有限元作业-研究生

目录

1基础部分....................................................................2

1.1模拟一带中心圆孔的矩形板受到均布拉力的作用......................2

1.1.1模拟结果输出................................................2

1.1.2命令流文件..................................................5

1.2用ANSYS模拟厚壁筒受内压问题..................................10

1.2.1模拟结果输出...............................................10

1.2.2命令流输出.................................................12

1.3用ANSYS模拟圆棒拉伸出现颈缩问题..............................15

1.3.1模拟结果输出...............................................15

1.4具有中心孔的薄壁圆筒受均匀拉伸.................................21

1.4.1模拟结果输出...............................................21

1.4.2命令流文件.................................................23

1.5用ANSYS求解剪切锁定超弹性梁问题.............................31

1.7用ANSYS表面效应单元模拟带穿透圆孔螺栓的弹塑性扭转问题......32

1.7.1模拟结果输出...............................................32

1.7.2命令流文件.................................................32

1.8用ANSYS模拟超弹性球压缩......................................38

1.9用ANSYS模拟长圆柱侧挤压接触问题.............................39

1.10采用Norton隐式蠕变模型模拟板材压力成型过程..................41

2提高部分...................................................................44

2.11用ANSYS模拟瞬态热传导问题..................................44

2.12应用ANSYS生成死单元模拟三点弯曲梁内裂纹扩展................46

2.13用ANSYS对I型钢柱进行非线性屈曲分析........................47

2.14用ANSYS模拟相变问题.........................................49

2.17用ANSYS-LSDYNA模拟陶瓷棒冲击侵彻铝板....................53

2.19用ANSYS求解含裂纹等厚度空心圆盘的J积分和强度因子问题.....54

1歙出部分

1.1模拟T中心圆孔的矩形板受到均布拉力的作用

1.1.1模拟结果输出

ANSYS

NODALSOLUTIONR1.4.5

STEP=112014

SUB=2010:33:34

TIME-1

SEQV(AVG)

DMX=.572E-03

SMN=7753.25

SMX-43692.8

7753.2515739.823726.431712.939699.5

11746.519733.127719.735706.243692.8

图1-1材料1的vonMises等效应力

图1-2材料1的等效塑性应变

ANSYS

NODALSOLUTIONR14-5

STEP=1MAR12014

SUB=2011:22:12

TIME-1

SEQV(AVG)

DMX-.438E-03

SMN=7755.76

SMX=55851.2

7755.7618443.629131.539819.450507.3

13099.723787.634475.445163.355851.2

图1-3材料2的Hill屈服等效应力

ANSYS

NODALSOLUTION

STEP=1MAR12014

SUB-2011:22:53

TIME=1

NLEPEQ(AVG)

RSYS=0

DMX-.438E-03

SMX=.004191

0.931E-03.001863.002794.003726

.466E-03.001397.002328.00326.004191

图1-4材料2的Hill屈服等效应变

ANSYS

NODALSOLUTION

STEP-1MAR12014

SUB=20

11:12:53

TIME=1

SEQV(AVG)

DMX=.596E-03

SMN-7520.43

SMX=44421

7520.4315720.623920.732120.840320.9

11620.519820.628020.836220.944421

图1-5材料3的vonMises等效应力

ANSYS

R14>5

0.002453.004907.00736.009814

.001227.00368.006134.008587.01104

图1-6材料3的vonMises等效应变

1.1.2命令流文件

WPSTYLE,,,,,”,。

/FILNAME,tensionofaplatew汕hole,0

!*

/NOPR

KEYW,PR_SET,1

KEYW,PR_STRUC,1

KEYW,PR_THERM,0

KEYW,PR_FLUID,0

KEYW,PR_ELMAG,0

KEYW,MAGNOD,0

KEYW,MAGEDG,0

KEYW,MAGHFE,0

KEYW,MAGELC,0

KEYW,PR_MULTI,0

KEYW,PR_CFD,0

/GO

!*

/COM,

/COM,PreferencesforGUIfilteringhavebeensettodisplay:

