITE,'!'
(A)
*VWRITE,'eis,',I
(A,F)
P=EleIS(I,1,1)
*VWRITE,P,0.,0.,0.,0.,0.
(E,E,E,E,E,E)
!*ENDIF
*ENDDO
*CFCLOS

说明:补充资料仅用于学习参考,请勿用于其它任何用途。