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04-BS-6 · May 2013

Question 8 of 8: Stepped circular shaft — torsion

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

Notes on this paper

National Exams — May 2013 — 04-BS-6 Mechanics of Materials. Three-hour, closed-book exam (one double-sided hand-written aid sheet permitted, approved Casio/Sharp calculator only). Format: eight questions offered; any five constitute a complete paper and only the first five appearing in the answer book are marked. All eight are solved below for completeness. No credit is given in the original exam for solutions built by superposing existing standard solutions on Questions 1 and 6 — both are solved here by direct integration/equilibrium as required.

Reference texts: Hibbeler, Mechanics of Materials (10th ed., Pearson) — beam deflection by integration (Ch. 12), stress transformation and Mohr's circle (Ch. 9), columns and buckling (Ch. 13), combined axial & bending loading (Ch. 8), torsion of circular shafts (Ch. 5), transformed-section method for composite beams (Ch. 6), shear and moment diagrams (Ch. 6-7); Beer, Johnston & DeWolf, Mechanics of Materials (7th ed., McGraw-Hill) — cross-check reference for the same topics.

Question 8: Stepped circular shaft — torsion (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.

ABCD2800 N.m (CW)2000 N.m (CCW)1500 N.m/m (CW)1000 mm800 mm1200 mmQ8: shaft ABCD (AB solid 50mm; BCD hollow 50/40mm)
Shaft ABCD: AB solid (50 mm), BCD hollow (50/40 mm); torque senses as marked.

Given.

QuantityValue
ABsolid, 50 mm dia., 1000 mm long
BC, CDhollow, 50 mm OD / 40 mm ID; 800 mm, 1200 mm long
Applied torques2800 N·m CW at B; 2000 N·m CCW at C; 1500 N·m/m CW along CD
$G$, $F_y$ (shear)80 GPa, 150 MPa

Find. (a) $\tau_{max}$ in the shaft, and its variation across the radius at that section; (b) the angle of twist at D.

Approach. Taking CCW (matching the torque at C) as positive, sum the applied torques from each cut to the free end D to build the internal torque diagram $T(x)$, then apply $\tau=Tr/J$ per segment (tracking the change in $J$ at B) and sum $\theta=\int T/(GJ)\,dx$ segment-by-segment for the total twist.

  1. Internal torque diagram. With CCW $=+$: $T_B=-2800$, $T_C=+2000$ N·m, and the distributed torque totals $1500\times1.2=-1800$ N·m (CW) over CD. Summing from each cut to the free end D: $$T_{CD}(x)=-1500(3.0-x)\ \text{N}\!\cdot\!\text{m}\ (x\text{ in m from A});\quad T_{CD}(1.8)=-1800,\ T_{CD}(3.0)=0$$ $$T_{BC}=T_C+(\text{dist. total})=2000-1800=+200\ \text{N}\!\cdot\!\text{m}$$ $$T_{AB}=T_B+T_C+(\text{dist. total})=-2800+2000-1800=\boxed{-2600\ \text{N}\!\cdot\!\text{m}}$$ Reaction at the fixed wall A: $+2600$ N·m (equal and opposite to $T_{AB}$), confirming overall equilibrium.
  2. Polar moments of inertia. $$J_{solid}=\frac{\pi(25)^4}{2}=6.136\times10^{5}\ \text{mm}^4\ (\text{AB}),\qquad J_{hollow}=\frac{\pi(25^4-20^4)}{2}=3.623\times10^{5}\ \text{mm}^4\ (\text{BCD})$$
  3. Shear stress in each segment. $\tau=|T|r_{outer}/J$: $$\tau_{AB}=\frac{(2600\times10^3)(25)}{6.136\times10^5}=105.9\ \text{MPa}$$ $$\tau_{BC}=\frac{(200\times10^3)(25)}{3.623\times10^5}=13.8\ \text{MPa}$$ $$\tau_{CD}\big|_{x=C}=\frac{(1800\times10^3)(25)}{3.623\times10^5}=\boxed{124.2\ \text{MPa}}\quad(\text{maximum, in the hollow shaft just past C})$$ Although AB carries the largest torque (2600 N·m), the hollow section just past C — carrying "only" 1800 N·m through a smaller $J$ — produces the larger stress and governs; all values remain below the 150 MPa yield.
  4. Radial variation at the governing section (just past C). Shear stress is linear in $r$, $\tau(r)=Tr/J$, but exists only for $20\le r\le25$ mm (no material inside the bore): $$\tau(20\ \text{mm})=\frac{(1800\times10^3)(20)}{3.623\times10^5}=99.4\ \text{MPa},\qquad \tau(25\ \text{mm})=124.2\ \text{MPa}$$ i.e. a straight line from 99.4 MPa at the bore to 124.2 MPa at the outer surface — with a discontinuity (zero stress, no material) for $r<20$ mm, unlike a solid shaft's stress line which would run all the way to zero at the centre.
  5. Part (b): angle of twist at D. Summing each segment (constant-torque segments directly, CD by integrating the linear $T(x)$): $$\theta_{AB}=\frac{T_{AB}L_{AB}}{GJ_{solid}}=\frac{(-2600\times10^3)(1000)}{(80\,000)(6.136\times10^5)}=-0.05297\ \text{rad}$$ $$\theta_{BC}=\frac{T_{BC}L_{BC}}{GJ_{hollow}}=\frac{(200\times10^3)(800)}{(80\,000)(3.623\times10^5)}=+0.00552\ \text{rad}$$ $$\theta_{CD}=\int_0^{1200}\frac{T_{CD}(s)}{GJ_{hollow}}\,ds=-0.03727\ \text{rad}$$ $$\theta_D=\theta_{AB}+\theta_{BC}+\theta_{CD}=\boxed{-0.0847\ \text{rad}=-4.85^\circ}$$
QuantityResult
$T_{AB}$, $T_{BC}$, $T_{CD}(C^+)$−2600, +200, −1800 N·m
$\tau_{max}$ (location)124.2 MPa, hollow section just past C
$\tau$ at bore ($r=20$ mm)99.4 MPa
$\theta_D$−0.0847 rad = −4.85°
Back to the paper →
-2600 N.m (AB)200 N.m (BC)-1800 N.m (at C+)Q8: internal torque diagram T(x)
Internal torque diagram T(x) (CCW positive).