Email this article 
Application of gas dynamics numerical methods for the analysis of nitrogen oxide formation process and choosing low emission combustor design
- Authors: 1 11, 1 11
-
Affiliations:
- JSC «Aviadvigatel», Perm
- Issue: Vol 5, No 1 (2006)
- Pages: 101-112
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/256
- DOI: https://doi.org/10.18287/2541-7533-2006-0-1%20(9)-101-112
- ID: 256
Cite item
Full Text
Abstract
The paper deals with the problems of mathematical modeling of physical and chemical processes in gas-turbine engine combustors. Multicomponent reacting gas flow in a combustor is calculated. Using the results of a series of combustor parametrical calculations a liner design is selected with a minimum level of nitrogen oxide emission.
About the authors
1 1
JSC «Aviadvigatel», Perm
Author for correspondence.
Email: sadohina@ssau.ru
Russian Federation
1 1
JSC «Aviadvigatel», Perm
Email: sadohina@ssau.ru
Russian Federation
References
- Турбулентность / Под. ред. П. Брэдшоу. – М.: Машиностроение, 1980.
- A. A.Westenberg. Comb. Sci. Tech., 4:59, 1971.
- J. Warnatz. NOx Formation in High Temperature Processes. University of Stuttgart, Germany.
- R. W. Schefer, M. Namazian, J Kelly. Combustion Research Facility News, vol. 3, # 4, Sandia, 1991.
- L. D. Smoot, P. J. Smith. NOx Pollutant Formation in a Turbulent Coal System. Coal Combustion and Gasification, p. 373, Plenum, NY, 1985.
- CFX-TASCflow Theory Documentation, AEATechnology, 2002.
Supplementary files
