Effect of plasma-based azimuthal mode excitation on supersonic jet flow

5th Flow Control Conference

Volumn , Issue , 2010, Pages

  Gaitonde, D V ^a   Samimy, M ^b  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b The Ohio State University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AXISYMMETRIC; AXISYMMETRIC STRUCTURE; AZIMUTHAL DIRECTION; AZIMUTHAL MODES; CIRCULAR CROSS-SECTIONS; COHERENT STRUCTURE; DOUBLE HELIX; DUTY CYCLES; EXCITATION EVENTS; HAIRPIN-LIKE; HELICAL STRUCTURES; HIGHER MODE; INITIAL STAGES; JET AXIS; NUMBER OF ACTUATORS; PHASE-AVERAGED FLOW; PLASMA ACTUATOR; SHEAR LAYER; SUB-STRUCTURES; SUCCESSIVE RINGS; SUPERSONIC JET FLOW; SURFACE HEATING; TIME-AVERAGED;

ACTUATORS; FLOW CONTROL; SUPERSONIC AERODYNAMICS;

PLASMA DIAGNOSTICS;

EID: 78649527923     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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