On the effect of inflow distortions of propeller noise
On the effect of inflow distortions of propeller noise
Propellers usually operate in non-uniform flows, which is expected to modify the behaviour of the emitted noise field. In this framework, an experimental campaign with far-field noise measurements of a two-blade propeller, immersed in a non-uniform flow, has been performed in the anechoic facility at the University of Southampton. A parametric analysis of the effects of different flow non-uniformities, generated by different masks positioned at the nozzle exhaust, was performed at constant thrust. Results show that non-uniformities in the incoming flow exalt the interaction tones. Tonal peaks, starting from the third blade passage frequency harmonic, register variations in the order of tens of decibels, up to a maximum of 12db. Experimental outcomes are compared with tonal noise predictions obtained by using a frequency domain formulation, based on integrating the aerodynamic sources on the proper surface of the blade. The model captures the main features of the interaction tones and a good agreement is reached between measured and predicted values in both sound pressure levels and directivity.
Petricelli, Federico
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Palleja Cabre, Sergi
b841a96c-05d1-4f08-a197-8693cb3a3f90
Paruchuri, Chaitanya
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Joseph, Phillip
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Karimian, Amin
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Meloni, Stefano
9c310e86-4f90-4f61-a649-0b11763f0674
Camussi, Roberto
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Petricelli, Federico
8698b4b1-23cd-4932-9d62-f04a65e314a4
Palleja Cabre, Sergi
b841a96c-05d1-4f08-a197-8693cb3a3f90
Paruchuri, Chaitanya
5c1def64-6347-4be3-ac2d-b9f6a314b81d
Joseph, Phillip
9c30491e-8464-4c9a-8723-2abc62bdf75d
Karimian, Amin
8f2e1624-afff-4e07-b2cd-e780209608d7
Meloni, Stefano
9c310e86-4f90-4f61-a649-0b11763f0674
Camussi, Roberto
0da46d12-0aa9-4c11-9e06-a22ff80e79dc
Petricelli, Federico, Palleja Cabre, Sergi, Paruchuri, Chaitanya, Joseph, Phillip, Karimian, Amin, Meloni, Stefano and Camussi, Roberto
(2022)
On the effect of inflow distortions of propeller noise.
In 28th AIAA/CEAS Aeroacoustics Conference, 2022.
(doi:10.2514/6.2022-2938).
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Conference or Workshop Item
(Paper)
Abstract
Propellers usually operate in non-uniform flows, which is expected to modify the behaviour of the emitted noise field. In this framework, an experimental campaign with far-field noise measurements of a two-blade propeller, immersed in a non-uniform flow, has been performed in the anechoic facility at the University of Southampton. A parametric analysis of the effects of different flow non-uniformities, generated by different masks positioned at the nozzle exhaust, was performed at constant thrust. Results show that non-uniformities in the incoming flow exalt the interaction tones. Tonal peaks, starting from the third blade passage frequency harmonic, register variations in the order of tens of decibels, up to a maximum of 12db. Experimental outcomes are compared with tonal noise predictions obtained by using a frequency domain formulation, based on integrating the aerodynamic sources on the proper surface of the blade. The model captures the main features of the interaction tones and a good agreement is reached between measured and predicted values in both sound pressure levels and directivity.
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e-pub ahead of print date: 30 June 2022
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Funding Information:
The authors would like to acknowledge the financial support of the Royal Academy of Engineering (RF\201819 \ 18 \ 194). The first author would also like to thank Suresh Palani for his help during experimental measurements.
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© 2022, American Institute of Aeronautics and Astronautics Inc, AIAA., All rights reserved.
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Local EPrints ID: 468398
URI: http://eprints.soton.ac.uk/id/eprint/468398
PURE UUID: b9f737a8-4319-45fc-81df-0a7e224efc0c
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Date deposited: 12 Aug 2022 21:17
Last modified: 17 Mar 2024 04:10
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Author:
Federico Petricelli
Author:
Stefano Meloni
Author:
Roberto Camussi
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