Injection and Mixing Processes in High-Pressure Liquid Oxygen/Gaseous Hydrogen Rocket Combustors
Author:
Affiliation:
1. DLR, German Aerospace Research Center, Lampoldshausen, 74239 Hardthausen, Germany
2. National Aerospace Laboratory, Kakuda, Miyagi 981-1525, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.5647
Reference8 articles.
1. Coaxial atomization of a round liquid jet in a high speed gas stream: A phenomenological study
2. Propellant injection in a liquid oxygen/gaseous hydrogen rocket engine
3. Atomization and Breakup of Cryogenic Propellants Under High-Pressure Subcritical and Supercritical Conditions
4. Rocket engine coaxial injector liquid/gas interface flow phenomena
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