Experimental Study of a NACA0015 Circulation Control Airfoil Using Synthetic Jet Actuation
Author:
Affiliation:
1. King Mongkut’s Institute of Technology Ladkrabang, 10520 Bangkok, Thailand
2. University of Auckland, Auckland 1142, New Zealand
Funder
University of Auckland
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J060508
Reference68 articles.
1. SmithM. A. (ed.), Jet-Flap Development. Mr. I. M. Davidson’s Lecture Before the Royal Aeronautical Society, Vol. 68, Iliffe Transport Publication Ltd., London, 1955, pp. 688–689.
2. Numerical analysis of the effect of vortex control mechanism on longitudinal aerodynamics of lifting body
3. Flight Performance of a Circulation Controlled STOL Aircraft
4. AbramsonJ. “Two-Dimensional Subsonic Wind Tunnel Evaluation of Two Related Cambered 15-Percent-Thick Circulation Control Airfoils,” David W Taylor Naval Ship Research and Development Center ASED-373, Sept. 1977.
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