The objective of this research was to develop an integrated theoretical and computational framework for treating combustion dynamics of cryogenic and hydrocarbon propellants under conditions representative of contemporary liquid rocket engines.
Theoretical, Numerical, and Experimental Investigations of the Fundamental Processes That Drive Combustion Instabilities in Liquid Rocket Engines
2012
12 pages
Report
No indication
English
Combustion & Ignition , Rocket Engines & Motors , Liquid propellant rocket engines , Simulators , Acoustics , Combustion stability , Computation science , Fuel injectors , Laboratory equipment , Symposia , Briefing charts , Lre(Liquid rocket engine) , Aclres(Actively controlled lre simulator) , Supercritical combustion , Swirl injectors , Acoustic flame interaction , High fidelity modeling , Multiphase flow dynamics , Acoustic models
Three-dimensional analysis of combustion instabilities in liquid rocket engines
Tema Archive | 1993
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