Email this article Influence of Simplifying a Geometrical Model of the Gas Turbine Engine Combustion Chamber on the Results of Numerical Modeling
- Authors: Aleksandrov Y.B.1, Sabirzyanov A.N.1, Yavkin V.B.1
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Affiliations:
- Tupolev Kazan National Research Technical University
- Issue: Vol 60, No 4 (2017)
- Pages: 575-582
- Section: Aircraft and Rocket Engine Theory
- URL: https://journal-vniispk.ru/1068-7998/article/view/230305
- DOI: https://doi.org/10.3103/S1068799817040146
- ID: 230305
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Abstract
We studied the geometric models of combustion chambers depending on their simplification. It is shown that the error in calculating the parameters does not exceed 8 % under the constraint of the geometrical model of the gas turbine engine (GTE) combustion chamber by an angular sector with a burner device.
About the authors
Yu. B. Aleksandrov
Tupolev Kazan National Research Technical University
Author for correspondence.
Email: alexwischen@rambler.ru
Russian Federation, ul. Karla Marksa 10, Kazan, 420111 Tatarstan
A. N. Sabirzyanov
Tupolev Kazan National Research Technical University
Email: alexwischen@rambler.ru
Russian Federation, ul. Karla Marksa 10, Kazan, 420111 Tatarstan
V. B. Yavkin
Tupolev Kazan National Research Technical University
Email: alexwischen@rambler.ru
Russian Federation, ul. Karla Marksa 10, Kazan, 420111 Tatarstan
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