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Reduction of propeller-strut interaction noise by porosity

Reduction of propeller-strut interaction noise by porosity
Reduction of propeller-strut interaction noise by porosity

Propeller operation in close proximity to a strut involves interactions from multiple sources, significantly contributing to noise generation. This study aims to reduce this interaction noise by employing a porous strut as a noise mitigation strategy. The paper presents experimental measurements of far-field noise for three types of rods: two solid rods with varying diameters and one porous rod. These rods were installed both upstream and downstream of the propeller flow at various distances. The porous rod proved to be an effective noise mitigation device, demonstrating reductions in Overall Acoustic Power Levels (OAPWL) of up to 3 dB when placed downstream and up to 6dB when placed upstream of the propeller. The study also introduced an analytical framework designed to predict the unsteady lift on propellers due to porous struts situated downstream. The model utilizes the potential function around porous cylinders to derive the upwash velocity induced on the propeller, thereby estimating the unsteady lift on the propellers. This model provides a valuable tool for understanding and quantifying the noise reduction capabilities of porous struts in practical applications, with the analytical predictions showing trends similar to the experimental data. Numerical simulations are also performed as part of the study to evaluate the unsteady lift from the propeller and understand the flow physics causing these lift variations. These simulations revealed that even minor fluctuations in unsteady loading could lead to substantial increases in radiated noise at higher harmonics, emphasizing the importance of precise control in mitigating noise.

American Institute of Aeronautics and Astronautics
Crawshaw, Luca
94b61e36-5ff4-442e-bde6-c094b12b6e46
Karimian, Amin
8f2e1624-afff-4e07-b2cd-e780209608d7
Paruchuri, Chaitanya C.
5c1def64-6347-4be3-ac2d-b9f6a314b81d
Parry, A.B.
77463a31-d1dd-4f20-9ec3-9cce4f5972b2
Palleja-Cabre, Sergi
b841a96c-05d1-4f08-a197-8693cb3a3f90
Arcondoulis, Elias
0fd27ccb-de74-454e-8c91-28b636b54d1d
Crawshaw, Luca
94b61e36-5ff4-442e-bde6-c094b12b6e46
Karimian, Amin
8f2e1624-afff-4e07-b2cd-e780209608d7
Paruchuri, Chaitanya C.
5c1def64-6347-4be3-ac2d-b9f6a314b81d
Parry, A.B.
77463a31-d1dd-4f20-9ec3-9cce4f5972b2
Palleja-Cabre, Sergi
b841a96c-05d1-4f08-a197-8693cb3a3f90
Arcondoulis, Elias
0fd27ccb-de74-454e-8c91-28b636b54d1d

Crawshaw, Luca, Karimian, Amin, Paruchuri, Chaitanya C., Parry, A.B., Palleja-Cabre, Sergi and Arcondoulis, Elias (2024) Reduction of propeller-strut interaction noise by porosity. In 30th AIAA/CEAS Aeroacoustics Conference, 2024. American Institute of Aeronautics and Astronautics.. (doi:10.2514/6.2024-3386).

Record type: Conference or Workshop Item (Paper)

Abstract

Propeller operation in close proximity to a strut involves interactions from multiple sources, significantly contributing to noise generation. This study aims to reduce this interaction noise by employing a porous strut as a noise mitigation strategy. The paper presents experimental measurements of far-field noise for three types of rods: two solid rods with varying diameters and one porous rod. These rods were installed both upstream and downstream of the propeller flow at various distances. The porous rod proved to be an effective noise mitigation device, demonstrating reductions in Overall Acoustic Power Levels (OAPWL) of up to 3 dB when placed downstream and up to 6dB when placed upstream of the propeller. The study also introduced an analytical framework designed to predict the unsteady lift on propellers due to porous struts situated downstream. The model utilizes the potential function around porous cylinders to derive the upwash velocity induced on the propeller, thereby estimating the unsteady lift on the propellers. This model provides a valuable tool for understanding and quantifying the noise reduction capabilities of porous struts in practical applications, with the analytical predictions showing trends similar to the experimental data. Numerical simulations are also performed as part of the study to evaluate the unsteady lift from the propeller and understand the flow physics causing these lift variations. These simulations revealed that even minor fluctuations in unsteady loading could lead to substantial increases in radiated noise at higher harmonics, emphasizing the importance of precise control in mitigating noise.

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More information

e-pub ahead of print date: 30 May 2024
Venue - Dates: 30th AIAA/CEAS Aeroacoustics Conference, 2024, , Rome, Italy, 2023-06-04 - 2023-06-07

Identifiers

Local EPrints ID: 495333
URI: http://eprints.soton.ac.uk/id/eprint/495333
PURE UUID: 658c24ef-98d1-46b1-abb9-064d545a90a0
ORCID for Amin Karimian: ORCID iD orcid.org/0000-0002-1282-9153
ORCID for Sergi Palleja-Cabre: ORCID iD orcid.org/0000-0002-5414-7716

Catalogue record

Date deposited: 11 Nov 2024 17:33
Last modified: 12 Nov 2024 03:08

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Contributors

Author: Luca Crawshaw
Author: Amin Karimian ORCID iD
Author: A.B. Parry
Author: Elias Arcondoulis

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