22-Mec-A7 Advanced Strength of Materials · December 2018
Question 2 of 8: Strain rosette on a bar under torsion + axial load
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 2: Strain rosette on a bar under torsion + axial load (20 marks)
Given. Solid shaft, $d=55\text{ mm}$; rectangular (0/45/90) rosette on the free surface with the 0° gauge axial.
Given data
Diameter $d$
55 mm
$\varepsilon_0$ (axial)
$230\times10^{-6}$
$\varepsilon_{45}$
$-40\times10^{-6}$
$\varepsilon_{90}$ (hoop)
$-120\times10^{-6}$
$E,\ \nu$
40 GPa, 0.3
Find. The axial force $P$ and the torque $T$ that produce these surface strains.
Approach. On the traction-free surface the hoop stress is zero, so the axial stress follows directly from $\varepsilon_0$ (giving $P$); the engineering shear strain from the rosette gives the surface shear stress (giving $T$).
Check: A pure axial state would give $\varepsilon_{90}=-\nu\varepsilon_0=-69\times10^{-6}$, but the gauge reads $-120\times10^{-6}$. The mismatch is gauge scatter/misalignment; the free surface still has $\sigma_\text{hoop}=0$, so we take $\sigma_\text{axial}=E\varepsilon_0$ and do not invent a hoop stress.
Axial stress and force (free surface: $\sigma_\text{hoop}=0$). With one non-zero normal stress, $\varepsilon_0=\sigma_\text{axial}/E$, so
$$\sigma_\text{axial}=E\varepsilon_0=(40\,000)(230\times10^{-6})=9.20\text{ MPa},$$
$$P=\sigma_\text{axial}\,A=(9.20)(2376)=\boxed{21.86\text{ kN}}.$$
Shear strain from the rosette. For a 0/45/90 rosette,
$$\gamma_{xy}=2\varepsilon_{45}-\varepsilon_0-\varepsilon_{90}=2(-40)-230-(-120)=-190\times10^{-6}.$$
Shear stress via the shear modulus.
$$G=\frac{E}{2(1+\nu)}=\frac{40}{2(1.3)}=15.38\text{ GPa},\qquad \tau=G\,\gamma_{xy}=(15\,385)(190\times10^{-6})=2.923\text{ MPa}.$$
Torque from the torsion formula. $\tau=Tr/J$ gives
$$T=\frac{\tau J}{r}=\frac{(2.923)(8.984\times10^{5})}{27.5}=\boxed{95.5\text{ N}\cdot\text{m}}.$$