A short refresher on drag, Cd, frontal area and CdA.
Aerodynamic drag is the force that is created as an object moves through the air.
The equation for drag is:
Drag Force = ½ × Air Density × Cd × Area × Airspeed²
Worth remembering that
CdA = Cd × Area
To lower CdA we want to minimise Cd and Area.
Area is the frontal area: the outline of the rider and bike as the air sees them, projected onto a plane square to the airflow.
For a racing cyclist, frontal area is usually around 0.3 to 0.4 m².
Cd represents drag from the shape of an object. Lower Cd is less drag.
For the same frontal area, the airfoil has around a sixth of the drag of the half-sphere.details
Even the most aero-efficient cyclists do not actually have a very aerodynamic shape.
A cyclist is a "bluff body", meaning their aerodynamic wake is not much smaller than their frontal area.
Because the flow separates rather than staying attached, where it separates — and therefore how large the wake is — depends on speed and on surface finish. That is the subject of the companion entry, Variable CdA.
A note on the numbers. Every drag coefficient in this article is referenced to frontal area, and each is quoted over the range of Reynolds number appropriate to its own shape. The vehicles are quoted at their own operating speeds.