A class of airfoils designed for high lift in incompressible flow
Author:
Affiliation:
1. Douglas Aircraft Co., Long Beach, Calif.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1973-86
Reference8 articles.
1. The prediction of separation of the turbulent boundary layer
2. An experimental flow with zero skin friction throughout its region of pressure rise
Cited by 6 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Maximization of the lift/drag ratio of airfoils with a turbulent boundary layer: Sharp estimates, approximation, and numerical solutions;Computational Mathematics and Mathematical Physics;2009-03
2. A criteria for surface pressure specification in aerodynamic shape design;28th Aerospace Sciences Meeting;1990-01-08
3. High-lift airfoil design from the hodograph;Journal of Aircraft;1984-10
4. Section design for hydrofoil wings with flaps;Advanced Marine Vehicles Conference;1978-04-17
5. Some opportunities for progress in ultra-light aeronautics;2nd International Symposium on the Technology and Science of Low Speed and Motorless Flight;1974-08-16
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