Solved: The streamwise velocity component of a steady,
Chapter 10, Problem 98P(choose chapter or problem)
Problem 98P
The streamwise velocity component of a steady, incompressible, laminar, flat plate boundary layer of boundary layer thickness δ is approximated by the sine wave profile of Prob. 10-104. Generate expressions for displacement thickness and momentum thickness as functions of δ based on this sine wave approximation. Compare the approximate values of δ*/δ and δ/δ to the values of δ*/δ and θ/δ obtained from the Blasius solution.
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