At a point in a loaded part the in-plane principal stresses are σ₁ = 170 MPa and σ₂ = −20 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 on the surface of a shaft in torsion is in pure shear with τₓᵧ = −70 MPa (σₓ = σᵧ = 0). Find the normal stress σθ on a plane whose normal is rotated 25° counter-clockwise from the x-axis.
A point in a thin plate is in plane stress: σₓ = 30 MPa, σᵧ = 70 MPa and τₓᵧ = −20 MPa, with σz = 0. Find the absolute maximum shear stress τabs at the point (considering all planes in three dimensions).
A point has σₓ = 30 MPa, σᵧ = 80 MPa and τₓᵧ = −10 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 point in a loaded part has σₓ = −40 MPa, σᵧ = 50 MPa and τₓᵧ = 30 MPa (tension positive). Find the shear stress τθ on a plane whose normal is rotated 50° counter-clockwise from the x-axis (positive in the same sense as τₓᵧ).
A point in a loaded part has σₓ = 100 MPa, σᵧ = −10 MPa and τₓᵧ = −60 MPa (tension positive). Find the normal stress σθ on a plane whose normal is rotated 20° counter-clockwise from the x-axis.
Answer key
- 1. σavg = 75 MPa
- 2. σθ = −53.62 MPa
- 3. τabs = 39.14 MPa
- 4. θs = 55.9 °
- 5. τθ = 39.11 MPa
- 6. σθ = 48.57 MPa
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