Table of Contents

MESO2

DELETEME This law does not seem to exist in the code.
LMESO2.F does not exist.
ITYPE = 295 corresponds to law FCZM

Description

Elastic visco-plastic constitutive law for solidification problem (continuous casting) (always used with THSOL2)

The model

For liquid element: ferrostatic pression
For solid element: EVP-law (see GROB)
For mushy element: EVP-law with parameters interpolated between solid and liquid state

Files

Prepro: LMESO2.F

Availability

Plane stress stateNO
Plane strain stateNO
Axisymmetric stateYES
3D stateNO
Generalized plane stateNO

Input file

Parameters defining the type of constitutive law

Line 1 (2I5, 60A1)
ILLaw number
ITYPE 295
COMMENT Any comment (up to 60 characters) that will be reproduced on the output listing.

Integer parameters

Line 1 (3I5)
NINTVnumber of sub-steps used to integrate numerically the constitutive equation in time-step
METK0 analytical stiffness matrix
1 stiffness matrix computed by perturbation
ISOL0 use of total stresses in the constitutive law
1 use of effective stresses in the constitutive law

Real parameters

Line 1 (3G10.0)
COOYlevel of liquid surface
TStemperatures (see THSOL2)
TL
Line 2 (7G10.0)
EOreference YOUNG's elastic modulus ($E_o$)
BEcorresponding temperature coefficient ($b_E$)
ANUOreference POISSON's ratio ($\nu_0$)
BNUcorresponding temperature coefficient ($b_\nu$)
ANOreference strain rate exponent ($n_o$)
let us recall that:
E=$E_o$exp($-b_o T$)
$\nu = \nu_o exp(\nu_K T$), where T is the absolute temperature (K)
BOreference strain rate coefficient ($B_o$)
Qcorresponding temperature coefficient (Q)
Line 3 (7G10.0)
AMOreference hardening exponent ($m_o$)
AKSOreference hardening saturation coefficient ($K_{so}$)
GAMMAOreference hardening parameter ($\gamma_o$)
TETAOreference hardening coefficient ($\theta_o$)
BTETAcorresponding temperature coefficient ($b_\theta$)
AKOOreference initial yield limit ($K_{oo}$)
BKcorresponding temperature coefficient ($b_K$)
Line 4 (2G10.0)
RGA2perfect GAZ constant in correct unity system
CTQTAYLOR QUINNEY coefficient
0 for solidification case
< 0 for semi-coupled thermomechanical analysis when the $\sigma(8)$ has to be constant and null CTQ has to be used

Number of stresses

4

Meaning

SIG(1) $\sigma_{11}$
SIG(2) $\sigma_{22}$
SIG(3) $\sigma_{12}$
SIG(4) $\sigma_{33}$

State variables

Number of state variables

3

List of state variables

Q(1)THICK
Q(2) current yield limit in tension, its initial value is $K_o$ exp (-$b_K$ T), where T is the absolute temperature (K)
Q(3) $\varepsilon^{P}$ equivalent nonlinear strain