If the velocity of the relative wind increases, what happens to lift for a given airfoil at a fixed angle of attack?

Prepare for the Theory of Rotary Wing Flight Test. Study with multiple choice questions; each has hints and explanations to help you get ready for your exam.

Multiple Choice

If the velocity of the relative wind increases, what happens to lift for a given airfoil at a fixed angle of attack?

Explanation:
Increasing the relative wind speed raises the dynamic pressure on the wing, and lift scales with that dynamic pressure. For an airfoil, lift is L = q S CL, where q = 1/2 ρ V^2. At a fixed angle of attack, CL stays roughly the same, so doubling the wind speed makes q increase by a factor of four, and lift increases accordingly (approximately four times as much). This holds as long as you’re not near stall, where CL would start to fall and lift wouldn’t keep rising with speed.

Increasing the relative wind speed raises the dynamic pressure on the wing, and lift scales with that dynamic pressure. For an airfoil, lift is L = q S CL, where q = 1/2 ρ V^2. At a fixed angle of attack, CL stays roughly the same, so doubling the wind speed makes q increase by a factor of four, and lift increases accordingly (approximately four times as much). This holds as long as you’re not near stall, where CL would start to fall and lift wouldn’t keep rising with speed.

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