All available failure criteria are listed together with their failure mode abbreviations as used in failure mode plots.
Terms:
e = strain, s = stress
1 = material 1 direction, 2 = material 2 direction, 3 = out-of-plane normal direction, 12 = in-plane shear, 13 and 23 = out-of-plane shear terms
I = principal I direction, II = principal II direction, III = principal III direction
t = tension, c = compression
Criteria:
Maximum Strain: e1t, e1c, e2t, e2c, e12
Maximum Stress: s1t, s1c, s2t, s2c,s3t, s3c, s12, s23, s13
Tsai-Wu 2D and 3D: tw
Tsai-Hill 2D and 3D: th
Hashin: hf (fiber failure), hm (matrix failure), hd (delamination failure)
Puck (simplified, 2D and 3D Puck implementations are available): pf (fiber failure), pmA (matrix tension failure), pmB (matrix compression failure), pmC (matrix shear failure), pd (delamination)
LaRC 2D and 3D: lft3 (fiber tension failure), lfc4 (fiber compression failure under transverse compression), lfc6 (fiber compression failure under transverse tension), lmt1 (matrix tension failure), lmc2/5 (matrix compression failure)
Cuntze 2D and 3D: cft (fiber tension failure), cfc (fiber compression failure), cmA (matrix tension failure), cmB (matrix compression failure), cmC (matrix wedge shape failure)
Sandwich failure criteria:
Wrinkling: wb (wrinkling bottom face), wt (wrinkling top face)
Core Failure: cf
Shear Crimping failure criteria: sc
Isotropic failure criteria - Von Mises: vMe (strain) and vMs (stress)
Weighting factor: The inverse reserve factor of each failure mode is multiplied by the accordant weighting factor.
1: no safety
2: safety of two