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laws:dvree

DVREE

Description

Simple damage constitutive law.

The model

This law is used for mechanical analysis for solids.

Files

Prepro: LDVREE.F
Lagamine: DVREE.F

Availability

Plane stress state NO
Plane strain state YES
Axisymmetric state NO
3D state NO
Generalized plane state NO

Input file

Parameters defining the type of constitutive law

Line 1 (2I5, 60A1)
ILLaw number
ITYPE 592
COMMNT Any comment (up to 60 characters) that will be reproduced on the output listing

Integer parameters

Line 1 (3I5)
NINTV = 1 (by default)
ISOL = 0 : Use of total stresses in the constitutive law
≠ 0 : Use of effective stresses in the constitutive law (see annex 8)
ITEMOIN = 1 : Constitutive matrix computed by perturbation
= 0 : Secant matrix
= -1 : Analytical tangent matrix

Real parameters

Line 1 (3G10.0)
E YOUNG's elastic modulus
ANU POISSON's ratio
FT Tensile strength
Line 2 (3G10.0)
ALPHA 1st parameter controlling the final stress
BETA 2nd parameter controlling the shape of the softening curve
ETA Ratio of the compressive stress limit over the tensile stress limit
Line 3 (2G10.0)
DIV Time integration parameter
RHOS Specific mass

Stresses

Number of stresses

4 (2D only)

Meaning

The stresses are the components of CAUCHY stress tensor in global (X,Y,Z) coordinates.

For the 2D state :

SIG(1)$\sigma_{xx}$
SIG(2)$\sigma_{yy}$
SIG(3)$\sigma_{xy}$
SIG(4)$\sigma_{zz}$

State variables

Number of state variables

10

List of state variables

2D plane strain or axisymmetric analysis :

Q(1) THICK : Thickness (axisymmetric or plane stress state)
Q(2) D : Damage
Q(3) EPSTIL : Equivalent deformation
Q(4) RHOS : Actualised specific mass
Q(5) DXXT : Strain computed at the previous step
Q(6) DYYT : Strain computed at the previous step
Q(7) DZZT : Strain computed at the previous step
Q(8) DXYT : Strain computed at the previous step
Q(9) = 1 : FLAG : Flag for increasing damage
= 0 : FLAG : Flag for constant damage
Q(10) EPSD0 damage threshold
laws/dvree.txt · Last modified: 2020/08/25 15:46 (external edit)