Title: Modeling the Combustion Chamber Dynamics of Selectable-Thrust Rocket Motors
Abstract: Challenge Project C4C is dedicated to developing and applying high-performance computing capabilities to accelerate the development of hypergolic and hybrid rocket engine concepts. Computational fluid dynamics is employed to model chemically-reacting flows within engine combustion chambers, and computational chemistry is employed to characterize propellant physical and reactive properties. Accomplishments are presented and discussed.
Publication Year: 2010
Publication Date: 2010-06-01
Language: en
Type: article
Indexed In: ['crossref']
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