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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...

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Détails bibliographiques
Cote:Libro Electrónico
Auteur principal: Keavey, Mike
Format: Électronique eBook
Langue:Inglés
Publié: Bradford, England : Emerald Group, 2004.
Collection:International journal of numerical methods for heat & fluid flow ; v. 14, no. 4.
Sujets:
Accès en ligne:Texto completo