/COM,Structural

!*

/PREP7

!*

ET,1,PLANE182

!*

KEYOPT,1,1,0

KEYOPT,1,3,0

KEYOPT,1,6,0

!*

!*

MPTEMP,,,,,,,,

MPTEMP,l,0

MPDATA,EX,l„30e6

MPDATA,EY,l„30e6

MPDATA,EZ,l„30e6

MPDATA,PRXY,l„0.3

MPDATA,PRYZ,l„0.3

MPDATA,PRXZ,l„0.3

MPDATA,GXY,1„11,54e6

MPDATA,GYZ,1„11.54e6

MPDATA,GXZ,l„11.54e6

TB,BISO,1,1,2,

TBTEMP,0

TBDATA„33e3,10e5„„

TB,HILL,1,1,6,

TBTEMP,0

TBDATA„1.5,1,1,1,1,1

!*

MPTEMP,,,,,,,,

MPTEMP,l,0

MPDATA,EX,2„30e6

MPDATA,EY,2,,30e6

MPDATA,EZ,2,,30e6

MPDATA,PRXY,2„0.3

MPDATA,PRYZ,2,,0.3

MPDATA,PRXZ,2„0.3

MPDATA,GXY,2„11.54e6

MPDATA,GYZ,2„11.54e6

MPDATA,GXZ,2„11,54e6

TB,BISO,2,1,2,

TBTEMP,0

TBDATA„33e3,10e5„„

TB,HILL,2,1,6,

TBTEMP,0

TBDATA„1,1.5,1,1,1,1

!*

MPTEMP,,,,,,,,

MPTEMP,l,0

MPDATA,EX,3„30e6

MPDATA,PRXY,3„0.3

TB,BISO,3,1,2,

TBTEMP,0

TBDATA„33e3,10e5„„

BLC4,0,0,0.4,0.4

CYL4,0,0,0.05,0,0,90

ASBA,1,2

CM,_Y,AREA

ASEL,,,,3

CM,_Y1,AREA

CMSEL,S,_Y

!*

SMRT,6

SMRT,5

SMRT,4

MSHAPE,0,2D

MSHKEY,0

!*

CM,_Y,AREA

ASEL,,,,3

CM,_Y1,AREA

CHKMSH；AREA'

CMSEL,S,_Y

!*

AMESH,_Y1

CMDELE,_Y

CMDELE,_Y1

CMDELE,_Y2

!*

FLST,5,26,2,ORDE,13

FITEM,5,1

FITEM,5,-3

FITEM,5,7

FITEM,5,-10

FITEM,5,128

FITEM,5,196

FITEM,5,209

FITEM,5,-210

FITEM,5,224

FITEM,5,-225

FITEM,5,265

FITEM,5,283

FITEM,5,-294

CM,_Y,ELEM

ESEL,,,,P51X

CM,_Y1,ELEM

CMSEL,S,_Y

CMDELE,_Y

!*

!*

EREF,_Y1,,,2,O,U

CMDELE,_Y1

!*

FINISH

/SOL

FLST,2,2,4,ORDE,2

FITEM,2,8

FITEM,2,-9

DL,P51X,,SYMM

FLST,2,1,4,ORDE,1

FITEM,2,3

/GO

!*

SFL,P51X,PRES,-30e3,

!*

ANTYPE,0

NLGEOM,1

NSUBST,20,le5,20

FINISH

/PREP7

FINISH

/SOL

/STATUS,SOLU

SOLVE

1.2用ANSYS模拟厚壁筒受内压问题

1.2.1模拟结果输出

ANSYS

DISPLACEMENTRl.4.5

STEP=1MAR142014

SUB=620:50:48

TIME-1

DMX=.094207

图1-7输出薄壁筒变形的前后

ANSYS

NODALSOLUTIONR14.5

STEP=1MAR32014

SUB=619:49:06

TIME-1

SEQV(AVG)

DMX=.094333

SMN=63.2618

SMX-200.484

63.261893.7555124.249154.743185.237

78.5087109.002139.496169.99200.484

图1-8vonMises等效应力

ANSYS

NODALSOLUTIONRl.i.5

STEP=1MAR142014

SUB=620:53:54

TIME-1

NLEPEQ(AVG)

RSYS=0

DMX=.094207

图1-9等效塑性应变

1.2.2命令流输出

WPSTYLE,,,,,,,,。

/FILNAME,pressureonthickcylinder,0

/PREP7

!*

/NOPR

KEYW,PR_SET,1

KEYW,PR_STRUC,1

KEYW,PR_THERM,0

KEYW,PR_FLUID,0

KEYW,PR_ELMAG,0

KEYW,MAGNOD,0

KEYW,MAGEDG,0

KEYW,MAGHFE,0

KEYW,MAGELC,0

KEYW,PR_MULTI,0

KEYW,PR_CFD,0

/GO

!*

/COM,

/COM,PreferencesforGUIfilteringhavebeensettodisplay:

