Wake Vortex Control Using Rapidly Actuated Segmented Gurney Flaps-Reference-Cited by-同舟云学术

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Wake Vortex Control Using Rapidly Actuated Segmented Gurney Flaps

Published:2006-01-09 Issue: Volume: Page:
ISSN:
Container-title:44th AIAA Aerospace Sciences Meeting and Exhibit
language:
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Author:

Matalanis Claude¹,Eaton John¹

Affiliation:

1. Stanford University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-481

Reference43 articles.

1. Design of Subsonic Airfoils for High Lift

2. 2Neuhart,D.H.,andPendergraftJr.,O.C."AWaterTunnelStudyofGurneyFlaps,"NASATM4071,1988.

3. Lift enhancement of an airfoil using a Gurney flap and vortex generators

4. 4Giguère,P.,Lemay,J.,andDumas,G."GurneyFlapEffectsandScalingforLow-SpeedAirfoils,"AIAA-95-1881-CP

5. 5Myose,R.,Heron,I.,andPapadakis,M."EffectofGurneyFlapsonaNACA0011Airfoil,"AIAA-96-0059.

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1. An Aerodynamic Investigation of an Isolated Stationary Formula 1 Wheel Assembly;Journal of Fluids Engineering;2012-02-01

2. Uniform Dividing Wing Ejecting Smoke of Slot Film Seeding;50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2012-01-09

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