Research Article

Numerical Simulation of Mixed-Mode Fatigue Crack Growth for Compact Tension Shear Specimen

Table 2

Values of forces F1 to F6 according to load angle α

αF2=F5F1 = F6F3 = F4

150.259 F0.742 F0.224 F
300.5 F0.933 F−0.067 F
450.707 F1.061 F−0.354 F
600.866 F1.116 F−0.616 F
750.966 F1.095 F−0.837 F
90FFF