At a point in a loaded part the in-plane principal stresses are σ₁ = 140 MPa and σ₂ = −30 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 = 160 MPa, σᵧ = −20 MPa and τₓᵧ = 40 MPa (tension positive). Find the smallest principal stress σ2.
A point in a loaded part has σₓ = −50 MPa, σᵧ = 100 MPa and τₓᵧ = −40 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 has σₓ = −10 MPa and σᵧ = −60 MPa. How large can the shear stress τxy (magnitude) become before the largest principal stress reaches 10 MPa?
A point in a loaded part has σₓ = −70 MPa, σᵧ = 0 MPa and τₓᵧ = 10 MPa (tension positive). Find the normal stress σθ on a plane whose normal is rotated 30° counter-clockwise from the x-axis.
A point in a loaded part has σₓ = 90 MPa, σᵧ = 50 MPa and τₓᵧ = −30 MPa (tension positive). Find the shear stress τθ on a plane whose normal is rotated 60° counter-clockwise from the x-axis (positive in the same sense as τₓᵧ).
Answer key
- 1. τmax = 85 MPa
- 2. σ2 = −28.49 MPa
- 3. θp = −75.96 °
- 4. τxy = 37.42 MPa
- 5. σθ = −43.84 MPa
- 6. τθ = −2.321 MPa
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