Investigation of the loop combustion chamber
- Авторы: Davydov N.V.1, Mingazov B.G.1, Sychenkov V.A.1, Mukhametgaleev T.K.1
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Учреждения:
- Tupolev Kazan National Research Technical University
- Выпуск: Том 60, № 3 (2017)
- Страницы: 406-411
- Раздел: Aircraft and Rocket Engine Theory
- URL: https://journals.rcsi.science/1068-7998/article/view/230197
- DOI: https://doi.org/10.3103/S1068799817030126
- ID: 230197
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Аннотация
As a result of the experimental-theoretical study of the loop (countercurrent) combustion chamber of the gas turbine engine, the data and theoretical dependences are obtained on the change in the combustion completeness and combustion temperature in various operating modes.
Об авторах
N. Davydov
Tupolev Kazan National Research Technical University
Email: vsychenkov@mail.ru
Россия, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
B. Mingazov
Tupolev Kazan National Research Technical University
Email: vsychenkov@mail.ru
Россия, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
V. Sychenkov
Tupolev Kazan National Research Technical University
Автор, ответственный за переписку.
Email: vsychenkov@mail.ru
Россия, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
T. Mukhametgaleev
Tupolev Kazan National Research Technical University
Email: vsychenkov@mail.ru
Россия, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
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