Safety Factor Evaluation
There are many theories available in the literature for predicting material failure, these can predict, for instance whether a ductile material will yield or not, or if a brittle material will crack under a given set of loads.
Tsai and Wu (Ref. 13, Ref. 22) proposed a stress-dependent criterion intended at modeling failure in composites. Under Tsai-Wu criterion, failure occurs when a given quadratic function of stress is grater than zero. The failure criterion is given by
here, σ is the stress tensor, F a fourth rank tensor (SI unit: 1/Pa^2) and f is a second rank tensor (SI unit: 1/Pa). For Tsai-Wu criterion, failure occurs when g(σ) ≥ 0.
Due to the symmetry of these tensors, the fourth rank tensor can be represented by a symmetric 6-by-6 matrix, and the second rank tensor by a 6-by-1 vector (see Voigt order in the section Tensor vs. Matrix Formulations).
Certain constraints ensure that the failure surface g(σ) = 0 forms a closed ellipsoid in the stress space. Also, thermodynamic considerations restrict the value of some components of the fourth rank tensor to be positive only. These restrictions are summarized as (no summation of the indices)
and
The failure index is computed from the failure criterion as
so failure is predicted for a failure index greater than one, fi ≥ 1.
The damage index is given by a boolean expression based on the failure criterion
here di = 1 means damage, and di = 0 represents a healthy material.
The safety factor, also called reserve factor or strength ratio, is computed by scaling the stress tensor such as the failure criterion is equal to zero
For a quadratic failure criterion, as the Tsai-Wu criterion, this means solving a quadratic equation for the safety factor variable sf
the safety factor is then obtained from the smallest positive root.
For a isotropic criteria, such as von Mises criterion, g(σ) = σmisests−1, and the safety factor is given by sf = σtsmises.
The margin of safety (Ref. 23) is then computed from the safety factor
Use the Safety subnode to set up variables which can be used to check the risk of failure according to various criteria. It can be used in combination with Linear Elastic Material or Nonlinear Elastic Material Models.
Following Tsai-Wu formalism, different orthotropic criteria can be defined by setting appropriate values for the coefficients in F and f tensors.
Anisotropic Tsai-Wu criterion
For this criterion, enter twenty one coefficients to define the 6-by-6 matrix F, and six coefficients to define the vector f. The failure criterion is evaluated from the expression
here, σij are the stress tensor components given in the local coordinate system of the parent node.
Orthotropic Tsai-Wu criterion
For this criterion, enter nine coefficients corresponding to the tensile strengths σtsi, compressive strengths σcsi, and shear strengths σssij given in the local coordinate system of the parent node. Tsai-Wu coefficients are then computed from
, , ,
, , ,
, ,
, ,
all the other coefficients in F and f tensors are set to zero.
Orthotropic Tsai-Hill criterion
For this criterion, enter six coefficients corresponding to the tensile strengths σtsi and shear strengths σssij given in the local coordinate system of the parent node. Tsai-Wu coefficients are then computed from
, , ,
, , ,
, ,
all the other coefficients in F and f tensors are set to zero. See also Hill Orthotropic Plasticity.
Orthotropic Hoffman criterion
For this criterion, enter nine coefficients corresponding to the tensile strengths σtsi, compressive strengths σcsi, and shear strengths σssij given in the local coordinate system of the parent node. Tsai-Wu coefficients are then computed from
, , ,
, , ,
, ,
, ,
all the other coefficients in F and f tensors are set to zero.
Orthotropic Jenkins criterion
Enter nine coefficients corresponding to the tensile strengths σtsi, compressive strengths σcsi, and shear strengths σssij given in the local coordinate system of the parent node. The failure criterion is then computed from
here, εsi is either the tensile strength or the compressive strength depending whether the stress in the i-direction, σi, is positive or negative. The absolute value of the shear stress σij in the ij-plane is compared to the corresponding shear strength σssij.
Orthotropic Waddoups criterion
Waddoups criterion is similar to Jenkins criterion, but the failure criterion is given in terms of strains, not strengths. For this criterion, enter nine coefficients corresponding to the ultimate tensile strains εtsi, ultimate compressive strains εcsi, and ultimate shear strains γssij given in the local coordinate system of the parent node. The failure criterion is then computed from
here, εsi is either the ultimate tensile strain or the ultimate compressive strain depending whether the strain in the i-direction, εi, is positive or negative. The absolute value of the shear strain γij in the ij-plane is compared to the corresponding ultimate shear strain γssij.
