Suppression of premature ignition in the pre-mixed inlet flow of a shcramjet

39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2003, Pages

  Schwartzentruber, Thomas E ^a   Sislian, Jean P ^a   Parent, Bernard ^b  

^a UNIVERSITY OF TORONTO   (Canada)

^b Seoul National University   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

ATMOSPHERIC THERMODYNAMICS; BOUNDARY LAYERS; FLOW FIELDS; HYDROGEN; MIXING; PROPULSION; REACTION KINETICS; TURBULENCE MODELS;

BACKWARD FACING STEP; FRICTIONAL FORCES; GLOBAL EQUIVALENCE RATIO; INLET CONFIGURATION; K-OMEGA TURBULENCE MODEL; MIXING EFFICIENCY; PREMATURE IGNITION; SHOCK INDUCED COMBUSTION;

IGNITION;

EID: 85086494575     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-5187     Document Type: Conference Paper

References (22)

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