Selecting x and y-axis as shown in figure,
px = – 50 N/mm2 ,
py = 100 N/mm2 ,
and q = 75 N/mm2 .

= 25 + 106.07
= 131.07 N/mm2

The principal plane makes an angle θ to y-axis in anticlockwise direction. Then

Plane of maximum shear makes 45° to it
θ = – 31.72 + 45.00 = 13.28°.
Normal stress on this plane is given by
px = \(\frac{p_x+p_y}2\) + \(\frac{p_x-p_y}2\) cos 2θ + q sin 2θ
= \(\frac{-50-100}2\) cos 2(13.28) + 75 sin (2 x 13.28)
= 25 – 67.08 + 33.54
= – 8.54 N/mm2
pt = qmax = 106.07 N/mm2
∴ Resultant stress p = \(\sqrt{(-8.51)^2+106.07^2}\)
= 106.41 N/mm2
Let ‘p’ make angle φ to tangential stress (maximum shear
stress plane). Then referring to Fig. (b)

tan φ = \(\frac{p_n}{p_t}\) = \(\frac{8.54}{106.07}\)
∴ φ = 4.6° as shown in Fig. (b).