Experimental Investigation of Influence of Edge Shape on the Aerodynamic Characteristics of Low Aspect Ratio Wings at Low Speeds
- 1 August 1955
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 22 (8) , 517-533
- https://doi.org/10.2514/8.3391
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
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- Remarks on Nonlinear Lift and Vortex SeparationJournal of the Aeronautical Sciences, 1954
- Leading-Edge Separation from Delta Wings at Supersonic SpeedsJournal of the Aeronautical Sciences, 1953
- A transformation of the hodograph equation and the determination of certain fluid motionsPhilosophical Transactions of the Royal Society of London. Series A, Mathematical and Physical Sciences, 1953
- The Lift Distribution on Low Aspect Ratio Wings at Subsonic SpeedsJournal of the Aeronautical Sciences, 1951
- First- and Second-Order Theory of Supersonic Flow Past Bodies of RevolutionJournal of the Aeronautical Sciences, 1951
- A Non‐linear Wing Theory and its Application to Rectangular Wings of Small Aspect RatioZAMM - Journal of Applied Mathematics and Mechanics / Zeitschrift für Angewandte Mathematik und Mechanik, 1939