Determine the drag coefficient of a 75kg skydiver with a projected area of 0.33m^2 and a terminal velocity of 60 m/s. Air density at the skydiver's altitude is 0.932 kg/m^3.
Hey there!
The drag force can be given with
Fd = 1/2 ρ v2 A cd
where
Fd = drag force (N)
cd = drag coefficient
ρ = density of fluid (0.932 kg/m3)
v = terminal velocity (60 m/s)
A = projected area (0.33 m2)
Hence the drag coefficient Cdis
(The value of Fd is taken as "mg" since the acceleration value is not specifically mentioned here for the drag)
Hence
is the drag Coefficient
I hope the solution helps... Feel free to comment and discuss further.... Cheers :)
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