The bypass duct of an aircraft engine is a low-pass lter allowing some spinning modes to radiate out-side the duct. The knowledge of the radiated modes can help in noise reduction, as well as the diagno-sis of noise generation mechanisms inside the duct. We propose a nonintrusive technique using a circular microphone array outside the engine measuring the complex noise spectrum on an arc of a circle. The ar-ray is placed at various axial distances from the inlet or the exhaust of the engine. Using a model of noise radiation from the duct, an overdetermined system of linear equations is constructed for the complex amplitudes of the radial modes for a xed circum-ferential mode. This system of linear equations is generally singular, indicating...
This paper continues an earlier companion paper in which the results of active control computer simu...
In recent experiments in the inlet of an UHBR Fan Rig for the very first time an array of wall-flush...
The influence of bifurcations in an aero-engine bypass duct on noise radiation was investigated thro...
The bypass duct of an aircraft engine is a low-pass filter allowing some spinning modes to radiate o...
An inverse technique for determining the mode amplitudes generated by turbofan inlets both for tonal...
Knowledge of the modal content of the sound field radiated from a turbofan inlet is important for so...
Knowledge of the modal content of the sound field radiated from a turbofan inlet is important for so...
A method suited for the decomposition of broadband noise into duct modes is presented. The inverse ...
The sound field within an aeroengine duct can be expressed as a superimposition of acoustic modes. K...
This paper is an experimental investigation of an inverse technique for deducing the amplitudes of t...
Significant progress has been made over the last few decades in the reduction of turbofan jet engine...
International audienceThe subject of this paper is the experimental investigation of the noise radia...
Modern high-bypass turbofan engines produce high levels of nuisance noise that has a significant imp...
The influence of bifurcations in an aero-engine bypass duct on noise radiation was investigated thro...
The work in this thesis elucidates the physical and mathematical concepts involved in understanding ...
This paper continues an earlier companion paper in which the results of active control computer simu...
In recent experiments in the inlet of an UHBR Fan Rig for the very first time an array of wall-flush...
The influence of bifurcations in an aero-engine bypass duct on noise radiation was investigated thro...
The bypass duct of an aircraft engine is a low-pass filter allowing some spinning modes to radiate o...
An inverse technique for determining the mode amplitudes generated by turbofan inlets both for tonal...
Knowledge of the modal content of the sound field radiated from a turbofan inlet is important for so...
Knowledge of the modal content of the sound field radiated from a turbofan inlet is important for so...
A method suited for the decomposition of broadband noise into duct modes is presented. The inverse ...
The sound field within an aeroengine duct can be expressed as a superimposition of acoustic modes. K...
This paper is an experimental investigation of an inverse technique for deducing the amplitudes of t...
Significant progress has been made over the last few decades in the reduction of turbofan jet engine...
International audienceThe subject of this paper is the experimental investigation of the noise radia...
Modern high-bypass turbofan engines produce high levels of nuisance noise that has a significant imp...
The influence of bifurcations in an aero-engine bypass duct on noise radiation was investigated thro...
The work in this thesis elucidates the physical and mathematical concepts involved in understanding ...
This paper continues an earlier companion paper in which the results of active control computer simu...
In recent experiments in the inlet of an UHBR Fan Rig for the very first time an array of wall-flush...
The influence of bifurcations in an aero-engine bypass duct on noise radiation was investigated thro...