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)
20° 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.
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.
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).
Centre and radius. $$\sigma_{avg}=\dfrac{\sigma_x+\sigma_y}{2}=10.0\text{ MPa},\qquad R=\sqrt{\left(\dfrac{\sigma_x-\sigma_y}{2}\right)^2+\tau_{xy}^2}=53.85\text{ MPa}.$$
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.
Read the plane’s stresses off the circle (confirmed by the transformation equations, used only as a check per the question’s instruction): $$\sigma_{n}=\sigma_{avg}+\dfrac{\sigma_x-\sigma_y}{2}\cos2\theta+\tau_{xy}\sin2\theta=35.45\text{ MPa}$$ $$\tau=-\dfrac{\sigma_x-\sigma_y}{2}\sin2\theta+\tau_{xy}\cos2\theta=-47.46\text{ MPa}$$ $$\boxed{\sigma_n=35.4\text{ MPa (tension)},\ \ \tau=-47.5\text{ MPa}}$$
Principal stresses and maximum shear (top and bottom of the circle): $$\boxed{\sigma_1=63.9\text{ MPa},\ \ \sigma_2=-43.9\text{ MPa},\ \ \tau_{max}=R=53.9\text{ MPa (at }\sigma_{avg}=10.0\text{ MPa)}}$$
Mohr’s circle: centre 10 MPa, R = 53.9 MPa, with points X, Y, the principal stresses, and the plane A′.