Email this article Study of flame stabilization in a model gas turbine combustor
- Authors: Mingazov B.G.1, Baklanov A.V.1
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Affiliations:
- Tupolev Kazan National Research Technical University
- Issue: Vol 59, No 3 (2016)
- Pages: 408-413
- Section: Aircraft and Rocket Engine Design and Development
- URL: https://journal-vniispk.ru/1068-7998/article/view/229804
- DOI: https://doi.org/10.3103/S1068799816030181
- ID: 229804
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Abstract
The paper reports the results of experimental studies and numerical calculations of the flame stabilization process in the model gas turbine combustor. The mathematical model of the process in the combustor is presented. Using this model, the main parameters of combustors with different ratios of total area of the holes in the combustion zone to total area of all holes, are determined.
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About the authors
B. G. Mingazov
Tupolev Kazan National Research Technical University
Email: andreybaklanov@bk.ru
Russian Federation, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
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
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