Email this article Investigation of the loop combustion chamber
- Authors: Davydov N.V.1, Mingazov B.G.1, Sychenkov V.A.1, Mukhametgaleev T.K.1
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Affiliations:
- Tupolev Kazan National Research Technical University
- Issue: Vol 60, No 3 (2017)
- Pages: 406-411
- Section: 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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Abstract
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.
About the authors
N. V. Davydov
Tupolev Kazan National Research Technical University
Email: vsychenkov@mail.ru
Russian Federation, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
B. G. Mingazov
Tupolev Kazan National Research Technical University
Email: vsychenkov@mail.ru
Russian Federation, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
V. A. Sychenkov
Tupolev Kazan National Research Technical University
Author for correspondence.
Email: vsychenkov@mail.ru
Russian Federation, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
T. Kh. Mukhametgaleev
Tupolev Kazan National Research Technical University
Email: vsychenkov@mail.ru
Russian Federation, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
