At a point in a loaded part the in-plane principal stresses are σ₁ = 80 MPa and σ₂ = −120 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 in a loaded part has σₓ = 110 MPa, σᵧ = −60 MPa and τₓᵧ = −60 MPa (tension positive). Find the smallest principal stress σ2.
A point has σₓ = −20 MPa, σᵧ = −80 MPa and τₓᵧ = −30 MPa (tension positive). Find the angle θs, between −90° and 90°, from the x-axis to the normal of the plane on which the shear stress has its maximum positive value +R (shear positive in the same sense as τₓᵧ).
A point in a loaded part has σₓ = −80 MPa, σᵧ = −50 MPa and τₓᵧ = 60 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 = −80 MPa, σᵧ = −70 MPa and τₓᵧ = 40 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 thin plate is in plane stress: σₓ = 70 MPa, σᵧ = 20 MPa and τₓᵧ = 40 MPa (σz = 0). The material has a yield strength of 275 MPa. Find the factor of safety n against yielding by the Tresca (maximum shear stress) criterion.
Answer key
- 1. σavg = −20 MPa
- 2. σ2 = −79.04 MPa
- 3. θs = −67.5 °
- 4. θp = 52.02 °
- 5. σθ = −42.86 MPa
- 6. n = 2.915
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