This paper reviews the basis of the beam former (BF) and polar correlation (PC) phased array methods and shows that these provide different information about axially distributed, non-compact noise sources, which nevertheless satisfy a simple integral relationship. The conventional BF method provides an image of the source PSD, whereas the PC method yields a ‘source strength’ which is an image of the axial wavenumber transform of the source CSD. However, the BF method can be generalised to provide an image of the source CSD. At first sight the generalised BF method is therefore more useful for diagnostic purposes but the results presented here suggest that the combined effects of resolution and source convection place serious limitations on ...
The present study reports a new development of the DAMAS microphone phased array processing methodol...
This work aims at improving the current state-of-the-art in noise source localization techniques and...
The most energetic modes of the turbulent mixing layer from an axisymmetric jet at Mach 0.85 are exa...
This paper reviews the state of the art of engine noise source evaluation using microphone arrays an...
A small-aperture microphone phased array provides noise source maps for turbulent mixing noise emitt...
This study relates to the imaging of noise sources that are distributed and strongly directional, su...
Axial fans operate in large numbers, often in the close vicinity of humans, therefore reducing their...
The primary objective of this investigation is to determine experimentally the sources of jet mixing...
... jet are investigated by direct numerical simulation. Details of the numerical method are briefly...
We propose a diagnostic technique to detect instability waves in a round jet using a conical microph...
The thesis describes two techniques for investigating experimentally the generation of noise by turb...
The measurement of the characteristics of the acoustic field generated by a set of sources is very i...
Significant spectral broadening of tone noise by jet shear-layer turbulence can occur if the tone fr...
A quantitative assessment of the acoustic source field produced by a laboratory-scale heated jet wit...
International audienceThis paper deals with the denoising of microphone array measurements. In many ...
The present study reports a new development of the DAMAS microphone phased array processing methodol...
This work aims at improving the current state-of-the-art in noise source localization techniques and...
The most energetic modes of the turbulent mixing layer from an axisymmetric jet at Mach 0.85 are exa...
This paper reviews the state of the art of engine noise source evaluation using microphone arrays an...
A small-aperture microphone phased array provides noise source maps for turbulent mixing noise emitt...
This study relates to the imaging of noise sources that are distributed and strongly directional, su...
Axial fans operate in large numbers, often in the close vicinity of humans, therefore reducing their...
The primary objective of this investigation is to determine experimentally the sources of jet mixing...
... jet are investigated by direct numerical simulation. Details of the numerical method are briefly...
We propose a diagnostic technique to detect instability waves in a round jet using a conical microph...
The thesis describes two techniques for investigating experimentally the generation of noise by turb...
The measurement of the characteristics of the acoustic field generated by a set of sources is very i...
Significant spectral broadening of tone noise by jet shear-layer turbulence can occur if the tone fr...
A quantitative assessment of the acoustic source field produced by a laboratory-scale heated jet wit...
International audienceThis paper deals with the denoising of microphone array measurements. In many ...
The present study reports a new development of the DAMAS microphone phased array processing methodol...
This work aims at improving the current state-of-the-art in noise source localization techniques and...
The most energetic modes of the turbulent mixing layer from an axisymmetric jet at Mach 0.85 are exa...