Discrete-Roughness-Element-Enhanced Swept-Wing Natural Laminar Flow at High Reynolds Numbers-Reference-Cited by-同舟云学术

Discrete-Roughness-Element-Enhanced Swept-Wing Natural Laminar Flow at High Reynolds Numbers

Published:2015-08 Issue:8 Volume:53 Page:2321-2334
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Malik Mujeeb¹,Liao Wei²,Li Fei¹,Choudhari Meelan¹

Affiliation:

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

2. National Institute of Aerospace, Hampton, Virginia 23666

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J053637

Reference41 articles.

1. HefnerJ. N.BushnellD. M. “An Overview of Concepts for Aircraft Drag Reduction,” Special Course on Concepts for Drag Reduction, AGARD Rept. No. 654, Essex, England, U.K. 1977, pp. 1–30.

2. DrakeA.HarrisC. A.KomadinaS. C.WangD. P.BenderA. M. “Environmentally Responsible Aviation N+2 Advanced Vehicle Study,” Northrop Grumman Systems Corporation Final Technical Report, NASA CR-2013-218304, 2013.

3. BushnellD. M.TuttleM. H. “Survey and Bibliography on Attainment of Laminar Flow Control in Air Using Pressure Gradient and Suction,” Vol. 1, NASA RP-1035, 1979.

4. BushnellD. M. “Overview of Aircraft Drag Reduction Technology,” Special Course on Skin Friction Drag Reduction, AGARD Rept. 786, Essex, England, U.K. 1992.

5. AIRCRAFT LAMINAR FLOW CONTROL

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