Simulation of a supersonic jet controlled by plasma actuators by the CESE method

Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting

Volumn 6, Issue , 2006, Pages 3775-3784

  He, H ^a,b,c   Yu, S T J ^a,b,c   Jou, G ^a,b,c   Adamovich, I ^a,b,c   Samimy, M ^a,b,c  

^a OHIO STATE UNIVERSITY   (United States)

^b Department of Mechanical Engineering ^*

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CONSERVATION ELEMENT AND SOLUTION ELEMENT (CESE); PLASMA ACTUATORS; SUPERSONIC JET CONTROLLED;

ACTUATORS; BOUNDARY CONDITIONS; COMPUTER SIMULATION; EULER EQUATIONS; MACH NUMBER; PLASMA DEVICES;

SUPERSONIC AERODYNAMICS;

EID: 34250873251     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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