Ramjet and scramjet engine cycle analysis for a generic hypersonic vehicle

A Collection of Technical Papers - 14th AIAA/AHI International Space Planes and Hypersonic Systems and Technologies Conference

Volumn 3, Issue , 2006, Pages 2510-2519

  Keshmiri, Shahriar ^a,c   Colgren, Richard ^a,c   Farokhi, Saeed ^a,c   Mirmirani, Maj ^b,c  

^a UNIVERSITY OF KANSAS   (United States)

^b CALIFORNIA STATE UNIVERSITY   (United States)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTORS; COMPUTER SIMULATION; HYPERSONIC AERODYNAMICS; SPACE RESEARCH; SPACECRAFT LANDING; SPACECRAFT PROPULSION;

COMBINED-CYCLE PROPULSION SYSTEM; ENGINE MODELS; SCRAMJET SYSTEM; SPACE LAUNCH MISSIONS;

RAMJET ENGINES;

EID: 33947258886     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2006-8158     Document Type: Conference Paper

References (14)

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3. Curran, E. T., and Stull, F. D., 'The Utilization of Supersonic Combustion Ramjet Systems at Low Mach Number," Aero Propulsion Laboratory, RTD-TDR63-4097, Jan. 1964.
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