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
✦ LIBER ✦
A new model for the cross spectrum and wavenumber-frequency spectrum of turbulent pressure fluctuations in a boundary layer
✍ Scribed by A. V. Smol’yakov
- Book ID
- 110215592
- Publisher
- SP MAIK Nauka/Interperiodica
- Year
- 2006
- Tongue
- English
- Weight
- 223 KB
- Volume
- 52
- Category
- Article
- ISSN
- 1063-7710
No coin nor oath required. For personal study only.
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