Slender wings with leading-edge vortex separation - A challenge for panel-methods and Euler-solvers
- 10 January 1983
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
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- Leading-Edge Separation from Delta Wings at Supersonic SpeedsJournal of the Aeronautical Sciences, 1953
- VIII. Stability of a viscous liquid contained between two rotating cylindersPhilosophical Transactions of the Royal Society A, 1923