Drag count
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A drag count is a single unit of drag as defined by aerospace engineers. Drag is generally computed using the equation:
\[\frac{1}{2} \rho v^2 C_d s\]
Where:
\[\rho\] is the air density \[v\] is the current airspeed \[C_d\] is the drag coefficient (a dimensionless constant, usually on the order of 0.02 to 0.04 for an aircraft in cruise) \[s\] is the aircraft wing area
A drag count of 1 is equal to \(C_d\) of 0.0001. So if, for example, the steady state drag coefficient is 0.0200 and someone sticks a hand out the window adding 5 drag counts, the new drag coefficient would be:
- 0.0200 + 0.0005 = 0.0205 or 205 drag counts.
Drag count is used as a crude measure for the change in drag coefficient (it is not a direct measure of drag as it is associated with a reference area, it is only valid for use as a relative assessment of change).
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