ISRO Mechanical & Aerospace 2015 - Question 13

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Topic: Strength of Materials

For the component loaded with a force F as shown in the figure, the axial stress at the corner point P is

Figure for question 13, ISRO Mechanical & Aerospace 2015

  • A. $\frac{F(3L-b)}{4b^{3}}$
  • B. $\frac{F(3L+b)}{4b^{3}}$
  • C. $\frac{F(3L+4b)}{4b^{3}}$
  • D. $\frac{F(3L-2b)}{4b^{3}}$

Answer: D. $\frac{F(3L-2b)}{4b^{3}}$

Explanation: The total axial stress $\sigma$ at the corner point P is the sum of the direct axial stress $\sigma_{a}$ and the bending stress $\sigma_{b}$. The direct axial stress is $\sigma_{a} = \frac{F}{Area} = \frac{F}{2b \times 2b} = \frac{F}{4b^{2}}$. The bending moment is $M = F(L-b)$. The section modulus is $Z = \frac{I}{Y} = \frac{(1/12)(2b)(2b)^{3}}{b} = \frac{4}{3}b^{3}$. The bending stress is $\sigma_{b} = \frac{M}{Z} = \frac{F(L-b)}{(4/3)b^{3}} = \frac{3F(L-b)}{4b^{3}}$. Adding both gives $\sigma = \frac{F}{4b^{2}} + \frac{3F(L-b)}{4b^{3}} = \frac{Fb + 3FL - 3Fb}{4b^{3}} = \frac{F(3L-2b)}{4b^{3}}$.

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