Simulated fuel injection through a wedge-shaped orifice into supersonic flow

31st Joint Propulsion Conference and Exhibit

Volumn , Issue , 1995, Pages

  Barber, M J ^a   Roe, L A ^b   Schetz, J A ^c  

^a France Compressor Products   (United States)

^b UNIVERSITY OF ARKANSAS   (United States)

^c VIRGINIA POLYTECHNIC INSTITUTE AND STATE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; COMBUSTORS; FUEL INJECTION; GEOMETRY; HEAT TRANSFER; HELIUM; ORIFICES; PROPULSION;

BOUNDARY-LAYER SEPARATION; CIRCULAR ORIFICES; GEOMETRIC DIFFERENCE; HELIUM CONCENTRATIONS; INJECTION SCHEMES; PROBE MEASUREMENTS; SCRAMJET COMBUSTORS; SUPERSONIC COMBUSTORS;

HYDROGEN FUELS;

EID: 84964437999     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1995-2559     Document Type: Conference Paper

References (16)

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