A point in a loaded part has σₓ = −60 MPa, σᵧ = 60 MPa and τₓᵧ = −60 MPa (tension positive). Find the largest principal stress σ1.
Mohr’s circle & stress transformation worksheet with answers
At a point in a loaded part the in-plane principal stresses are σ₁ = 110 MPa and σ₂ = −10 MPa (tension positive). Find the maximum in-plane shear stress τmax.
A point has σₓ = 130 MPa and σᵧ = 80 MPa. How large can the shear stress τxy (magnitude) become before the largest principal stress reaches 145 MPa?
A point has σₓ = 150 MPa, σᵧ = 110 MPa and τₓᵧ = −20 MPa (tension positive). Find the angle θs, between −90° and 90°, from the x-axis to the normal of the plane on which the shear stress has its maximum positive value +R (shear positive in the same sense as τₓᵧ).
A thin-walled cylindrical tank of inner diameter 1200 mm and wall thickness 6 mm holds gas at a gauge pressure of 0.5 MPa. It is made from plate welded along a helical seam at 50° to the axis of the cylinder. Find the magnitude of the shear stress |τn| acting along the weld seam.
A thin-walled cylindrical tank of inner diameter 1200 mm and wall thickness 8 mm holds gas at a gauge pressure of 1.2 MPa. It is made from plate welded along a helical seam at 25° to the axis of the cylinder. Find the normal stress σn acting across the weld seam.
Answer key
- 1. σ1 = 84.85 MPa
- 2. τmax = 60 MPa
- 3. τxy = 31.22 MPa
- 4. θs = −67.5 °
- 5. |τn| = 12.31 MPa
- 6. σn = 81.96 MPa
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