At a point in a loaded part the in-plane principal stresses are σ₁ = 160 MPa and σ₂ = 50 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 has σₓ = 0 MPa and σᵧ = 100 MPa, plus some shear stress. On an element rotated by 30° the normal stress in the rotated x′ direction is −9.6 MPa. Find the normal stress σy′ in the rotated y′ direction.
A point in a loaded part has σₓ = −20 MPa, σᵧ = 0 MPa and τₓᵧ = −60 MPa (tension positive). Find the maximum in-plane shear stress τmax.
A point has σₓ = 10 MPa, σᵧ = −80 MPa and τₓᵧ = −60 MPa (tension positive). The element is rotated 20° clockwise. Find the normal stress σy′ on the faces of the rotated element that are perpendicular to the rotated y′-axis.
A point in a loaded part has σₓ = 100 MPa, σᵧ = 100 MPa and τₓᵧ = −30 MPa (tension positive). Find the normal stress σθ on a plane whose normal is rotated 35° counter-clockwise from the x-axis.
A point in a loaded part has σₓ = 60 MPa, σᵧ = 100 MPa and τₓᵧ = 30 MPa (tension positive). Find the normal stress σθ on a plane whose normal is rotated 15° counter-clockwise from the x-axis.
Answer key
- 1. σavg = 105 MPa
- 2. σy′ = 109.6 MPa
- 3. τmax = 60.83 MPa
- 4. σy′ = −108 MPa
- 5. σθ = 71.81 MPa
- 6. σθ = 77.68 MPa
Full step-by-step solutions: practise this topic on examproblems.com.