Experimental study of a nozzle using fluidic counterflow for thrust vectoring

34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 1998, Pages

  Flamm, Jeffrey D ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

NASA; NOZZLES; PROPULSION;

CO-FLOWING STREAMS; COUNTERFLOW THRUST VECTORING; EXPERIMENTAL INVESTIGATIONS; INTERNAL PERFORMANCE; MASS ENTRAINMENT; NASA LANGLEY RESEARCH CENTER; NOZZLE PRESSURE RATIO; THRUST VECTORING;

FIGHTER AIRCRAFT;

EID: 84963787558     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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