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22-Mec-A7 Advanced Strength of Materials · Undated paper

Question 4 of 8: 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 Exam — 16-Mec-A7 Advanced Strength of Materials (May 2019). Open-book; eight problems of equal value; any five constitute a complete paper. Every problem is solved as a study resource.

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

Question 4: 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. A cantilevered aluminium-alloy bar of solid square section a×a under a centroidal compressive axial force and a torque, designed to the maximum-shear-stress criterion.

Given data
Axial force, P177 kN (compressive)
Torque, T$23\ \text{kN}\cdot\text{m}$
Yield strength$\sigma_Y=350$ MPa
Safety factorN = 2
Failure criterionmaximum shear stress (Tresca)

Find. the minimum allowable side dimension a.

PTasection
Square cantilever bar under axial force P and torque T; section side a.

Approach. Combine the axial normal stress with the torsional shear of a square shaft, form the Tresca equivalent, set it to the factored yield, and solve for a.

  1. Stress components. Axial $\sigma=P/a^2$; for a square section the peak torsional shear (mid-side) is $$\tau=\frac{T}{0.208\,a^{3}}.$$
  2. Tresca condition. With only $\sigma$ and $\tau$ acting, the maximum shear stress is $\sqrt{(\sigma/2)^2+\tau^2}$, so design requires $$\sqrt{\left(\tfrac{\sigma}{2}\right)^2+\tau^2}=\frac{\sigma_Y}{2N}=\frac{350}{4}=87.5\ \text{MPa}.$$
  3. Solve. Substituting $\sigma=177\times10^3/a^2$ and $\tau=23\times10^6/(0.208a^3)$ (a in mm) and solving numerically, $$a_{\min}=108.3\ \text{mm}\ \Rightarrow\ \boxed{a=109\ \text{mm}}.$$

Torsion controls the design: at the solution the shear term is roughly ten times the axial half-stress, so the required size is set almost entirely by T. Rounding up to 109 mm keeps the working stress just inside the allowable and honours the factor of safety.

Final results
Minimum dimensiona = 108.3 mm
Adopted (round up)a = 109 mm
Allowable shear87.5 MPa