请教学友关于shell181单元问题

qingtianzhu2011

请问广大学友shell181单元如何显示其内力，其单元对应的smisc值如何取，谢谢指点！

ferriswanglei

etable

qingtianzhu2011

etable我知道是列表，那smisc值具体如何取呢？

dlenme

qingtianzhu2011 发表于 2011-9-14 14:58
etable我知道是列表，那smisc值具体如何取呢？

你的意思是提取etable结果值，输出到文件？
*get命令可以实现

qingtianzhu2011

不是，我是想看shell181单元组成构件的内力图，但是不知道在etable命令中，shell181单元对应的smisc值是多少。

ferriswanglei

Name	Definition	O	R
EL	Element number and name	Y	Y
NODES	Nodes - I, J, K, L	-	Y
MAT	Material number	-	Y
THICK	Average thickness	-	Y
VOLU:	Volume	-	Y
XC, YC, ZC	Location where results are reported	-	4
PRES	Pressures P1 at nodes I, J, K, L; P2 at I, J, K, L; P3 at J,I; P4 at K,J; P5 at L,K; P6 at I,L	-	Y
TEMP	T1, T2, T3, T4 at bottom of layer 1, T5, T6, T7, T8 between layers 1-2, similarly for between next layers, ending with temperatures at top of layer NL(4*(NL+1) maximum)	-	Y
LOC	TOP, MID, BOT, or integration point location	-	1
S:X, Y, Z, XY, YZ, XZ	Stresses	3	1
S:1, 2, 3	Principal stresses	-	1
S:INT	Stress intensity	-	1
S:EQV	Equivalent stress	-	1
EPEL:X, Y, Z, XY	Elastic strains	3	1
EPEL:EQV	Equivalent elastic strains [7]	-	1
EPTH:X, Y, Z, XY	Thermal strains	3	1
EPTH:EQV	Equivalent thermal strains [7]	-	1
EPPL:X, Y, Z, XY	Average plastic strains	3	2
EPPL:EQV	Equivalent plastic strains [7]	-	2
EPCR:X, Y, Z, XY	Average creep strains	3	2
EPCR:EQV	Equivalent creep strains [7]	-	2
EPTO:X, Y, Z, XY	Total mechanical strains (EPEL + EPPL + EPCR)	3	-
EPTO:EQV	Total equivalent mechanical strains (EPEL + EPPL + EPCR)	-	-
NL:EPEQ	Accumulated equivalent plastic strain	-	2
NL:CREQ	Accumulated equivalent creep strain	-	2
NL:SRAT	Plastic yielding (1 = actively yielding, 0 = not yielding)	-	2
NLLWK	Plastic work	-	2
NL:HPRES	Hydrostatic pressure	-	2
SEND:ELASTIC, PLASTIC, CREEP	Strain energy densities	-	2
N11, N22, N12	In-plane forces (per unit length)	-	Y
M11, M22, M12	Out-of-plane moments (per unit length)	-	8
Q13, Q23	Transverse shear forces (per unit length)	-	8
ε11, ε22, ε12	Membrane strains	-	Y
k11, k22, k12	Curvatures	-	8
γ13, γ23	Transverse shear strains	-	8
LOCI:X, Y, Z	Integration point locations	-	5
SVAR:1, 2, ... , N	State variables	-	6
ILSXZ	SXZ interlaminar shear stress	-	Y
ILSYZ	SYZ interlaminar shear stress	-	Y
ILSUM	Magnitude of the interlaminar shear stress vector	-	Y
ILANG	Angle of interlaminar shear stress vector (measured from the element x-axis toward the element y-axis in degrees)	-	Y
Sm: 11, 22, 12	Membrane stresses	-	Y
Sb: 11, 22, 12	Bending stresses	-	Y
Sp: 11, 22, 12	Peak stresses	-	Y
St: 13, 23	Averaged transverse shear stresses	-	Y

Output Quantity Name	ETABLE and ESOL Command Input
	Item	E	I	J	K	L
N11	SMISC	1	-	-	-	-
N22	SMISC	2	-	-	-	-
N12	SMISC	3	-	-	-	-
M11	SMISC	4	-	-	-	-
M22	SMISC	5	-	-	-	-
M12	SMISC	6	-	-	-	-
Q13	SMISC	7	-	-	-	-
Q23	SMISC	8	-	-	-	-
ε11	SMISC	9	-	-	-	-
ε22	SMISC	10	-	-	-	-
ε12	SMISC	11	-	-	-	-
k11	SMISC	12	-	-	-	-
k22	SMISC	13	-	-	-	-
k12	SMISC	14	-	-	-	-
γ13	SMISC	15	-	-	-	-
γ23	SMISC	16	-	-	-	-
THICK	SMISC	17	-	-	-	-
P1	SMISC	-	18	19	20	21
P2	SMISC	-	22	23	24	25
P3	SMISC	-	27	26	-	-
P4	SMISC	-	-	29	28	-
P5	SMISC	-	-	-	31	30
P6	SMISC	-	32	-	-	33
Sm: 11	SMISC	34	-	-	-	-
Sm: 22	SMISC	35	-	-	-	-
Sm: 12	SMISC	36	-	-	-	-
Sb: 11	SMISC	37	-	-	-	-
Sb: 22	SMISC	38	-	-	-	-
Sb: 12	SMISC	39	-	-	-	-
Sp: 11 (at shell bottom)	SMISC	40	-	-	-	-
Sp: 22 (at shell bottom)	SMISC	41	-	-	-	-
Sp: 12 (at shell bottom)	SMISC	42	-	-	-	-
Sp: 11 (at shell top)	SMISC	43	-	-	-	-
Sp: 22 (at shell top)	SMISC	44	-	-	-	-
Sp: 12 (at shell top)	SMISC	45	-	-	-	-
St: 13	SMISC	46	-	-	-	-
St: 23	SMISC	47	-	-	-	-

具体见帮助文档

qingtianzhu2011

谢谢指导！谢谢！