At a point in a loaded part the in-plane principal stresses are σ₁ = 110 MPa and σ₂ = 70 MPa (tension positive). Find the maximum in-plane shear stress τmax.
Mohr’s circle & stress transformation worksheet with answers
A point in a loaded part has σₓ = 30 MPa, σᵧ = 90 MPa and τₓᵧ = 50 MPa (tension positive). Find the largest principal stress σ1.
A point has σₓ = 90 MPa, σᵧ = 70 MPa and τₓᵧ = −40 MPa (tension positive). The element is rotated 20° clockwise. Find the normal stress σy′ on the faces of the rotated element that are perpendicular to the rotated y′-axis.
A point has σₓ = 70 MPa and σᵧ = 0 MPa. How large can the shear stress τxy (magnitude) become before the largest principal stress reaches 120 MPa?
A point in a loaded part has σₓ = −40 MPa, σᵧ = 40 MPa and τₓᵧ = −30 MPa (tension positive). Find the normal stress σθ on a plane whose normal is rotated 35° counter-clockwise from the x-axis.
A thin-walled cylindrical tank of inner diameter 600 mm and wall thickness 5 mm holds gas at a gauge pressure of 1.5 MPa. It is made from plate welded along a helical seam at 40° to the axis of the cylinder. Find the normal stress σn acting across the weld seam.
Answer key
- 1. τmax = 20 MPa
- 2. σ1 = 118.3 MPa
- 3. σy′ = 46.63 MPa
- 4. τxy = 77.46 MPa
- 5. σθ = −41.87 MPa
- 6. σn = 71.41 MPa
Full step-by-step solutions: practise this topic on examproblems.com.