Control and stability of aircraft / W. J. Duncan
Tipo de material:
TextoDetalles de publicación: Cambridge : John Wright & Sons Ltd., 1952, 1959Descripción: 384 pTema(s):
Contenidos:
Introductory survey - Elementary machanics of flight - The equations of motion of rigid aircraft - Methods for solving the dynamical equations and for investigating stability - Longitudinal-symmetric motion - Lateral-antisymmetric motion - Flat controls in general - The measurement of aerodynamic derivatives - Controls for roll, pitch and yaw - Static stability - Stalling and the spin - The influence of distortion of the structure - The influence of the compressibility of the air - Flaps for landing and take-off - Sundry topics
Libro
| Biblioteca actual | Signatura topográfica | Estado | Fecha de vencimiento | Código de barras | |
|---|---|---|---|---|---|
| Koha Ingenieria | 531.373.2-537 DUN-Bloque 7 (Navegar estantería(Abre debajo)) | Disponible | A0327 | ||
| Koha Ingenieria | 531.373.2-537 DUN-Bloque 7 (Navegar estantería(Abre debajo)) | Disponible | A0328 |
Introductory survey - Elementary machanics of flight - The equations of motion of rigid aircraft - Methods for solving the dynamical equations and for investigating stability - Longitudinal-symmetric motion - Lateral-antisymmetric motion - Flat controls in general - The measurement of aerodynamic derivatives - Controls for roll, pitch and yaw - Static stability - Stalling and the spin - The influence of distortion of the structure - The influence of the compressibility of the air - Flaps for landing and take-off - Sundry topics
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