Comparison of scramjet and shcramjet propulsion for an hypersonic waverider configuration

44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2008, Pages

  Couture, D ^a,d   DeChamplain, A ^a,d   Stowe, R A ^b,e   Harris, P G ^b,e   Halswijk, W H C ^c   Moerel, J L P A ^c  

^a UNIVERSITÉ LAVAL   (Canada)

^b DEFENCE RESEARCH AND DEVELOPMENT CANADA VALCARTIER   (Canada)

^c TNO   (Netherlands)

^d Mechanical Engineering Department   (Canada)

^e Propulsion Group   (Canada)

Author keywords

[No Author keywords available]

Indexed keywords

AIR FUEL MIXTURES; AIR TEMPERATURE; AIRBREATHING APPLICATIONS; COMBUSTION EFFICIENCIES; COMPUTATIONAL TOOLS; DESIGN CONFIGURATIONS; DESIGN TOOL; DETONATION WAVES; FLIGHT SPEED; FUEL MIXING; HYPERSONIC SPEED; MASS-LIMITED; PERFORMANCE PARAMETERS; PRELIMINARY DESIGN; PRESSURE RECOVERY; SHOCK INDUCED COMBUSTION; SUBMODELS; WAVERIDER CONFIGURATION;

AERODYNAMICS; AIR INTAKES; COMBUSTION CHAMBERS; DESIGN; FUELS; IGNITION; MACH NUMBER; OPTIMIZATION; PROPULSION; VEHICLES;

HYPERSONIC VEHICLES;

EID: 77957850620     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (15)

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