Large-eddy simulations of high-pressure shear coaxial flows relevant for H2/O2 rocket engines

Large-eddy simulations of high-pressure shear coaxial flows relevant for H2/O2 rocket engines

The understanding and prediction of transient phenomena inside Liquid Rocket Engines (LREs) have been very difficult because of the many challenges posed by the conditions inside the combustion chamber. This is especially true for injectors involving liquid oxygen LOX and gaseous hydrogen GH₂. A wid...

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Bibliographic Details
Main Author: Masquelet, Matthieu Marc
Published: Georgia Institute of Technology 2013
Subjects:
Combustion
Supercritical
Scaling
LES
LRE
CFD
Computational fluid dynamics
Propulsion systems
Rocket engines
Rocket engines Combustion
Liquid propellant rocket engines
Online Access:http://hdl.handle.net/1853/47522

Internet

http://hdl.handle.net/1853/47522

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