Experimental Study of the Interaction of Controlled Disturbances from Two Sources in the Supersonic Boundary Layer of a Swept Wing-Reference-Cited by-同舟云学术

Experimental Study of the Interaction of Controlled Disturbances from Two Sources in the Supersonic Boundary Layer of a Swept Wing

Published:2023-12-09 Issue:2 Volume:18 Page:46-53
ISSN:2541-9447
Container-title:SIBERIAN JOURNAL OF PHYSICS
language:
Short-container-title:jour

Author:

Kolosov G. L.¹,Kosinov A. D.¹,Semionov N. V.¹,Yatskikh A. A.¹

Affiliation:

1. S. A. Khristianovich Institute of Theoretical and Applied Mechanics, SB RAS

Abstract

Experimental results of the interaction of disturbances from two point sources of periodic controlled pulsations in the supersonic boundary layer of a swept wing at a Mach number of 2 are presented. It is shown that as a result of the summation of disturbances, an interference pattern is formed and, for certain values of the wave numbers, it is possible to suppress the corresponding components of unstable waves.

Publisher

Novosibirsk State University (NSU)

Subject

Automotive Engineering

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