23% Circulation Controlled Elliptical Airfoil Modeled Using CFD-Reference-Cited by-同舟云学术

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23% Circulation Controlled Elliptical Airfoil Modeled Using CFD

Published:2011-06-14 Issue: Volume: Page:
ISSN:
Container-title:20th AIAA Computational Fluid Dynamics Conference
language:
Short-container-title:

Author:

Graham Henry¹,Hard Steven¹,Smith James¹

Affiliation:

1. West Virginia University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-3845

Reference22 articles.

1. Cμ -10 deg -5 deg 0 deg 5 deg 10 deg 2029 1.7421 2.0034 1.3567 0.088 1.6909 2.2668 2.8635 3.2908 2.6209 0.164 3.2172 3.8330 4.3940 4.6426 4.0611

2. Cμ -10 deg -5 deg 0 deg 5 deg 10 deg 0 -0.0840 0.0022 0.0339 0.0032 -0.0836

3. 005 -0.0496 0.0231 0.0331 -0.0040 -0.0928 0.02 0.0392 0.0751 0.0347 -0.0380 -0.1251 0.04 0.1557 0.1437 0.0425 -0.1162 -0.1606 0.088 0.3507 0.2526 0.0628 -0.1981 -0.3476 0.164 0.6455 0.4229 0.1023 -0.2671 -0.5424

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3. Mid-span PIV Measurements of a Low Aspect Ratio Circulation Control Wing;30th AIAA Applied Aerodynamics Conference;2012-06-25

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