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.
Related Journals of Aircraft Flight Mechanics
,International Journal of Advancements in Technology Journal of Aircraft,International Journal of Sustainable Aviation, International Journal of Aerospace Innovations,International Journal of Applied Aviation Studies,CEAS Aeronautical Journal.