Excitation of crossflow modes in a swept-airfoil boundary layer. Part 1. Surface receptivity-Reference-Cited by-同舟云学术

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Excitation of crossflow modes in a swept-airfoil boundary layer. Part 1. Surface receptivity

Published:2023-07 Issue: Volume:100 Page:256-269
ISSN:0997-7546
Container-title:European Journal of Mechanics - B/Fluids
language:en
Short-container-title:European Journal of Mechanics - B/Fluids

Author:

Borodulin V.I.,Ivanov A.V.,Kachanov Y.S.,Mischenko D.A.

Funder

Ministry of Education and Science of the Russian Federation

Seventh Framework Programme

European Commission

Publisher

Elsevier BV

Subject

General Physics and Astronomy,Mathematical Physics

Reference51 articles.

1. Basic experiments on transition in three-dimensional boundary layers dominated by crossflow instabilities;Bippes;Prog. Aerosp. Sci.,1999

2. Swept-wing boundary-layer receptivity to surface non-uniformities;Gaponenko;J. Fluid Mech.,2002

3. Receptivity coefficients at excitation of cross-flow waves by free-stream vortices in the presence of surface roughness;Borodulin;J. Fluid Mech.,2013

4. Receptivity coefficients at excitation of cross-flow waves due to scattering of free-stream vortices on surface vibrations;Borodulin;J. Fluid Mech.,2016

5. Swept-wing boundary-layer transition at various external perturbations: Scenarios, criteria, and problems of prediction;Borodulin;Phys. Fluids,2017

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. Excitation of crossflow modes in a swept-airfoil boundary layer, Part 2: Surface-vortex receptivity;European Journal of Mechanics - B/Fluids;2023-07

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