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Publikováno v:
Engineering Applications of Computational Fluid Mechanics, Vol 15, Iss 1, Pp 1134-1146 (2021)
The liquid rocket propellant burns inadequately in the combustion chamber; therefore, the exhaust gas reacts with oxygen and the heat that was generated, which in turn affects the thermal environment. By using finite-rate chemical kinetics and discre
Externí odkaz:
https://doaj.org/article/a75a4b120c9c4158800c3536ed36a68a
