AbstractThis article reviews the application of Computational Aero-Acoustics (CAA) to the prediction of acoustic propagation in turbofan ducts. The challenge of resolving the radiated sound field for realistic nacelle geometries is discussed and evidence is presented to indicate that current CAA is able to represent the effect of in-duct liners on far-field measured rig and engine data. Two approaches are presented for incorporating CAA predictions within liner optimisation schemes for a turbofan intake
The acoustic field within a duct containing a nonuniform steady flow was predicted. This analysis us...
Modern high-bypass turbofan engines produce high levels of nuisance noise that has a significant imp...
This report presents the results of a parametric study of the turbofan far-field noise radiation usi...
AbstractThis article reviews the application of Computational Aero-Acoustics (CAA) to the prediction...
AbstractThis article reviews the application of Computational Aero-Acoustics (CAA) to the prediction...
Novel techniques are presented to reduce noise from turbofan aircraft engines by optimising the acou...
Acoustic liners placed in the intake and bypass ducts of commercial turbofan aeroengines have played...
In modern turbofan engines, fan noise is one of the principle noise sources due to increased bypass ...
AbstractAccurate computation of multimode propagation in and radiation from a turbofan duct is impor...
The development of computational methods in acoustics has led to the introduction of analysis and de...
AbstractTwo critical areas for the design of quiet gas turbine engines, fan broadband and combustor ...
Prediction of Supersonic Fan Noise Generated by Turbofan Aircraft Engines was focussed on improving ...
The main object of this thesis is to investigate acoustic lining in turbofan ducts which have optima...
A symposium on the subject of ‘Computational Aero-Acoustics (CAA) for Aircraft Noise Prediction’ was...
Development of acoustic lining for turbofan nacelle modification to minimize fan compressor noise ra...
The acoustic field within a duct containing a nonuniform steady flow was predicted. This analysis us...
Modern high-bypass turbofan engines produce high levels of nuisance noise that has a significant imp...
This report presents the results of a parametric study of the turbofan far-field noise radiation usi...
AbstractThis article reviews the application of Computational Aero-Acoustics (CAA) to the prediction...
AbstractThis article reviews the application of Computational Aero-Acoustics (CAA) to the prediction...
Novel techniques are presented to reduce noise from turbofan aircraft engines by optimising the acou...
Acoustic liners placed in the intake and bypass ducts of commercial turbofan aeroengines have played...
In modern turbofan engines, fan noise is one of the principle noise sources due to increased bypass ...
AbstractAccurate computation of multimode propagation in and radiation from a turbofan duct is impor...
The development of computational methods in acoustics has led to the introduction of analysis and de...
AbstractTwo critical areas for the design of quiet gas turbine engines, fan broadband and combustor ...
Prediction of Supersonic Fan Noise Generated by Turbofan Aircraft Engines was focussed on improving ...
The main object of this thesis is to investigate acoustic lining in turbofan ducts which have optima...
A symposium on the subject of ‘Computational Aero-Acoustics (CAA) for Aircraft Noise Prediction’ was...
Development of acoustic lining for turbofan nacelle modification to minimize fan compressor noise ra...
The acoustic field within a duct containing a nonuniform steady flow was predicted. This analysis us...
Modern high-bypass turbofan engines produce high levels of nuisance noise that has a significant imp...
This report presents the results of a parametric study of the turbofan far-field noise radiation usi...