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DYNAMICS OF AIRCRAFT FLIGHT

Performance calculations can be classified into three main types: lift, thrust and slope. Firstly, since the lift profile is known and unmodifiable from the time an aircraft is designed, the mass at a given speed or the speed at a given mass must be determined. Then, once the thrust of the engines a...

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Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: LOUIS, GILLES
Formato: Electrónico eBook
Idioma:Inglés
Publicado: [S.l.] : JOHN WILEY, 2022.
Temas:
Acceso en línea:Texto completo (Requiere registro previo con correo institucional)