- #1
danny2010
- 14
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Homework Statement
a) The weight of the aircraft = 4000 N
b) Wing loading of the aircraft = 65N per sq m
c) Find the minimum drag, maximum lift to drag ratio and the minimum drag speed at sea level
Homework Equations
CD = 0.019 + 0.04 CL2
Where CD is coefficient of Drag
CL is coefficient of Lift
CL2 is square of coeff of lift