/MAT/LAW12 (3D_COMP)
Block Format Keyword This law describes a solid material using the Tsai-Wu formulation that is usually used to model composites. This material is assumed to be 3D orthotropic-elastic before the Tsai-Wu criterion is reached.
The material becomes nonlinear afterwards. The Tsai-Wu criterion can be set dependent on the plastic work and strain rate in each of the orthotropic directions and in shear to model material hardening. Stress based orthotropic criterion for brittle damage and failure is available. This material is a generalization and improvement of /MAT/LAW14 (COMPSO).
Format
(1) | (2) | (3) | (4) | (5) | (6) | (7) | (8) | (9) | (10) |
---|---|---|---|---|---|---|---|---|---|
/MAT/LAW12/mat_ID/unit_ID or /MAT/3D_COMP/mat_ID/unit_ID | |||||||||
mat_title | |||||||||
ρi | |||||||||
E11 | E22 | E33 | |||||||
ν12 | ν23 | ν31 | |||||||
G12 | G23 | G31 | |||||||
σt1 | σt2 | σt3 | δ | ||||||
B | n | fmax | Wrefp | ||||||
σt1y | σt2y | σc1y | σc2y | ||||||
σt12y | σc12y | σt23y | σc23y | ||||||
σt3y | σc3y | σt13y | σc13y | ||||||
α | Ef | c | ˙ε0 |
Definition
Field | Contents | SI Unit Example |
---|---|---|
mat_ID | Material
identifier. (Integer, maximum 10 digits) |
|
unit_ID | Unit identifier. (Integer, maximum 10 digits) |
|
mat_title | Material
title. (Character, maximum 100 characters) |
|
ρi | Initial density. (Real) |
[kgm3] |
E11 | Young's modulus in direction
1. (Real) |
[Pa] |
E22 | Young's modulus in
direction 2. (Real) |
[Pa] |
E33 | Young's modulus in
direction 3. (Real) |
[Pa] |
ν12 | Poisson's ratio between
directions 1 and 2. (Real) |
|
ν23 | Poisson's ratio between
directions 2 and 3. (Real) |
|
ν31 | Poisson's ratio between
directions 3 and 1. (Real) |
|
G12 | Shear modulus in direction
12. (Real) |
[Pa] |
G23 | Shear modulus in direction
23. (Real) |
[Pa] |
G31 | Shear modulus in direction
31. (Real) |
[Pa] |
σt1 | Stress at the beginning of
composite tensile/compressive failure in direction 1. 4 Default = 1030 (Real) |
[Pa] |
σt2 | Stress at the beginning of
composite tensile/compressive failure in direction 2. 4 Default = σt1 (Real) |
[Pa] |
σt3 | Stress at the beginning of
composite tensile/compressive failure in direction 3. 4 Default = σt2 (Real) |
[Pa] |
δ | Maximum damage factor.
4 Default = 0.05 (Real) |
|
B | Global plastic hardening
parameter. 3 (Real) |
|
n | Global plastic hardening
exponent. Default = 1.0 (Real) |
|
fmax | Maximum value of the
Tsai-Wu criterion limit. 3 Default = 1010 (Real) |
|
Wrefp | Reference plastic work per
unit solid volume. Default = 1.0 (in local unit system) (Real) |
[Jm3] |
σt1y | Yield stress in tension in
direction 1. 3 Default = 0.0 (Real) |
[Pa] |
σt2y | Yield stress in tension in
direction 2. Default = 0.0 (Real) |
[Pa] |
σc1y | Yield stress in
compression in direction 1. Default = 0.0 (Real) |
[Pa] |
σc2y | Yield stress in
compression in direction 2. Default = 0.0 (Real) |
[Pa] |
σt12y | Yield stress in tensile
shear in direction 12. Default = 0.0 (Real) |
[Pa] |
σc2y | Yield stress in
compressive shear in direction 12. Default = 0.0 (Real) |
[Pa] |
σt23y | Yield stress in tensile
shear in direction 23. Default = 0.0 (Real) |
[Pa] |
σc23y | Yield stress in
compressive shear in direction 23. Default = 0.0 (Real) |
[Pa] |
α | Fiber volume fraction.
