Numerical Study of Flow Separation Control over a OA209 Airfoil Using Deployable Vortex Generator
49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
01.01.2011
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
NUMERICAL STUDY OF FLOW SEPARATION CONTROL OVER A OA209 AIRFOIL USING DEPLOYABLE VORTEX GENERATOR
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