Shockwave induced turbulent boundary layer separation control with plasma actuators

47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition

Volumn , Issue , 2009, Pages

  Kalra, Chiranjeev S ^a   Zaidi, Sohail H ^a   Shneider, Mikhail N ^a   Miles, Richard B ^a  

^a Princeton University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACETONE; ACTUATORS; BOUNDARY LAYER FLOW; FLOW STRUCTURE; IMAGE PROCESSING; PLASMA CONFINEMENT; WIND TUNNELS;

BOUNDARY LAYER INTERACTION; BOUNDARY LAYER SEPARATION CONTROL; BOUNDARY LAYER STRUCTURE; INTERACTION REGION; PRINCETON UNIVERSITY; SEPARATION CONTROL; STATIC PRESSURE MEASUREMENTS; TURBULENT BOUNDARY LAYERS;

BOUNDARY LAYERS;

EID: 78549252458     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2009-1002     Document Type: Conference Paper

References (12)

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