Numerical Solution for Airfoils near Stall in Optimized Boundary-Fitted Curvilinear Coordinates
- 1 May 1979
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 17 (5) , 458-464
- https://doi.org/10.2514/3.61155
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
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