Allanw wrote:I don't know why Cd isn't an absolute measurement, which would allow for comparison. The relative figure used is only really helpful when looking at different specs of the exact same body style
Alan, have just noticed this early post about Cd....
The answer is that the whole point of Cd is that it is a coefficient for comparison purposes, irrespective of an area or a speed or air density. So you can compare large or small, of different or similar shapes.
So it does provide a good way of comparing, providing the area reference used is on the same basis; that could be frontal area, planform area, in the case of skin friction and boundary layer drag, total surface (wetted) area may be used.
Coefficients are deliberately constructed to be non-dimensional, as are many other parameters used in science and engineering e.g Mach No.
You need the area to produce an absolute comparison. Thus the mention of CdA comparisons, Cd x Area, and for a road vehicle, frontal area would be used.
For an aircraft, for total drag comparisons, planform area would usually be the reference for Cd (tot).
Hope that explains it, Cl and Cm, lift and pitching moment work in the same way.
To get the Actual drag (in say lbf) from a Cd you need not only the Area, but 'Q', the total dynamic head, caused by the airspeed and density = 1/2 x density x speed squared, effectively the kinetic energy in the wind.