I have searched for this and all I could find is the following:
TAUoct=(1/3)*sqrt[(sigma1- sigma2)^2+(sigma2-sigma3)^2+( sigma3-sigma1)^2]
This equation is all over the books and sources but I reckon sigma1 to sigma3 are principal stresses. Now for a plane having both normal and shear stresses what is the equation for octahedral stress? Can you introduce the source as well?
Thanks in advance,