Large Eddy Simulation of Supercritical Mixing and Combustion for Rocket Applications
Author:
Affiliation:
1. Stanford University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-0138
Reference47 articles.
1. Atomization and Breakup of Cryogenic Propellants Under High-Pressure Subcritical and Supercritical Conditions
2. Supercritical nitrogen free jet investigated by spontaneous Raman scattering
3. Visual characteristics and initial growth rates of round cryogenic jets at subcritical and supercritical pressures
4. EXPERIMENTAL STUDIES OF HIGH-PRESSURE CRYOGENIC FLAMES ON THE MASCOTTE FACILITY
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