Isothermal modeling of swirling flow aerodynamic structure in a two-stage burner

Abstract

The work motivation is determined by the extensive use of interacting swirling flows in counter vortex quenchers and vortex combustion chambers. To optimize the design of such devices, it is necessary to understand the structure of the flow and the mechanisms of interaction of co

Keywords

• vortex burners
• coaxial swirling flows
• high-speed visualization
• laser-Doppler anemometer
• precessing vortex core