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22-Mec-A7 Advanced Strength of Materials · May 2013

Question 3 of 8: Strain-Gauge Rosette on a Bar in Combined Torsion and Tension

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

Notes on this paper

Paper format: National Exams, May 2013 — 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 as a study resource.

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: Strain-Gauge Rosette on a Bar in Combined Torsion and Tension (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. A 50 mm solid shaft carrying axial force P and torque T; a 0°/45°/90° rosette (0° axial).

Given data
Diameter / geometryd = 50 mm; A = 1963.5 mm2, J = 6.136×105 mm4
Gauge strainsε0 = 800×10−6, ε45 = −200×10−6, ε90 = −400×10−6
Elastic constantsE = 80 GPa, v = 0.28, G = E/[2(1+v)] = 31.25 GPa

Find. The axial load P and the torque T that produced these surface strains.

Approach. On the free surface of the bar the axial gauge reads the axial strain directly, giving the axial stress and hence P; the rosette’s shear strain follows from the three readings, giving the surface shear stress and hence T.

  1. Axial stress and load. The bar surface is free (radial and hoop stresses zero), so the axial gauge measures $\varepsilon_{axial}=\sigma/E$: $$\sigma=E\,\varepsilon_0=(80\,000)(800\times10^{-6})=64\ \text{MPa},\qquad P=\sigma A=64(1963.5).$$ $$\boxed{P \approx 125.7\ \text{kN}}$$
  2. Shear strain from the rosette. For a rectangular (0/45/90) rosette, $$\gamma_{xy}=2\varepsilon_{45}-\varepsilon_0-\varepsilon_{90}=2(-200)-800-(-400)=-800\times10^{-6}.$$
  3. Surface shear stress. Using the shear modulus, $$\tau=G\,\gamma_{xy}=(31\,250)(-800\times10^{-6})=-25\ \text{MPa}\quad(|\tau|=25\ \text{MPa}).$$
  4. Torque. From the torsion formula $\tau=Tr/J$ with r = 25 mm, $$T=\frac{\tau J}{r}=\frac{25\,(6.136\times10^{5})}{25}=6.136\times10^{5}\ \text{N}\cdot\text{mm}.$$ $$\boxed{T \approx 0.614\ \text{kN}\cdot\text{m}\ (614\ \text{N}\cdot\text{m})}$$
Question 3 — results
QuantityValue
Axial stress σ64 MPa
Axial load P125.7 kN
Shear strain γxy−800×10−6
Shear stress τ25 MPa
Torque T0.614 kN·m

Check: for a free bar surface the transverse gauge should read −vε0 = −224×10−6, whereas the measured ε90 = −400×10−6. The excess is attributed to gauge/measurement scatter; because the hoop stress on the surface is genuinely zero, the axial stress is taken from ε0 directly. (Treating the readings as a general plane-stress state would give σx = 59.7 MPa, P = 117 kN, plus a spurious hoop stress that cannot physically exist here.)