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

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.


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

Student

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