Rectilinear uniform gas flow with thermal efficiency in propulsion equipment of aircrafts
Автор: Tolstopyatov M.I., Zuev A.A., Kishkin A.A., Zhuikov D.A., Nazarov V.P.
Журнал: Сибирский аэрокосмический журнал @vestnik-sibsau
Рубрика: Авиационная и ракетно-космическая техника
Статья в выпуске: 4 (44), 2012 года.
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The article considers a model of distribution of thermal and dynamic boundary layers distribution in the process of turbulent flow of the gas stream. Expression for determination of energy thickness is presented and expression for the determination of local thermal efficiency coefficient in the form of Stanton criterion. Comparative analysis of the theories of different authors is presented as well.
Turbulent flow, boundary layer, heat exchange, thermal efficiency coefficient
Короткий адрес: https://sciup.org/148176888
IDR: 148176888