/COM,Structural

!*

!*

ET,1,SOLID185

!*

HNISH

/SOL

FINISH

/PREP7

!*

MPTEMP,,,,,,,,

MPTEMP,l,0

MPDATA,EX,l„200e3

MPDATA,PRXY,l„0.3

TB,BISO,1,1,2,

TBTEMP,0

TBDATA,,200,0,,,,

CYLIND,200,100,0,100,0,90,

MSHAPE,0,3D

MSHKEYJ

!*

CM,_Y,VOLU

VSEL,,,,1

CM,_Y1,VOLU

CHKMSH；VOLU'

CMSEL,S,_Y

!*

VMESH,_Y1

!*

CMDELE,_Y

CMDELE,_Y1

CMDELE,_Y2

!*

FLST,2,2,5,ORDE,2

FITEM,2,2

HTEM,2,5

DA,P51X,SYMM

FLST,2,2,5,ORDE,2

FITEM,2,1

FITEM,2,6

DA,P51X,SYMM

FLST,2,1,5,ORDE,1

HTEM,2,4

/GO

!*

SFA,P51X,1,PRES,100

!*

ANTYPE.0

NSUBST,10,le5,2

/STATUS,SOLU

SOLVE

HNISH

/POST1

PLDISP,2

PLDISP,1

PLDISP,1

!*

PLNSOL,S,EQV,0,1.0

!*

PLNSOL,NL,EPEQ,0,1.0

PLNSOL,EPPL,EQV,0,1.0

!*

PLNSOL,EPELJNT,0,1.0

!*

PLNSOL,NL,EPEQ,0,1.0

HNISH

1.3用ANSYS模拟圆棒拉伸出现颈缩问题

1.3.1模拟结果输出

图1-10输出变形

ANSYS

NODALSOLUTIONRl.4.5

SUB-1APR12014

TIME-120:52:58

SEQVtAVG)

DMX=5.6

SMN=45.587

SMX-304.365

45.587103.093160.599218.106275.612

74.3401131.846189.353246.859304.365

图1-11材料vonMises应力

图1-12材料塑性等效应变

1.3.2命令流文件

WPSTYLE,,,,,”,。

!*

/NOPR

KEYW,PR_SET,1

KEYW,PR_STRUC,1

KEYW,PR_THERM,0

KEYW,PR_FLUID,0

KEYW,PR_ELMAG,0

KEYW,MAGNOD,0

KEYW,MAGEDG,0

KEYW,MAGHFE,0

KEYW,MAGELC,0

KEYW,PR_MULTI,0

KEYW,PR_CFD,0

/GO

!*

/COM,

/COM,PreferencesforGUIfilteringhavebeensettodisplay:

/COM,Structural

i*

/PREP7

!*

ET,1,PLANE182

!*

KEYOPT,1,1,0

KEYOPT,1,3,1

KEYOPT,1,6,0

!*

!*

MPTEMP,,,,,,,,

MPTEMP,l,0

MPDATA,EX,l„200e3

MPDATA,PRXY,l„0.3

TB,NLIS,1,1,4,

TBTEMP,0

TBDATA„200,0,400,0.192„

K,2,5.88,,,

K,3,6,50,,

K,4„50„

FLST,2,4,3

FITEM,2,1

FITEM,2,2

FITEM,2,3

FITEM,2,4

A,P51X

FLST,5,1,4,ORDE,1

FITEM,5,2

CM,_Y,LINE

LSEL,,,,P51X

CM,_Y1,LINE

CMSEL„_Y

!*

LESIZE,_Y1,,,40,,,,,1

!*

FLST,5,1,4,ORDE,1

FITEM,5,1

CM,_Y,LINE

LSEL,,,,P51X

CM,_Y1,LINE

CMSEL„_Y

!*

LESIZE,_Y1,,,8,,,,,1

!*

MSHAPE,0,2D

MSHKEY,1

!*

CM,_Y,AREA

ASEL,,,,1

CM,_Y1,AREA

CHKMSH；AREA'

CMSEL,S,_Y

!*

AMESH,_Y1

!*

CMDELE,_Y

CMDELE,_Y1

CMDELE,_Y2

I*

FINISH

/SOL

FLST,2,2,4,ORDE,2

FITEM,2,1

FITEM,2,4

DL,P51X,,SYMM

FLST,2,1,4,ORDE,1

FITEM,2,3

!*

/GO

DL,P51X,,UY,5.6

ANTYPE,0

NLGEOMJ

NSUBST,100,le5,50

/STATUS,SOLU

SOLVE

FINISH

/POST1

!*

/EFACET,!

