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04-BS-6 · Undated paper

Question 4 of 8: Principal Stresses and Maximum Shear Stress by Mohr's Circle

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

Notes on this paper

National Exam, May 2019 — 04-BS-06: Mechanics of Materials. Closed book, one 8.5"×11" handwritten aid sheet permitted, 3 hours, 8 questions of equal value (any 5 of 8 constitute a complete paper — all 8 are answered here as a complete study resource).

Reference texts: R.C. Hibbeler, Mechanics of Materials, 10th ed. (Pearson) — axial deformation of statically indeterminate assemblies, beam deflection by integration, shear/moment diagrams, plane-stress transformation and Mohr's circle, column buckling, torsion of circular shafts, composite (transformed-section) beams, combined axial-flexural loading, transverse shear.

Question 4: Principal Stresses and Maximum Shear Stress by Mohr's Circle

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.

QuantityValue
$\sigma_x$150 MPa (tension)
$\sigma_y$30 MPa (tension)
$\tau_{xy}$60 MPa

Find. $\sigma_1,\sigma_2$ and their plane orientation; $\tau_{max}$ and its plane orientation — all via Mohr's circle geometry.

30 MPa30 MPa150 MPa60 MPa
Plane-stress element: sigma_x=150 MPa, sigma_y=30 MPa, tau_xy=60 MPa.
sigmatauXYsigma1sigma2tau_max2*theta_p = 45 deg
Mohr's circle: center 90 MPa, R=84.85 MPa; sigma1/sigma2/tau_max marked.

Approach. Plot points $X=(\sigma_x,-\tau_{xy})$ and $Y=(\sigma_y,\tau_{xy})$, the diameter of Mohr's circle; the center and radius give $\sigma_{1,2}$ directly, and the angle to $X$ gives the physical rotation to the principal plane.

  1. Circle center and radius. $$\sigma_{avg}=\frac{\sigma_x+\sigma_y}{2}=\frac{150+30}{2}=90\text{ MPa}$$ $$R=\sqrt{\left(\frac{\sigma_x-\sigma_y}{2}\right)^2+\tau_{xy}^2}=\sqrt{60^2+60^2}=84.85\text{ MPa}$$
  2. Part (a) — Principal stresses. $$\boxed{\sigma_1=\sigma_{avg}+R=174.85\text{ MPa},\qquad \sigma_2=\sigma_{avg}-R=5.15\text{ MPa}}$$
  3. Part (b) — Orientation of the principal plane. From the circle, the angle from point $X$ to the $\sigma_1$ axis is $$2\theta_p=\tan^{-1}\!\left(\frac{\tau_{xy}}{(\sigma_x-\sigma_y)/2}\right)=\tan^{-1}(1)=45^{\circ}\Rightarrow \theta_p=22.5^{\circ}$$ Rotating the stress element $22.5^{\circ}$ counterclockwise from the $x$-face aligns it with the $\sigma_1=174.85$ MPa plane (the $\sigma_2$ plane is $90^{\circ}$ away, perpendicular).
  4. Part (c)&(d) — Maximum shear stress and its plane. The top of the circle gives $$\boxed{\tau_{max}=R=84.85\text{ MPa},\ \text{with an average normal stress }\sigma_{avg}=90\text{ MPa on that plane}}$$ located at $\theta_s=\theta_p-45^{\circ}=-22.5^{\circ}$ (i.e. $22.5^{\circ}$ clockwise from the $x$-face) — always $45^{\circ}$ from the principal planes.
ResultValue
$\sigma_1$174.85 MPa, at $\theta_p=22.5^{\circ}$ CCW from x-axis
$\sigma_2$5.15 MPa, at $\theta_p+90^{\circ}$
$\tau_{max}$84.85 MPa, at $\theta_s=-22.5^{\circ}$ ($\sigma_{avg}=90$ MPa on that face)