At a point in a loaded part the in-plane principal stresses are σ₁ = 180 MPa and σ₂ = −110 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 800 mm² carries an axial tensile force of 40 kN. Find the normal stress σθ on a section whose normal makes an angle of 40° with the bar axis (tension positive).
A point in a loaded part has σₓ = −20 MPa, σᵧ = 80 MPa and τₓᵧ = 20 MPa (tension positive). Find the maximum in-plane shear stress τmax.
A point in a loaded part has σₓ = 20 MPa, σᵧ = 50 MPa and τₓᵧ = −10 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 = 120 MPa and τₓᵧ = 60 MPa (tension positive). Find the normal stress σθ on a plane whose normal is rotated 45° counter-clockwise from the x-axis.
A point in a loaded part has σₓ = −50 MPa, σᵧ = −80 MPa and τₓᵧ = 50 MPa (tension positive). Find the normal stress σθ on a plane whose normal is rotated 25° counter-clockwise from the x-axis.
Answer key
- 1. σavg = 35 MPa
- 2. σθ = 29.34 MPa
- 3. τmax = 53.85 MPa
- 4. θp = −73.15 °
- 5. σθ = 150 MPa
- 6. σθ = −17.06 MPa
Full step-by-step solutions: practise this topic on examproblems.com.