Journal of Aeronautics & Aerospace Engineering

Journal of Aeronautics & Aerospace Engineering
Open Access

ISSN: 2168-9792

+32466902144

Aircraft Flight Mechanics

Flight mechanics is the application of Newton’s laws (F=ma and M=Iα) to the study of vehicle trajectories (performance), stability, and aerodynamic control. There are two basic problems in airplane flight mechanics: airplane performance, stability and control characteristics and performance, stability, and control characteristics, The latter is called airplane sizing and is based on the definition of a standard mission profile. For commercial airplanes including business jets, the mission legs are take-off, climb, cruise, descent, and landing.

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