Chapter 4, Problem 4.17P

An excellent approximation for the two-dimensional incompressible laminar boundary layer on the flat surface in Fig, P4.17 is $u\approx U\left(2\frac{y}{\delta }-2\frac{y^3}{{\delta }^3}+\frac{y^4}{{\delta }^4}\right)$ for $y\le \delta$ where $\delta =C{x}^{1/2}$, C = const

(a) Assuming a no-slip condition at the wall, find an expression for the velocity component v(x, y) for y ??. (b) Then mid the maximum value of v at the station x = 1 m, for the particular case of airflow, when U = 3 m/s and $\delta =1.1$ cm.