Fundamental studies of cavity-based flameholder concepts for supersonic combustors

Journal of Propulsion and Power

Volumn 17, Issue 1, 2001, Pages 146-153

  Gruber, M R ^a,d   Baurle, R A ^b,d   Mathur, T ^b,d   Hsu, K Y ^c,d  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b Taitech Inc   (United States)

^c Innovative Scientic Solutions   (United States)

^d NONE   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTION; DRAG; FUEL INJECTION; HYDROCARBONS; PRESSURE EFFECTS; SHOCK WAVES; SUPERSONIC FLOW; UNSTEADY FLOW;

AFT RAMP ANGLE; CAVITY BASED FLAMEHOLDERS; CAVITY FLOWS; FLAMEHOLDING; LENGTH TO DEPTH RATIO; SUPERSONIC COMBUSTION RAMJET ENGINE; SUPERSONIC COMBUSTORS;

RAMJET ENGINES;

EID: 0034850130     PISSN: 07484658     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.5720     Document Type: Article

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