Email this article A technique of gaseous fuel and air mixture quality identification behind the swirl burner of gas turbine engine combustion chamber
- Authors: Baklanov A.V.1, Neumoin S.P.2
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Affiliations:
- Tupolev Kazan National Research Technical University
- AO KMPO
- Issue: Vol 60, No 1 (2017)
- Pages: 90-96
- Section: Aircraft and Rocket Engine Design and Development
- URL: https://journals.rcsi.science/1068-7998/article/view/230004
- DOI: https://doi.org/10.3103/S1068799817010135
- ID: 230004
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Abstract
This paper presents the research results on studying the carbon dioxide concentration fields in a jet behind the swirl burners of various design. A technique of identifying the gaseous fuel and air mixture quality in the jet behind the swirl burners was developed.
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About the authors
A. V. Baklanov
Tupolev Kazan National Research Technical University
Author for correspondence.
Email: andreybaklanov@bk.ru
Russian Federation, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
S. P. Neumoin
AO KMPO
Email: andreybaklanov@bk.ru
Russian Federation, ul. Dement’eva 1, Kazan, Tatarstan, 420036
