At a point in a loaded part the in-plane principal stresses are σ₁ = 190 MPa and σ₂ = −30 MPa (tension positive). Find the maximum in-plane shear stress τmax.
Mohr’s circle & stress transformation worksheet with answers
At a point in a loaded part the in-plane principal stresses are σ₁ = 150 MPa and σ₂ = 0 MPa (tension positive). Find the maximum in-plane shear stress τmax.
A point in a loaded part has σₓ = 0 MPa, σᵧ = −20 MPa and τₓᵧ = 50 MPa (tension positive). Find the angle θp from the x-axis to the direction of the largest principal stress, between −90° and 90°.
A point in a loaded part has σₓ = −60 MPa, σᵧ = −50 MPa and τₓᵧ = 50 MPa (tension positive). Find the maximum in-plane shear stress τmax.
A point in a loaded part has σₓ = −40 MPa, σᵧ = 80 MPa and τₓᵧ = −60 MPa (tension positive). Find the normal stress σθ on a plane whose normal is rotated 20° clockwise from the x-axis.
A thin-walled cylindrical tank of inner diameter 400 mm and wall thickness 8 mm holds gas at a gauge pressure of 2.5 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 = 110 MPa
- 2. τmax = 75 MPa
- 3. θp = 39.35 °
- 4. τmax = 50.25 MPa
- 5. σθ = 12.6 MPa
- 6. σn = 49.59 MPa
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