Influence of Simplifying a Geometrical Model of the Gas Turbine Engine Combustion Chamber on the Results of Numerical Modeling-Reference-Cited by-同舟云学术

Influence of Simplifying a Geometrical Model of the Gas Turbine Engine Combustion Chamber on the Results of Numerical Modeling

Published:2017-10 Issue:4 Volume:60 Page:575-582
ISSN:1068-7998
Container-title:Russian Aeronautics
language:en
Short-container-title:Russ. Aeronaut.

Author:

Aleksandrov Yu. B.,Sabirzyanov A. N.,Yavkin V. B.

Publisher

Allerton Press

Subject

Aerospace Engineering

Link

http://link.springer.com/content/pdf/10.3103/S1068799817040146.pdf

Reference7 articles.

1. Mingazov B.G. and Baklanov A.V., Study of Flame Stabilization in a Model Gas Turbine Combustor, Izv.Vuz. Av. Tekhnika, 2016, vol. 59, no. 3, pp. 106–110 [Russian Aeronautics (Engl. Transl.), vol. 59, no. 3, pp. 408–413].

2. Kutsenko, Yu.G., Chislennye metody otsenki emissionnykh characteristik kamer sgoraniya gazoturbinnykh dvigatelei (Numerical Methods for Estimation of Emission Characteristics in GTE Combustion Chambers), Ekaterinburg; Perm’: UrO RAN, 2006.

3. Sabirzyanov, A.N., Yavkin, V.B., Aleksandrov, Yu.B., Markushin, A.N., and Baklanov, A.V., Modeling of Emission Characteristics in GTE Combustion Chambers, Vestnik KGTU im. A.N. Tupoleva, 2014, no. 2, pp. 62–70

4. Peeters, T., Numerical Modeling of Turbulence Natural-Gas Diffusion Flames, PhD thesis, Delft Technical University. Delft, 1995.

5. Aleksandrov, Yu.B, Mingazov. B.G., and Tokmovtsev, Yu.V., Software for Automated Processing and Analysis of Gas Dynamics and Combustion Processes in Combustion Chambers of Gas Turbine Engines (Servis 3D), The Certificate on State Registration of the Computer Program no. 2016611856, KNRTU–KAI, 2016.

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