Simulation of LOx/GH2 single coaxial injector at high pressure conditions
Author:
Affiliation:
1. German Aerospace Center (DLR)
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2017-4765
Reference52 articles.
1. Thermophysical characteristics of shear-coaxial LOX–H2 flames at supercritical pressure
2. Supercritical (and subcritical) fluid behavior and modeling: drops, streams, shear and mixing layers, jets and sprays
3. THEORY, MODELING AND ANALYSIS OF TURBULENT SUPERCRITICAL MIXING
4. MIXING AND COMBUSTION OF CRYOGENIC OXYGEN-HYDROGEN SHEAR-COAXIAL JET FLAMES AT SUPERCRITICAL PRESSURE
5. INJECTION OF FLUIDS INTO SUPERCRITICAL ENVIRONMENTS
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