Cargando…
Numerical methods in aerospace : civil aviation and space exploration /
Transonic flutter and active flap control, in two dimensions, are simulated by coupling independent structural dynamic and inviscid aerodynamic models, in the time domain. A flight control system, to actively control the trailing edge flap motion, has also been incorporated and, since this requires...
| Clasificación: | Libro Electrónico |
|---|---|
| Autor principal: | |
| Formato: | Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Bradford, England :
Emerald Group,
2004.
|
| Colección: | International journal of numerical methods for heat & fluid flow ;
v. 14, no. 4. |
| Temas: | |
| Acceso en línea: | Texto completo |
| Sumario: | Transonic flutter and active flap control, in two dimensions, are simulated by coupling independent structural dynamic and inviscid aerodynamic models, in the time domain. A flight control system, to actively control the trailing edge flap motion, has also been incorporated and, since this requires perfect synchronisation of fluid, structure and control signal, the ''strong'' coupling approach is adopted. The computational method developed is used to perform transonic aeroelastic and aeroservoelastic calculations in the time domain, and used to compute stability (flutter) boundaries of 2D wing. |
|---|---|
| Descripción Física: | 1 online resource (167 pages) |
| Bibliografía: | Includes bibliographical references. |
| ISBN: | 1845447379 9781845447373 |