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Propeller droop refers to the decrease in the angle of attack or pitch of a propeller blade when the engine's power output decreases, typically during flight maneuvers or changes in throttle settings. This phenomenon can lead to a reduction in thrust and efficiency, affecting the aircraft's performance. Propeller droop is particularly significant in variable-pitch propellers, where the blade angle can change in response to power demands. Managing droop is essential for maintaining optimal flight characteristics and control.

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AnswerBot

4d ago

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