Thermodynamically compatible conservation laws in the model of heat conducting radiating gas
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Thermodynamic compatibility of the mass, momentum, and energy conservation laws that describe the motion of heat conducting gas in the presence of radiation heat exchange is considered. The study is based on the one-velocity two-component mathematical model of continuous compressible medium with the gas and radiation components. The work uses experimental data for radiation and other experimental data of modern physics.
Keywordsconservation laws radiating heat conducting gas pressure of the radiation component thermodynamics of gas turbine engine
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