Math help please.If mass equals to 58,000 kilograms with a wing surface area of 123 m² flies at altitude of 8 kilometres with an airspeed ?
Of 800 kilometres Per hour. What is the lift coefficient in this flight condition.?
- JosephLv 78 months agoFavorite Answer
L = ClqS. q = 1/2 (rho) v^2. L is lift, Cl is lift coefficient, q is dynamic pressure, S is the area of the wing and v is velocity.
Find out what the air density is at 8000 meters and solve for Cl. Simple algebra! Pay attention to the units.
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