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Stress on oblique section with direct and shear stress

Short answer

For a biaxial stress with shear, on a plane with normal at angle θ, normal stress σn = (σx+σy)/2 + {(σx-σy)/2}cos2θ + τxy sin2θ; shear stress τ = -{(σx-σy)/2}sin2θ + τxy cos2θ.

Derive an expression for the normal stress and shear stress on an oblique section of a rectangular strained body when it is subjected to direct stresses in two perpendicular directions accompanied with simple shear stress.

Problem: a rectangular element carries direct stresses σx\sigma_x and σy\sigma_y (tensile) on two perpendicular faces, together with a shear stress τxy\tau_{xy} on all four faces. Find the normal stress σn\sigma_n and shear stress τ\tau on an oblique section whose normal makes angle θ\theta with the xx-axis (the section makes θ\theta with the face on which σx\sigma_x acts).

            sy
        B ------- 
          |\
   txy <- | \  AB = oblique
     sx <-|  \  section
          |___\ A
    (wedge ABC, unit thickness)

Let the oblique face AB have area dAdA. Then the vertical face has area dAcos⁡θdA\cos\theta and the horizontal face has area dAsin⁡θdA\sin\theta.

Forces on the wedge

  • On the vertical face: horizontal force σx dAcos⁡θ\sigma_x\,dA\cos\theta and vertical force τxy dAcos⁡θ\tau_{xy}\,dA\cos\theta.
  • On the horizontal face: vertical force σy dAsin⁡θ\sigma_y\,dA\sin\theta and horizontal force τxy dAsin⁡θ\tau_{xy}\,dA\sin\theta.

The shear stress τxy\tau_{xy} is taken so that the shear forces on the two faces act in the senses required by complementary shear.

Normal stress

Resolve all forces along the normal to AB (direction θ\theta from the xx-axis):

σn dA=σx dAcos⁡θcos⁡θ+σy dAsin⁡θsin⁡θ+τxy dAcos⁡θsin⁡θ+τxy dAsin⁡θcos⁡θ\sigma_n\,dA = \sigma_x\,dA\cos\theta\cos\theta + \sigma_y\,dA\sin\theta\sin\theta + \tau_{xy}\,dA\cos\theta\sin\theta + \tau_{xy}\,dA\sin\theta\cos\theta σn=σxcos⁡2θ+σysin⁡2θ+2τxysin⁡θcos⁡θ\sigma_n = \sigma_x\cos^2\theta + \sigma_y\sin^2\theta + 2\tau_{xy}\sin\theta\cos\theta

Using cos⁡2θ=1+cos⁡2θ2\cos^2\theta = \frac{1+\cos2\theta}{2}, sin⁡2θ=1−cos⁡2θ2\sin^2\theta = \frac{1-\cos2\theta}{2} and 2sin⁡θcos⁡θ=sin⁡2θ2\sin\theta\cos\theta = \sin2\theta:

σn=σx+σy2+σx−σy2cos⁡2θ+τxysin⁡2θ\sigma_n = \frac{\sigma_x+\sigma_y}{2} + \frac{\sigma_x-\sigma_y}{2}\cos2\theta + \tau_{xy}\sin2\theta

Shear stress

Resolve along the plane AB (perpendicular to the normal):

τ dA=−σx dAcos⁡θsin⁡θ+σy dAsin⁡θcos⁡θ+τxy dA(cos⁡2θ−sin⁡2θ)\tau\,dA = -\sigma_x\,dA\cos\theta\sin\theta + \sigma_y\,dA\sin\theta\cos\theta + \tau_{xy}\,dA\left(\cos^2\theta - \sin^2\theta\right) τ=−σx−σy2sin⁡2θ+τxycos⁡2θ\tau = -\frac{\sigma_x-\sigma_y}{2}\sin2\theta + \tau_{xy}\cos2\theta

(the sign of τ\tau depends on the direction chosen as positive along AB; reversing that direction only changes the sign, not the magnitude).

Result

σn=σx+σy2+σx−σy2cos⁡2θ+τxysin⁡2θ,τ=−σx−σy2sin⁡2θ+τxycos⁡2θ\sigma_n = \frac{\sigma_x+\sigma_y}{2} + \frac{\sigma_x-\sigma_y}{2}\cos2\theta + \tau_{xy}\sin2\theta, \qquad \tau = -\frac{\sigma_x-\sigma_y}{2}\sin2\theta + \tau_{xy}\cos2\theta

Principal stresses: setting τ=0\tau = 0 gives tan⁡2θp=2τxyσx−σy\tan2\theta_p = \dfrac{2\tau_{xy}}{\sigma_x-\sigma_y} and σ1,2=σx+σy2±(σx−σy2)2+τxy2\sigma_{1,2} = \dfrac{\sigma_x+\sigma_y}{2} \pm \sqrt{\left(\dfrac{\sigma_x-\sigma_y}{2}\right)^2 + \tau_{xy}^2}.

✓ Answer checked by Claude Opus 5.5 (high effort)

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