Back-scattering correction and further extensions of amiet's trailing-edge noise model. Part 1: theory

By M. Roger, Stéphane Moreau. 2005

469 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Biomedical Engineering, Environmental Engineering

View Paper: https://www.semanticscholar.org/paper/ddcbb0de55105b581dbe34e0bb77b931c544df13

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

1. Jörg Schepers
2. Stéphane Moreau
3. M. Roger
4. S. Oerlemans
5. G. Robert
6. Y. Rozenberg
7. Sanjiva K. Lele
8. William R. Wolf

In Biomedical Engineering

1. Jörg Schepers
2. S. Oerlemans
3. M. Azarpeyvand
4. Stéphane Moreau
5. M. Roger
6. William R. Wolf
7. Sanjiva K. Lele
8. João Luiz F. Azevedo

In Environmental Engineering

1. Stéphane Moreau
2. M. Roger
3. Jörg Schepers
4. S. Oerlemans
5. G. Robert
6. Y. Rozenberg
7. Sanjiva K. Lele
8. William R. Wolf

Citations in the corpus

• Prediction of noise from serrated trailing edges (2015, background): “Amiet’s model agrees well with experimental observations, especially at high frequencies (Roger & Moreau 2005).”
• Back-scattering correction and further extensions of Amiet's trailing-edge noise model. Part II: Application (2009, background): “Now in the first part of the paper [8], a scattered pressure P1 equal in amplitude to the incident pressure P0 is applied with opposite phases on both sides of the airfoil.”
• Wall-Pressure Spectral Model Including the Adverse Pressure Gradient Effects (2012, background): “The diffraction of wall-pressure fluctuations near edges yields the so-called trailing-edge noise [1–4], which constitutes the most basic aeroacoustic mechanism of a surface of limited extent embedded in a clean flow.”
• Competing Broadband Noise Mechanisms in Low-Speed Axial Fans (2004, unknown): “A leading-edge correction fully taking into account the finite chord length (second iteration and correction I2 to I) has been derived recently [20,22,24].”
• Prediction of Wind Turbine Noise and Validation against Experiment (2009, methodology): “The effect of a leading edge back-scattering correction to Amiet’s formulation was investigated by Roger and Moreau [18], but they found this correction to be negligible for large wind turbine blades.”
• Convective effects and the role of quadrupole sources for aerofoil aeroacoustics (2012, background): “Several analytical formulations for trailing-edge noise prediction use information on wall-pressure PSD collected in the trailing-edge region (Amiet 1976; Howe 1978, 2001; Roger & Moreau 2005; Moreau & Roger 2009).”