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22-Mec-A7 Advanced Strength of Materials · May 2018

Question 4 of 8: Biaxial Plate — Inverse Problem and Principal Stresses

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

Notes on this paper

Paper format. National Exams, May 2018 — 16-Mec-A7 Advanced Strength of Materials. Open-book, 3 hours, eight problems of equal value; a complete paper is any five. All eight problems are solved here 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 4: Biaxial Plate — Inverse Problem and Principal Stresses (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 biaxially stressed square plate of side 1.8 m; the two elongations and $\sigma_x$ are known, and $E$ is given.

Given data
Elongations$\delta_x=0.18\ \text{mm}$, $\delta_y=0.75\ \text{mm}$ over $L=1800\ \text{mm}$
Strains$\varepsilon_x=1.00\times10^{-4}$, $\varepsilon_y=4.167\times10^{-4}$
Known stress$\sigma_x=50\ \text{MPa}$
Modulus$E=200\ \text{GPa}$

Find. (a) $\sigma_y$ and $v$; (b) the principal stresses and their orientation once $\tau_{xy}=100\ \text{MPa}$ is added.

Approach. Write both plane-stress Hooke equations; eliminate $\sigma_y$ to get a quadratic in $v$, then back-substitute. For part (b) apply the in-plane principal-stress formula to $(\sigma_x,\sigma_y,\tau_{xy})$.

  1. Hooke’s law, both directions. $E\varepsilon_x=\sigma_x-v\sigma_y$ gives $20=50-v\sigma_y$, so $v\sigma_y=30$. $E\varepsilon_y=\sigma_y-v\sigma_x$ gives $83.33=\sigma_y-50v$.
  2. Eliminate $\sigma_y$. With $\sigma_y=30/v$, substitution yields $50v^2+83.33v-30=0$, whose admissible root is $$\boxed{v=0.304,\qquad \sigma_y=98.6\ \text{MPa}}$$ ($vt 0.5$, so the result is physically admissible).
  3. Add the shear and locate the centre / radius. $\sigma_{\text{avg}}=\tfrac12(50+98.6)=74.3\ \text{MPa}$; $R=\sqrt{\left(\tfrac{50-98.6}{2}\right)^2+100^2}=102.9\ \text{MPa}$.
  4. Principal stresses. $$\boxed{\sigma_1=177.2\ \text{MPa},\qquad \sigma_2=-28.6\ \text{MPa}}$$
  5. Orientation. $\tan2\theta_p=\dfrac{2\tau_{xy}}{\sigma_x-\sigma_y}=\dfrac{200}{-48.6}$, so $\theta_{p1}=51.8^\circ$ from the x-axis to the $\sigma_1$ direction ($\sigma_2$ at $141.8^\circ$).
Results
QuantityValue
Poisson’s ratio $v$0.304
Transverse stress $\sigma_y$98.6 MPa
Major principal stress $\sigma_1$177.2 MPa at $51.8^\circ$
Minor principal stress $\sigma_2$−28.6 MPa at $141.8^\circ$