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Analysis of combustion models applicability for designing combustion chamber with a large number of nozzles
- Authors: Mingazov B.G.1, Yavkin V.B.1, Sabirzyanov A.N.1, Baklanov A.V.2
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Affiliations:
- Kazan State Technical University
- Kazan Research National Technical University named after A.N. Tupolev - KAI
- Issue: Vol 10, No 5 (2011)
- Pages: 208-214
- Section: ISSUE WITHOUT SECTION
- URL: https://journals.ssau.ru/vestnik/article/view/2761
- DOI: https://doi.org/10.18287/2541-7533-2011-0-5(29)-208-214
- ID: 2761
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Abstract
Applications of models for predicting the parameters of gas-turbine engine combustion chamber process are discussed in the paper. Characteristic simulation results for different models ofcombustion are presented.
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About the authors
B. G. Mingazov
Kazan State Technical University
Author for correspondence.
Email: ming@adeu.kstu-kai.ru
Doctor of Technical Sciences, Professor
Head of the Department of Aircraft Engines and Power Plants
Russian FederationV. B. Yavkin
Kazan State Technical University
Email: vb.yavkin@gmail.com
Candidate of Technical Sciences
Associate Professor of the Department of Aircraft Engines and Power Plants
Russian FederationA. N. Sabirzyanov
Kazan State Technical University
Email: sabirzan@sd.kstu-kai.ru
Candidate of Technical Sciences
Associate Professor of the Department of Special Engines
Russian FederationA. V. Baklanov
Kazan Research National Technical University named after A.N. Tupolev - KAI
Email: andreybaklanov@bk.ru
Post-graduate Student of the Department of Aircraft Engines and Power Plants
Russian FederationReferences
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