PLNSOL,S,EQV,0,1.0

!*

/EFACET,1

PLNSOL,NL,EPEQ,0,1.0

1.4具有中，讨L的薄壁圆筒受均匀拉伸

1.4.1模拟结果输出

图1-13非对称载荷函数

ANSYS

R1A.5

图1-15圆筒在z方向的应力——应变曲线

1.4.2命令流文件

/BATCH

/COM,ANSYSRELEASE14.5UP2012091809:30:1603/09/2014

/input,menust,tmp,"

/GRA,POWER

/GST,ON

/PLO,INFO,3

/GRO,CURL,ON

/CPLANE,1

/REPLOT,RESIZE

WPSTYLE„„„„0

/INPUT,'part4','txt','D:\feixianxingyouxianyuan\part4V,,0

FINISH

*DEL,_FNCNAME

*DEL,_FNCMTID

*DEL,_FNCCSYS

*SET,_FNCNAME,'myload'

*SET,_FNCCSYS,0

!/INPUT,myfunction.func,,,1

*DIM,%_FNCNAME%,TABLE,6,8,1,,,,%_FNCCSYS%

j

!Beginofequation:-((100)sin({TIME}))-(6.52/1.5)

*SET,%_FNCNAME%(0,0,1),0.0,-999

*SET,%_FNCNAME%(2,0,1),0.0

*SET,%_FNCNAME%(3,0,1),0.0

*SET,%_FNCNAME%(4,0,l),0.0

*SET,%_FNCNAME%(5,0,1),0.0

*SET,%_FNCNAME%(6,0,1),0.0

*SET,%_FNCNAME%(O,1,1),1.0,-1,9,1,1,0,0

*SET,%_FNCNAME%(0,2,l),0.0,-2,0,100,0,0,-1

*SET,%_FNCNAME%(0,3,1),0,-3,0,1,-2,2,-1

*SET,%_FNCNAME%(0,4,1),0.0,-1,0,6.52,0,0,0

*SET,%_FNCNAME%(0,5,1),0.0,-2,0,1.5,0,0,-1

*SET,%_FNCNAME%(0,6,1),0.0,-4,0,1,-1,4,-2

*SET,%_FNCNAME%(0,7,1),0.0,-1,0,1,-3,2,-4

*SET,%_FNCNAME%(0,8,l),0.0,99,0,1,-1,0,0

!Endofequation:-((100)sin({TIME}))-(6.52/1.5)

!->

VPLOT

FLST,2,1,5,ORDE,1

FITEM,2,1

/GO

!*

!*

SFA,P51X,1,PRES,%MYLOAD%

/STATUS,SOLU

SOLVE

FINISH

/POST1

!*

PLNSOL,S,EQV,0,1.0

wpoff,0,0,85

wprot,0,-45,0

FILE,'zcj'；rst7.,

NUMVAR,200

S0LU,191,NCMIT

STORE,MERGE

FILLDATA,191„„1,1

REALVAR,191,191

NUMVAR,200

FILLDATA,191,,,,1,1

REALVAR,191,191

!*

NPLOT

NPLOT

VPLOT

EPLOT

NPLOT

EPLOT

NLIST,ALL,,,,NODE,NODE,NODE

elist,all,„0,0

!*

!*

NLIST,ALL,,,,NODE,NODE,NODE

ESEL,S,,,3168

FINISH

/PDS

FINISH

/AUX12

FINISH

/POST26

NUMVAR,200

FILLDATA,191„„1,1

REALVAR,191,191

FINISH

/P0ST1

FINISH

/SOL

FINISH

/PREP7

LPLOT

LSEL,S,,,2

vlist,all

VPLOT

EPLOT

EPLOT

EPLOT

EPLOT

EPLOT

NPLOT

NPLOT

NPLOT

NPLOT

NPLOT

NPLOT

NSEL,S,,,516

VPLOT

EPLOT

EPLOT

ESEL,S,,,3168

EPLOT

ESEL,S,,,3168

NPLOT

VPLOT

APLOT

VPLOT

EPLOT

FINISH

/POST26

FILE/zcj'/rst','.'

