Flow of air develops in a horizontal cylindrical duct, of
diameter D 5 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 5 ðy=δÞ
1=7
. The inlet flow is U 5 50 ft/s
at section 1 . At section 2 , the boundary-layer thickness is
δ2 5 4 in. Evaluate the static gage pressure at section 2 ,
located at L 5 20 ft. Find the average wall shear stress.
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