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Thermophysics and Aeromechanics

2025 year, number 6

The role of the mechanism of interaction between the controlled disturbances in the process of emission of acoustic disturbances by a supersonic boundary layer

A.D. Kosinov, M.V. Piterimova
Khristianovich Institute of Theoretical and Applied Mechanics SB RAS, Novosibirsk, Russia
Keywords: controlled disturbances, supersonic boundary layer, acoustic wave emission, flat plate

Abstract

The results of hot-wire measurements of periodic controlled disturbances of the mass flow beyond the boundary layer on a flat plate are discussed, and their wave characteristics reflecting the acoustic properties of the supersonic boundary layer are estimated. The possibility of emitting subharmonic disturbances at a Mach number of 2.5 is demonstrated for the first time.