Investigation of the loop combustion chamber
- Авторлар: Davydov N.V.1, Mingazov B.G.1, Sychenkov V.A.1, Mukhametgaleev T.K.1
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Мекемелер:
- Tupolev Kazan National Research Technical University
- Шығарылым: Том 60, № 3 (2017)
- Беттер: 406-411
- Бөлім: Aircraft and Rocket Engine Theory
- URL: https://journals.rcsi.science/1068-7998/article/view/230197
- DOI: https://doi.org/10.3103/S1068799817030126
- ID: 230197
Дәйексөз келтіру
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.
Авторлар туралы
N. Davydov
Tupolev Kazan National Research Technical University
Email: vsychenkov@mail.ru
Ресей, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
B. Mingazov
Tupolev Kazan National Research Technical University
Email: vsychenkov@mail.ru
Ресей, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
V. Sychenkov
Tupolev Kazan National Research Technical University
Хат алмасуға жауапты Автор.
Email: vsychenkov@mail.ru
Ресей, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
T. Mukhametgaleev
Tupolev Kazan National Research Technical University
Email: vsychenkov@mail.ru
Ресей, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
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