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22-Mec-A7 Advanced Strength of Materials · May 2014

Question 3 of 8: Torque and Axial Load from a Strain-Gauge Rosette

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

Notes on this paper

Paper format: National Exams, May 2014 — 07-Mec-A7 Advanced Strength of Materials. Open-book, 3 hours; any five of the eight problems constitute a complete paper and all problems are of equal value. All eight problems are solved.

Reference texts: A. C. Ugural & S. K. Fenster, Advanced Strength and Applied Elasticity, 4th ed.; A. P. Boresi & R. J. Schmidt, Advanced Mechanics of Materials, 6th ed.; R. C. Hibbeler, Mechanics of Materials, 10th ed.; S. P. Timoshenko & J. M. Gere, Theory of Elastic Stability, 2nd ed.

Question 3: Torque and Axial Load from a Strain-Gauge Rosette (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. $d=50$ mm; rectangular (0°/45°/90°) rosette with $\varepsilon_0=250\,\mu\varepsilon$ (axial), $\varepsilon_{45}=-50\,\mu\varepsilon$, $\varepsilon_{90}=-150\,\mu\varepsilon$; $E=40$ GPa, $v=0.3$.

Find. The applied axial load $P$ and torque $T$.

Approach. On the free (outer) surface the circumferential stress is zero, so the axial gauge alone fixes $\sigma_x$ and hence $P$. The rosette’s three readings give the surface shear strain $\gamma_{xy}$, which through $G$ gives the torsional shear stress and thus $T=\tau J/r$.

  1. Axial stress and load. The bar surface is traction-free in the hoop direction ($\sigma_{\text{hoop}}=0$), so $\sigma_x=E\varepsilon_0$: $$\sigma_x=40\times10^{3}(250\times10^{-6})=10.0\ \text{MPa}\;\Rightarrow\;P=\sigma_x\!\cdot\!\tfrac{\pi}{4}d^{2}=10.0\,(1963.5)=\boxed{19.6\ \text{kN}}.$$
  2. Surface shear strain. For a rectangular rosette the engineering shear strain is $$\gamma_{xy}=2\varepsilon_{45}-\varepsilon_0-\varepsilon_{90}=2(-50)-250-(-150)=-200\ \mu\varepsilon.$$
  3. Shear stress. With $G=\dfrac{E}{2(1+v)}=\dfrac{40}{2.6}=15.38$ GPa, $$\tau=G\,\gamma_{xy}=15.38\times10^{3}(200\times10^{-6})=3.08\ \text{MPa}.$$
  4. Torque. Using $\tau=\dfrac{T\,r}{J}$ with $J=\dfrac{\pi d^{4}}{32}=6.136\times10^{5}\ \text{mm}^4$ and $r=25$ mm, $$T=\frac{\tau J}{r}=\frac{3.08\,(6.136\times10^{5})}{25}=\boxed{75.5\ \text{N}\cdot\text{m}}.$$

Check / note. A pure axial + torsion surface would give $\varepsilon_{90}=-v\varepsilon_0=-75\,\mu\varepsilon$, whereas the gauge reads $-150\,\mu\varepsilon$. This mismatch is gauge scatter / minor bending, not evidence of a hoop stress: the outer fibre is a free surface, so $\sigma_{\text{hoop}}=0$ is enforced and $\sigma_x=E\varepsilon_0$ is the correct axial reading. We do not invent a transverse stress to reconcile $\varepsilon_{90}$.

QuantityResult
Axial stress $\sigma_x$$10.0$ MPa
Axial load $P$$19.6$ kN
Shear stress $\tau$$3.08$ MPa
Torque $T$$75.5$ N·m