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A turbulent boundary layer velocity profile is approximated by for y o and u = U for y> 6. (Hint: C U U Use

   

A turbulent boundary layer velocity profile is approximated by for y o and u = U for y> 6. (Hint: C U U Use the integral momentum equation to derive an expression for the dependence of the boundary thickness (6) and skin friction coefficient (Cf) on the local Reynolds number. = 1/5 0.0468 = 5 (R) /4 dx 2 dp for = 0) dx C de

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