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Airplane Longitudinal Stability, Aerospace Engineering Lecture 52
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Aerospace Engineering Lectures - Airplane Longitudinal Stability, Aerospace Engineering Lecture 52

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Longitudinal static stability of an airplane and the reason why a horizontal tail or a canard is needed in the aircraft is explained. The main forces and moments on the airplane in pitching motion are outlined and the concepts of absolute angle of attack, trim condition, and the criteria for longitudinal static stability of airplanes is discussed. #aerospaceengineering #gateaerospaceengineering #aerodynamics #flight

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