Investigation of the loop combustion chamber
- Autores: Davydov N.V.1, Mingazov B.G.1, Sychenkov V.A.1, Mukhametgaleev T.K.1
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Afiliações:
- Tupolev Kazan National Research Technical University
- Edição: Volume 60, Nº 3 (2017)
- Páginas: 406-411
- Seção: 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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Resumo
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.
Sobre autores
N. Davydov
Tupolev Kazan National Research Technical University
Email: vsychenkov@mail.ru
Rússia, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
B. Mingazov
Tupolev Kazan National Research Technical University
Email: vsychenkov@mail.ru
Rússia, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
V. Sychenkov
Tupolev Kazan National Research Technical University
Autor responsável pela correspondência
Email: vsychenkov@mail.ru
Rússia, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
T. Mukhametgaleev
Tupolev Kazan National Research Technical University
Email: vsychenkov@mail.ru
Rússia, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
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