Transversely Isotropic Softening Material

Constitutive Law

This MPM Material is a transversely isotropic, elastic material, but once it fails, it develops anisotropic damage and will become orthotropic. The material is available only in OSParticulas. The constitutive law for this material is

      [math]\displaystyle{ \mathbf{\sigma} = (\mathbf{I} - \mathbf{D}) \mathbf{C}( \mathbf{\varepsilon}- \mathbf{\varepsilon}_{res}) }[/math]

where C is stiffness tensor for the underlying transversely isotropic material and D is an anisotropic 4^th rank damage tensor appropriate for damage in transversely isotropic materials, and [math]\displaystyle{ \mathbf{\varepsilon}_{res} }[/math] is any residual strain (such as thermal or solvent induced strains).

The MPM implementation of softening isotropic materials is described in Nairn, Hammerquist, and Aimene The extension to transversely isotropic will be in a future publication.

TransIsoSoftening 1 and 2

TransIsoSoftening 1 and TransIsoSoftening 2 give identical materials but with different initial orientations. TransIsoSoftening 1 has the unrotated axial direction along the z (or θ if axisymmetric) axis while TransIsoSoftening 2 has unrotated axial direction along the y (or Z if axisymmetric) axis. You can change the unrotated direction to any other orientation when defining material points (in MPM) or elements (in FEA) by selecting rotation angles for particles or elements. For 2D analyses, the two options allow for axial direction in the x-y (or r-θ if axisymmetric) analysis plane (TransIsoSoftening 2) or normal to that plane (TransIsoSoftening 1). For 3D analyses, only TransIsoSoftening 1 is allowed (and it the only one needed).

Damage Initiation

Damage initiation is controlled by attaching a damage initiation law to the material. These laws define a failure envelop. Once the response reaches the envelop, the damage process is initiated and the normal to the crack plane is calculated depending on type of failure. The normal is need to find the anisotropic D tensor (which involves rotating analysis into the crack axis system where the x axis is aligned with the crack normal.

The only damage surface currently allowed for a transversely isotropic softening material is the TIFailure initiation law.

Damage Evolution

Damage evolution is determined by softening laws laws to predict degradation of normal and shear tractions across the crack plane. You need to attach four softening laws to this material. These four laws handle degradation of axial modulus (E_A), axial shear modulus (G_A), transverse tensile modulus (E_T), and transverse shear modulus (G_T). Areas under these laws correspond to fracture toughnesses G_Ic and lumped G_IIc/G_IIIc for the material for various crack orientations.

In brief, this material models crack initiation and propagation through damage mechanics. The softening law properties tie the damage mechanics to toughness properties for the material. The scheme can handle interacting cracks (which become interacting damage zones) and 3D cracks.

Material Properties

When the material is undamaged, its response is identical to properties entered for the underlying transversely isotropic material. Once those are specified, you have to attach one damage initiation law and four softening laws to define how the material responds after initiation of damage.

Property	Description	Units	Default
(Transversely Isotropic Properties)	Enter all properties needed to define the underlying transversely isotropic material response	varies	varies
Initiation	Attach damage initiation law by name or ID that is compatible with this material. Once attached, enter all required material properties for that law.	none	TIFailure
SofteningEA	Attach a softening law (by name or ID) for propagation of tensile damage that changes EA. Once attached, enter all required properties for that law by prefacing each property with "EA-".	none	Linear
SofteningGA	Attach a softening law (by name or ID) for propagation of shear damage that changes GA. Once attached, enter all required properties for that law by prefacing each property with "GA-".	none	Linear
SofteningET	Attach a softening law (by name or ID) for propagation of tensile damage that changes ET. Once attached, enter all required properties for that law by prefacing each property with "ET-".	none	Linear
SofteningGT	Attach a softening law (by name or ID) for propagation of shear damage that changes GT. Once attached, enter all required properties for that law by prefacing each property with "GT-".	none	Linear
shearFailureSurface	Select failure surface assumed when modeling shear damage in 3D calculations. Use 1 for an elliptical failure criterion based on current degraded shear strengths. Use 0 for a rectangular failure surface that encloses the elliptical failure criterion. The elliptical surface is preferred, but rectangular is more efficient.	none	1
(other)	Properties common to all materials	varies	varies

History Variables

This material stores several history variables that track the extent of the damage and orientation of the damage plane:

1. 0, 0.75, 0.8, 0.85, 0.95, 1.05, 1.15, 1.25, or 1 higher than previous 7 to indicate undamaged (0), damage propagation (0.75, 0.8, 0.85, 0.95, 1.05, 1.15, 1.25), or post failure (decohesion) state of the particle.
   • 0.75, 0.8, or 0.85 indicate failure by transverse tension, axial shear, or rolling shear and axial direction along z axis in the crack axis system
   • 0.95 or 1.05 indicate failure by axial tension or transverse shear and axial direction along x axis in the crack axis system
   • 1.15 or 1.25 indicate failure by axial shear or transverse tension and axial direction along y axis in the crack axis system
2. δ_n or the maximum normal cracking strain.
3. δ_xy or the maximum x-y shear cracking strain.
4. δ_xz or the maximum x-z cracking strain (zero for 2D).
5. d_n or damage variable for normal loading. It varies from 0 to 1 where 1 is complete damage or failure.
6. d_xy or damage variable for x-y shear loading. It varies from 0 to 1 where 1 is complete damage or failure.
7. d_xz or damage variable for x-z shear loading. It varies from 0 to 1 where 1 is complete damage or failure (zero for 2D).
8. For 2D it is cos(θ), but for 3D it is Euler angle α.
9. For 2D it is sin(θ), but for 3D it is Euler angle β.
10. For 2D it is not used, but for 3D it is Euler angle γ.
11. A_c/V_p where A_c is crack area within the particle and V_p is particle volume.

Variables 8-10 define the normal to the damage crack plane. For 2D, θ is the counter clockwise angle from the x axis to the crack normal. For 3D, (α, β, γ) are the three Euler angles for the normal direction using a Z-Y-Z rotation scheme. You can use the damagenormal archiving option to save enough information for plotting the normal. Although damaged normal is a unit vector, it is archived with magnitude equal to A_c/V_p (which gets another history variable archived and the value is used for some visualization options).

This material also tracks the cracking strain which can be saved by using the plasticstrain archiving option. The strain is archived in the global axis system. If you also archive the damagenormal, you will be able to plot a vector along the crack-opening displacement vector.