Influence of a fan of rarefaction waves on the development of a disturbance in a supersonic boundary layer

Гапонов, С. А.; Kosinov, A. D.; Маслов, А. А.; Shevel'kov, S. G.

doi:10.1007/bf00851585

Search citation statements

Order By: Relevance

Paper Sections

Select...

Introduction1

Citation Types

Supporting

Mentioning

Contrasting

Year Published

2000

2017

Publication Types

Select...

Other1

Book1

Relationship

Self Cite1

Independent1

Authors

Journals

Cited by 2 publications

(1 citation statement)

References 3 publications

Supporting

Mentioning

Contrasting

Order By: Relevance

“…If the issues of stability of the laminar boundary layer at subsonic speeds were studied thoroughly in both experimental and theoretical papers [1,2], for supersonic speeds these problems are less investigated [1,[3][4][5][6][7][8].…”

Section: Introductionmentioning

confidence: 99%

On the oblique breakdown mechanism in a supersonic boundary layer on a swept wing at Mach 2

Panina

Kosinov

Семёнов

et al. 2017

AIP Conference Proceedings

Self Cite

View full text Add to dashboard Cite

Abstract.The results of an experimental study of the controlled pulsations development in the spanwise modulated boundary layer of a swept wing are presented in the paper. The experiments were conducted at Mach 2 and unit Reynolds number Re1 = 6×10 6 m -1 . The square stickers were applied to induce the spanwise modulation of mean flow in the boundary layer. It was obtained, that the presence of roughness leads to a decrease of the disturbance source efficiency at the subharmonic and fundamental frequency, and the oblique breakdown mechanism begins to appear at smaller values of the longitudinal coordinate x as compared with the case of a smooth wing.

show abstract