Guidelines for selecting the appropriate Failure Criterion to calculate the Factor of Safety of your design.
Failure Criterion Evaluation
Theoretical predictions for failure of lamina are compared with experiments by comparing failure envelopes (outside the envelope, lamina failure occurs) under various biaxial states of stress. A lamina is assumed to be under a state of plane stress with non-zero stress components being σ1, σ2 and τ12. Directions 1 and 2 represent ply orientation direction and transverse to ply orientation direction respectively.
A schematic of failure envelope for a particular failure theory is shown, for example, Tsai-Wu failure criterion. X and S are normal and shear strengths of the lamina respectively. t and c represent tensile and compressive loadings. The open circles in the second plot show some sample experimental results for τ12 > 0.
Failure envelopes for the other failure criteria (Tsai-Hill and Maximum Stress criteria) are superimposed and accuracy of predictions evaluated against experimental results for selecting the best failure criterion.
For multi-directional laminates, it is difficult to evaluate which failure theory to use. Similar failure envelopes are constructed for laminates. However, for FPF (first ply failure), which the program uses, there is a wide variation between theoretical predictions and experimental observations due to several reasons.
Based on such observations some recommendations are made to help you select among the different failure theories.
Maximum Stress Criterion
For matrix dominated failure, the maximum stress criterion is best applied to a lamina when cross-fiber stress σ2 > 0. You can check this stress for each ply using Composite Options in the Stress Plot PropertyManager.
The Tsai-Hill criterion is best applied to a lamina when strengths are equal in tension and compression. For matrix dominated failure, the Tsai-Hill criterion is best applied to a lamina when cross-fiber stress σ2 < 0.
The Tsai-Wu criterion is best applied for unequal strengths in tension and compression. For matrix dominated failure, the Tsai-Wu criterion is best applied to a lamina when cross-fiber stress σ2 < 0.