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The diagrams below illustrate three flow situations and the associated pressure distribution on the sphere. In (a) the fluid is inviscid, and no viscous boundary layer exists. The flow is symmetrical about f = 900 and the pressure distribution on the front and back of the sphere is the same. No net pressure force exists and the sphere exhibits no drag.

In (b) viscosity has been included and the flow over the sphere is laminar up to the point of separation. A turbulent wake behind the sphere alters the pressure distribution, with pressures on the front of the sphere being larger than those at the back. The pressure force is now a major contribution to the drag.

In (c) the Reynolds number is high enough that the flow has become turbulent before reaching
f = 900. The turbulent flow stays attached onto the rear surface before finally separating to yield a smaller turbulent wake. Some pressure recovery occurs on the back of the sphere and reduces the pressure drag. This term more than compensates for the increased viscous drag of the turbulent flow.

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