Email this article 
Influence of the turbine ignition, flame tube suspension and nozzles on the combustion chamber characteristics
- Authors: Matveev S.G.1, Orlov M.Y.1, Zubrilin I.A.1
-
Affiliations:
- Samara State Aerospace University
- Issue: Vol 12, No 3-1 (2013): Vestnik SSAU
- Pages: 156-162
- Section: ISSUE WITHOUT SECTION
- URL: https://journals.ssau.ru/vestnik/article/view/74
- DOI: https://doi.org/10.18287/1998-6629-2013-0-3-1(41)-156-162
- ID: 74
Cite item
Full Text
Abstract
The paper presents a mathematical model of the working process of a gas turbine engine combustion chamber that makes it possible to take into account the effect of the flame tube suspension, ignition and turbine nozzles on the working process of the combustion chamber and to estimate the effect.
About the authors
S. G. Matveev
Samara State Aerospace University
Author for correspondence.
Email: pfu@ssau.ru
Candidate of Technical Science
Associate Professor of the Department of Heat Engineering and Heat Engines
Russian FederationM. Yu. Orlov
Samara State Aerospace University
Email: adler65@mail.ru
Candidate of Technical Science
Associate Professor of the Department of Heat Engineering and Heat Engines
Russian FederationI. A. Zubrilin
Samara State Aerospace University
Email: zubrilin416@mail.ru
Laboratory Engineer
Russian FederationReferences
Supplementary files
