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

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