National Acoustic Laboratories Library

Statistical estimation of trailing edge noise from finite wall-mounted airfoils (Record no. 2680)

MARC details
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fixed length control field nam a22 7a 4500
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control field OSt
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control field 20170106161907.0
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fixed length control field 170106b xxu||||| |||| 00| 0 eng d
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Transcribing agency National Acoustics Laboratories
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Title Statistical estimation of trailing edge noise from finite wall-mounted airfoils
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Summary, etc It is important to be able to accurately model the flow and noise generated by finite wall-mounted airfoil flows because of the many engineering applications in which these flows occur. One method for predicting turbulent trailing edge noise is the Reynolds-averaged Navier-Stokes based statistical noise model (RSNM) of Doolan et al. (Proceedings of 20th International Congress on Acoustics, ICA 2010). The RSNM method has previously been used successfully on a range of two-dimensional geometry-flow cases. In this paper a new turbulent velocity cross-spectrum model and improved implementation are proposed to allow the RSNM method to be used to effectively and efficiently predict turbulent trailing edge noise from more complex three-dimensional cases. Reynolds-averaged Navier-Stokes (RANS) simulations of a series of wing-in-junction cases are used in combination with the developed acoustic model to predict the far-field noise and compared against experimental noise measurements.
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Personal name Jesse Coombs
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Relationship information Proceedings 9-11 November 2016, Brisbane, Australia
Title Acoustics 2016
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Uniform Resource Identifier <a href="http://dspace.nal.gov.au/xmlui/bitstream/handle/123456789/540/p39.pdf?sequence=3&isAllowed=y">http://dspace.nal.gov.au/xmlui/bitstream/handle/123456789/540/p39.pdf?sequence=3&isAllowed=y</a>
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Source of classification or shelving scheme Universal Decimal Classification
Koha item type Journal article

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