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...
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) |
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