Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
National Exams May 2015 – 04-BS-6: Mechanics of Materials
3 hours duration, closed book (one hand-written aid sheet permitted). Any five of the eight
questions constitute a complete paper; all eight are solved below as a complete study resource.
Reference texts: R.C. Hibbeler, Mechanics of Materials, 10th ed.
(Ch. 5 torsion, Ch. 6 shear/moment diagrams & composite beams, Ch. 7 transverse shear,
Ch. 8 combined loadings, Ch. 9 stress transformation, Ch. 12 deflection by integration,
Ch. 13 buckling); F. Beer & E.R. Johnston, Mechanics of Materials; W. Gere &
B. Goodno, Mechanics of Materials (alternates). A wide-flange (W-shape) properties
table printed on the exam's last page supplies the section used in Question 2.
[Figure not reproduced: Stepped shaft, fixed at A: T B =12 kN·m and T D =3 kN·m act in one rotational sense, T C =7 kN·m in the opposite sense (confirmed from the arrow curvature/arrowhead position on the source drawing); linear shear-stress distribution shown for the governing segment CD. See the official exam paper.]
Given.
Segment
Length (mm)
Diameter (mm)
AB
1200
80 (solid)
BC
800
60 (solid)
CD
1400
40 (solid)
G = 80 GPa, fy = 250 MPa (shear); TB=12 kN·m, TD=3
kN·m (same rotational sense); TC=7 kN·m (opposite sense); shaft fixed at
A.
Find. (a) Maximum shear stress and its radial variation. (b) Angle of twist at
D relative to A. (c) The effect of doubling every torque.
Approach. Take the sense of TB and TD as positive
(TC is then negative). Cut each segment and sum the applied torques to one side of the
cut to get the internal torque; apply $\tau=Tr/J$ in each segment (the governing one is whichever
gives the largest τ, not necessarily the largest T) and sum $\phi=TL/(GJ)$ segment by segment
for the total twist at D.
Internal torque in each segment (cutting from D back to A, signs per the arrows).
$$T_{CD}=T_D=+3\ \text{kN}\cdot\text{m}$$
$$T_{BC}=T_C+T_D=-7+3=-4\ \text{kN}\cdot\text{m}\ (4\ \text{kN}\cdot\text{m in the sense of }T_C)$$
$$T_{AB}=T_B+T_C+T_D=12-7+3=+8\ \text{kN}\cdot\text{m}$$
Check: the fixed-end reaction must equal the sum of every applied torque,
$12-7+3=8$ kN·m $=T_{AB}$ — confirms the segment signs.
(a) Shear stress in every segment, $\tau=16T/(\pi d^3)$.
$$\tau_{AB}=\frac{16(8\times10^6)}{\pi(80)^3}=79.6\ \text{MPa}, \qquad
\tau_{BC}=\frac{16(4\times10^6)}{\pi(60)^3}=94.3\ \text{MPa}$$
$$\tau_{CD}=\frac{16(3\times10^6)}{\pi(40)^3}=\boxed{238.7\ \text{MPa}}$$
Even though $T_{AB}$ is the largest internal torque, the much smaller 40 mm diameter of segment
CD makes it govern: $$\boxed{\tau_{max}=238.7\ \text{MPa, in segment CD}}$$ — below the
250 MPa shear yield, so the shaft remains elastic. The distribution is LINEAR across the
cross-section: zero at the shaft centre, rising to 238.7 MPa at the outer radius (r = 20 mm).
(b) Angle of twist at D relative to A.
$$J_{AB}=\frac{\pi(80)^4}{32}=4.021\times10^6\ \text{mm}^4, \quad
J_{BC}=\frac{\pi(60)^4}{32}=1.272\times10^6\ \text{mm}^4, \quad
J_{CD}=\frac{\pi(40)^4}{32}=0.2513\times10^6\ \text{mm}^4$$
$$\phi_{AB}=\frac{T_{AB}L_{AB}}{GJ_{AB}}=+1.710^\circ, \qquad
\phi_{BC}=\frac{T_{BC}L_{BC}}{GJ_{BC}}=-1.801^\circ, \qquad
\phi_{CD}=\frac{T_{CD}L_{CD}}{GJ_{CD}}=+11.969^\circ$$
$$\boxed{\phi_{D/A}=\phi_{AB}+\phi_{BC}+\phi_{CD}=1.710-1.801+11.969=11.88^\circ}\
\text{(net, in the sense of }T_B\text{ and }T_D\text{)}$$
(c) Effect of doubling every torque. Doubling every applied torque doubles
every internal torque and hence every stress (elastic, linear in T):
$$\tau_{CD,doubled}=2(238.7)=477.5\ \text{MPa} \gg f_y=250\ \text{MPa}$$
$$\boxed{\text{Segment CD would YIELD} \text{ — the outer fibres exceed 250 MPa shear
stress and the torsion formula }\tau=Tr/J\text{ no longer applies; the shaft develops a plastic
core in CD and the angle of twist grows disproportionately faster than the (now doubled) torque.}}$$
Final Results.
Quantity
Value
TAB, TBC, TCD
+8, −4, +3 kN·m
(a) τmax
238.7 MPa, in segment CD (governs despite the smaller torque)