At a point in a loaded part the in-plane principal stresses are σ₁ = 0 MPa and σ₂ = −90 MPa (tension positive). Find the maximum in-plane shear stress τmax.
Mohr’s circle & stress transformation worksheet with answers
A point on the surface of a shaft in torsion is in pure shear with τₓᵧ = −90 MPa (σₓ = σᵧ = 0). Find the normal stress σθ on a plane whose normal is rotated 60° counter-clockwise from the x-axis.
A point has σₓ = 90 MPa and σᵧ = 20 MPa. How large can the shear stress τxy (magnitude) become before the largest principal stress reaches 145 MPa?
A point in a thin plate is in plane stress: σₓ = −40 MPa, σᵧ = −20 MPa and τₓᵧ = −10 MPa, with σz = 0. Find the absolute maximum shear stress τabs at the point (considering all planes in three dimensions).
A point in a thin plate is in plane stress: σₓ = −60 MPa, σᵧ = 100 MPa and τₓᵧ = −20 MPa (σz = 0). The material has a yield strength of 250 MPa. Find the factor of safety n against yielding by the Tresca (maximum shear stress) criterion.
A point in a thin plate is in plane stress: σₓ = 150 MPa, σᵧ = 0 MPa and τₓᵧ = 60 MPa (σz = 0). The material has a yield strength of 350 MPa. Find the factor of safety n against yielding by the Tresca (maximum shear stress) criterion.
Answer key
- 1. τmax = 45 MPa
- 2. σθ = −77.94 MPa
- 3. τxy = 82.92 MPa
- 4. τabs = 22.07 MPa
- 5. n = 1.516
- 6. n = 1.822
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