Computational and experimental study of the two-phase mixing in gas-dynamic ignition system


如何引用文章

全文:

开放存取 开放存取
受限制的访问 ##reader.subscriptionAccessGranted##
受限制的访问 订阅存取

详细

The work is devoted to the determination of main peculiarities of the two-phase mixture formation in the flow duct of the gas-dynamic ignition system. The paper presents a mathematical model and the results of a numerical and experimental investigation of the peculiarities of the unsteady gas flow as well as the processes of the fragmentation and evaporation of droplets in the resonance cavity of the gas-dynamic ignition system. Different configurations of injectors for liquid supply are considered, and the influence of the most significant factors on heat release and concentration of the evaporated liquid in the resonance cavity is investigated. The obtained data may be used for choosing the injectors and the regimes of the liquid fuel supply, which enable one to ensure the stable conditions for igniting two-phase fuel mixtures in the gas-dynamic ignition system.

作者简介

K. Arefyev

Central Institute of Aviation Motor named after P.I. Baranov; Moscow State Technical University named after N.E. Bauman

编辑信件的主要联系方式.
Email: arefyev@ciam.ru
俄罗斯联邦, Moscow; Moscow

A. Voronetsky

Moscow State Technical University named after N.E. Bauman

编辑信件的主要联系方式.
Email: voron@bmstu.ru
俄罗斯联邦, Moscow

S. Suchkov

Moscow State Technical University named after N.E. Bauman

Email: voron@bmstu.ru
俄罗斯联邦, Moscow

M. Ilchenko

Central Institute of Aviation Motor named after P.I. Baranov

Email: voron@bmstu.ru
俄罗斯联邦, Moscow

补充文件

附件文件
动作
1. JATS XML

版权所有 © Pleiades Publishing, Ltd., 2017