For steady viscous flow through a circular tube (Fig. E3.4), the axial velocity profile is given approximately by
u=U0(1−Rr)m
so that u varies from zero at the wall (r=R), or no slip, up to a maximum u=U0 at the centerline r=0. For highly viscous (laminar) flow m≈21, while for less viscous (turbulent) flow m≈71. Compute the average velocity if the density is constant.