Statics S4 slide 9: Maximum shear stress on an oblique sectionFrom lectureCurrent spec2:25 marks6 min

ENGR5004 Statics session 04, slide 9 (Stress on oblique cuts of rod under uniaxial load, exercise)

A rod of normal cross-sectional area A0A_0 carries a centric axial load PP. On an oblique section whose normal makes angle θ\theta with the rod axis (area AθA_\theta, with A0=Aθcos⁡θA_0 = A_\theta\cos\theta), the internal force resolves into a normal component F=Pcos⁡θF = P\cos\theta and a shear component V=Psin⁡θV = P\sin\theta, giving

σ=PA0cos⁡2θ(2),τ=PA0sin⁡θcos⁡θ(3)\sigma = \frac{P}{A_0}\cos^2\theta \quad (2), \qquad \tau = \frac{P}{A_0}\sin\theta\cos\theta \quad (3)

Formulas you may need
  • σ=FAθ\sigma = \dfrac{F}{A_\theta}, τ=VAθ\tau = \dfrac{V}{A_\theta}, Aθ=A0cos⁡θA_\theta = \dfrac{A_0}{\cos\theta} (learn this)
  • sin⁡2θ=2sin⁡θcos⁡θ\sin 2\theta = 2\sin\theta\cos\theta, cos⁡2θ=cos⁡2θ−sin⁡2θ\cos 2\theta = \cos^2\theta - \sin^2\theta (learn this)
  1. (a)
    Show that τ=0\tau = 0 for θ=0∘\theta = 0^\circ and θ=90∘\theta = 90^\circ.
    [1]
  2. (b)
    Demonstrate that τ\tau reaches its maximum for θ=45∘\theta = 45^\circ, and find τmax\tau_{max}.
    [3]
  3. (c)
    Show that on the same 45∘45^\circ section the normal stress also equals P/(2A0)P/(2A_0).
    [1]