For any "geeks" out there other than me, here's the equation you could use to calculate it:
D = Cd * A * .5 * V^2
Drag from the air is the coefficient of drag (this is how aerodynamic your steed is...a typical car = .3, a typical m/c = .9). A is the frontal area in square feet (typical car = 20, typical m/c = 8), and velocity must be expressed in ft/sec. (This equation is simplified since at a given altitude air viscosity will not change much.)
(This is mostly just for fun since Cd always has to be tested in a wind tunnel for empirical values and A must be meticulously calculated. Also this "simplified" equation will not yield "correct" units, they would need to be converted to lb-f, then to HP to be useful for us

Anybody got a spare wind tunnel?