Отправить статью по E-mail To the Problem of Optimal Thermal Protection of Surfaces in Supersonic Flows
- Авторы: Garaev K.1, Mukhametzyanov I.2
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Учреждения:
- Tupolev Kazan National Research Technical University
- Chistopol Branch “Vostok”
- Выпуск: Том 62, № 1 (2019)
- Страницы: 52-58
- Раздел: Aero- and Gas-Dynamics of Flight Vehicles and Their Engines
- URL: https://journals.rcsi.science/1068-7998/article/view/230826
- DOI: https://doi.org/10.3103/S1068799819010070
- ID: 230826
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Аннотация
The optimization problem of heat and mass transfer in the boundary layer on permeable profiles in supersonic gas flows is considered. Unlike the previous works of this direction, the analytical formula for optimal gas flow through the permeable surface is obtained in the present work, it is more convenient for application in engineering practice. The results of computing experiment are given.
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Об авторах
K. Garaev
Tupolev Kazan National Research Technical University
Email: m.ilshat@mail.ru
Россия, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
I. Mukhametzyanov
Chistopol Branch “Vostok”
Автор, ответственный за переписку.
Email: m.ilshat@mail.ru
Россия, ul. Engel’sa 127a, Chistopol, Tatarstan, 422981
