Numerical Investigation of Gaseous Hydrogen and Liquid Oxygen Combustion under Subcritical Condition
Author:
Affiliation:
1. Sharif University of Technology, Azadi Ave., P.O. Box 11365-11155, Tehran 1458889694, Iran
Publisher
American Chemical Society (ACS)
Subject
Energy Engineering and Power Technology,Fuel Technology,General Chemical Engineering
Link
https://pubs.acs.org/doi/pdf/10.1021/acs.energyfuels.9b02050
Reference71 articles.
1. Behavior of a Liquid Jet near the Thermodynamic Critical Region
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3. Propellant injection in a liquid oxygen/gaseous hydrogen rocket engine
4. INJECTION OF FLUIDS INTO SUPERCRITICAL ENVIRONMENTS
5. Atomization and Breakup of Cryogenic Propellants Under High-Pressure Subcritical and Supercritical Conditions
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