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Engineering, 07.07.2020 17:01 annabanana1298

The velocity profile in a turbulent boundary layer flow with zero pressure gradient (over a flat plate, length L) may be approximated by the 1/6-power profile expression, u/U = (y/delta)^1/6.
The wall shear stress can be expressed as tau_w = 0.0233_p U^2 (v/U delta)^1/4. Using the Karman integral
equation, obtain expression for (a) delta/x, (b) C_f for this velocity profile, (c) drag force on the entire flat plate.

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