Mohr’s circle & stress transformation: practice problems with step-by-step solutions
Also called: principal stresses · plane stress
Free Mohr’s circle & stress transformation practice problems with diagrams, hints and full worked solutions. New values every time, at three levels: principal stresses, maximum shear and principal direction, stress on an inclined plane.
Learn Mohr’s circle & stress transformation from scratch
Before this: Axial stress & strain
1Why stress depends on direction
In the axial lesson, stress was one number: force over area. But the stress at a point depends on the direction of the cut you look at.
Twist a piece of chalk until it breaks. It breaks along a spiral at 45°, not straight across. On that 45° plane the tension is largest, and chalk is weak in tension.
To describe the stress at one point, engineers draw a tiny square, the stress element, with the stresses on its faces:
- σx and σy are normal stresses, at right angles to the faces. Positive means tension (arrows pointing out), negative means compression.
- τxy is the shear stress, along the faces. It tries to turn the square into a diamond.
Rotate the square, and the stresses on its faces change. This lesson shows how to find them for every direction, and which directions are the most dangerous.
Self-check At a point, σx = −40 MPa. What does this mean?
- A compression of 40 MPa in the x-direction
- A compression of 40 MPa in the y-direction
- A shear stress of 40 MPa
- A tension of 40 MPa in the x-direction
Answer: A compression of 40 MPa in the x-direction. With the usual sign rule tension is positive, so a negative σx is compression, acting on the faces normal to x.
2Mohr’s circle
Mohr’s circle is a picture of all the directions at once. Every point on the circle is one possible cut through the point in the part.
Draw normal stress σ to the right and shear stress τ upwards. Then plot two points:
- point x at (σx, τxy): the stresses on the face normal to x,
- point y at (σy, −τxy): the stresses on the face normal to y.
The circle goes through both points. Its centre C lies on the σ-axis, halfway between them. Its radius R follows from Pythagoras:
C = (σx + σy) / 2 R = √( ((σx − σy)/2)² + τxy² )
Where the circle crosses the σ-axis, the shear stress is zero. These two values are the principal stresses, the largest and smallest normal stress at the point. The top of the circle is the largest in-plane shear stress:
σ1 = C + R σ2 = C − R τmax = R
Self-check σx = 50 MPa, σy = 10 MPa and τxy = 15 MPa. What is σ1?
- 45 MPa
- 50 MPa
- 55 MPa
- 65 MPa
Answer: 55 MPa. C = 30 MPa and R = √(20² + 15²) = 25 MPa, so σ1 = 55 MPa. 65 adds 20 + 15 instead of using Pythagoras; 50 ignores the shear stress.
3Angles: double on the circle
Rotating the element by an angle θ moves its point on Mohr’s circle by 2θ, in the same direction. Counter-clockwise is positive.
The direction of σ1 is the angle θp from the x-axis, found from:
tan 2θp = 2τxy / (σx − σy)
Mind the quadrant. If σx − σy is negative, add 180° to 2θp when τxy > 0, or subtract 180° when τxy < 0. Then halve it.
The planes of maximum shear lie 45° away from the principal directions (90° on the circle).
For a plane whose normal is rotated θ from the x-axis, the stresses are:
σθ = C + (σx − σy)/2 · cos 2θ + τxy · sin 2θ
τθ = −(σx − σy)/2 · sin 2θ + τxy · cos 2θ
Self-check At a point, tan 2θp = 1 and σx − σy is positive. What is θp?
- 22.5°
- 45°
- 90°
- −67.5°
Answer: 22.5°. 2θp = 45°, so θp = 22.5°. Answering 45° forgets to halve the angle from the circle. −67.5° is the direction of σ2, 90° away.
4The method step by step
- Write down σx, σy and τxy with their signs: tension positive, compression negative.
- Find the centre C = (σx + σy)/2.
- Find the radius R = √(((σx − σy)/2)² + τxy²).
- Principal stresses: σ1 = C + R and σ2 = C − R. Largest in-plane shear: τmax = R.
- Directions: tan 2θp = 2τxy/(σx − σy), check the quadrant, then halve.
- For a given plane θ: use the σθ and τθ equations with 2θ.
A quick sketch of the circle, even a rough one, shows you the signs and which point is σ1.
5A worked example
Follow every step. Try to predict the next one before you open it.
Worked exampleA point has σx = 80 MPa, σy = 20 MPa and τxy = 40 MPa. Find the principal stresses, τmax, the direction θp of σ1, and the normal stress on a plane rotated 45° counter-clockwise.
1Both normal stresses are tension. The shear stress is positive.
2C = (80 + 20) / 2 = 50 MPa
R = √(30² + 40²) = 50 MPa
3σ1 = 50 + 50 = 100 MPa σ2 = 50 − 50 = 0 MPa
τmax = R = 50 MPa
4tan 2θp = 2 · 40 / (80 − 20) = 1.333
σx − σy is positive, so no correction is needed: 2θp = 53.1° and θp = 26.6° counter-clockwise from x.
5With θ = 45°, 2θ = 90°: cos 2θ = 0 and sin 2θ = 1.
σθ = 50 + 30 · 0 + 40 · 1 = 90 MPa
6The sum σx + σy = 100 MPa equals σ1 + σ2 = 100 MPa. This sum is the same for every rotation, so it is a quick check.
Also, 90 MPa lies between σ2 = 0 and σ1 = 100 MPa, as every normal stress must.
Answer σ1 = 100 MPa, σ2 = 0, τmax = 50 MPa, θp = 26.6° and σ45° = 90 MPa.
6Common mistakes
- Adding (σx − σy)/2 and τxy directly. The radius combines them with Pythagoras.
- Using θ instead of 2θ in the transformation equations, or forgetting to halve the angle read from the circle.
- Dropping a minus sign: a compressive stress must go in as a negative number.
- Plotting point y at (σy, +τxy). It is at −τxy, on the opposite side of the centre from x.
- Missing the quadrant of 2θp when σx < σy.
Self-check σx = 60 MPa, σy = 0 and τxy = 40 MPa. What is the maximum in-plane shear stress?
- 30 MPa
- 40 MPa
- 50 MPa
- 70 MPa
Answer: 50 MPa. τmax = R = √(30² + 40²) = 50 MPa. 70 adds 30 + 40; 30 ignores the shear stress; 40 is only τxy.
7How exam questions look
- Easy: principal stresses. Given σx, σy and τxy, find σ1 or σ2. Variants: pure shear, or an axial bar cut at an angle.
- Medium: maximum shear and principal direction. Find τmax = R or the angle θp, between −90° and 90°.
- Hard: stress on an inclined plane. Use the σθ or τθ equation with 2θ. Variants combine axial load and torsion, or use the principal stresses in a failure check such as von Mises or Tresca.
Write C and R down first. Almost every question in this topic is answered from those two numbers.
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