Conditions for the Appearance of Boundary-Free Circulation Zones in Supersonic Axisymmetric Accelerating Flows

摘要

The mechanism of appearance of boundary-free circulation zones - circulating flows arising behind the Mach disk of an underexpanded supersonic jet is investigated. Ideas on the mechanism of formation of circulation zones and the criteria for their occurrence are formulated within the near-axis approximation. Technical possibilities of realization flows that satisfy these criteria are analyzed with the help of numerical simulation. A comparison is made with the results of a study of the formation of circulation zones in axisymmetric nozzles at the overexpansion mode.