Leading-Edge Roughness Effects on 63(3)-418 Airfoil Performance-Reference-Cited by-同舟云学术

Leading-Edge Roughness Effects on 63(3)-418 Airfoil Performance

Published:2011-01-04 Issue: Volume: Page:
ISSN:
Container-title:49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

White Edward¹,Kutz Douglas¹,Freels Justin¹,Monschke Jason¹,Grife Ronald²,Sun Yuping³,Chao David⁴

Affiliation:

1. Texas A&M University

2. Vestas Technology R&D Americans, Inc

3. Vestas Technology R&D Americas, Inc.

4. Vestas Technology R&D Americans, Inc.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-352

Reference12 articles.

1. Abbot,I.H.,andA.E.vonDoenhoff.1959.TheoryofWingSections.Dover.

2. Barlow,J.B.,W.HRaeandA.Pope.1999.Low-SpeedWindTunnelTesting,3rded.Wiley.

3. von Doenhoff,A.E., and Horton, E.A. 1958.ALow-Speed Experimental Investigation of the Effect of a Sandpaper TypeofRoughnessonBoundary-LayerTransition,NACATech.Rep.TR1349.

4. Downs, R.S. III, E.B. White, and N.A. Denissen. 2008. Transition induced by random distributed roughness. AIAA Journal46:451.

5. Review of Published Data on the Effect of Roughness on Transition from Laminar to Turbulent Flow

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