On the nonlinear development of controlled disturbances in the supersonic boundary layer of a swept wing-Reference-Cited by-同舟云学术

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On the nonlinear development of controlled disturbances in the supersonic boundary layer of a swept wing

Published:2017 Issue: Volume: Page:
ISSN:0094-243X
Container-title:AIP Conference Proceedings
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Author:

Kolosov G. L.,Kosinov A. D.,Yermolaev Yu. G.,Semionov N. V.

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Link

http://aip.scitation.org/doi/pdf/10.1063/1.5007527

Reference25 articles.

1. Basic experiments on transition in three-dimensional boundary layers dominated by crossflow instability

2. STABILITY AND TRANSITION OF THREE-DIMENSIONAL BOUNDARY LAYERS

3. Crossflow disturbances in three-dimensional boundary layers: nonlinear development, wave interaction and secondary instability

4. Some observations of the transition process on the windward face of a long yawed cylinder

5. Secondary instability of crossflow vortices

Cited by 1 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. Evolution of localized artificial disturbance in 2D and 3D supersonic boundary layers;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2018-07-12

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