Modified Tsai-Hill criterion
This criterion is derived from Tsai-Wu theory for two-dimensional plane stress problems (Ref. 23). It is available in 2D for the Pate interface and the Solid Mechanics interface in plane stress, and for the Shell interface in 3D. Enter the coefficients corresponding to the tensile strengths σtsi, compressive strengths σcsi, and shear strengths σssij given in the local coordinate system of the parent node. The failure criterion is then computed from the in plane stresses
Tsai-Wu coefficients are then computed from
, or
, or
or
all the other coefficients in F and f tensors are set to zero.
Azzi-Tsai-Hill criterion
This criterion is derived from Tsai-Wu theory for two-dimensional plane stress problems. It is available in 2D for the Pate interface and the Solid Mechanics interface in plane stress, and for the Shell interface in 3D. Enter the coefficients corresponding to the tensile strengths σtsi, compressive strengths σcsi, and shear strengths σssij given in the local coordinate system of the parent node. The failure criterion is then computed from the in plane stresses
Tsai-Wu coefficients are then computed from
, or
, or
or
all the other coefficients in F and f tensors are set to zero.
Norris criterion
This criterion is derived from Tsai-Wu theory for two-dimensional plane stress problems. It is available in 2D for the Pate interface and the Solid Mechanics interface in plane stress, and for the Shell interface in 3D. Enter the coefficients corresponding to the tensile strengths σtsi, compressive strengths σcsi, and shear strengths σssij given in the local coordinate system of the parent node. The failure criterion is then computed from the in plane stresses
Tsai-Wu coefficients are then computed from
, or
, or
all the other coefficients in F and f tensors are set to zero.
Isotropic von Mises criterion
Von Mises criterion is one of the simplest isotropic criteria to predict yielding in metals and other ductile materials. The failure criterion is computed from the isotropic tensile strength σts
The effective von Mises stress σmises is defined from the deviatoric stress tensor, see the section about plasticity and von Mises Criterion. For ductile materials the tensile strength corresponds to the yield stress, while for brittle materials it corresponds to the failure strength.
Isotropic Tresca criterion
Tresca criterion is similar to von Mises criterion. The failure criterion is computed from the isotropic tensile strength σts
here, Tresca effective stress is defined in terms of principal stresses, σtresca = σ1 − σ3, see Tresca Criterion. For ductile materials the tensile strength corresponds to the yield stress, while for brittle materials it corresponds to the failure strength.
Isotropic Rankine criterion
St. Venant criterion is similar to Tresca criterion, as the failure criterion is given in terms of principal stresses. For this criterion, enter the tensile strength σts, and the compressive strength σcs. The failure criterion is then computed from
here, σs is either the tensile strength or the compressive strength depending whether the principal stress, σpi, is positive or negative. For ductile materials the tensile strength corresponds to the yield stress, while for brittle materials it corresponds to the failure strength.
Isotropic St. Venant criterion
St. Venant criterion is similar to Waddoups criterion, as the failure criterion is given in terms of strains, not strengths. For this criterion, enter the ultimate tensile strains εts, and the ultimate compressive strains εcs. The failure criterion is then computed from
here, εs is either the ultimate tensile strain or the ultimate compressive strain depending whether the principal strain, εpi, is positive or negative. For ductile materials the ultimate tensile strain corresponds to the strain at yielding, while for brittle materials it corresponds to the strain at failure.
Isotropic Mohr-Coulomb criterion
Mohr-Coulomb criterion is similar to Tresca criterion, as the failure criterion is given in terms of principal stresses, see Mohr-Coulomb Criterion for soil plasticity. For this criterion, enter the cohesion c, and the angle of internal friction φ. The failure criterion is then computed from
here, the principal stresses are sorted as σp1≥σp2≥σp3.
The cohesion and the angle of internal friction are related to the tensile and compressive strengths by the expressions
and
Isotropic Drucker-Prager criterion
Drucker-Prager criterion approximates the Mohr-Coulomb criterion by a smooth function (a cone in the stress space). The failure criterion is computed from the stress invariants I1 and J2, and two material parameters, α and k, see Drucker-Prager Criterion for soil plasticity
The material parameters α and k are related to the cohesion c and angle of internal friction φ in the Mohr-Coulomb criterion by the expressions
and
The symbol ± is related to either matching the tensile meridian (positive sign) or matching the compressive meridian (negative sign) of Mohr-Coulomb’s pyramid. Also, the cohesion and the angle of internal friction are related to the tensile and compressive strengths, see Isotropic Mohr-Coulomb criterion.
User Defined
The user defined option allows you to write explicitly how the failure criterion and the safety factor depend on stress and/or strain. These could be analytic functions of stress or strain tensor components, principal stresses, principal strains, stress or strain invariants, or data interpolated from tables.
You can add any number of Safety nodes to a single material model. The contents of this feature will not affect the analysis results as such, as this feature does not account for post-failure analysis. You can add Safety nodes after having performed an analysis and just do an Update Solution in order to access to the new variables for result evaluation.