Experimental investigations on the effects of divergent trailing edge and Gurney flaps on a supercritical airfoil
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Published:2007-03
Issue:2-3
Volume:11
Page:91-99
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ISSN:1270-9638
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Container-title:Aerospace Science and Technology
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language:en
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Short-container-title:Aerospace Science and Technology
Author:
Li Y.C.,Wang J.J.,Hua J.
Subject
Aerospace Engineering
Reference13 articles.
1. R.D. Gregg, R.W. Hoch, P.A. Henne, Application of divergent trailing-edge airfoil technology to the design of a derivative wing, SAE Paper 892288, 1989
2. P.A. Henne, R.D. Gregg, New airfoil design concept, AIAA Paper 89-2201, 1989
3. C.S. Jang, J.C. Ross, R.M. Cummings, Computational evaluation of an airfoil with a Gurney flap, AIAA Paper 92-2708, 1992
4. Aerodynamics of Gurney flaps on a single-element high-lift wing;Jeffrey;Journal of Aircraft,2000
5. Design of subsonic airfoils for high lift;Liebeck;Journal of Aircraft,1978
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