A Semi-empirical model of a nanosecond pulsed plasma actuator for flow control simulations with LES

50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition

Volumn , Issue , 2012, Pages

  Gaitonde, D V ^a   Mccrink, M H ^a  

^a OHIO STATE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC SPEED; CONTROL APPLICATIONS; CONTROL SIMULATION; CURRENT MODELS; CYLINDRICAL COMPONENTS; DEPOSITION MODELS; DIELECTRIC BARRIER DISCHARGES; EXPERIMENTAL INVESTIGATIONS; GAUSSIANS; HEATING DISTRIBUTIONS; INDUCED WAVES; PHENOMENOLOGICAL MODELS; POWER INPUT; PULSED PLASMA; QUANTITATIVE FEATURES; SEMIEMPIRICAL MODELS; WAVE SHAPE; WAVE SPEED;

AEROSPACE ENGINEERING; EXHIBITIONS; FLOW CONTROL;

ACTUATORS;

EID: 84872372084     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2012-184     Document Type: Conference Paper

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