Experimental Studies of the Impact of Periodic Modulation of the Flow on the De-velopment of Disturbances in the Boundary Layer of a Swept Wing at a M = 2.5

Author:

Yatskikh Aleksey A.1,Panina Alexandra V.2,Kocharin Vasilii L.2,Yermolaev Yury G.1,Kosinov Alexander D.1,Semionov Nikolai V.2

Affiliation:

1. Khristianovich Institute of Theoretical and Applied Mechanics SB RAS; Novosibirsk State University

2. Khristianovich Institute of Theoretical and Applied Mechanics SB RAS

Abstract

The results of experimental studies on the impact of periodic flow modulation on the development of natural disturbances and artificial localized wave packets in the boundary layer of a swept wing with a leading edge swept angle of 40 degrees at a Mach number M = 2.5 are presented. The boundary layer was modulated using periodic roughness on the model surface. Artificial wave packets were generated by a pulsed glow discharge. Hot-wire anemometer measurements showed that, according to the experimental conditions, periodic modulation of the boundary layer leads to the stabilization of the development of controlled localized disturbances and to an increase in the growth of natural disturbances.

Publisher

Novosibirsk State University (NSU)

Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Issledovanie vliyaniya skorosti nabegayushchego potoka na techenie, indutsiruemoe dielektricheskim bar'ernym razryadom;Журнал экспериментальной и теоретической физики;2023-05-15

2. Analysis of the Effect of the Incoming Flow Velocity on the Flow Induced by a Dielectric Barrier Discharge;Journal of Experimental and Theoretical Physics;2023-05

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