Inviscid models of the classic hybrid rocket

40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2004, Pages

  Majdalani, Joseph ^a,b   Vyas, Anand B ^a,c  

^a UNIVERSITY OF TENNESSEE   (United States)

^b Aerospace and Biomedical Engineering ^*  (United States)

^c Marquette University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FUELS; PROPULSION; ROCKETS;

EULER'S EQUATION; EXACT SOLUTION; GASEOUS OXIDIZER; HARMONIC INJECTION; HYBRID ROCKET ENGINES; MATHEMATICAL TREATMENTS; PARALLEL MOTION; VORTICITY DISTRIBUTION;

ENGINES;

EID: 85088685521     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-3474     Document Type: Conference Paper

References (17)

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15. Knuth, W. H., Chiaverini, M. J., Sauer, J. A., and Gramer, D. J., "Solid-Fuel Regression Rate Behavior of Vortex Hybrid Rocket Engines," Journal of Propulsion and Power, Vol. 18, No. 3, 2002, pp. 600-609.
16. Karabeyoglu, M. A., Altman, D., and Cantwell, B. J., "Combustion of Liquifying Hybrid Propellants: Part 1, General Theory," Journal of Propulsion and Power, Vol. 18, No. 3, 2002, pp. 610-620.
17. Karabeyoglu, M. A., and Cantwell, B. J., "Combustion of Liquifying Hybrid Propellants: Part 2, Stability of Liquid Films," Journal of Propulsion and Power, Vol. 18, No. 3, 2002, pp. 621-630.