Тип публикации: статья из журнала

Год издания: 2016

Идентификатор DOI: 10.1007/s10891-016-1495-4

Ключевые слова: acoustic vibrations, ignition, stabilization of a flame, supersonic flow, swirling flow

Аннотация: Results of numerical simulation and experimental investigation of the working process of a vortex igniter-stabilizer are presented. It is shown that a high-temperature pulsating swirling jet provides reliable ignition of a fuel and its stable combustion at a main-flow velocity of up to 2.5 M.

Журнал: Journal of Engineering Physics and Thermophysics

Выпуск журнала: Т. 89, № 5

Номера страниц: 1325-1332

ISSN журнала: 10620125

Место издания: Минск

Издатель: Springer New York Consultants Bureau

• Piralishvili S.A. (P.A. Solov′ev Rybinsk State Aviation Technical University)
• Vereshchagin I.M. (P.A. Solov′ev Rybinsk State Aviation Technical University)
• Markovich D.M. (S. S. Kutateladze Institute of Thermophysics,Siberian Branch of the Russian Academy of Sciences)
• Lobasov A.S. (S. S. Kutateladze Institute of Thermophysics,Siberian Branch of the Russian Academy of Sciences)

• Ядро РИНЦ (eLIBRARY.RU)