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Obtain the expression for normal and tangential stresses on a plane BE inclined at an angle θ with BC subjected to compound stresses as shown in fig.

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Consider the unit thickness of the element. Applying equations of equilibrium to the free body diagram of wedge BCE.

Let σn and τ be the normal and shear stresses on the plane BE,

∑Fx = 0 

σx (BC) – τxy (EC) – τ (EB) cos (90 – θ) − σn (EB) cos θ = 0 

∑Fy = 0 

σx (EC) + τxy (BC) + τ (EB) sin (90 – θ) − σn (EB) sin θ = 0 

Dividing both equations by BE replacing

sin θ = EC/ BE and cos θ = BC/ BE

σx cos θ + τxy sin θ – τ sin θ − σn cos θ = 0 ...(i)

σy sin θ + τxy cos θ + τ cos θ − σn sin θ = 0 ...(ii)

Multiplying equation (i) and cos θ, (ii) by sin θ and then adding, 

σx cos2 θ + τxy sin θ cos θ – σn cos2 θ + σy sin2 θ + τxy cos θ sin θ − σn sin2 θ = 0 

σx cos2 θ + σy sin2 θ + 2τxy sin θ cos θ = σ

or σn = σx cos2 θ + σy sin2 θ + τxy sin 2θ

Putting 

cos2 θ = (1 + cos 2θ)/2 and sinθ = (1 - cos 2θ)/2

Multiplying equation (i) by sin θ, (ii) by cos θ and then subtracting (ii) from (i) 

x cos θ sin θ + τxy sin2 θ – τ sin2 θ) (σy sin θ cos θ + τxy cos2 θ + τ cos2 θ = 0 (σx – σy) cos θ sin θ + τxy (sin2 θ − cos2 θ) − τ = 0 

τ = (σx + σy)/ 2 sin 2θ – τxy cos θ (cos2 θ – sin2 θ = cos 2θ)

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