Serpinsky O. S., Frantsuzov M.S

DOI Number XXX-YYY-ZZZ

Conference Number HiSST 2018_3130978

The development of technologies and materials used for high-speed ramjets makes it possible to significantly increase the life of the engine. In this regard, an obligatory element of the combustion chamber design is an active cooling system that provides acceptable values of the temperature of the fire walls. Numerical simulation of the conjugate heat exchange problem allows to predict the thermal state of the walls of the combustion chamber and to reveal physical features

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In Categories: Flight Mechanics, HiSST 2018, Hypersonic Flight Dynamics, Propulsion Systems and Components, Thermal and Energy Management Systems
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