Consider incompressible flow in the entrance of a circular tube, as in Fig. P3.53. The inlet flow is uniform, u1=U0. The flow at section 2 is developed pipe flow. Find the wall drag force F as a function of (p1,p2,ρ,U0,R) if the flow at section 2 is
(a) Laminar: u2=umax(1−R2r2)
(b) Turbulent: u2≈umax(1−Rr)1/7