학술논문
Modeling the Combustion Chamber Dynamics of Selectable-Thrust Rocket Motors
Document Type
Conference
Source
2010 DoD High Performance Computing Modernization Program Users Group Conference High Performance Computing Modernization Program Users Group Conference (HPCMP-UGC), 2010 DoD. :177-183 Jun, 2010
Subject
Language
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.