Effects of ring groove and duty cycle on plasma actuator performance in high speed jets

49th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition

Volumn , Issue , 2011, Pages

  Hahn, C ^a   Kearney Fischer, M ^a   Samimy, M ^a  

^a OHIO STATE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATION MECHANISM; CONTROL MECHANISM; CURRENT TRACES; DUTY CYCLES; HIGH-SPEED JET; INNER SURFACES; MIXING ENHANCEMENT; NOISE CONTROL APPLICATIONS; NOISE RADIATIONS; NOZZLE EXITS; NOZZLE EXTENSION; PARTICLE IMAGE VELOCIMETRIES; PLASMA ACTUATOR; PLASMA ARC; PLASMA FORMATIONS; RING GROOVES; SCHLIEREN IMAGE; SUPERSONIC JETS;

ACOUSTIC VARIABLES CONTROL; ACTUATORS; AEROSPACE ENGINEERING; NOZZLES; PLASMAS; RADIATION EFFECTS; REYNOLDS NUMBER; VELOCITY MEASUREMENT;

SUPERSONIC AERODYNAMICS;

EID: 82555181281     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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