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22-Mec-A7 Advanced Strength of Materials · May 2015

Question 7 of 8: Sizing a Square Bar Under Axial Load and Torque

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

Notes on this paper

Paper format. National Exams, May 2015 — 07-Mec-A7 Advanced Strength of Materials. Open-book, 3 hours. Eight problems of equal value; any five constitute a complete paper. All eight are solved here.

Reference texts. Ugural & Fenster, Advanced Strength and Applied Elasticity (4th ed.); Boresi & Schmidt, Advanced Mechanics of Materials (6th ed.); Hibbeler, Mechanics of Materials (10th ed.); Timoshenko & Goodier, Theory of Elasticity.

Question 7: Sizing a Square Bar Under Axial Load and Torque (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. Square bar, side b, carrying axial P and torque T; design by Tresca with a factor of safety of 3.

Given data
Yield stress, σY310 MPa
Axial force, P195 kN
Torque, T17 kN·m
Factor of safety, N3
Square-torsion constantτmax = T/(0.208 b3)

Find. The minimum side b for (a) axial (normal) P and (b) P applied parallel to the section.

P = 195 kNT = 17 kN·mbRigid support
Square-section bar built into a rigid support, loaded by centroidal axial force P and torque T.

Approach. Combine the normal stress from P with the torsional shear from T at the most-stressed point; the Tresca criterion limits the maximum in-plane shear to $\sigma_Y/(2N)$. Solve the resulting nonlinear equation for b.

  1. Allowable shear. The maximum-shear-stress criterion with safety factor 3 gives $$\tau_{\text{allow}}=\frac{\sigma_Y}{2N}=\frac{310}{6}=51.7\ \text{MPa}.$$
  2. (a) Axial + torsion. The axial stress is $\sigma=P/b^2$ and the torsional shear $\tau=T/(0.208b^3)$. The largest shear in the element combining a normal and a shear stress is $\tau_{\max}=\sqrt{(\sigma/2)^2+\tau^2}$, so $$\sqrt{\Big(\frac{P}{2b^2}\Big)^2+\Big(\frac{T}{0.208b^3}\Big)^2}=51.7\ \text{MPa}\ \Rightarrow\ \boxed{b=117\ \text{mm}.}$$ At this size $\sigma=14.3$ MPa and $\tau=51.2$ MPa—torsion dominates.
  3. (b) P applied parallel to the section. Now P is a transverse shear force, not an axial load; its peak (centroidal) shear in a rectangular section is $\tau_P=1.5P/b^2$, acting on the same faces as the torsional shear, so they add: $$\frac{1.5P}{b^2}+\frac{T}{0.208b^3}=51.7\ \text{MPa}\ \Rightarrow\ \boxed{b=133\ \text{mm}.}$$ A larger section is needed because a transverse shear stress superposes directly on the torsional shear rather than combining under a square root.
Check: Part (b) superposes the maximum transverse-shear stress on the maximum torsional shear. Both peak at the mid-point of the side faces parallel to P (the neutral axis for transverse shear, the mid-side for torsion of a square), and on one of those faces they act in the same direction, so the arithmetic sum is the elementary-theory maximum, not an over-estimate. Bending from P is neglected because no member length or eccentricity is given; if a length were supplied, the bending stress at the support would have to be added to part (b).
Final results — Question 7
CaseMinimum side b
(a) P normal (axial) + torque117 mm
(b) P parallel (transverse shear) + torque133 mm