Effect of Inflow Conditions on the Noise Reduction Through Leading Edge Serrations
Author:
Affiliation:
1. Dusseldorf University of Applied Sciences, D-40476 Dusseldorf, Germany
2. Brandenburg University of Technology Cottbus–Senftenberg, D-03046 Cottbus, Germany
3. Berlin Technical University, D-10623 Berlin, Germany
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference36 articles.
1. On the reduction of aerofoil–turbulence interaction noise associated with wavy leading edges
2. Aeroacoustic source mechanisms of a wavy leading edge undergoing vortical disturbances
3. Aerofoil broadband noise reductions through double-wavelength leading-edge serrations: a new control concept
4. An analytic solution for the noise generated by gust–aerofoil interaction for plates with serrated leading edges
5. Statistical–Empirical Modeling of Airfoil Noise Subjected to Leading-Edge Serrations
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