ISRO Mechanical & Aerospace 2015 - Question 8

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Topic: Strength of Materials

A thin cylindrical shell of diameter (d), length (l) and thickness (t) is subjected to an internal pressure (p). The ratio of the longitudinal strain to hoop strain is

  • A. $\frac{m-2}{2m-1}$
  • B. $\frac{2m-1}{m-2}$
  • C. $\frac{m-2}{2m+1}$
  • D. $\frac{m+2}{2m+2}$

Answer: A. $\frac{m-2}{2m-1}$

Explanation: The longitudinal strain is given by $\epsilon_{l} = \frac{1}{E}[\sigma_{l} - \mu\sigma_{h}] = \frac{1}{E}[\frac{\sigma_{h}}{2} - \mu\sigma_{h}] = \frac{\sigma_{h}}{2E}[1 - 2\mu]$. The hoop strain is $\epsilon_{h} = \frac{1}{E}[\sigma_{h} - \mu\sigma_{l}] = \frac{1}{E}[\sigma_{h} - \frac{\mu\sigma_{h}}{2}] = \frac{\sigma_{h}}{2E}[2 - \mu]$. The required ratio is $\frac{\epsilon_{l}}{\epsilon_{h}} = \frac{(1 - 2\mu)}{(2 - \mu)}$. Using the relationship $\mu = \frac{1}{m}$, the ratio simplifies to $\frac{1 - 2(1/m)}{2 - (1/m)} = \frac{m-2}{2m-1}$.

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