In pilot's formula of lift, higher AOA is equal to _____.

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Multiple Choice

In pilot's formula of lift, higher AOA is equal to _____.

Explanation:
Higher angle of attack raises the lift coefficient, so the wing can produce the same lift at a lower dynamic pressure. Since lift roughly equals ½ ρ V^2 S Cl, if you increase Cl by increasing the angle of attack while keeping the same weight (lift needed), the speed can be reduced to keep L the same. In other words, for a given amount of lift, boosting angle of attack lets you fly slower. (Just remember that too high an angle of attack can lead to a stall, where lift drops instead of increasing.)

Higher angle of attack raises the lift coefficient, so the wing can produce the same lift at a lower dynamic pressure. Since lift roughly equals ½ ρ V^2 S Cl, if you increase Cl by increasing the angle of attack while keeping the same weight (lift needed), the speed can be reduced to keep L the same. In other words, for a given amount of lift, boosting angle of attack lets you fly slower. (Just remember that too high an angle of attack can lead to a stall, where lift drops instead of increasing.)

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