NivaarExam PrepOfficial exam papers ↗

22-Mec-A7 Advanced Strength of Materials · December 2017

Question 6 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, December 2017 — 16-Mec-A7 Advanced Strength of Materials. Open-book, 3 hours; any five of eight problems constitute a complete paper (all problems of equal value). All eight problems are solved as a study resource.

Reference texts. Boresi & Schmidt, Advanced Mechanics of Materials (6th); Ugural & Fenster, Advanced Mechanics of Materials and Applied Elasticity (5th); Timoshenko & Goodier, Theory of Elasticity (3rd); Hibbeler, Mechanics of Materials (10th).

Question 6: 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. A 1 m square plate in biaxial plane stress.

Given data
$\varepsilon_x$$0.53\ \text{mm}/1000\ \text{mm}=0.53\times10^{-3}$
$\varepsilon_y$$0.66\ \text{mm}/1000\ \text{mm}=0.66\times10^{-3}$
$\sigma_x$$160\ \text{MPa}$
$E$$200\ \text{GPa}$

Find. (a) $\sigma_y$ and $\nu$; (b) the thickness strain $\varepsilon_z$.

Approach. Write the two in-plane Hooke’s-law equations for plane stress and solve the pair simultaneously for the two unknowns $\sigma_y$ and $\nu$; then use the out-of-plane law for $\varepsilon_z$.

  1. Hooke’s law, plane stress. $E\varepsilon_x=\sigma_x-\nu\sigma_y\Rightarrow \nu\sigma_y=160-106=54$; and $E\varepsilon_y=\sigma_y-\nu\sigma_x\Rightarrow \sigma_y-160\nu=132$.
  2. Eliminate $\nu$. Substituting $\nu=54/\sigma_y$ gives $\sigma_y^2-132\,\sigma_y-8640=0$.
  3. Solve (part a). The positive root is $$\boxed{\sigma_y=180\ \text{MPa},\qquad \nu=\frac{54}{180}=0.30}$$ which is admissible ($\nu\lt0.5$).
  4. Thickness strain (part b). $$\varepsilon_z=-\frac{\nu}{E}(\sigma_x+\sigma_y)=-\frac{0.30}{200\,000}(160+180)=\boxed{-5.1\times10^{-4}}.$$
Results — plate properties and strain
QuantityValue
$\sigma_y$180 MPa
Poisson’s ratio $\nu$0.30
Thickness strain $\varepsilon_z$$-5.1\times10^{-4}$