A typical wind-tunnel nozzle consists of two profiles, the first of which is concave, the second convex. It is important to avoid boundary layer separation in both parts of the nozzle, but in the case of a turbulent boundary layer, convex curvature reduces turbulent kinetic energy and skin friction, whilst concave curvature has the opposite effect (relative to a flat plate). The boundary layer over the concave surface is thicker than that over a flat plate, whilst the boundary layer over a convex surface is thinner, and therefore less prone to separation. The concave section is therefore more elongated than the convex section.
Note that the coke-bottle section on a Formula 1 car also features a convex-concave transition, although in this case the airflow is external and the convex section comes first as the sidepods taper inwards.

An approximate macroscopic geometrical isomorphism, which was only implicate in the laws of physics, until the world of engineering made it explicate.
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