Separation Control by External Acoustic Excitation at Low Reynolds Numbers-Reference-Cited by-同舟云学术

Separation Control by External Acoustic Excitation at Low Reynolds Numbers

Published:2013-06 Issue:6 Volume:51 Page:1506-1515
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

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.J052191

Reference21 articles.

1. 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.

2. SimonsM., Model Aircraft Aerodynamics, 4th ed., Special Interest Model Books, Dorset, England, U.K., 1999, pp. 227–259.

3. Span Efficiencies of Wings at Low Reynolds Numbers

4. Boundary-Layer Stability and Transition

5. Low-Reynolds-number separation on an airfoil

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