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The interaction between the flat plate and the flow can be expressed in terms of a friction coefficient that will be different in the laminar and turbulent flow regimes. By analogy with solid friction, the coefficient, Cf, is the friction force per unit area divided by the normal force due to the dynamic pressure of the fluid. This quantity can be expressed in terms of the Reynolds number so that in the laminar region, Cf = 1.33 (Re)-0.5, and in the turbulent region:          Cf = 0.074 (Re)-0.2. These quantities are shown in the logarithmic plot opposite which also indicates the range of the transition region between the two limiting flow types.

From the point of view of skin friction laminar flow is a clear advantage. As will be seen in the following discussion, turbulent flow can sometimes provide an overall drag advantage because of its effects on the pressure distribution around a vehicle. In these cases, the increased skin friction drag is more than compensated for by the reduced pressure drag.

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