SIMULATION OF THE WORKING PROCESS OF A SUPERSONIC COMBUSTOR WITH A VORTEX IGNITER-STABILIZER

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-fl ow velocity of up to 2.5 M.
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-fl ow velocity of up to 2.5 M.
Author:  Sh. A. Piralishvili D. M. Markovich A. S. Lobasov and I. M. Vereshchagin
Keywords:  stabilization of a flame, swirling fl ow, acoustic vibrations, supersonic flow, ignition.
Page:  1325