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Mechanics

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The streamlined shape and the flat plate shown in the top diagram are scaled such that their drag is the same. The drag coefficient for the streamline shape is about CD = 0.04 whilst that for the disc is CD = 1.1.

The two lower diagrams show the flow around these two bodies. The real flow around the streamline shape has an initial laminar boundary layer that then becomes turbulent towards the end of the body. The turbulent wake is small in area and the pressure recovery across the shape is good. For the flat plate, flow separation occurs at the sharp corners and there is no pressure recovery behind the body. The large area wake has a considerable kinetic energy associated with the turbulent motion and this energy has to be provided by the flow.

In human-powered systems drag reduction by careful shape selection is an essential component for success.

From: Wegener, "What Makes Airplanes Fly?" Springer-Verlag (1991)