Acoustic Radiation of a Turbulent Boundary Layer Over a Flat Smooth Boundary

Abstract A consistent theory of sound generation in a turbulent boundary layer developing over a flat smooth boundary at low Mach numbers is presented. The main source of sound and the long-wavelength part of pressure fluctuations on the boundary are incoming shear (viscous) waves generated by Lighthill quadrupoles in the near-wall region of the turbulent boundary layer. It is shown that with an increase in the Reynolds number (decrease in viscosity), the role of viscosity in sound generation does not decrease, but instead increases. Quantitative estimates of the spectrum of the sound power density generated in a turbulent boundary layer are given.

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Publication Details

Journal
Acoustical Physics
Published
2024-12-01
DOI
https://doi.org/10.1134/s1063771024603133
Citations
1
Primary Topic
Aerodynamics and Acoustics in Jet Flows
Type
article
Field-Weighted Citation Impact
1.30
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article

Acoustic Radiation of a Turbulent Boundary Layer Over a Flat Smooth Boundary

V. F. Kopiev, I. V. Belyaev, M. A. Mironov
1 citations
Acoustical Physics
Aerodynamics and Acoustics in Jet Flows
1.30
article

Acoustic Radiation of a Turbulent Boundary Layer Over a Flat Smooth Boundary

V. F. Kopiev, I. V. Belyaev, M. A. Mironov
article en
1 citations

Abstract

Abstract A consistent theory of sound generation in a turbulent boundary layer developing over a flat smooth boundary at low Mach numbers is presented. The main source of sound and the long-wavelength part of pressure fluctuations on the boundary are incoming shear (viscous) waves generated by Lighthill quadrupoles in the near-wall region of the turbulent boundary layer. It is shown that with an increase in the Reynolds number (decrease in viscosity), the role of viscosity in sound generation does not decrease, but instead increases. Quantitative estimates of the spectrum of the sound power density generated in a turbulent boundary layer are given.

Acoustical PhysicsVol. 70(6)
Moscow Regional Research Institute of Obstetrics and Gynecology (RU)
Openalex Percentile: Top 11%
Aerodynamics and Acoustics in Jet Flows
1.30
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