Reduced-order Modeling and Acoustic Optimization of the Noise Generated by Boundary Layer Instabilities Convecting Over an Elastic Trailing-Edge
Author:
Affiliation:
1. University of Melbourne
Publisher
American Institute of Aeronautics and Astronautics
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1. Direct Numerical Simulation of the Acoustic Response of a NACA-0012 Airfoil with an Elastic Serrated Trailing-Edge;30th AIAA/CEAS Aeroacoustics Conference (2024);2024-05-30
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