/UI,COLL,1

NUMVAR,200

SOLU,191,NCMIT

STORE,MERGE

FILLDATA,191,,,,1,1

REALVAR,191,191

!*

*

FINISH

/SOL

FINISH

/PREP7

FINISH

/POST26

NUMVAR,200

FILLDATA,191,,,,1,1

REALVAR,191,191

!*

!*

!*

!*

FINISH

/POST26

FILE,'zcj','ref,

/UI,COLL,1

NUMVAR,200

SOLU,191,NCMIT

STORE,MERGE

FILLDATA,191,,,」』

REALVAR,191,191

!*

FINISH

/SOLU

FINISH

/POST1

FINISH

/POST26

FILE,'zcj','rst'；.'

/UI,COLL,1

NUMVAR,200

SOLU,191,NCMIT

STORE,MERGE

FILLDATA,191,,,,1,1

REALVAR,191,191

!*

!*

!*

!*

FORCE,TOTAL

SHELL,TOP

LAYERP26,0

ESOL,2,1890,678,S,Z,stress

!*

!*

!*

!*

FORCE,TOTAL

SHELL,TOP

LAYERP26,0

ESOL,2,1619,664,S,Z,stress

!*

NUMVAR,200

FILLDATA,191,,”1,1

REALVAR,191,191

!*

i*

!*

I*

FORCE,TOTAL

SHELL,TOP

LAYERP26,0

ESOL,3,1619,690,NL,EPEQ,strain

i*

!*

!*

!*

FORCE,TOTAL

SHELL,TOP

LAYERP26,0

ESOL,3,1619,664,NL,EPEQ,strain

!*

NUMVAR,200

FILLDATA,!91„„1,1

REALVAR,191,191

PLVAR,2,3,,,,,,,,,

1.5用ANSYS求解剪切锁定超弹性梁问题

NODALSOLUTIONANSYS

R1M5

图1-16梁在丫方向的位移

ANSYS

ELEMENTSOLUTIONR14.5

shearLock

图1-17梁的vonMises等效应力

1.7用ANSYS表面效应单元模拟带穿透圆孔螺栓的弹塑性扭转问题

1.7.1模拟结果输出

1-18模拟带穿透圆孔螺栓的等效应力

1.7.2命令流文件

/COM,PreferencesforGUIfilteringhavebeensettodisplay:

/COM,Structural

!*

/PREP7

!*

ET,1,SOLID185

!*

ET,2,SURF154

i*

MPTEMP,,,,,,,,

MPTEMP,l,0

MPDATA,EX,l„2.0e3

MPDATA,PRXY,l„0.3

TB,BISO,1,1,2,

TBTEMP,0

TBDATA„200,0„„

CYL4,,,50,,,,400

CYL4,,,80,,50,,30

FLST,2,2,6,ORDE,2

FITEM,2,1

FITEM,2,-2

VGLUE,P51X

wpoff,0,0,200

wprot,0,-90,0

CYLIND,5,,-100,100,0,360,

VSBV,3,1

CM,_Y,VOLU

VSEL,,,,4

CM,_Y1,VOLU

CHKMSH；VOLU'

CMSEL,S,_Y

!*

VSWEEP,_Y1

!*

CMDELE,_Y

CMDELE,_Y1

CMDELE,_Y2

!*

VPLOT

SMRT,6

SMRT,7

MSHAPE,1,3D

MSHKEY,0

!*

CM,_Y,VOLU

VSEL,,,,2

CM,_Y1,VOLU

CHKMSH；VOLU'

