At a point in a loaded part the in-plane principal stresses are σ₁ = 20 MPa and σ₂ = −40 MPa (tension positive). Find the maximum in-plane shear stress τmax.
Mohr’s circle & stress transformation worksheet with answers
A point has σₓ = 150 MPa and σᵧ = −20 MPa, plus some shear stress. On an element rotated by 15° the normal stress in the rotated x′ direction is 153.6 MPa. Find the normal stress σy′ in the rotated y′ direction.
A point in a loaded part has σₓ = 80 MPa, σᵧ = −20 MPa and τₓᵧ = 30 MPa (tension positive). Find the maximum in-plane shear stress τmax.
A point in a loaded part has σₓ = 30 MPa, σᵧ = −50 MPa and τₓᵧ = −50 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 in a loaded part has σₓ = −60 MPa, σᵧ = −40 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.
A point in a thin plate is in plane stress: σₓ = −70 MPa, σᵧ = −50 MPa and τₓᵧ = −50 MPa (σz = 0). Find the von Mises equivalent stress σvM.
Answer key
- 1. τmax = 30 MPa
- 2. σy′ = −23.6 MPa
- 3. τmax = 58.31 MPa
- 4. θp = −25.67 °
- 5. σθ = −19.09 MPa
- 6. σvM = 106.8 MPa
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