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Problem 9.85 [Difficulty: 3] Given: Racing shell for crew approximated by half-cylinder: L 7.32 m D 457 mm V 6.71 m s Find: (a) Location of transition on hull (b) Thickness of turbulent BL at the rear of the hull (c) Skin friction drag on hull Solution: Basic equations: FD CD 1 2 ρ V 2 A (Drag) Transition occurs at Ret 5 10 5 so the location of transition would be: xt Ret ν V xt 0.0745 m For the turbulent boundary layer δ x 0.382 Rex 0.2 Therefore δ 0.382 L ReL 0.2 The Reynolds number at x = L is: ReL V L ν 4.91 10 7 so the BL thickness is: δ 0.382 L ReL 0.2 δ 0.0810 m The wetted area of the hull is: A π D 2 L 5.2547 m 2 For this Reynolds number: CD 0.455 log ReL 2.58 2.36 10 3 So the drag force is: FD CD 1 2 ρ V 2 A FD 278 N Note that the rowers must produce an average power of P FD V 1.868 kW to move the shell at this speed.
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