Specifying the dimensions of the reverse current area of a 3-D gas-turbine engine combustion chamber model using the ANSYS FLUENT software

Бирюк В. В.; V. V. Biryuk; M. Yu. Orlov; Орлов М. Ю.; I. A. Zubrilin; Зубрилин И. А.; Yu. A. Sinegovskiy; Синеговский Ю. А.; A. V. Krivtsov; Кривцов А. В.

doi:10.18287/2541-7533-2011-0-5(29)-44-48

Specifying the dimensions of the reverse current area of a 3-D gas-turbine engine combustion chamber model using the ANSYS FLUENT software

Authors: Biryuk V.V.¹, Orlov M.Y.¹, Zubrilin I.A.¹, Sinegovskiy Y.A.¹, Krivtsov A.V.¹
Affiliations:
1. Samara State Aerospace University
Issue: Vol 10, No 5 (2011)
Pages: 44-48
Section: ISSUE WITHOUT SECTION
URL: https://journals.ssau.ru/vestnik/article/view/2736
DOI: https://doi.org/10.18287/2541-7533-2011-0-5(29)-44-48
ID: 2736

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Abstract

The paper describes numerical modeling of the reverse current area using a three-dimensional model of an aviation gas turbine engine combustion chamber. The research was carried out at various angles of installing blades in a swirler. Graphs of the twist parameter versus geometrical characteristics of the reverse current area are presented.