ISRO Mechanical & Aerospace 2006 - Question 67

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Topic: Fluid Mechanics

For laminar flow over a flat plate, the thickness of the boundary layer at a distance from the leading edge is found to be 5 mm. The thickness of the boundary layer at a downstream section, which is at twice the distance of the previous section from the leading edge, will be-

  • A. 10 mm
  • B. $5\sqrt{2}mm$
  • C. $5/\sqrt{2}mm$
  • D. 2.5 mm

Answer: B. $5\sqrt{2}mm$

Explanation: For laminar flow over a flat plate, boundary layer thickness $\delta \propto \sqrt{x}$. Given $\delta_{1} = 5~mm$ at distance $x_{1}$. At $x_{2} = 2x_{1}$, $\frac{\delta_{1}}{\delta_{2}} = \sqrt{\frac{x_{1}}{x_{2}}} = \sqrt{\frac{x_{1}}{2x_{1}}} = \frac{1}{\sqrt{2}}$. Thus, $\delta_{2} = \delta_{1}\sqrt{2} = 5\sqrt{2}mm$.

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