5 (Real) |
|
Ef | Fiber Young's modulus.
5 (Real) |
[Pa] |
c | Global strain rate coefficient.
(Real) |
|
˙ε0 | Reference strain
rate. (Real) |
[12] |
ICC | Strain rate effect flag.
3
(Integer) |
▸Example (Carbon)
Comments
- This material requires an orthotropic solid property (/PROP/TYPE6 (SOL_ORTH), /PROP/TYPE21 (TSH_ORTH), or /PROP/TYPE22 (TSH_COMP). It can only be used with solid elements for a 3-dimensional analysis. This law is compatible with 10-node tetrahedron and 4-node tetrahedron elements. The orthotropic material directions are set in the property entries.
- Stress-strain relation in
elastic phase.
The stresses and strains are related as:
ε11=1E11σ11−ν21E22σ22−ν31E33σ33ε22=1E22σ22−ν12E11σ11−ν32E33σ33ε33=1E33σ33−ν13E11σ11−ν23E22σ22γ12=12G12σ12ν21E22=ν12E11γ23=12G23σ23ν32E33=ν23E22γ31=12G31σ31ν13E11=ν31E33Where,- εij
- Strains
- σij
- Stresses
- γ12 , γ23 and γ31
- Distortions in the corresponding material directions
Figure 1. - Tsai-Wu criterion:The material is assumed to be elastic until the Tsai-Wu criterion is fulfilled. After exceeding the Tsai-Wu criterion limit F(W*p,˙ε) , the material becomes nonlinear:
- If F(σ)<F(W*p,˙ε) : elastic
- If F(σ)>F(W*p,˙ε) : nonlinear
Where,- Stress
F(σ)
in element for Tsai-Wu criterion
computed as: F(σ)=F1σ1+F2σ2+F3σ3+F11σ21+F22σ22+F33σ23+F44σ212+F55σ223+F66σ231+2F12σ1σ2+2F23σ2σ3+2F13σ1σ3
The coefficients of the Tsai-Wu criterion are determined from the limiting stresses when the material becomes nonlinear in directions 1, 2, 3 or 12, 23, 31 (shear) in compression or tension as:F1=−1σc1y+1σt1y F2=−1σc2y+1σt2y F3=−1σc3y+1σt3y F11=1σc1yσt1y F22=1σc2yσt2y F33=1σc3yσt3y F44=1σc12yσt12y F55=1σc23yσt23y F66=1σc31yσt31y F12=−12√(F11F22) F23=−12√(F22F33) F13=−12√(F11F33) -
F(W*p,˙ε)
is the variable Tsai-Wu criterion
limit defined:F(W*p,˙ε)=[1+B(W*p)n]⋅[1+c⋅ln(˙ε˙ε0)]Where,
- Wpref
- Reference plastic work
- W*p=WpWrefp
- Relative plastic work
- B
- Plastic hardening parameter
- n
- Plastic hardening exponent
- ˙ε0
- Reference true strain rate
- c
- Strain rate coefficient
F(W*p,˙ε) the maximum value of the Tsai-Wu criterion limit depends on ICC:- If ICC=1
- fmax⋅(1+c⋅ln(˙ε˙εo))
- If ICC=2
- fmax
Where, fmax=(σmaxσy)2
- Stress damage:
When the limiting stress value of σti is reached in tension, the corresponding stress value is scaled as σreducedi=(1−Di)σti . The value of damage Di is updated on each time step with incremental damage parameter δ .
Di=∑iδiAfter Di reaches the value of 1, the stress in corresponding direction is set to 0. The damage is irreversible, that is, if a value of Di is attained the material will not reach any lower damage value.
- Fiber reinforcement:
These parameters allow you to define additional fiber reinforcement in the 11 direction. Additional stress in direction 11 will be added equal to α⋅Ef⋅ε11 .