Создание модельного отсека камеры сгорания с имитацией стенки жаровой трубы для испытаний авиационных воспламенителей

Abstract

This work presents a universal model combustion chamber section with simulation of the flame tube wall designed for testing aviation igniters. The setup allows reproduction of key ignition processes and provides data on the characteristics of various igniter designs. The design process of the section is described, and results of three-dimensional modeling and experimental analysis, including determination of ignition limits under atmospheric conditions, are presented.