Consider viscous flow over a flat plate of length L. The Reynolds number based on flat plate length is 4 Million. Analytically compute an expression for drag coefficient if transition occurs at Reynolds number based on x Rex equal to 2 Million. Numerically compute the drag coefficient for this case.

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Explanation:

0.025 seconds

Explanation: You just have to divide the time between the # of flaps divided by the 1.25 m/s

Explanation:

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