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04-BS-6 · December 2014

Question 4 of 8: Mohr’s Circle for Plane Stress

Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)

Notes on this paper

04-BS-6: Mechanics of Materials — National Exams, December 2014

3 hours duration. Closed book (one hand-written aid sheet permitted). Any FIVE of the eight questions constitute a complete paper; all eight are solved below as a complete study resource.

Reference texts: Hibbeler, Mechanics of Materials, 10th ed.; Beer, Johnston, DeWolf & Mazurek, Mechanics of Materials, 7th ed.; Gere & Goodno, Mechanics of Materials, 8th ed.

Question 4: Mohr’s Circle for Plane Stress (20 marks)

Question text not reproduced: the examination questions are © Engineers and Geoscientists BC. Open the official past paper (linked at the top of this page) to read the question, then follow the worked solution below.

Given.

Normal stress, right (x) face40 MPa, compressive (points into the element)
Normal stress, top (y) face60 MPa, tensile
Shear stress, right face20 MPa, pointing up (+y on +x face ⇒ τxy=+20 MPa)
Inclined plane20° from the horizontal, from the bottom-left corner

Find. (a) the stress components on the 20° inclined plane, using Mohr’s circle; (b) the maximum in-plane shear stress and its associated normal stress and orientation.

40 MPa (C)60 MPa (T)20 MPa20°Element in plane stress (arrows = actual sense)
Stress element (arrows show the actual sense read off the source figure) and the 20° inclined cutting plane.

Approach. Plot points X(σx,τxy) and Y(σy,−τxy) on the σ-τ plane, draw the circle through them, then rotate by 2θ (measured on the circle) to the point representing the inclined face.

  1. Sign convention. σx=−40 MPa, σy=+60 MPa, τxy=+20 MPa (standard +y-on-+x-face convention; the right-face arrow points into the element, confirming compression).
  2. Centre and radius. $$\sigma_{avg}=\dfrac{\sigma_x+\sigma_y}{2}=10.0\text{ MPa},\qquad R=\sqrt{\left(\dfrac{\sigma_x-\sigma_y}{2}\right)^2+\tau_{xy}^2}=53.85\text{ MPa}.$$
  3. Locate the inclined plane. A cut 20° above the horizontal, from the bottom-left corner, has its outward normal rotated 90° further — i.e. the face is at $\theta=20^{\circ}-90^{\circ}=-70^{\circ}$ from the x-axis (a diagram check: rotating a line by 20° rotates its normal by the same 20°, and the x-face’s own edge is vertical, 90° from this horizontal reference). On the circle this is a rotation of $2\theta=-140^{\circ}$ from point X.
  4. Read the plane’s stresses off the circle (confirmed by the transformation equations, used only as a check per the question’s instruction): $$\sigma_{n}=\sigma_{avg}+\dfrac{\sigma_x-\sigma_y}{2}\cos2\theta+\tau_{xy}\sin2\theta=35.45\text{ MPa}$$ $$\tau=-\dfrac{\sigma_x-\sigma_y}{2}\sin2\theta+\tau_{xy}\cos2\theta=-47.46\text{ MPa}$$ $$\boxed{\sigma_n=35.4\text{ MPa (tension)},\ \ \tau=-47.5\text{ MPa}}$$
  5. Principal stresses and maximum shear (top and bottom of the circle): $$\boxed{\sigma_1=63.9\text{ MPa},\ \ \sigma_2=-43.9\text{ MPa},\ \ \tau_{max}=R=53.9\text{ MPa (at }\sigma_{avg}=10.0\text{ MPa)}}$$
σ (MPa)τ (MPa)X(σx,τxy)Y(σy,-τxy)σ1=63.9σ2=-43.9A' (35.5, -47.5)center=10.0 MPa, R=53.9 MPa
Mohr’s circle: centre 10 MPa, R = 53.9 MPa, with points X, Y, the principal stresses, and the plane A′.
QuantityValue
Centre, radius10.0 MPa, 53.85 MPa
σn, τ on 20° plane35.4 MPa, -47.5 MPa
Principal stresses σ1, σ263.9 MPa, -43.9 MPa
Maximum in-plane shear τmax53.9 MPa (at σ=10.0 MPa)