Modeling of Radiation Heat Transfer in Liquid Rocket Engines
Modeling of Radiation Heat Transfer in Liquid Rocket Engines
Modeling of Radiation Heat Transfer in Liquid Rocket Engines
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Conclud<strong>in</strong>g Remarks• The effects <strong>of</strong> gas and surface radiation onthe wall temperature, coolant pressure,temperature and Mach number werestudied• The results presented demonstrate thatalthough the <strong>in</strong>crease <strong>in</strong> heat flux due toradiation is small, it can have a significanteffect on the wall temperature and coolantflow characteristics
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