Roughness induced transition delay in a swept-wing boundary layer in presence of freestream disturbances, Part 2: Acoustic stabilization-Reference-Cited by-同舟云学术

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Roughness induced transition delay in a swept-wing boundary layer in presence of freestream disturbances, Part 2: Acoustic stabilization

Published:2024-03 Issue: Volume:104 Page:173-181
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.

Funder

European Commission

Ministry of Education and Science of the Russian Federation

Publisher

Elsevier BV

Subject

General Physics and Astronomy,Mathematical Physics

Reference17 articles.

1. Roughness induced transition delay in a swept-wing boundary layer in presence of freestream disturbances. Part 1. Turbulence effects;Borodulin;Eur. J. Mech. B/Fluids.,2024

2. Leading-edge roughness as a transition control mechanism;Saric;AIAA Paper 98-0781,1998

3. Experimental study of instability modes in three-dimensional boundary layer;Mueller,1988

4. Effect of sound and micro-sized roughness on crossflow dominated transition;Takagi;Bull. Amer. Phys. Soc.,1991

5. Effect on micro-sized roughness on transition in swept-wing flows;Radeztsky;AIAA Paper 93-0076,1993

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. Roughness induced transition delay in a swept-wing boundary layer in presence of freestream disturbances, Part 1: Turbulence effects;European Journal of Mechanics - B/Fluids;2024-01

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