A boundary layer for laminar flow of a fluid over the plate, as shown in Figure $2,$ is to be

approximated by the equation u$/$U $=($y $/8)-+$ C$2($y$/8)2+$ G$3(/8)3.$ Determine the

constants G$,2$ and S using the boundary conditions when u$=$U$,$ yE when

du$/$dy$=0,$ y$=8$ and when d$2$u$/$dy$2=0,$ y$=0.$ Then, obtain the thickness of the

boundary layer as a function of x and Rex using the momentum integral technique.