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Elementary ideas of viscous flows - Aerodynamics - Aerospace Engineering Previous Year Questions
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| Paper | Year / session | Questions in this view | Open |
|---|---|---|---|
| Aerospace Engineering (AE) 2025 | 2025 | 1 | View paper |
All Elementary ideas of viscous flows previous year questions
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2025 · Aerospace Engineering · Aerodynamics · Elementary ideas of viscous flows
Aerospace Engineering (AE) 2025
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 \(x\), \(\frac{\delta}{x}\) is proportional to _____.
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