/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.
= 0
No strain rate effect

(Real)

˙ε0 Reference strain rate.

(Real)

[12]
ICC Strain rate effect flag. 3
= 1 (Default)
Strain rate effect on fmax
= 2
No strain rate effect on fmax

(Integer)

Example (Carbon)

Comments

  1. 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.
  2. Stress-strain relation in elastic phase.

    The stresses and strains are related as:

    ε11=1E11σ11ν21E22σ22ν31E33σ33
    ε22=1E22σ22ν12E11σ11ν32E33σ33
    ε33=1E33σ33ν13E11σ11ν23E22σ22
    γ12=12G12σ12ν21E22=ν12E11γ23=12G23σ23ν32E33=ν23E22γ31=12G31σ31ν13E11=ν31E33

    Where,
    εij
    Strains
    σij
    Stresses
    γ12 , γ23 and γ31
    Distortions in the corresponding material directions
    For example, for γ12 :

    mat_law12_distortion
    Figure 1.
  3. 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+cln(˙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+cln(˙ε˙εo))
      If ICC=2
      fmax

      Where, fmax=(σmaxσy)2

  4. Stress damage:

    When the limiting stress value of σti is reached in tension, the corresponding stress value is scaled as σreducedi=(1Di)σti . The value of damage Di is updated on each time step with incremental damage parameter δ .

    Di=iδi

    After 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.

  5. 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 αEfε11 .