Quantification of Flow Structures Generated by an Oscillating Fence in a Flat Plate Laminar Boundary Layer-Reference-Cited by-同舟云学术

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Quantification of Flow Structures Generated by an Oscillating Fence in a Flat Plate Laminar Boundary Layer

Published:2008-01-07 Issue: Volume: Page:
ISSN:
Container-title:46th AIAA Aerospace Sciences Meeting and Exhibit
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Author:

Hind Michael¹,Lindberg William¹,Naughton Jonathan¹

Affiliation:

1. University of Wyoming

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-600

Reference6 articles.

1. The control of flow separation by periodic excitation

2. 2Saini,M.S.,Lindberg,W.R.,Naughton,J.W.,2005,"EffectofanOscillatingFenceActuatorona StationaryandPitch OscillatingWing,"46thAIAAAerospaceSciencesMeetingandExhibit,No.AIAA2008-0280,2008.

3. 3Singh,P.K.,Lindberg,W.R.,Naughton,J.W.,2005,"FlowStructuresGeneratedbyOscillatingFences in BoundaryLayer Flows,"35thAIAAFluidDynamicsConference,Toronto.

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Effect of an Oscillating Fence Actuator on a Stationary and Pitch Oscillating Wing;46th AIAA Aerospace Sciences Meeting and Exhibit;2008-01-07

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