Unsteady streamlines near the trailing edge of NACA 0012 airfoil at a Reynolds number of 125,000
- 1 January 1990
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 28 (1) , 169-170
- https://doi.org/10.2514/3.10368
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
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