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The drag coefficient, CD, associated with a sphere is shown plotted against of Reynolds number, Re =rVD/m. Both axes of the plot are logarithmic. For a given body size, D, fluid density, r, and dynamic viscosity, m, the Reynolds number scales as the velocity, V, of the fluid with respect to the sphere.

In the Reynolds number range below about 5, the drag coefficient is large and increases with decreasing Re. This region is known as "Stokes flow" and FD = 3pmDV, where D is the diameter of the sphere and V the velocity. The drag increases linearly with the velocity.

Between 103 < Re < 105 the drag coefficient is about 0.5 and approximately constant. In this range the viscous forces are less important than the pressure forces acting on the sphere. It is in this range that the drag increases as the square of the speed.

From: Wegener, 
"What Makes Airplanes Fly?" 
Springer-Verlag (1991)
At Re ~ 5 x 105 the drag coefficient drops by a factor of about five and a new flow situation has been established. The flow over the sphere has become turbulent and the boundary layer stays attached to the sphere well past its maximum cross-section decreasing the size of the wake behind the sphere. The attached turbulent boundary layer decreases the pressure drop, reducing this drag component.