Performance of a dual-mode combustor with multi-staged fuel injection

40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2004, Pages

  Kobayashi, Kan ^a,b   Tomioka, Sadatake ^a,b   Kato, Kanenori ^a,c   Murakami, Atsuo ^a,c   Kudo, Kenji ^a,c   Mitani, Tohru ^a,c  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^b Engine System Team   (Japan)

^c Engine System Team

Author keywords

[No Author keywords available]

Indexed keywords

FUEL INJECTION; FUELS; FUNCTIONS; NOZZLES; PROPULSION; RAMJET ENGINES; STAGES;

COMBUSTION EFFICIENCIES; CROSS SECTIONAL AREA; EQUIVALENCE RATIOS; SCRAMJET COMBUSTORS; STAGED FUEL INJECTIONS; THRUST INCREMENT; TOTAL TEMPERATURES; TOTAL-PRESSURE LOSS;

COMBUSTORS;

EID: 85088689626     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-3482     Document Type: Conference Paper

References (11)

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