Aircraft drag coefficient and aerodynamic drag?
i'm desinging small aircraft (model) , i'm working on aerodyanmic drag. have deep camber, high lift, low speed airfoil. there formula use calculate drag on particular airfoil? know there standard drag coefficient formula being:
drag coefficient= 2fd on pv2a
fd= drag force
p= mass density
v= speed
a= referance area
referance area being planform because aircraft, , straight wing, there formula?
thanks.
i'm desinging small aircraft (model) , i'm working on aerodyanmic drag. have deep camber, high lift, low speed airfoil. there formula use calculate drag on particular airfoil? know there standard drag coefficient formula being: drag coefficient= 2fd over...
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