The streamwise velocity component of a steady,
Chapter 10, Problem 95P(choose chapter or problem)
Problem 95P
The streamwise velocity component of a steady, incompressible, laminar, flat plate boundary layer of boundary layer thickness δ is approximated by the simple linear expression, u = Uy/δ for y< δ, and u = U for y > δ (Fig. P10-102), Generate expressions for displacement thickness and momentum thickness as functions of 8, based on this linear approximation. Compare the approximate values of δ*/δand θ/δ to the values of δ*/δ and θ/δobtained from the Blasius solution.
FIGURE P10-102
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