Spanwise Variation in Circulation and Drag of Wings at Moderate Reynolds Number-Reference-Cited by-同舟云学术

Spanwise Variation in Circulation and Drag of Wings at Moderate Reynolds Number

Published:2013-05 Issue:3 Volume:50 Page:791-797
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Yang S. L.¹,Spedding G. R.¹

Affiliation:

1. Department of Aerospace and Mechanical Engineering, University of Southern California, Los Angeles, California 90089-1191

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C031981

Reference14 articles.

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3. Span Efficiencies of Wings at Low Reynolds Numbers

4. McGheeR. J.WalkerB. S.MillardB. F. “Experimental Results for the Eppler 387 Airfoil at Low Reynolds Numbers in the Langley Low-Turbulence Pressure Tunnel,” NASA TM-4062, 1988, pp. 25–26.

5. SeligM. S.GuglielmoJ. J.BroerenA. P.GiguereP., Summary of Low-Speed Airfoil Data, Vol. 1, Soar Tech Publ., Virginia, Beach, 1995, pp. 19–20.

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