Effects of Flat-Plate Extension of Trailing Edge on Noise Generation for NACA 0012 Airfoil at Moderate Reynolds Numbers Using Direct Noise Simulations
28th AIAA/CEAS Aeroacoustics 2022 Conference
2022-01-01
Conference paper
Electronic Resource
English
Aeroelastic Dynamics of a NACA 0012 Airfoil at Transitional Reynolds Numbers
British Library Conference Proceedings | 2009
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