Two-Dimensional Wind Tunnel and Computational Investigation of a Microtab Modified S809 Airfoil-Reference-Cited by-同舟云学术

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Two-Dimensional Wind Tunnel and Computational Investigation of a Microtab Modified S809 Airfoil

Published:2005-01-10 Issue: Volume: Page:
ISSN:
Container-title:43rd AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Baker Jonathon¹,Standish Kevin¹,van Dam Cornelis¹

Affiliation:

1. University of California Davis

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-1186

Reference25 articles.

1. Active Load Control for Airfoils using Microtabs

2. Computational Investigation of Finite Width Microtabs for Aerodynamic Load Control

3. Lecture Notes for the von Kármán Institute for Fluid Dynamics Lecture Series: Numerical Techniques for Viscous Flow Computation in Turbomachinery Bladings, von;Pulliam T.H.,1985

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