CMSEL,S,_Y

!*

VMESH,_Y1

!*

CMDELE,_Y

CMDELE,_Y1

CMDELE,_Y2

I*

FLST,5,2,5,ORDE,2

FITEM,5,7

FITEM,5,-8

ASEL,S,,,P51X

APLOT

NSEL,ALL

NSLA,S,1

NPLOT

TYPE,2

MAT,1

REAL,

ESYS,0

SECNUM,

TSHAP,LINE

!*

FLST,5,128,1,ORDE,4

FITEM,5,73

FITEM,5,-104

FITEM,5,217

FITEM,5,-312

CM,_Y,node

NSEL,,,,P51X

CM,_Yl,node

CMSEL„_Y

!*

CMSEL„_Y1

ESURF,0

CMSEL„_Y

CMDELE,_Y

CMDELE,_Y1

!*

ESEL,S,TYPE„2

EPLOT

!*

LOCAL,11,1,0,0,0,,,,1,1,

FLST,2,96,2,ORDE,2

FITEM,2,33892

FITEM,2,-33987

EMODIF,P51X,ESYS,11,

EPLOT

CM,e_surf,NODE

!*

/REP

!*

CMSEL,S,E_SURF

EPLOT

CM,e_surf,ELEM

FLST,3,1,9,ORDE,1

FITEM,3,1

CM,_Y,ELEM

CMSEL,,P51X

CM,_Y1,ELEM

CMSEL,S,_Y

CMDELE,_Y

!*

SFE,_Y1,2,PRES,,1O,,,

i*

LSWRITE,1,

LSWRITE,2,

LSWRITE,1,

ALLSEL,ALL

EPLOT

FLST,2,1,5,ORDE,1

FITEM,2,2

!*

DA,P5IX,ALL,。

FINISH

/SOL

ANTYPE,0

NLGEOMJ

NSUBST,10,10,10

/STATUS,SOLU

SOLVE

FINISH

/POST1

PLDISP,2

PLNSOL,S,EQV,0,1.0

PLNSOL,NL,EPEQ,0,1.0

PLNSOL,S,EQV,0,1.0

1.8用ANSYS模拟超弹性球压缩

1.232593.507225.781858.0564810.3311

2.36994.644536.919169.1937911.4684

1-19弹性球模拟Mises等效应力

-9.4121-7.09713-4.78216-2.46718-.15221

-8.25462-5.93964-3.62467-1.30971.00528

1-20弹性球HPRE应力

1.9用ANSYS模拟长圆柱侧挤压接触问题

ANSYS

DISPLACEMENTRl心

STEP=1MAR92014

SUB-1619:54:59

TIME-1

RSYS-0

DMX=20.6603

1-21模型变形前后示意图

875302.418E+07.583E+07.748E+07

1-22模拟模型Mises等效应力

1.10采用Norton隐式蠕变模型模拟板材压力成型过程

1-23板材模拟蠕变结果（蠕变比率为10.0）

ANSYS

ELEMENTSOLUTION

0.017375.034751.052126.069502

.008688.026063.043438.060814.078189

1-24板材模拟最终厚度（蠕变比率为10.0）

ANSYS

ELEMENTSOLUTION

0.166403.332806.499209.665613

.083202.249605.416008.582411.748814

1-25板材模拟蠕变结果（蠕变比率为1.0）

1-26板材模拟最终厚度（蠕变比率为1.0）

ANSYS

ELEMENTSOLUTIONR14..5

STEP-1APR82014

SUB=3821:23:18

TIME=1

EPCREQV(NOAVG)

DMX-.891287

SMX=.756743

.168165.33633.504495.672661

.084083.252248.420413.588578.756743

1-27板材模拟蠕变结果（蠕变比率为0.0）

1・28板材模拟最终厚度（蠕变比率为0.0）

表1-1不同蠕变判据下模拟板材蠕变应变和最终壳厚

蠕变比率判据蠕变应变最终壳厚

10.00.751930.078189

1.00.748610.078143

00.756740.078255

2提高部分

2.11用ANSYS模拟瞬态热传导问题

ANSYS

POST262

MAR122014

15:39:12

FWTNO.1

TIME

2-1模拟铜的温度T随时间t的变化

ANSYS

NODALSOLUTIONR14..5

STEP=2APR102014

SUB=2515:12:36

TIME«3600

TEMP(AVG)

RSYS=0

SMN=31.8243

SMX-31.8382

31.8243

3：.482

2-2铜的模拟温度云图

ANSYS

NODALSOLUTIONR14.5

STEP=2APR102014

SUB-2515:13:20

TIME-3600

TEMP(AVG)

RSYS=0

SMN-35.4833

SMX=35.6093

35.483335.511335.539335.567335.5953

35.497335.525335.553335.581335.6093

2-3铁的模拟温度云图

ANSYS

NODALSOLUTIONR14..5

STEP=2APR102014

SUB=25

15:11:35

TIME«3600

TEMP(AVG)

RS