A COMPARISON OF MODELS FOR THE WAVENUMBE
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W.R. Graham
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Article
📅
1997
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Elsevier Science
🌐
English
⚖ 366 KB
Aircraft cabin noise due to the fuselage boundary layer is determined by, among other factors, the wavenumber-frequency spectrum of the fluctuating boundary layer pressures, a quantity for which a number of models have been proposed. In this work predictions for the sound radiated by a boundary laye