Aerospace Engineering > GATE 2015 > Aircraft Performance
An aircraft, with a wing loading is gliding at w/s=500 N/m2 and (L/D)max=10 and CL=0.69 Considering the free stream density ρ∞=0.9 kg/m3, the equilibrium glide speed (in m/s) is
Correct : 39.5 to 40.5
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