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On the universal trends in the noise reduction due to wavy leading edges in aerofoil-vortex interaction

On the universal trends in the noise reduction due to wavy leading edges in aerofoil-vortex interaction
On the universal trends in the noise reduction due to wavy leading edges in aerofoil-vortex interaction
Existing studies suggest that wavy leading edges (WLEs) offer substantial reduction of broadband noise generated by an aerofoil undergoing upstream vortical disturbances. In this context, there are two universal trends in the frequency spectra of the noise reduction which have been observed and reported to date: (i) no significant reduction at low frequencies followed by (ii) a rapid growth of the noise reduction that persists in the medium-to-high frequency range. These trends are known to be insensitive to the aerofoil type and flow condition used. This paper aims to provide comprehensive understandings as to how these universal trends are formed and what the major drivers are. The current work is based on very-high-resolution numerical simulations of a semi-infinite flat-plate aerofoil impinged by a prescribed divergence-free vortex in an inviscid base flow at zero incidence angle, continued from recent work by the authors (Turner & Kim, J. Fluid Mech., vol. 811, 2017, pp. 582–611). One of the most significant findings in the current work is that the noise source distribution on the aerofoil surface becomes entirely two-dimensional (highly non-uniform in the spanwise direction as well as streamwise) at high frequencies when the WLE is involved. Also, the sources downstream of the LE make crucial contributions to creating the universal trends across all frequencies. These findings contradict the conventional LE-focused one-dimensional source analysis that has widely been accepted for all frequencies. The current study suggests that the universal trends in the noise-reduction spectra can be properly understood by taking the downstream source contributions into account, in terms of both magnitude and phase variations. After including the downstream sources, it is shown in this paper that the first universal trend is due to the conservation of total (surface integrated) source energy at low frequencies. The surface-integrated source magnitude that decreases faster with the WLE correlates very well with the noise-reduction spectrum at medium frequencies. In the meantime, the high-frequency noise reduction is driven almost entirely by destructive phase interference that increases rapidly and consistently with frequency, explaining the second universal trend.
0022-1120
186-211
Turner, Jacob
8618df92-3b0c-46e6-a482-dd12b261d9a7
Kim, Jae
fedabfc6-312c-40fd-b0c1-7b4a3ca80987
Turner, Jacob
8618df92-3b0c-46e6-a482-dd12b261d9a7
Kim, Jae
fedabfc6-312c-40fd-b0c1-7b4a3ca80987

Turner, Jacob and Kim, Jae (2019) On the universal trends in the noise reduction due to wavy leading edges in aerofoil-vortex interaction. Journal of Fluid Mechanics, 871, 186-211. (doi:10.1017/jfm.2019.314).

Record type: Article

Abstract

Existing studies suggest that wavy leading edges (WLEs) offer substantial reduction of broadband noise generated by an aerofoil undergoing upstream vortical disturbances. In this context, there are two universal trends in the frequency spectra of the noise reduction which have been observed and reported to date: (i) no significant reduction at low frequencies followed by (ii) a rapid growth of the noise reduction that persists in the medium-to-high frequency range. These trends are known to be insensitive to the aerofoil type and flow condition used. This paper aims to provide comprehensive understandings as to how these universal trends are formed and what the major drivers are. The current work is based on very-high-resolution numerical simulations of a semi-infinite flat-plate aerofoil impinged by a prescribed divergence-free vortex in an inviscid base flow at zero incidence angle, continued from recent work by the authors (Turner & Kim, J. Fluid Mech., vol. 811, 2017, pp. 582–611). One of the most significant findings in the current work is that the noise source distribution on the aerofoil surface becomes entirely two-dimensional (highly non-uniform in the spanwise direction as well as streamwise) at high frequencies when the WLE is involved. Also, the sources downstream of the LE make crucial contributions to creating the universal trends across all frequencies. These findings contradict the conventional LE-focused one-dimensional source analysis that has widely been accepted for all frequencies. The current study suggests that the universal trends in the noise-reduction spectra can be properly understood by taking the downstream source contributions into account, in terms of both magnitude and phase variations. After including the downstream sources, it is shown in this paper that the first universal trend is due to the conservation of total (surface integrated) source energy at low frequencies. The surface-integrated source magnitude that decreases faster with the WLE correlates very well with the noise-reduction spectrum at medium frequencies. In the meantime, the high-frequency noise reduction is driven almost entirely by destructive phase interference that increases rapidly and consistently with frequency, explaining the second universal trend.

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Accepted Manuscript - Turner & Kim - Accepted Manuscript
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Accepted/In Press date: 11 April 2019
e-pub ahead of print date: 17 May 2019
Published date: 25 July 2019

Identifiers

Local EPrints ID: 430735
URI: http://eprints.soton.ac.uk/id/eprint/430735
ISSN: 0022-1120
PURE UUID: 2032a520-62d8-4dcf-899c-72a8196cc3f9
ORCID for Jacob Turner: ORCID iD orcid.org/0000-0002-0522-4340
ORCID for Jae Kim: ORCID iD orcid.org/0000-0003-0476-2574

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Date deposited: 09 May 2019 16:30
Last modified: 16 Mar 2024 07:49

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Author: Jacob Turner ORCID iD
Author: Jae Kim ORCID iD

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