Comparison of physical and aerodynamic ramps as fuel injectors in supersonic flow

Journal of Propulsion and Power

Volumn 14, Issue 2, 1998, Pages 135-145

  Fuller, Raymond P ^a,e   Wu, Pei Kuan ^a,d   Nejad, Abdollah S ^b,d   Schetz, Joseph A ^c,e  

^a WRIGHT PATTERSON AIR FORCE BASE   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

^c Bradley Department of Electrical and Computer Engineering   (United States)

^d Kaiser Marquardt   (United States)

^e AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; COMBUSTORS; FLOW INTERACTIONS; JETS; MIXING; PRESSURE DROP; RAMJET ENGINES; REYNOLDS NUMBER; SAMPLING; SUPERSONIC FLOW; VORTEX FLOW;

FLUSH WALL AERODYNAMIC RAMP INJECTORS; MACH NUMBER; SCRAMJET COMBUSTORS;

FUEL INJECTION;

EID: 0032023254     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/2.5278     Document Type: Review

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