shear stress
Syntax
Formula
q = T_i1i2i3...id v_i1 v_i2 v_i3 ... v_id
Input
sigma | stressTensor |
m | normal vector the the slip or twinning plane |
n | Burgers vector (slip) or twin shear direction (twinning) |
Output
tauMax | maximum shear stress |
m | active plane |
n | active direction |
tau | shear stresses with respect to all planes |
Options
symmetrise | consider also all symmetrically equivalent planes and directions |