Direct Numerical Simulation of supersonic Boundary Layer Stabilization Using Grooved Wavy Surface-Reference-Cited by-同舟云学术

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Direct Numerical Simulation of supersonic Boundary Layer Stabilization Using Grooved Wavy Surface

Published:2010-01-04 Issue: Volume: Page:
ISSN:
Container-title:48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
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Author:

Novikov Andrey¹,Egorov Ivan¹,Fedorov Alexander²

Affiliation:

1. TsAGI

2. Moscow Institute of Physics and Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-1245

Reference9 articles.

1. Experimental studies of stability and transition in high-speed wakes

2. Numerical modeling of the disturbances of the separated flow in a rounded compression corner

3. Direct numerical simulation of disturbances generated by periodic suction-blowing in a hypersonic boundary layer

Cited by 6 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. Instability evolution in the hypersonic boundary layer over a wavy wall;Journal of Fluid Mechanics;2022-06-06

2. Effect of Distributed Surface Roughness on the Stability of High-Speed Flows.;AIAA SCITECH 2022 Forum;2022-01-03

3. Effect of Parametric Variation of Sinusoidal Surface Roughness on High-Speed Boundary Layer Stability;AIAA AVIATION 2021 FORUM;2021-07-28

4. Effect of Shape of Two-Dimensional Smooth Hump on Boundary Layer Instability;International Journal of Aeronautical and Space Sciences;2020-03-23

5. Second Mode Suppression in Hypersonic Boundary Layer by Roughness: Design and Experiments;AIAA Journal;2015-10

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