Turbofan engine thrust augmentation with pulse detonation aftburners - Nozzle influence -

38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2002, Pages

  Mawid, M A ^a   Park, T W ^a   Sekar, B ^b   Arana, C ^b  

^a Engineering Research and Analysis Company   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CHEMISTRY MODELING; DESIGN CONFIGURATIONS; DIVERGENT NOZZLES; ENGINE PERFORMANCE; EXPERIMENTAL INVESTIGATIONS; IDEAL PERFORMANCE; POWER CONDITIONS; PRELIMINARY ASSESSMENT;

AFTERBURNERS (ENGINE); AFTERBURNERS (OVEN); COMPUTATIONAL FLUID DYNAMICS; DETONATION; ENGINES; NOZZLES; PROPULSION; SEA LEVEL;

PULSE DETONATION ENGINES;

EID: 84896693223     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (16)

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