About Calculation of Combined Cooling Systems for Propulsion Engines
- Авторы: Borisov D.M.1, Shuraev Y.A.1, Mironov V.V.1
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Учреждения:
- Federal State Unitary Enterprise State Scientific Center Keldysh Research Center
- Выпуск: Том 65, № 13 (2018)
- Страницы: 1024-1028
- Раздел: Article
- URL: https://journals.rcsi.science/0040-6015/article/view/173166
- DOI: https://doi.org/10.1134/S0040601518130049
- ID: 173166
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Аннотация
A numerical method is proposed for solving conjugate heat transfer problems as applied for calculation of combined cooling systems for combustion chambers of propulsion systems. A procedure is presented for joint calculation of temperature conditions of gaseous cooling film and cooling system elements in the entire cross-section of a combustion chamber, including the inner wall material. The numerical results and their verification are presented.
Об авторах
D. Borisov
Federal State Unitary Enterprise State Scientific Center Keldysh Research Center
Автор, ответственный за переписку.
Email: borisovdm62@mail.ru
Россия, Moscow, 125438
Y. Shuraev
Federal State Unitary Enterprise State Scientific Center Keldysh Research Center
Email: borisovdm62@mail.ru
Россия, Moscow, 125438
V. Mironov
Federal State Unitary Enterprise State Scientific Center Keldysh Research Center
Email: borisovdm62@mail.ru
Россия, Moscow, 125438
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