The principal stresses at a point in a strained material are
′p′1 and ′p′2. The resultant stress ′p′r on the plane carrying the maximum shear stress would be
[p21+p222]1/2
Shear stress, τ=(p1−p22)
The resultant stress, pr=√σ2+τ2
The other method is
pr=√p21cos2θ+p22sin2θ
For maximum shear stress plane
θ=45∘
pr=√p21+p222