Heat Flux Evaluation in Oxygen/Methane Thrust Chambers by RANS Approach
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Publisher
American Institute of Aeronautics and Astronautics
Reference21 articles.
1. Hot-Gas-Side Heat Transfer Characteristics of a Ribbed Combustor
2. Shear and Swirl Coaxial Injector Studies of LOX/GCH4 Rocket Combustion Using Non-Intrusive Laser Diagnostics
3. Transcritical oxygen/transcritical or supercritical methane combustion
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1. Heat Transfer and Combustion Simulation of Seven-Element O2/CH4 Rocket Combustor;Journal of Propulsion and Power;2019-11
2. Review on film cooling of liquid rocket engines;Propulsion and Power Research;2018-03
3. Coupled numerical simulation of combustion and regenerative cooling in LOX/Methane rocket engines;Applied Thermal Engineering;2016-08
4. Numerical Study of Heat Transfer in Film Cooled Thrust Chambers;48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2012-07-30
5. Coupled Heat Transfer Analysis in Regeneratively Cooled Thrust Chambers;48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2012-07-30
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