What is it about?
Wall heat transfer analysis are of primary importance in liquid rocket engine design. The contribution of radiative heat flux is evaluated for two pairs of propellants (hydrogen/oxygen and methane/oxygen). Operating conditions where its role becomes importance are identified and a tool for quick preliminary evaluation is proposed.
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This page is a summary of: Numerical Investigation on Radiative Heat Loads in Liquid Rocket Thrust Chambers, Journal of Propulsion and Power, September 2019, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.b37536.
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