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

Question 2 of 8: Plane-Stress Plate — Inverse Problem

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 2: Plane-Stress Plate — Inverse Problem (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. Square plate, side $1.6$ m; biaxial plane stress ($\sigma_z=\tau=0$); $\delta_x=0.8$ mm, $\delta_y=0.25$ mm; $\sigma_y=60$ MPa; $E=200$ GPa.

Find. (a) $\sigma_x$ and Poisson’s ratio $v$; (b) the through-thickness strain $\varepsilon_z$.

Approach. Convert the measured elongations to strains, then invert the two-dimensional Hooke’s law: two equations in the two unknowns $\sigma_x$ and $v$ (eliminating $\sigma_x$ leaves a quadratic in $v$). Finally apply the out-of-plane Hooke relation for $\varepsilon_z$.

  1. In-plane strains. Uniform stress over a side of $1600$ mm gives $$\varepsilon_x=\frac{0.8}{1600}=5.00\times10^{-4},\qquad \varepsilon_y=\frac{0.25}{1600}=1.5625\times10^{-4}.$$
  2. Plane-stress Hooke’s law. With $\sigma_z=0$, $$E\varepsilon_x=\sigma_x-v\,\sigma_y=100\ \text{MPa},\qquad E\varepsilon_y=\sigma_y-v\,\sigma_x=31.25\ \text{MPa}.$$
  3. Eliminate $\sigma_x$. From the first equation $\sigma_x=100+60v$; substituting into the second and rearranging, $$60\,v^{2}+100\,v-28.75=0\;\Rightarrow\;\boxed{v=0.25}$$ (the negative root $v=-1.92$ is inadmissible). This value is physically valid ($0\lt v\lt 0.5$).
  4. Back-substitute for $\sigma_x$. $$\sigma_x=100+60(0.25)=\boxed{115\ \text{MPa (tension)}}.$$
  5. Thickness strain. Out-of-plane, $\varepsilon_z=-\dfrac{v}{E}\left(\sigma_x+\sigma_y\right)$, $$\varepsilon_z=-\frac{0.25}{200\,000}\,(115+60)=-2.19\times10^{-4}.$$ The plate thins slightly, as expected under biaxial tension.
QuantityResult
Poisson’s ratio, $v$$0.25$
Normal stress $\sigma_x$$115$ MPa (tension)
Thickness strain $\varepsilon_z$$-2.19\times10^{-4}$ ($-218.8\ \mu\varepsilon$)