Wind-Tunnel Study of a Circulatis Elliptical Airfoi
Author:
Affiliation:
1. Air Force Institute of Technology,
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.58868
Reference13 articles.
1. An Experimental Investigation of a Low-Speed Circulation-Controlled Aerofoil
2. 2Englar, R. J. * 'Two-Dimensional Subsonic Wind Tunnel Tests of Two 15-Percent Thick Circulation Control Airfoils," Naval Ship Research and Development Center, Bethesda, Md., AD900210, NSRDC Technical Note AL-211, Aug. 1971.
3. Two Dimensional Subsonic Wind Tunnel Tests on a 20 Percent Thick, 5 Percent Cambered Circulation Control Airfoil
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