Optimum supersonic wings with subsonic leading edges
Author:
Affiliation:
1. Delft University of Technology, Delft, the Netherlands
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45307
Reference20 articles.
1. The Supersonic Conical Wing of Minimum Drag
2. The Minimum Drag of Thin Wings in Frictionless Flow
3. Theoretical Determination of the Minimum Drag of Airfoils at Supersonic Speeds
Cited by 3 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. Shock Wave Drag Reduction;Annual Review of Fluid Mechanics;2004-01-21
2. Aircraft drag reduction—a review;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2003-01-01
3. Supersonic aircraft drag reduction;21st Fluid Dynamics, Plasma Dynamics and Lasers Conference;1990-06-18
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