Extensions and limitations of analytical airfoil broadband noise models
By M. Roger, Stéphane Moreau. 2010
142 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Biomedical Engineering, Computational Mechanics
View Paper: https://www.semanticscholar.org/paper/659962f5c4a42b7ec281cfdaa3b9da94ec710290
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In Aerospace Engineering
In Biomedical Engineering
In Computational Mechanics
Citations in the corpus
- On the reduction of aerofoil–turbulence interaction noise associated with wavy leading edges (2016, background): “…camber, etc, on ATI noise have been studied by Atassi, Subramaniam & Scott (1990), Lockard & Morris (1998), Evers & Peake (2002), Devenport, Staubs & Glegg (2010), Roger & Carazo (2010), Roger & Moreau (2010), Ayton & Peake (2013), Gill, Zhang & Joseph (2013) and Kim, Lee & Cheong (2015).”
- Noise reduction mechanisms of sawtooth and combed-sawtooth trailing-edge serrations (2018, background): “Increasing the frequency (figure 8b), the dipole is tilted toward the leading edge of the aerofoil (Roger & Moreau 2010).”