Damage Evolution

Damage evolution specifies how the material degrades after one or more damage initiation criteria are met.

This page discusses:

Background

Damage Evolution Options

The Damage Evolution options appear when you select Use damage evolution during the definition of a damage criterion. Multiple forms of damage evolution may act on a material at the same time—one for each defined damage initiation criterion.

Damage evolution can be specified by Type (displacement or energy) and by Softening method. Your selections of type and softening method determine the equation used to evaluate damage evolution.

Damage Evolution Based on Displacement

When you define damage evolution based on effective plastic displacement (Type=Displacement), the effective plastic displacement, u ¯ p l , is defined with the evolution equation

u ¯ ˙ p l = L ε ¯ ˙ p l ,

where L is the characteristic length of the element.

The evolution of the damage variable with the relative plastic displacement can be specified in tabular, linear, or exponential form. Instantaneous failure occurs if the plastic displacement at failure, u ¯ f p l , is specified as 0. However, this choice is not recommended. Use it with care because it causes a sudden drop of the stress at the material point that can lead to dynamic instabilities.

  • For the tabular form, you can specify the damage variable directly as a tabular function of equivalent plastic displacement, d = d ( u ¯ p l ) .
  • For the linear form, you can specify the effective plastic displacement, u ¯ f p l , at the point of failure (full degradation). Then, the damage variable increases according to

    d ˙ = L ε ¯ ˙ p l u ¯ f p l = u ¯ ˙ p l u ¯ f p l .

    This definition ensures that when the effective plastic displacement reaches the value u ¯ p l = u ¯ f p l , the material stiffness fully degrades ( d = 1 ). The linear damage evolution law defines a truly linear stress-strain softening response only if the effective response of the material is perfectly plastic (constant yield stress) after damage initiation.
  • For the exponential form, you can specify the relative plastic displacement at failure, u ¯ f p l , and the exponent α . The damage variable is given as

    d = 1 e α ( u ¯ p l / u ¯ f p l ) 1 e α .

Damage Evolution Based on Energy

When you define damage evolution based on fracture energy (Type=Energy), you can specify the fracture energy ( G f ) per unit area to be dissipated during the damage process directly. Instantaneous failure occurs if G f is specified as 0. However, this choice is not recommended and must be used with care because it causes a sudden drop in the stress at the material point that can lead to dynamic instabilities.

The evolution in the damage can be specified in linear or exponential form.

  • For the linear form, once the damage initiation criterion is met, the damage variable increases according to

    d ˙ = L ε ¯ ˙ p l u ¯ f p l = u ¯ ˙ p l u ¯ f p l ,

    where the equivalent plastic displacement at failure is computed as

    u ¯ f p l = 2 G f σ y 0 ,

    and σ y 0 is the value of the yield stress at the time when the failure criterion is reached.
  • For the exponential form, the damage variable given as

    d = 1 exp ( 0 u ¯ p l σ ¯ y u ¯ ˙ p l G f ) .

    The formulation of the model ensures that the energy dissipated during the damage evolution process is equal to G f .

Once the damage initiation criterion is reached, the effective plastic displacement, u ¯ ˙ p l , is defined with the evolution equation

u ¯ ˙ p l = L ε ¯ ˙ p l .

When multiple damage criteria are active, the damage variable, D , captures the combined effect of all active mechanisms and is computed in terms of individual damage variables, d i , for each mechanism. You can choose to combine some of the damage variables in a multiplicative sense to form an intermediate variable, d m u l t , as follows:

d m u l t = 1 Π k N m u l t ( 1 d k ) .

Then, the overall damage variable is computed as the maximum of d m u l t and the remaining damage variables:

D = max { d m u l t , max j N max ( d j ) } .

Main Options

Input Data Description

Type

This setting is available for ductile metals only. For fiber-reinforced composites, the energy type of damage evolution is used.

Select Displacement to define damage as a function of the total (for elastic materials in cohesive elements) or the plastic (for bulk elastic-plastic materials) displacement after damage initiation. This type corresponds to the Displacement at Failure field in the data table.

Select Energy to define damage evolution in terms of the energy required for failure (fracture energy) after the initiation of damage. This type corresponds to the Failure Energy field in the data table.

Softening

This setting is available for ductile metals only. For fiber-reinforced composites, linear softening is used.

Select Linear to define a linear softening stress-strain response for linear elastic materials or a linear evolution of the damage variable with deformation for elastic-plastic materials. Linear softening is the default method.

Select Exponential to define an exponential softening stress-strain response for linear elastic materials or an exponential evolution of the damage variable with deformation for elastic-plastic materials. For the displacement type of damage evolution, an Exponential Law Parameter field in the data table is also added.

Select Tabular to define the evolution of the damage variable with deformation in tabular form and is available only when you select Displacement for the type. The Displacement at Failure field in the data table is replaced by a Damage Variable field and a Displacement field, and you can add additional rows to define the displacements.

Use temperature-dependent data

Specifies material parameters that depend on temperature. A Temperature field appears in the data table. For more information, see Specifying Material Data as a Function of Temperature and Independent Field Variables.
Number of field variables Specify material parameters that depend on field variables. Field columns appear in the data table for each field variable you add. For more information, see Specifying Material Data as a Function of Temperature and Independent Field Variables.

Degradation

This option is available for ductile metals only.

Select Maximum to specify that the current damage evolution mechanism interacts with other damage evolution mechanisms in a maximum sense to determine the total damage from multiple mechanisms. Maximum is the default selection.

Select Multiplicative to specify that the current damage evolution mechanism interacts in a multiplicative manner with other damage evolution mechanisms defined using this form to determine the total damage from multiple mechanisms. Other damage evolution mechanisms defined using the maximum degradation will interact with the combination of those using the multiplicative form.

Damage Stabilization Options

Damage stabilization specifies the viscosity coefficients used in the viscous regularization scheme for the damage model for traction separation laws and fiber-reinforced materials. Viscous regularization improves convergence as the material fails. Damage stabilization options are available for fiber-reinforced composites only.

Input Data Description
Viscosity coefficient in the longitudinal tensile direction Viscosity coefficient for fiber tension, η f t .
Viscosity coefficient in the longitudinal compressive direction Viscosity coefficient for fiber compression, η f c .
Viscosity coefficient in the transverse tensile direction Viscosity coefficient for matrix tension, η m t .
Viscosity coefficient in the transverse compressive direction Viscosity coefficient for matrix compression, η m c .