Table of Contents

DAM-EP-TH

Description

Elastic-(visco)-plastic constitutive law fully coupled with damage for solid elements at variable temperature

The model

Mechanical analysis of thermo-elasto-(visco)-plastic-damage isotropic solids undergoing large strains, plastic mixed hardening and damage isotropic hardening are assumed.
:!: Error in mechanical computation if elastic strain is not negligible compared to the plasticity. Small example at the end.

Files

Prepro: LZDMGC.F

Availability

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

Input file

Parameters defining the type of constitutive law

Line 1 (2I5, 60A1)
ILLaw number
ITYPE 215
COMMENT Any comment (up to 60 characters) that will be reproduced on the output listing.

Integer parameters

Line 1 (6I5)
NTEMPnumber of temperatures at which material date are given
NINTV number of sub-steps used to integrate numerically the constitutive equation in a time step
MNINTVMax. of number of sub-steps (0$\rightarrow$100)
MITERAnumber of sub-iteration (0$\rightarrow$10)
MUTIPnumber of multiplicator for sub-steps (0$\rightarrow$2)
IVISC = 0 (EP LAW)
= 1 (EVP LAW)

Real parameters

Line 1 (6G10.0)
TAU ratio of volumetric damage to deviatoric damage
ECROU = 0 for isotropic hardening
= 1 for kinematic hardening
∈ [0,1] for mixed hardening
COEFQ TAYLOR-QINNEY's coefficient (q)
DNMAX 0 for EP without damage
(0,1) $rightarrow$ Max. damage value at initial fracture
otherwise $\rightarrow$ 0.95 limit damage value
PROCprecision of iteration
(0 $\rightarrow$1.D-3)
THICKthickness for plane state

Real parameters

Repeated NTEMP times

Line 1 (7G10.0)
T temperature
E YOUNG's elastic modulus at temperature T
ANU POISSON's ratio at temperature T
ALPHA thermal expansion coefficient ($\alpha$) at temperature T
RP$\Phi$ lower yield limit $\sigma_0$ at temperature T
ET elasto-plastic tangent modulus ($E_t$) at temperature T1
RD$\Phi$ initial damage limit at temperature T
DTGdamage tangent modulus at temperature T
Line 2 (G10.0)
VISCO visco fluid parameter (unit : time)

Stresses

Number of stresses

6 for 3D state
4 for the other cases

Meaning

The stresses are the components of CAUCHY stress tensor in global (X,Y,Z) coordinates.
For the 3-D state:

SIG(1)$\sigma_{XX}$
SIG(2)$\sigma_{YY}$
SIG(3)$\sigma_{ZZ}$
SIG(4)$\sigma_{XY}$
SIG(5)$\sigma_{XZ}$
SIG(6)$\sigma_{YZ}$

For the other cases:

SIG(1)$\sigma_{XX}$
SIG(2)$\sigma_{YY}$
SIG(3)$\sigma_{XY}$
SIG(4)$\sigma_{ZZ}$

State variables

Number of state variables

28 for 3D state
26 for the other cases

List of state variables

Q(1)= element thickness (t) in plane stress state
= 1 in plane strain state
= circumferential strain rate $\dot{\varepsilon_\theta}$ in axisymmetric state
= 0 in 3-D state
= element thickness (t) in generalized plane state
Q(2)= 0 if the current state is elastic
= 1 if the current state is elasto-plastic
Q(3)= 0 if the current state is not damage
= 1 if the current state is damage
Q(4) generalized plastic strain ($\alpha$)
Q(5) amount of current deviatoric damage (D)
Q(6) plastic hardening level (R)
Q(7) damage hardening level (B)
Q(8) back stresses for kinematic and mixed hardening
Q(N) (N = 14 for 3-D state, N = 12 for other cases)
Q(N+1) equivalent plastic strain
Q(N+2) equivalent stress
Q(N+3) thermodynamic reaction conjugated to deviatoric damage ($Y_{d}$)
Q(N+4) thermodynamic reaction conjugated to volumetric damage ($Y_{*}$)
Q(N+5) plastic work per unit volume
Q(N+6) damage work per unit volume
Q(N+7) total strain energy per unit volume (elastic + plastic + damage)
Q(N+8) part of the dissipated power converted into heat
Q(N+9)current temperature
Q(N+10fracture criteria
Q(N+15)

Example of the error that might occur: