On the effects of sound in subsonic boundary layer flows
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Accepted version
Author(s)
Raposo, H
Mughal, MS
Ashworth, R
Type
Conference Paper
Abstract
The study of acoustic receptivity in quiet disturbance environments can be
decomposed into several sub-problems. One such problem consists of determining the response of the unsteady boundary layer to acoustic forcing in the freestream. In this paper, we describe two methods to characterize the acoustic boundary layer response based on the linear stability equations. In their inviscid form, we first show how to determine the reflection coefficient. The sum of the incident and reflected waves then drives the unsteady Stokes motion within the boundary layer, for which a double-layer high Strouhal number asymptotic solution is obtained. The outer layer solution is calculated numerically whereas the inner layer solution, introduced to satisfy the no-slip condition, is determined analytically. The full linear stability equations can also be integrated numerically to directly obtain a complete disturbance profile accounting for the effects of viscosity. A comparison between these models and the linearised unsteady boundary layer equation (LUBLE) model shows good agreement at high Strouhal number, low Mach number and for downstream-travelling waves. However, for near sonic Mach numbers and for upstream-travelling waves, the LUBLE are shown to be not valid because the assumption that the acoustic wavelength is long compared to the boundary layer thickness no longer holds.
decomposed into several sub-problems. One such problem consists of determining the response of the unsteady boundary layer to acoustic forcing in the freestream. In this paper, we describe two methods to characterize the acoustic boundary layer response based on the linear stability equations. In their inviscid form, we first show how to determine the reflection coefficient. The sum of the incident and reflected waves then drives the unsteady Stokes motion within the boundary layer, for which a double-layer high Strouhal number asymptotic solution is obtained. The outer layer solution is calculated numerically whereas the inner layer solution, introduced to satisfy the no-slip condition, is determined analytically. The full linear stability equations can also be integrated numerically to directly obtain a complete disturbance profile accounting for the effects of viscosity. A comparison between these models and the linearised unsteady boundary layer equation (LUBLE) model shows good agreement at high Strouhal number, low Mach number and for downstream-travelling waves. However, for near sonic Mach numbers and for upstream-travelling waves, the LUBLE are shown to be not valid because the assumption that the acoustic wavelength is long compared to the boundary layer thickness no longer holds.
Editor(s)
Sherwin, S
Schmid, P
Wu, Xuesong
Date Issued
2021-07-31
Date Acceptance
2019-12-12
Citation
IUTAM Laminar-Turbulent Transition, 2021, 38, pp.1-1
ISBN
3030679012
9783030679019
Publisher
Springer
Start Page
1
End Page
1
Journal / Book Title
IUTAM Laminar-Turbulent Transition
Volume
38
Copyright Statement
© 2021 The Editor(s) (if applicable) and The Author(s), under exclusive license to Springer Nature Switzerland AG. The final publication is available at Springer via https://dx.doi.org/10.1007/978-3-030-67902-6
Sponsor
Innovate UK
Identifier
http://hdl.handle.net/10044/1/88926
Grant Number
113022
Source
9th IUTAM Symposium on Laminar-Turbulent Transition
Publication Status
Published
Start Date
2019-09-02
Finish Date
2019-09-06
Coverage Spatial
Imperial College London
Date Publish Online
2021-07-31