At a point in a loaded part the in-plane principal stresses are σ₁ = 190 MPa and σ₂ = −100 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 bar with cross-sectional area 500 mm² carries an axial tensile force of 150 kN. Find the normal stress σθ on a section whose normal makes an angle of 50° with the bar axis (tension positive).
A point has σₓ = −60 MPa, σᵧ = 80 MPa and τₓᵧ = 50 MPa (tension positive). The element is rotated 40° counter-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 = 10 MPa, σᵧ = 120 MPa and τₓᵧ = −30 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 = 160 MPa, σᵧ = −50 MPa and τₓᵧ = 50 MPa (tension positive). Find the normal stress σθ on a plane whose normal is rotated 45° clockwise from the x-axis.
A point in a thin plate is in plane stress: σₓ = −40 MPa, σᵧ = 60 MPa and τₓᵧ = 30 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.
Answer key
- 1. σavg = 45 MPa
- 2. σθ = 124 MPa
- 3. σy′ = −27.09 MPa
- 4. θp = −75.69 °
- 5. σθ = 5 MPa
- 6. n = 3.044
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