Active Aeroelastic Wing Aerodynamic Model Development and Validation for a Modified F/A-18A

A new aerodynamic model has been developed and validated for a modified F/A-18A used for the Active Aeroelastic Wing (AAW) research program. The goal of the program was to demonstrate the advantages of using the inherent flexibility of an aircraft to enhance its performance. The research aircraft wa...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Cumming, Stephen B., Diebler, Corey G.
Format:	Report
Sprache:	eng
Schlagworte:	Aircraft Design, Testing And Performance
Online-Zugang:	Volltext bestellen
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