Transonic shock-free aerofoil design by an analytic hodograph method
Author:
Affiliation:
1. Nationaal Luchtvaartlaboratorium, Amsterdam, Netherlands
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1974-539
Reference8 articles.
1. NLR-TR T-172, July 1967.
2. Privat communication, 1971.
3. Springer Verlag, New York, 1972.
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. Elements of Airfoil Design Methodology;Applied Computational Aerodynamics;1990-01-01
2. A spectral hodograph method for shockless transonic two-dimensional flow;4th Applied Aerodynamics Conference;1986-06-09
3. Transonic Airfoils with a Given Pressure Distribution;14th Fluid and Plasma Dynamics Conference;1981-06-23
4. Lifting-line theory for a swept wing at transonic speeds;Quarterly of Applied Mathematics;1979
5. The calculation of aerodynamic characteristics of wing-body combinations at subsonic flight speeds;Proceedings of the Fifth International Conference on Numerical Methods in Fluid Dynamics June 28 – July 2, 1976 Twente University, Enschede;1976
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