Effect of Airfoil Aerodynamic Loading on Trailing Edge Noise Sources
By Stéphane Moreau, M. Roger. 2005
142 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Computational Mechanics, Environmental Engineering
View Paper: https://www.semanticscholar.org/paper/3ca2c9b9e18efe83b18cb45859b55312974862ec
How researchers see this paper
The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.
In Aerospace Engineering
- Stéphane Moreau
- M. Roger
- Sanjiva K. Lele
- William R. Wolf
- João Luiz F. Azevedo
- Christophe Bogey
- Christophe Bailly
- Jörg Schepers
In Computational Mechanics
- Stéphane Moreau
- M. Roger
- Sanjiva K. Lele
- William R. Wolf
- João Luiz F. Azevedo
- Christophe Bailly
- Christophe Bogey
- Sergio Pirozzoli
In Environmental Engineering
- Stéphane Moreau
- M. Roger
- Sanjiva K. Lele
- William R. Wolf
- João Luiz F. Azevedo
- Jörg Schepers
- S. Oerlemans
- G. Robert
Citations in the corpus
- Convective effects and the role of quadrupole sources for aerofoil aeroacoustics (2012, background): “Recently, Roger & Moreau (2004) and Moreau & Roger (2005) measured far-field sound and surface pressure on a cambered controlled-diffusion aerofoil and Sagrado & Hynes (2012) investigated the interaction of a turbulent boundary layer with the trailing edge of a NACA0012 aerofoil.”
- Competing Broadband Noise Mechanisms in Low-Speed Axial Fans (2004, methodology): “This was verified and themodel was validated by a comparison with simultaneous measurements of wall-pressure spectra and far-field noise performed in the Ecole Centrale de Lyon (ECL) anechoic wind tunnels on a thin cambered CD airfoil developed byValeo [20,21].”