Lift Formula
Lift = CL x ½ p V2 (squared) S CL is the co-efficient of lift (AoA) p (rho) is the air density V (velocity) The airspeed S is the surface area of the wing In simple terms, L = AoA x Airspeed
Definition: Lift Formula
Lift = CL x ½ p V2 (squared) S CL is the co-efficient of lift (AoA) p (rho) is the air density V (velocity) The airspeed S is the surface area of the wing In simple terms, L = AoA x Airspeed
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