Question 6 of 8: Internal Torque, Maximum Shear Stress, and Angle of Twist in a Stepped Shaft
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 6: Internal Torque, Maximum Shear Stress, and Angle of Twist in a Stepped Shaft
Applied torques: 500 N·m CCW at B, 1000 N·m CW at C, 200 N·m CCW at D. $G=80$ GPa, $\tau_Y=160$ MPa.
Find. (a) the maximum shear stress in the shaft, with its radial distribution at that section; (b) the angle of twist at D, in degrees.
Stepped shaft A-B-C-D, fixed at A; torques 500 CCW at B, 1000 CW at C, 200 CCW at D.
Approach. Working from the free end D back to the fixed end A (method of sections), find the internal torque carried by each segment; compute $\tau=T\rho/J$ (max at the outer radius) per segment to find the governing one; sum $\theta_i=T_iL_i/(GJ_i)$ for the total twist at D.
Internal torque per segment (taking CCW as $+$, consistent with the free end): cutting successively from D toward A and summing the torques on the freed portion,
$$T_{CD}=+200\text{ N}\!\cdot\!\text{m},\qquad T_{BC}=-1000+200=-800\text{ N}\!\cdot\!\text{m},\qquad T_{AB}=500-1000+200=-300\text{ N}\!\cdot\!\text{m}$$
(Check: the fixed-end reaction is $-T_{AB}=+300$ N·m, and $300+500-1000+200=0$ — equilibrium confirmed.)
Polar moments of inertia.
$$J_{AB}=\tfrac{\pi}{32}(0.030^4-0.020^4)=6.381\times10^{-8}\text{ m}^4$$
$$J_{BC}=\tfrac{\pi}{32}(0.040)^4=2.513\times10^{-7}\text{ m}^4,\qquad J_{CD}=\tfrac{\pi}{32}(0.020)^4=1.571\times10^{-8}\text{ m}^4$$
Shear stress per segment ($\tau=T\,c/J$, outer radius $c$).
$$\tau_{AB}=\frac{300(0.015)}{6.381\times10^{-8}}=70.5\text{ MPa},\quad \tau_{BC}=\frac{800(0.020)}{2.513\times10^{-7}}=63.7\text{ MPa},\quad \tau_{CD}=\frac{200(0.010)}{1.571\times10^{-8}}=127.3\text{ MPa}$$
$$\boxed{\tau_{max}=127.3\text{ MPa, in segment CD}}\quad(<\tau_Y=160\text{ MPa})$$
At that section, $\tau$ varies linearly with radius from $0$ at the shaft centre to $127.3$ MPa at $\rho=10$ mm (solid section — no discontinuity, unlike the hollow $AB$ segment which would jump from $0$ at $\rho=10$ mm to a finite value across the bore).
Angle of twist at D.
$$\theta_D=\frac{T_{AB}L_{AB}}{GJ_{AB}}+\frac{T_{BC}L_{BC}}{GJ_{BC}}+\frac{T_{CD}L_{CD}}{GJ_{CD}}$$
$$=\frac{-300(0.6)}{80\times10^9(6.381\times10^{-8})}+\frac{-800(0.4)}{80\times10^9(2.513\times10^{-7})}+\frac{200(0.6)}{80\times10^9(1.571\times10^{-8})}$$
$$=-0.03526-0.01592+0.09549=0.04432\text{ rad}$$
$$\boxed{\theta_D=2.54^{\circ}}$$