Slender wings with leading-edge vortex separation - A challenge for panel methods and Euler solvers
- 1 October 1984
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 21 (10), 751-759
- https://doi.org/10.2514/3.45038
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
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- Slender Wings with Leading Edge Vortex-SeparationPublished by Springer Science and Business Media LLC ,1982
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- VIII. Stability of a viscous liquid contained between two rotating cylindersPhilosophical Transactions of the Royal Society A, 1923