The Effect of Steady Flow Distortion on Acoustic Mode Propagation in a Straight Annular Duct
The Effect of Steady Flow Distortion on Acoustic Mode Propagation in a Straight Annular Duct
Steady flow distortion in turbofan intakes results from non-axisymmetric nacelle geometry and non-zero flow incidence. It may have a significant effect on the propagation and attenuation of acoustic modes generated by the fan propagating through a lined intake. In order to study this effect, the propagation of a single incident mode of the azimuthal order m through a circumferentially distorted axial mean flow in a uniform, lined annular duct has been calculated by using an ACTRAN TM model and compared to results obtained by an eigenmode approach to validate both methods.
Turbofan engine noise, Fan noise, Aircraft noise, computational aeroacoustics (CAA), ACOUSTICS, Aeroacoustics, PREDICTION, ACTRAN
Prinn, Albert G.
002e8d99-00a1-487e-a8ec-510c9f703a5b
Astley, Richard Jeremy
cb7fed9f-a96a-4b58-8939-6db1010f9893
Sugimoto, Rie
cb8c880d-0be0-4efe-9990-c79faa8804f0
Rarata, Zbigniew
93cc0733-a371-48ff-916c-720f149e2f2d
October 2014
Prinn, Albert G.
002e8d99-00a1-487e-a8ec-510c9f703a5b
Astley, Richard Jeremy
cb7fed9f-a96a-4b58-8939-6db1010f9893
Sugimoto, Rie
cb8c880d-0be0-4efe-9990-c79faa8804f0
Rarata, Zbigniew
93cc0733-a371-48ff-916c-720f149e2f2d
Prinn, Albert G., Astley, Richard Jeremy, Sugimoto, Rie and Rarata, Zbigniew
(2014)
The Effect of Steady Flow Distortion on Acoustic Mode Propagation in a Straight Annular Duct.
FFT Acoustic Simulation Conference 2014: Actran Users' Meeting, Diamant Conference & Business Centre, Brussels, Belgium.
15 - 16 Oct 2014.
25 pp
.
Record type:
Conference or Workshop Item
(Other)
Abstract
Steady flow distortion in turbofan intakes results from non-axisymmetric nacelle geometry and non-zero flow incidence. It may have a significant effect on the propagation and attenuation of acoustic modes generated by the fan propagating through a lined intake. In order to study this effect, the propagation of a single incident mode of the azimuthal order m through a circumferentially distorted axial mean flow in a uniform, lined annular duct has been calculated by using an ACTRAN TM model and compared to results obtained by an eigenmode approach to validate both methods.
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Published date: October 2014
Additional Information:
Presentation only
Venue - Dates:
FFT Acoustic Simulation Conference 2014: Actran Users' Meeting, Diamant Conference & Business Centre, Brussels, Belgium, 2014-10-15 - 2014-10-16
Keywords:
Turbofan engine noise, Fan noise, Aircraft noise, computational aeroacoustics (CAA), ACOUSTICS, Aeroacoustics, PREDICTION, ACTRAN
Identifiers
Local EPrints ID: 426805
URI: http://eprints.soton.ac.uk/id/eprint/426805
PURE UUID: 6f6111b7-a73c-4e94-b4b6-47f1b3885f75
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Date deposited: 12 Dec 2018 17:31
Last modified: 16 Mar 2024 03:36
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Contributors
Author:
Albert G. Prinn
Author:
Zbigniew Rarata
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