Computational Analysis of the Control Authority of Plasma Actuators for Airfoil Flows at Low Angle of Attack
AIAA Scitech 2020 Forum
2020-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
SEPARATION CONTROL ON HIGH ANGLE OF ATTACK AIRFOIL USING PLASMA ACTUATORS
British Library Conference Proceedings | 2003
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Tema Archiv | 2004
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