Numerical simulation of transonic separated flows over low-aspect ratio wings
- 6 January 1986
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
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- Slender wings with leading-edge vortex separation - A challenge for panel-methods and Euler-solversPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
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- Recent advances in the solution of three-dimensional flow over wings with leading edge vortex separationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979