Numerical Assessment of Turbulence-Cascade Noise Reduction and Aerodynamic Penalties from Serrations
Author:
Affiliation:
1. DAAA, ONERA, Université Paris-Saclay, 92320 Châtillon, France
2. DAAA, ONERA, Université Paris-Saclay, 92190 Meudon, France
3. Ecole Centrale de Lyon, 69130 Ecully, France
Funder
Horizon 2020 Framework Programme
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J061301
Reference26 articles.
1. Aeroacoustic design and broadband noise predictions of a fan stage with serrated outlet guide vanes
2. Aeroacoustic study of a wavy stator leading edge in a realistic fan/OGV stage
3. An advanced synthetic eddy method for the computation of aerofoil–turbulence interaction noise
4. Synthetic turbulence methods for computational aeroacoustic simulations of leading edge noise
5. On the effects of anisotropic turbulence on leading edge noise
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