ABAQUS模拟梁单元断裂的本构方程(VUMAT)

* TEMPNEW, STRETCHNEW, DEFGRADNEW, FIELDNEW,

C WRITE ONLY -

* STRESSNEW, STATENEW, ENERINTERNNEW, ENERINELASNEW )

C

INCLUDE 'VABA_PARAM.INC'

C

DIMENSION COORDMP(NBLOCK,*), CHARLENGTH(NBLOCK), PROPS(NPROPS),

1 DENSITY(NBLOCK), STRAININC(NBLOCK,NDIR+NSHR),

2 RELSPININC(NBLOCK,NSHR), TEMPOLD(NBLOCK),

3 STRETCHOLD(NBLOCK,NDIR+NSHR),

4 DEFGRADOLD(NBLOCK,NDIR+NSHR+NSHR),

5 FIELDOLD(NBLOCK,NFIELDV), STRESSOLD(NBLOCK,NDIR+NSHR),

6 STATEOLD(NBLOCK,NSTATEV), ENERINTERNOLD(NBLOCK),

7 ENERINELASOLD(NBLOCK), TEMPNEW(NBLOCK),

8 STRETCHNEW(NBLOCK,NDIR+NSHR),

9 DEFGRADNEW(NBLOCK,NDIR+NSHR+NSHR),

1 FIELDNEW(NBLOCK,NFIELDV),

2 STRESSNEW(NBLOCK,NDIR+NSHR), STATENEW(NBLOCK,NSTATEV),

3 ENERINTERNNEW(NBLOCK), ENERINELASNEW(NBLOCK)

C

CHARACTER*80 CMNAME

DIMENSION INTV(2)

PARAMETER ( ZERO = 0.D0, ONE = 1.D0, TWO = 2.D0, THREE = 3.D0,

* THIRD = ONE / THREE, HALF = 0.5D0, TWOTHDS = TWO / THREE,

* OP5 = 1.5D0 )

C

C THE STATE VARIABLES ARE STORED AS:

C STATE(*,1) = ELEMENT DELETE

*

*

open(100,file='E:\Temp_ABAQUS\model\00.txt')

F = PROPS(1) 【本构参数

G = PROPS(2) 【本构参数

H = PROPS(3) 【本构参数

T = PROPS(4) 【判据参数

*

*

*

DO K = 1, NBLOCK

C

STATENEW(K,2)=STATEOLD(K,2)+STRAININC(K,1)

IF(STATEOLD(K,1).EQ.ONE)THEN

STRESSNEW(K,1)=F*(exp(H*STATENEW(K,2))

1 -exp(G*STATENEW(K,2))) 【材料本构关系式,计算应力

IF(STRESSNEW(K,1).GE.T)THEN 【应力判定

STATENEW(K,1)=ZERO

write(100,*) 'K=',K 【写入数据

write(100,*) 'steptime=',STEPTIME 【写入数据

write(100,*) ' stress-crack=',STRESSNEW(K,1) 【写入数据

ELSE

STATENEW(K,1)=ONE

STRESSPOWER = HALF *

1 ( ( STRESSOLD(K,1)+STRESSNEW(K,1) )*STRAININC(K,1) ) 【更新应力

C

C

ENERINTERNNEW(K) = ENERINTERNOLD(K)

1 + STRESSPOWER / DENSITY(K) 【更新内能

END IF

ELSE

STATENEW(K,1)=ZERO

END IF

END DO

RETURN

END

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