The effect of acoustic forcing on trailing edge separation and near wake development of an airfoil
- 25 July 1988
- 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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- Analysis and Correlation of Data on Pressure Fluctuations in Separated FlowJournal of Aircraft, 1972
- The stability of an incompressible two-dimensional wakeJournal of Fluid Mechanics, 1972