A laminar boundary layer velocity profile is approximated
Chapter 9, Problem 9.29(choose chapter or problem)
A laminar boundary layer velocity profile is approximated by the two straight-line segments indicated in Fig. P9.29. Use the momentum integral equation to determine the boundary layer thickness, \(\delta= \delta (x)\), and wall shear stress, \(\tau_w =\tau_w (x)\). Compare these results with those in Table 9.2.
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