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04-BS-6 · December 2015

Question 3 of 8: Stepped Circular Shaft — Torsion

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

Notes on this paper

National Exams December 2015 — 04-BS-6: Mechanics of Materials (3 hours, closed book, one hand-written aid sheet permitted). Any FIVE of the eight questions constitute a complete paper on the official exam; every question is answered below.

Reference texts: Hibbeler, Mechanics of Materials, 10th ed. (beam deflection, torsion, transformation of stress, combined loading, columns); CISC Handbook of Steel Construction (W-shape section properties, attached to this exam).

Question 3: 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.

Given. The printed figure shows the curved torque arrows at C and D sweep the same rotational sense, while the arrow at B sweeps the opposite sense — i.e. TB opposes TC and TD.

SegmentDiameterLength
AB40 mm (solid)400 mm
BC60 mm (solid)1500 mm
CD40 mm outer / 30 mm inner (hollow)800 mm

TB = 7 kN·m (CCW), TC = 4 kN·m (CW), TD = 1 kN·m (CW); G = 80 GPa; shear yield τY = 250 MPa.

40 mm dia60 mm diahollow 40/30 mmABCD7 kN·m (CCW)4 kN·m (CW)1 kN·m (CW)4001500800-2+5+1T(kN·m)
Stepped shaft ABCD (fixed at A) with the applied torques and the resulting internal-torque diagram (CW positive).

Find. τmax in the shaft and its distribution over the governing cross-section; the angle of twist at D; the consequence of doubling all three torques.

Approach. Take CW as positive, sum the applied torques on the free-end side of a cut through each segment to get the internal torque, then apply $\tau=Tc/J$ and $\phi=\sum TL/(GJ)$ segment by segment.

  1. Internal torque per segment (cut then sum everything toward the free end D): $$T_{AB}=T_B+T_C+T_D = -7+4+1 = -2\ \text{kN}\cdot\text{m}\qquad T_{BC}=T_C+T_D=5\ \text{kN}\cdot\text{m}\qquad T_{CD}=T_D=1\ \text{kN}\cdot\text{m}$$
  2. Shear stress in each segment, $\tau = Tc/J$ with $J=\pi d^4/32$ (solid) or $\pi(d_o^4-d_i^4)/32$ (hollow): $$J_{AB}=\frac{\pi(40)^4}{32}=2.513\times10^5\ \text{mm}^4 \;\Rightarrow\; \tau_{AB}=\frac{(2\times10^6)(20)}{2.513\times10^5}=159.2\ \text{MPa}$$ $$J_{BC}=\frac{\pi(60)^4}{32}=1.272\times10^6\ \text{mm}^4 \;\Rightarrow\; \tau_{BC}=\frac{(5\times10^6)(30)}{1.272\times10^6}=117.9\ \text{MPa}$$ $$J_{CD}=\frac{\pi(40^4-30^4)}{32}=1.718\times10^5\ \text{mm}^4 \;\Rightarrow\; \tau_{CD}=\frac{(1\times10^6)(20)}{1.718\times10^5}=116.4\ \text{MPa}$$ $$\boxed{\tau_{max}=159.2\ \text{MPa, in segment AB}\ (<\tau_Y=250\ \text{MPa}\Rightarrow\text{still elastic})}$$ The stress is zero at the shaft centre and increases linearly to this value at the outer radius (part (a) sketch below).
  3. Angle of twist at D (segment twists accumulate with sign): $$\phi_D=\sum\frac{T_iL_i}{GJ_i}=\frac{(-2\times10^6)(400)}{80000(2.513\times10^5)}+\frac{(5\times10^6)(1500)}{80000(1.272\times10^6)}+\frac{(1\times10^6)(800)}{80000(1.718\times10^5)}$$ $$\boxed{\phi_D = 0.09210\ \text{rad} = 5.28^{\circ}}$$
  4. Part (c): doubling the loads. Every internal torque and hence every stress scales by exactly 2 (linear elasticity), so $$\tau_{AB,\text{doubled}} = 2(159.2)=318.3\ \text{MPa} > \tau_Y = 250\ \text{MPa}$$ Segment AB would yield in shear. The elastic formulas $\tau=Tc/J$ and $\phi=TL/(GJ)$ would no longer hold for AB — the shaft would develop a plastic (yielded) outer annulus there, the twist would grow disproportionately faster than the applied torque, and the design would need to be re-sized (or the AB diameter increased) to remain safe; segments BC and CD (235.8 and 232.8 MPa doubled) would still be elastic but with very little margin left.
τmax=159.2 MPar=20 mm0linear in r (τ=Tr/J)
Shear-stress distribution across the AB cross-section (r=20 mm) — linear in r, zero at the centre.
QuantityValue
TAB / TBC / TCD−2 / 5 / 1 kN·m
τAB / τBC / τCD159.2 / 117.9 / 116.4 MPa
τmax159.2 MPa (segment AB), elastic
φD0.0921 rad = 5.28°
Loads doubledτAB→318.3 MPa > 250 MPa — AB yields