Local heat transfer parameters in the areas of the developing temperature boundary layer in the cavities of gas turbines
Автор: Zuev A.A., Arngold A.A., Falkova E.V., Tolstopyatov M.I., Dubynin P.A.
Журнал: Сибирский аэрокосмический журнал @vestnik-sibsau
Рубрика: Авиационная и ракетно-космическая техника
Статья в выпуске: 3 т.23, 2022 года.
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In this work, an analytical determination of the local heat transfer coefficient in the planes of rotation of gas turbines is carried out using an affine-like model for the distribution of temperature and dynamic spatial boundary layers with a convective component (at Pr
Rotational motion of the flow, gas cavities of turbopump unit, affine-like model, energy loss thickness equations, heat transfer coefficient
Короткий адрес: https://sciup.org/148325780
IDR: 148325780 | DOI: 10.31772/2712-8970-2022-23-3-437-450
