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An aircraft is flying in level flight at a speed of 200 km/hr through air (density, ρ=1.2 kg/m3, and viscosity μ=1.6×10−5 Ns/m2). The lift coefficient at this speed is 0.4 and the drag coefficient is 0.0065. The mass of the aircraft is 800 kg. The effective lift area of the aircraft is

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An aircraft is flying in level flight at a speed of 200 km/hr through air (density, ρ=1.2 kg/m3, and viscosity μ=1.6×105 Ns/m2). The lift coefficient at this speed is 0.4 and the drag coefficient is 0.0065. The mass of the aircraft is 800 kg. The effective lift area of the aircraft is



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