At a point in a loaded part the in-plane principal stresses are σ₁ = 120 MPa and σ₂ = 80 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 = 40 MPa, σᵧ = 110 MPa and τₓᵧ = 10 MPa (tension positive). Find the smallest principal stress σ2.
A point in a loaded part has σₓ = 10 MPa, σᵧ = −30 MPa and τₓᵧ = −10 MPa (tension positive). Find the maximum in-plane shear stress τmax.
A point has σₓ = 130 MPa and σᵧ = 30 MPa. How large can the shear stress τxy (magnitude) become before the largest principal stress reaches 170 MPa?
A point in a thin plate is in plane stress: σₓ = 160 MPa, σᵧ = 20 MPa and τₓᵧ = −40 MPa (σz = 0). The material has a yield strength of 355 MPa. Find the factor of safety n against yielding by the Tresca (maximum shear stress) criterion.
A point in a loaded part has σₓ = 40 MPa, σᵧ = 120 MPa and τₓᵧ = 30 MPa (tension positive). Find the normal stress σθ on a plane whose normal is rotated 30° counter-clockwise from the x-axis.
Answer key
- 1. τmax = 20 MPa
- 2. σ2 = 38.6 MPa
- 3. τmax = 22.36 MPa
- 4. τxy = 74.83 MPa
- 5. n = 2.081
- 6. σθ = 85.98 MPa
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