High-lift airfoil design from the hodograph
Author:
Affiliation:
1. Ben-Gunon University of the Negev, Beersheva, Israel
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45039
Reference8 articles.
1. 3Cohen M J Hodograph Design Method for Compressible Flow Problems Journal of Applied Mechanics Vol 29,1962 pp 533 548
2. 4Liebeck, R H and Ormsbee, A I Optimization of Airfoils for Maximum Lift Journal of Aircraft Vol 7 Sept Oct 1970pp409415
3. 6Liebeck, R H and Smith AMO A Class of Airfoils Designed for High Lift Without Separation in Incompressible Flow Journal of Aircraft Vol10,Oct 1973pp610617
Cited by 2 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. Hodograph method for airfoil design - The general case;Journal of Aircraft;1996-07
2. Inverse method for airfoil design;Journal of Aircraft;1995-09
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