Theoretical, Numerical, and Experimental Investigations of the Fundamental Processes That Drive Combustion Instabilities in Liquid Rocket Engines
GEORGIA INST OF TECH ATLANTA SCHOOL OF AEROSPACE ENGINEERING
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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.
- Combustion and Ignition
- Liquid Propellant Rocket Engines