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- W2099945681 abstract "The test setup and first experimental results of model scale tests to investigate the sound radiation through the aero engine nozzles and the jet shear layers are presented. Fan rearward noise was simulated by a mode generator and loudspeakers. Tones and broadband noise were generated. Radial mode analysis in the bypass duct allowed characterising the generated sound field. An aerodynamic source and a siren were used to generate sound in the hot core where loudspeakers could not be applied. A polar microphone array in the downstream anechoic chamber and an azimuthal array that could be traversed along the jet axis delivered data to determine both the polar far-field directivity and the azimuthal modal breakdown. Various configurations were tested." @default.
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- W2099945681 date "2008-05-05" @default.
- W2099945681 modified "2023-09-27" @default.
- W2099945681 title "Turbomachinery Exhaust Noise Radiation Experiments - Part 1: Polar Directivity Measurements" @default.
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- W2099945681 doi "https://doi.org/10.2514/6.2008-2857" @default.
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