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Experimental study of the aerodynamic noise radiated by cylinders with different cross-sections and yaw angles

Experimental study of the aerodynamic noise radiated by cylinders with different cross-sections and yaw angles
Experimental study of the aerodynamic noise radiated by cylinders with different cross-sections and yaw angles
Vortex shedding from cylinders has been extensively studied due to its occurrence in many engineering fields. Many experimental studies reported in the literature focus on the aerodynamics of the vortex shedding process but the literature about the radiated noise is more scarce. The aim of the work presented here is to extend the available noise data. Aero-acoustic wind tunnel tests were carried out using cylinders with different cross-sections: circular, square, rectangular and elliptical. Flow speeds between 20 and 50 m/s were used, corresponding to Reynolds numbers in the range from 1.6×104 to 1.2×105. The dependence of the noise on the yaw angle, flow speed, cross-sectional shape, angle of attack and radiation angle (directivity) is assessed. The results obtained are compared, where possible, with those found in the literature for similar cases. It is intended that the results can be used for the validation and calibration of numerical and empirical aerodynamic noise prediction models.
0022-460X
108-129
Latorre Iglesias, Eduardo
3cdb7920-9f71-48fa-8f09-34557e5ce9a4
Thompson, David
bca37fd3-d692-4779-b663-5916b01edae5
Smith, Malcolm
1bc8608d-0178-4793-8f73-46a6c6b9b279
Latorre Iglesias, Eduardo
3cdb7920-9f71-48fa-8f09-34557e5ce9a4
Thompson, David
bca37fd3-d692-4779-b663-5916b01edae5
Smith, Malcolm
1bc8608d-0178-4793-8f73-46a6c6b9b279

Latorre Iglesias, Eduardo, Thompson, David and Smith, Malcolm (2016) Experimental study of the aerodynamic noise radiated by cylinders with different cross-sections and yaw angles. Journal of Sound and Vibration, 361, 108-129. (doi:10.1016/j.jsv.2015.09.044).

Record type: Article

Abstract

Vortex shedding from cylinders has been extensively studied due to its occurrence in many engineering fields. Many experimental studies reported in the literature focus on the aerodynamics of the vortex shedding process but the literature about the radiated noise is more scarce. The aim of the work presented here is to extend the available noise data. Aero-acoustic wind tunnel tests were carried out using cylinders with different cross-sections: circular, square, rectangular and elliptical. Flow speeds between 20 and 50 m/s were used, corresponding to Reynolds numbers in the range from 1.6×104 to 1.2×105. The dependence of the noise on the yaw angle, flow speed, cross-sectional shape, angle of attack and radiation angle (directivity) is assessed. The results obtained are compared, where possible, with those found in the literature for similar cases. It is intended that the results can be used for the validation and calibration of numerical and empirical aerodynamic noise prediction models.

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Accepted/In Press date: 28 September 2015
e-pub ahead of print date: 23 October 2015
Published date: 20 January 2016
Organisations: Dynamics Group

Identifiers

Local EPrints ID: 383766
URI: http://eprints.soton.ac.uk/id/eprint/383766
ISSN: 0022-460X
PURE UUID: b54f9512-f0a4-4b7a-bd2b-05da835dca2e
ORCID for David Thompson: ORCID iD orcid.org/0000-0002-7964-5906

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Date deposited: 30 Nov 2015 12:06
Last modified: 15 Mar 2024 02:53

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Contributors

Author: Eduardo Latorre Iglesias
Author: David Thompson ORCID iD
Author: Malcolm Smith

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