Flow Control over NACA 23012 Airfoil Model by Surface HF Plasma Actuator
50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
01.01.2012
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Flow Control over NACA 23012 Airfoil Model by Surface HF Plasma Actuator
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