Mohr’s circle & stress transformation worksheet with answers

Free printable Mohr’s circle & stress transformation worksheet: 6 problems from easy to exam level, with an answer key. Print it or save it as a PDF.

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1.Easy
τxy​ = −110MPapure shear

A point on the surface of a shaft in torsion is in pure shear with τₓᵧ = −110 MPa (σₓ = σᵧ = 0). Find the normal stress σθ on a plane whose normal is rotated 35° counter-clockwise from the x-axis.

τxy = −110 MPaθ = 35°
σθ = MPa
2.Easy
100 kN100 kNθ = 35°A = 400 mm²

A bar with cross-sectional area 400 mm² carries an axial tensile force of 100 kN. Find the magnitude of the shear stress |τθ| on a section whose normal makes an angle of 35° with the bar axis.

P = 100 kNA = 400 mm²θ = 35°
|τθ| = MPa
3.Medium
σx​ = 10σy​ = 50τxy​ = −30MPa

A point in a loaded part has σₓ = 10 MPa, σᵧ = 50 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°.

σx = 10 MPaσy = 50 MPaτxy = −30 MPa
θp = °
4.Medium
σx​ = 70σy​ = 20τxy​ = 50MPa

A point has σₓ = 70 MPa, σᵧ = 20 MPa and τₓᵧ = 50 MPa (tension positive). The element is rotated 45° clockwise. Find the normal stress σy′ on the faces of the rotated element that are perpendicular to the rotated y′-axis.

σx = 70 MPaσy = 20 MPaτxy = 50 MPaθ = -45°
σy′ = MPa
5.Hard
σx​ = −30σy​ = 100τxy​ = 40MPa

A point in a loaded part has σₓ = −30 MPa, σᵧ = 100 MPa and τₓᵧ = 40 MPa (tension positive). Find the normal stress σθ on a plane whose normal is rotated 20° clockwise from the x-axis.

σx = −30 MPaσy = 100 MPaτxy = 40 MPaθ = -20°
σθ = MPa
6.Hard
σx​ = 110σy​ = 50τxy​ = −60MPa

A point in a loaded part has σₓ = 110 MPa, σᵧ = 50 MPa and τₓᵧ = −60 MPa (tension positive). Find the shear stress τθ on a plane whose normal is rotated 50° counter-clockwise from the x-axis (positive in the same sense as τₓᵧ).

σx = 110 MPaσy = 50 MPaτxy = −60 MPaθ = 50°
τθ = MPa

Answer key

  1. 1. σθ = −103.4 MPa
  2. 2. |τθ| = 117.5 MPa
  3. 3. θp = −61.85 °
  4. 4. σy′ = 95 MPa
  5. 5. σθ = −40.5 MPa
  6. 6. τθ = −19.13 MPa

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