Transient Loading of Supersonic Rectangular Airfoils
Author:
Affiliation:
1. University of California, Los Angeles
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.1757
Reference11 articles.
1. Loads on a Supersonic Wing Striking a Sharp-Edged Gust
2. The Transient Reaction of an Airfoil Due to Change in Angle of Attack at Supersonic Speed
3. Transient Loading of Airfoils at Supersonic Speeds
Cited by 7 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. Aerodynamische Grundlagen;Grundlagen der Aeroelastik;1974
2. Unsteady Airfoil Theory;Advances in Applied Mechanics;1958
3. A general solution for the rectangular airfoil in supersonic flow;Quarterly of Applied Mathematics;1953
4. On the Unsteady Motion of a Thin Rectangular Wing in Supersonic Flow;Journal of the Aeronautical Sciences;1951-11
5. Aerodynamics of a Supersonic Rectangular Wing Striking a Sharp-Edged Gust;Journal of the Aeronautical Sciences;1951-08
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