Experimental optimization of transverse jet injector geometries for mixing into a supersonic flow

29th AIAA Fluid Dynamics Conference

Volumn , Issue , 1998, Pages 1-24

  Price, Bradford B ^a   Elliot, Gregory S ^a   Ogot, Madara ^a  

^a RUTGERS UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FLUID DYNAMICS; MIXING; NEODYMIUM LASERS; SIMULATED ANNEALING; SUPERSONIC AERODYNAMICS; WIND TUNNELS;

CIRCULAR CROSS-SECTIONS; CROSS SECTIONAL AREA; EQUIVALENT AREAS; EXPERIMENTAL OPTIMIZATION; ND:YAG PULSED LASER; SIMULATED ANNEALING METHOD; SUPERSONIC WIND TUNNEL; TRANSVERSE INJECTION;

FIGHTER AIRCRAFT;

EID: 84959347187     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-3019     Document Type: Conference Paper

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