On the Unsteady Motion of a Thin Rectangular Wing in Supersonic Flow
Author:
Affiliation:
1. Cornell University, Ithaca, N.Y.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.2109
Reference11 articles.
1. The Source-Flow in Supersonic and Incompressible Theories
2. The Linearized Subsonic and Supersonic Flow About Inclined Slender Bodies of Revolution
3. Transient Loading of Supersonic Rectangular Airfoils
4. ON THE LINEARIZED POTENTIAL THEORY OF UNSTEADY SUPERSONIC MOTION
Cited by 5 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. REFERENCES;Wing Theory in Supersonic Flow;1969
2. Unsteady Airfoil Theory;Advances in Applied Mechanics;1958
3. Slender-Body Theory-Review and Extension;Journal of the Aeronautical Sciences;1953-02
4. A general solution for the rectangular airfoil in supersonic flow;Quarterly of Applied Mathematics;1953
5. On the General Solution for Unsteady Motion of a Rectangular Wing in Supersonic Flow;Journal of the Aeronautical Sciences;1952-06
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