A COMPARISON OF MODELS FOR THE WAVENUMBE
A COMPARISON OF MODELS FOR THE WAVENUMBERβFREQUENCY SPECTRUM OF TURBULENT BOUNDARY LAYER PRESSURES
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W.R. Graham
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Article
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1997
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Elsevier Science
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English
β 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