Modeling the Combustion Chamber Dynamics of Selectable-Thrust Rocket Motors
2010
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.
Keywords:
- Correction
- Source
- Cite
- Save
- Machine Reading By IdeaReader
6
References
0
Citations
NaN
KQI