Streamwise vortex breakdown in supersonic flows
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DOI: 10.1063/1.4982901
Abstract: Transition processes in supersonic streamwise vortices with wake flows are numerically simulated for Mach numbers from 1.5 to 5.0. This paper discusses the effect of an axial velocity deficit on the breakdown for a fixed… read more here.
Keywords: breakdown supersonic; supersonic flows; mach; breakdown ... See more keywords