Theoretical Determination of the Minimum Drag of Airfoils at Supersonic Speeds
- 1 December 1952
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 19 (12) , 813-822
- https://doi.org/10.2514/8.2493
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
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- The Minimum Drag of Thin Wings in Frictionless FlowJournal of the Aeronautical Sciences, 1951
- Leading-Edge Singularities in Thin-Airfoil TheoryJournal of the Aeronautical Sciences, 1950
- Supersonic Aerodynamics-Principles and Applications The Tenth Wright Brothers LectureJournal of the Aeronautical Sciences, 1947
- Mathematical Analysis of Random NoiseBell System Technical Journal, 1944
- On the motion of a pendulum in a turbulent fluidQuarterly of Applied Mathematics, 1943
- Some Aspects of Non-Stationary Airfoil Theory and Its Practical ApplicationJournal of the Aeronautical Sciences, 1941