Computational and experimental analysis of mach 5 air flow over a cylinder with a nanosecond pulse discharge

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

Volumn , Issue , 2012, Pages

  Bisek, Nicholas J ^a   Poggie, Jonathan ^a   Nishihara, Munetake ^b   Adamovich, Igor ^b  

^a WRIGHT PATTERSON AIR FORCE BASE   (United States)

^b Ohio State University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIR FLOW; COMPRESSION WAVES; COMPUTATIONAL STUDIES; CYLINDER SURFACE; DIELECTRIC BARRIER DISCHARGE PLASMAS; DIELECTRIC BARRIER DISCHARGES; DISCHARGE PULSE; EXPERIMENTAL ANALYSIS; HIGH-FIDELITY MODELING; LOCAL TEMPERATURE; LOW TEMPERATURES; NANOSECOND PULSE; PHENOMENOLOGICAL MODELS; PULSE SOURCES; REDUCED ORDER; SCHLIEREN PHOTOGRAPHY; SHOCK-SHOCK INTERACTIONS; STAND-OFF DISTANCE (SOD); THERMALIZATION; THREE DIMENSIONAL EFFECT; THREE DIMENSIONAL SIMULATIONS; THREE-DIMENSIONAL COMPRESSION; TIME-SCALES; TWO-DIMENSIONAL SIMULATIONS;

ACTUATORS; AEROSPACE ENGINEERING; CYLINDERS (SHAPES); DIELECTRIC DEVICES; EXHIBITIONS; EXPERIMENTS; FLOW CONTROL; SHOCK WAVES; SURFACE PROPERTIES; THREE DIMENSIONAL;

THREE DIMENSIONAL COMPUTER GRAPHICS;

EID: 84872406620     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2012-186     Document Type: Conference Paper

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