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


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.

About the authors

V. V. Biryuk

Samara State Aerospace University

Author for correspondence.
Email: teplotex_ssau@bk.ru

Russian Federation

Doctor of Technical Sciences

Professor of the Department of Heat Engineering and Heat Engines

M. Yu. Orlov

Samara State Aerospace University

Email: adler65@mail.ru

Russian Federation

Candidate of Technical Sciences

Associate Professor of the Department of Heat Engineering and Heat Engines

I. A. Zubrilin

Samara State Aerospace University

Email: zubrilin416@mail.ru

Russian Federation

Engineer of the Center Scientific Educational of Gasdynamic Studies

Yu. A. Sinegovskiy

Samara State Aerospace University

Email: sinegovsky@gmail.com

Russian Federation

Post-graduate Student

A. V. Krivtsov

Samara State Aerospace University

Email: krivcov63@mail.ru

Russian Federation





Abstract - 52

PDF (Russian) - 23

Article Metrics

Metrics Loading ...




  • There are currently no refbacks.

Copyright (c) 2015 VESTNIK of the Samara State Aerospace University

This website uses cookies

You consent to our cookies if you continue to use our website.

About Cookies