22-Mec-A7 Advanced Strength of Materials · December 2018
Question 6 of 8: Square cantilever bar — axial + torsion design (Tresca, SF = 3)
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Exams, December 2018 — 16-Mec-A7 Advanced Strength of Materials. Open-book, 3 hours. Eight problems of equal value; any five constitute a complete paper. All eight problems are solved as a study resource.
Reference texts. Boresi & Schmidt, Advanced Mechanics of Materials (6th ed.); Ugural & Fenster, Advanced Strength and Applied Elasticity (5th ed.); Hibbeler, Mechanics of Materials (10th ed.); Timoshenko & Goodier, Theory of Elasticity (3rd ed.).
Question 6: Square cantilever bar — axial + torsion design (Tresca, SF = 3) (20 marks)
Find. Minimum $a$ for (a) $P$ acting axially (normal to the section) and (b) $P$ acting parallel to the section (transverse shear).
Approach. Locate the critical surface point (mid-side of the square, where torsional shear peaks). For (a) that point sees axial normal stress plus torsional shear; for (b) it sees transverse shear plus torsional shear. Apply Tresca ($\tau_\text{max}=\sigma_Y/2N$) and solve for $a$.
The allowable shear is $\tau_\text{allow}=\dfrac{\sigma_Y}{2N}=\dfrac{350}{6}=58.33\text{ MPa}.$
(a) Axial + torsion. At the mid-side, $\sigma=P/a^2$ (normal) and $\tau=T/\alpha a^3$ (shear). The maximum shear stress for this $(\sigma,\tau)$ state is
$$\tau_\text{max}=\sqrt{\left(\tfrac{\sigma}{2}\right)^2+\tau^2}=\sqrt{\left(\frac{P}{2a^2}\right)^2+\left(\frac{T}{\alpha a^3}\right)^2}=\tau_\text{allow}.$$
Solving numerically (torsion dominates: at the solution $\sigma=12.5$ MPa, $\tau=58.0$ MPa),
$$\boxed{a_\text{(a)}=118.4\text{ mm}}.$$
(b) Transverse + torsion. If $P$ is applied parallel to the section it produces a transverse shear force. With no length given, bending is neglected (flagged below) and only the transverse shear is retained. For a rectangular section the peak transverse shear is $1.5V/A=1.5P/a^2$, which superposes on the torsional shear (both are pure shear at the critical point):
$$\tau_\text{max}=\frac{T}{\alpha a^3}+\frac{1.5P}{a^2}=\tau_\text{allow}.$$
Solving (at the solution $\tau_\text{tor}=43.0$ MPa, $\tau_V=15.4$ MPa),
$$\boxed{a_\text{(b)}=130.8\text{ mm}}.$$
Interpret. Case (b) requires a larger section: a transverse shear of $1.5P/a^2$ adds directly to torsion, whereas the axial normal stress of case (a) combines only through the $(\sigma/2)$ term in $\tau_\text{max}$ and so is less damaging here.
Check: Part (b) gives no member length, so the bending moment $PL$ from the offset/parallel load cannot be formed; the transverse-shear-only reading is the intended simplification. If a length were supplied, bending would dominate and control the design.