High angle-of-attack airfoil performance improvement by internal acoustic excitation
- 1 March 1994
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 32 (3) , 655-657
- https://doi.org/10.2514/3.12034
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
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- Boundary-Layer Control on Wings Using Sound and Leading-Edge SerrationsAIAA Journal, 1981