2016•Russian AeronauticsRequires access

Study of flame stabilization in a model gas turbine combustor

Б. Г. Мингазов, А. В. Бакланов

Abstract

The paper reports the results of experimental studies and numerical calculations of the flame stabilization process in the model gas turbine combustor. The mathematical model of the process in the combustor is presented. Using this model, the main parameters of combustors with different ratios of total area of the holes in the combustion zone to total area of all holes, are determined.

About this research paper

What this paper is about

Why it matters

OpenAlex reports 3 citations for this work. Citation counts describe recorded attention and do not establish research quality.

Key contribution

A contribution statement is not available in the OpenAlex record.

Method / approach

Method details are not available in the OpenAlex metadata.

Main findings

Findings are not separately available in the OpenAlex metadata.

Limitations

Limitations are not available in the OpenAlex metadata.

Applications

Application details are not available in the OpenAlex metadata.

Available abstract

Key concepts: Combustor, Gas turbines, Combustion, Combustion chamber, Materials science, Nuclear engineering, Process (computing), Mechanics