Vol. 328 No. 7 (2017)
Isothermal modeling of swirling flow aerodynamic structure in a two-stage burner
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
