On Prediction of Aircraft Trajectory at High Angles of Attack: Preliminary Results for a Pitching Aerofoil
AIAA Modeling and Simulation Technologies Conference and Exhibit
2008-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Aerodynamics of a Pitching Aerofoil at Low Reynolds Numbers
British Library Conference Proceedings | 1997
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