Control of Crossflow Transition at High Reynolds Numbers Using Discrete Roughness Elements-Reference-Cited by-同舟云学术

Control of Crossflow Transition at High Reynolds Numbers Using Discrete Roughness Elements

Published:2016-01 Issue:1 Volume:54 Page:39-52
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Li Fei¹,Choudhari Meelan¹,Carpenter Mark¹,Malik Mujeeb¹,Chang Chau-Lyan¹,Streett Craig¹

Affiliation:

1. Computational AeroSciences Branch, NASA Langley Research Center, Hampton, Virginia 23681

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J054067

Reference34 articles.

1. ArgüellesP.BischoffM.BusquinP.DrosteB. A. C.EvansR.KröllW.LagardèreJ.L.LinaA.LumsdenJ.RanqueD.RasmussenS.ReutlingerP.RobinsR.TerhoH.WittlövA. “European Aeronautics: A Vision for 2020,” Office for Official Publications of the European Communities, Luxembourg, Jan. 2001.

2. Leading-edge roughness as a transition control mechanism

3. Secondary instability of crossflow vortices and swept-wing boundary-layer transition

4. Simulation of swept-wing vortices using nonlinear parabolized stability equations

5. Mechanisms and passive control of crossflow-vortex-induced transition in a three-dimensional boundary layer

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