Airplane Equation of Motion, Aerospace Engineering Lecture 30
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The equations of motion of an aircraft in flight are derived using Newton's laws, Simplifications to these equations are then made for unaccelerated, level flight where Lift = Weight and Drag = Thrust of the aircraft. The angles defining aircraft flight path, thrust line, and the angle of attack are explained. #aerospaceengineering #gateaerospaceengineering #aircraftperformance #flight
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