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For a two-dimensional incompressible flow over a flat plate, the laminar boundary layer thickness at a distance \(x\) from the leading edge is \(\delta\). If \(Re_{x}\) is the Reynolds number defined based on length scale x, \(\left(\dfrac{\delta}{x}\right)\) is proportional to ______.

  • A.\({Re_{x}}^{-1/2}\)
  • B.\({Re_{x}}^{-1}\)
  • C.\({Re_{x}}^{-3/2}\)
  • D.\({Re_{x}}^{-2}\)

Answer: A

\(\delta/x\) is proportional to \(Re_{x}^{-1/2}\).

For a laminar boundary layer on a flat plate, the Blasius solution gives

\[ \frac{\delta}{x} \approx \frac{5.0}{\sqrt{Re_{x}}} \]

The scaling follows from balancing inertia, \(U^{2}/x\), with viscous diffusion, \(\nu U/\delta^{2}\), which gives \(\delta \sim \sqrt{\nu x/U}\). So the boundary layer grows as \(\sqrt{x}\) and \(\delta/x\) falls as \(Re_{x}^{-1/2}\). The exponent −1/5 belongs to the turbulent boundary layer; −1, −3/2 and −2 do not arise for either.

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