Experiments on Discrete Roughness Element Technology for Swept-Wing Laminar Flow Control

Author:

Saric William S.1,West David E.1,Tufts Matthew W.1,Reed Helen L.1

Affiliation:

1. Texas A&M University, College Station, Texas 77843-3141

Funder

NASA LaRC through Analytical Mechanics Associates, Inc

WPAFB through General Dynamics IT

Texas AM University Foundation through the George Eppright ’26 Chair.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference33 articles.

1. ArnalD.ArchambaudJ. P. “Laminar-Turbulent Transition Control: NLF, LFC, HLFC,” Advances in Laminar-Turbulent Transition Modeling, AVT-151 RTO AVT/VKI, Lecture Series, von Kármán Inst. for Fluid Dynamics, Rhode St. Genèse, Belgium, 2009.

2. SaricW. S.ReedH. L.BanksD. W. “Flight Testing of Laminar Flow Control in High-Speed Boundary Layers,” NATO RTO MP-AVT-111/RSM, Vol. 32, 2004, pp. 1–8.

3. Experiments in nonlinear saturation of stationary crossflow vortices in a swept-wing boundary layer

4. Leading-edge roughness as a transition control mechanism

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