Flow of air develops in a horizontal cylindrical duct, of diameter $D=15$ in., following a well-rounded entrance. A turbulent boundary grows on the duct wall, but the flow is not yet fully developed. Assume that the velocity profile in the boundary layer is $u / U=(y / \delta)^{1 / 7} .$ The inlet flow is $U=50 \mathrm{ft} / \mathrm{s}$ at section ?. At section ? , the boundary-layer thickness is $\delta_{2}=4$ in. Evaluate the static gage pressure at section ? located at $L=20$ ft. Find the average wall shear stress.