Abstract. The work is devoted to experimental and nu merical study of aerodynamic structure of a swirl flow in isothermal model of a vortex burner device that is characterized by the fluid flow supply via two sequentially-mounted tangential swirlers. Depending on the way of the flow supply into the second-stage swirler, either co-swirl or counter-swirl of two flows can be realized. The effect of the second-stage supply direction on the resulting aerodynamic structure has been investigated. Using LDA measurement system the profiles of averaged axial and tangential velocity co mponents were obtained. Experiments have sh own that in the co-swirl case the flow inside the vortex burner model is characterized by strong non-uniformity, wh ile in the counter-swirl regime a rapid mixing of the flows from the first and second stages occurs, resulting in a uniform distribution of the flo w across the chamber section. Nu merical simu lation of 3D isothermal turbulent flow has been performed for the counter-swirl regime using the differential Reynolds stress model in the time-dependent formu lation. Using the Qcriterion for the identificat ion of vortices in numerical data arrays, the evolution of large-scale vortex structures of the swirl flo w inside the vortex chamber has been visualized, indicating the presence of two spiral-shape vortex filaments in the vortex chamber. The periodic character of dynamics of these vortex structures has been revealed.