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

Question 6 of 8: Strain Rosette — Transformation, Principal Strains and Yield

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 6: Strain Rosette — Transformation, Principal Strains and Yield (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 0–45–90 rectangular rosette with the 0° gauge along $x$; plane-stress plate with $E=90\ \text{GPa}$, $v=0.28$.

Given data
Rosette readings$\varepsilon_0=600\,\mu$, $\varepsilon_{45}=400\,\mu$, $\varepsilon_{90}=300\,\mu$
Cartesian strains$\varepsilon_x=600\,\mu$, $\varepsilon_y=300\,\mu$, $\gamma_{xy}=2\varepsilon_{45}-\varepsilon_0-\varepsilon_{90}=-100\,\mu$
Elastic constants$E=90\ \text{GPa}$, $v=0.28$

Find. (a) $\varepsilon_{x'},\varepsilon_{y'},\gamma_{x'y'}$ at $+60^\circ$; (b) principal strains and directions; (c) the yield strength implied by the max-shear criterion.

Approach. Reduce the rosette to $(\varepsilon_x,\varepsilon_y,\gamma_{xy})$, rotate them to $60^\circ$, take the principal strains from the strain Mohr’s circle, convert to principal stresses by plane-stress Hooke’s law, and apply Tresca.

  1. Rotate to $+60^\circ$. With $\tfrac{\varepsilon_x+\varepsilon_y}{2}=450\,\mu$, $\tfrac{\varepsilon_x-\varepsilon_y}{2}=150\,\mu$, $\tfrac{\gamma_{xy}}{2}=-50\,\mu$ and $2\theta=120^\circ$: $$\boxed{\varepsilon_{x'}=331.7\,\mu,\quad \varepsilon_{y'}=568.3\,\mu,\quad \gamma_{x'y'}=-209.8\,\mu}$$ (the sum $\varepsilon_{x'}+\varepsilon_{y'}=900\,\mu$ equals $\varepsilon_x+\varepsilon_y$, a useful check).
  2. Principal strains. $\varepsilon_{1,2}=450\pm\sqrt{150^2+50^2}=450\pm158.1\,\mu$, so $$\boxed{\varepsilon_1=608.1\,\mu,\qquad \varepsilon_2=291.9\,\mu}$$
  3. Principal directions. $\tan2\theta_p=\dfrac{\gamma_{xy}}{\varepsilon_x-\varepsilon_y}=\dfrac{-100}{300}$, giving $\theta_p=-9.2^\circ$ (to $\varepsilon_1$); $\varepsilon_2$ lies at $80.8^\circ$.
  4. Principal stresses (plane stress). $\sigma_{1,2}=\dfrac{E}{1-v^2}(\varepsilon_{1,2}+v\,\varepsilon_{2,1})$ with $\dfrac{E}{1-v^2}=97.66\ \text{GPa}$: $\sigma_1=67.4\ \text{MPa}$, $\sigma_2=45.1\ \text{MPa}$ (both tensile, $\sigma_3=0$).
  5. Max-shear yield. With both in-plane principals positive, the extreme pair is $\sigma_1$ and $\sigma_3=0$, so $$\boxed{\sigma_Y=\sigma_1-\sigma_3=67.4\ \text{MPa}}$$
Results
QuantityValue
Strains at $+60^\circ$$\varepsilon_{x'}=331.7\,\mu$, $\varepsilon_{y'}=568.3\,\mu$, $\gamma_{x'y'}=-209.8\,\mu$
Principal strains$\varepsilon_1=608.1\,\mu$ at $-9.2^\circ$, $\varepsilon_2=291.9\,\mu$ at $80.8^\circ$
Principal stresses$\sigma_1=67.4$, $\sigma_2=45.1\ \text{MPa}$
Yield strength (max shear)67.4 MPa
Check: Because both in-plane principal stresses are tensile, the out-of-plane $\sigma_3=0$ is the minimum principal stress; the maximum shear therefore uses $\sigma_1-\sigma_3$, not $\sigma_1-\sigma_2$. Using $\sigma_1-\sigma_2$ would understate the driving shear and overstate the yield strength.