Fundamentals of Supercritical Mixing and Combustion of Cryogenic Propellants
Author:
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/5.9781600866760.0339.0367
Reference60 articles.
1. Propellant injection in a liquid oxygen/gaseous hydrogen rocket engine
2. Atomization and Breakup of Cryogenic Propellants Under High-Pressure Subcritical and Supercritical Conditions
3. Coaxial atomization of a round liquid jet in a high speed gas stream: A phenomenological study
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