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Derivation of plane stress transformation equations

Short answer

Wedge equilibrium yields σθ=(σx+σy)/2+((σx-σy)/2)cos2θ+τxy sin2θ and τθ=-((σx-σy)/2)sin2θ+τxy cos2θ. Principal stresses σ1,2=(σx+σy)/2±√[((σx-σy)/2)²+τxy²] occur where τθ=0; tan2θp=2τxy/(σx-σy). Maximum shear stress equals the radius of Mohr’s circle, on planes at 45° to principal planes.

For a body in a state of plane stress with stresses sigma_x, sigma_y and tau_xy, derive expressions for the normal and shear stresses on an inclined plane at angle theta. Hence obtain the principal stresses, the position of the principal planes and the maximum shear stress.

Sign convention

Tensile normal stress positive. Shear stress τxy\tau_{xy} is positive when it acts in the +y+y direction on the face whose outward normal is +x+x. Angle θ\theta is measured anticlockwise from the xx axis to the normal of the inclined plane.

        sy (top face)
      ^   ^
   +-----------+
   |           |  txy on the +x face points up (+y)
 <-|           |->  sx
   |           |
   +-----------+
      sy (bottom face)

Equilibrium of a wedge

Take a triangular wedge with the inclined face of area dAdA, normal at θ\theta. The areas of the vertical face and horizontal face are dAcos⁡θdA\cos\theta and dAsin⁡θdA\sin\theta.

Forces along the normal nn (∑Fn=0\sum F_n = 0):

σθ dA=σxcos⁡2θ dA+σysin⁡2θ dA+2τxysin⁡θcos⁡θ dA\sigma_\theta\,dA = \sigma_x\cos^2\theta\,dA + \sigma_y\sin^2\theta\,dA + 2\tau_{xy}\sin\theta\cos\theta\,dA

Forces along the plane (∑Ft=0\sum F_t = 0):

τθ dA=−(σx−σy)sin⁡θcos⁡θ dA+τxy(cos⁡2θ−sin⁡2θ) dA\tau_\theta\,dA = -(\sigma_x-\sigma_y)\sin\theta\cos\theta\,dA + \tau_{xy}(\cos^2\theta-\sin^2\theta)\,dA

Using double-angle identities:

σθ=σx+σy2+σx−σy2cos⁡2θ+τxysin⁡2θ\boxed{\sigma_\theta = \frac{\sigma_x+\sigma_y}{2}+\frac{\sigma_x-\sigma_y}{2}\cos2\theta+\tau_{xy}\sin2\theta} τθ=−σx−σy2sin⁡2θ+τxycos⁡2θ\boxed{\tau_\theta = -\frac{\sigma_x-\sigma_y}{2}\sin2\theta+\tau_{xy}\cos2\theta}

Principal stresses

Principal planes have τθ=0\tau_\theta = 0:

tan⁡2θp=2τxyσx−σy\tan2\theta_p = \frac{2\tau_{xy}}{\sigma_x-\sigma_y}

This gives two values of 2θp2\theta_p that differ by 180∘180^\circ, so the two principal planes are 90∘90^\circ apart. Substituting back:

σ1,2=σx+σy2±(σx−σy2)2+τxy2\sigma_{1,2} = \frac{\sigma_x+\sigma_y}{2}\pm\sqrt{\left(\frac{\sigma_x-\sigma_y}{2}\right)^2+\tau_{xy}^2}

(Equivalently dσθ/dθ=0d\sigma_\theta/d\theta = 0.)

Maximum shear stress

Setting dτθ/dθ=0d\tau_\theta/d\theta = 0:

tan⁡2θs=−σx−σy2τxy\tan2\theta_s = -\frac{\sigma_x-\sigma_y}{2\tau_{xy}}

so θs=θp±45∘\theta_s = \theta_p \pm 45^\circ (planes of maximum shear are at 45∘45^\circ to the principal planes).

τmax=(σx−σy2)2+τxy2=σ1−σ22\tau_{max} = \sqrt{\left(\frac{\sigma_x-\sigma_y}{2}\right)^2+\tau_{xy}^2} = \frac{\sigma_1-\sigma_2}{2}

On these planes the normal stress is σavg=(σx+σy)/2\sigma_{avg} = (\sigma_x+\sigma_y)/2.

✓ Answer checked by Claude Opus 5.5 (high effort)

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