At a point in a loaded part the in-plane principal stresses are σ₁ = 150 MPa and σ₂ = −60 MPa (tension positive). Find the normal stress σavg that acts on the planes of maximum in-plane shear stress.
Mohr’s circle & stress transformation worksheet with answers
A point in a loaded part has σₓ = 90 MPa, σᵧ = 70 MPa and τₓᵧ = 20 MPa (tension positive). Find the smallest principal stress σ2.
A point in a loaded part has σₓ = 0 MPa, σᵧ = 110 MPa and τₓᵧ = 50 MPa (tension positive). Find the maximum in-plane shear stress τmax.
A point in a loaded part has σₓ = 0 MPa, σᵧ = 50 MPa and τₓᵧ = 30 MPa (tension positive). Find the maximum in-plane shear stress τmax.
A point in a thin plate is in plane stress: σₓ = 0 MPa, σᵧ = 50 MPa and τₓᵧ = −30 MPa (σz = 0). Find the von Mises equivalent stress σvM.
A thin-walled cylindrical tank of inner diameter 600 mm and wall thickness 12 mm holds gas at a gauge pressure of 1.2 MPa. It is made from plate welded along a helical seam at 20° to the axis of the cylinder. Find the normal stress σn acting across the weld seam.
Answer key
- 1. σavg = 45 MPa
- 2. σ2 = 57.64 MPa
- 3. τmax = 74.33 MPa
- 4. τmax = 39.05 MPa
- 5. σvM = 72.11 MPa
- 6. σn = 28.25 MPa
Full step-by-step solutions: practise this topic on examproblems.com.