Question
What is the aerofoil lift (in newtons) on a wing of area 88 m² if the air passes at speed over its top surface at 280 m·s⁻¹ and bottom surface at 150 m·s⁻¹? (Assume standard air density ρ = 1.2 kg·m⁻³)
What is the aerofoil lift (in newtons) on a wing of area 88 m² if the air passes at speed over its top surface at 280 m·s⁻¹ and bottom surface at 150 m·s⁻¹? (Assume standard air density ρ = 1.2 kg·m⁻³)
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