Downstream perforations for the reduction of turbulence-aerofoil interaction noise: Part II - theoretical investigation
Downstream perforations for the reduction of turbulence-aerofoil interaction noise: Part II - theoretical investigation
This paper presents a theoretical study of introducing a single gap or slot downstream of the leading edge of a thin rigid plate on aeroacoustic scattering. This is investigated as an elementary model for understanding the effect of downstream perforations on gust-aerofoil interaction noise. Across the slot it is supposed there is zero pressure jump, and a wake is shed from the upstream slot edge such that an unsteady Kutta condition is satisfied. The resulting mixed boundary value problem is reformulated as a Wiener–Hopf problem, and reduced to asingular integral equation suitable for numerical solution. Wave components of the solution may be identified, and plausibly related to diffracted fields by each junction. Theoretical results are compared to experimental results considering sets of perforations. The model is found to be in line with overall qualitative trends in the change in far-field sound power level observed experimentally, but does not account for oscillations from this trend.
Priddin, Matthew
ad066553-99e6-4373-942a-f6413fffd2fc
Ayton, Lorna
e38b13c1-fd88-4b3e-9115-f9fa80c8b538
Palleja Cabre, Sergi
b841a96c-05d1-4f08-a197-8693cb3a3f90
Paruchuri, Chaitanya
5c1def64-6347-4be3-ac2d-b9f6a314b81d
Joseph, Phillip
9c30491e-8464-4c9a-8723-2abc62bdf75d
2 August 2021
Priddin, Matthew
ad066553-99e6-4373-942a-f6413fffd2fc
Ayton, Lorna
e38b13c1-fd88-4b3e-9115-f9fa80c8b538
Palleja Cabre, Sergi
b841a96c-05d1-4f08-a197-8693cb3a3f90
Paruchuri, Chaitanya
5c1def64-6347-4be3-ac2d-b9f6a314b81d
Joseph, Phillip
9c30491e-8464-4c9a-8723-2abc62bdf75d
Priddin, Matthew, Ayton, Lorna, Palleja Cabre, Sergi, Paruchuri, Chaitanya and Joseph, Phillip
(2021)
Downstream perforations for the reduction of turbulence-aerofoil interaction noise: Part II - theoretical investigation.
In AIAA AVIATION 2021 FORUM.
(doi:10.2514/6.2021-2147).
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Conference or Workshop Item
(Paper)
Abstract
This paper presents a theoretical study of introducing a single gap or slot downstream of the leading edge of a thin rigid plate on aeroacoustic scattering. This is investigated as an elementary model for understanding the effect of downstream perforations on gust-aerofoil interaction noise. Across the slot it is supposed there is zero pressure jump, and a wake is shed from the upstream slot edge such that an unsteady Kutta condition is satisfied. The resulting mixed boundary value problem is reformulated as a Wiener–Hopf problem, and reduced to asingular integral equation suitable for numerical solution. Wave components of the solution may be identified, and plausibly related to diffracted fields by each junction. Theoretical results are compared to experimental results considering sets of perforations. The model is found to be in line with overall qualitative trends in the change in far-field sound power level observed experimentally, but does not account for oscillations from this trend.
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e-pub ahead of print date: 28 July 2021
Published date: 2 August 2021
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Local EPrints ID: 452757
URI: http://eprints.soton.ac.uk/id/eprint/452757
PURE UUID: 3d7cbc8a-e31e-456f-a571-42da14a9455e
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Date deposited: 17 Dec 2021 18:21
Last modified: 17 Mar 2024 03:48
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Author:
Matthew Priddin
Author:
Lorna Ayton
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