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Modelling jet-surface interaction noise from cranked wings

Modelling jet-surface interaction noise from cranked wings
Modelling jet-surface interaction noise from cranked wings
A strip implementation of Amiet’s theory has been used to model the jet-surface interaction noise produced by the cranked wing geometry seen on commercial jet airliners. Because it is the geometry that has changed between strips, not the incident pressure, the noise produced by each strip has been summed coherently. This coherent addition has been verified as converging on the infinite-span solution as the number of strips is increased, and to equal that of a single strip of the same overall span. Jet-surface interaction noise predictions from both strip and infinite-span implementations of Amiet’s theory have been validated against installed jet noise measurements with a low aspect ratio plate. The finite span implementation shows an improvement in spectra at low frequencies, however, it under-predicts at azimuthal observer angles near the plane of the plate. Finally, the OASPL directivity of a cranked wing has been calculated both using strip theory and assuming infinite span (both swept and unswept). Of the three, the strip theory model agrees best with the measured data.
Dawson, Martin
f75e1b11-09a9-4548-8f17-2810914c785a
Lawrence, Jack
59a5a96a-8824-4bae-a22a-739ad4ce9144
Self, Rodney
8b96166d-fc06-48e7-8c76-ebb3874b0ef7
Kingan, Michael
602dbb17-6645-44bc-bb8c-825c17671b18
Dawson, Martin
f75e1b11-09a9-4548-8f17-2810914c785a
Lawrence, Jack
59a5a96a-8824-4bae-a22a-739ad4ce9144
Self, Rodney
8b96166d-fc06-48e7-8c76-ebb3874b0ef7
Kingan, Michael
602dbb17-6645-44bc-bb8c-825c17671b18

Dawson, Martin, Lawrence, Jack, Self, Rodney and Kingan, Michael (2020) Modelling jet-surface interaction noise from cranked wings. In AIAA Aviation 2020 Forum. (doi:10.2514/6.2020-2551).

Record type: Conference or Workshop Item (Paper)

Abstract

A strip implementation of Amiet’s theory has been used to model the jet-surface interaction noise produced by the cranked wing geometry seen on commercial jet airliners. Because it is the geometry that has changed between strips, not the incident pressure, the noise produced by each strip has been summed coherently. This coherent addition has been verified as converging on the infinite-span solution as the number of strips is increased, and to equal that of a single strip of the same overall span. Jet-surface interaction noise predictions from both strip and infinite-span implementations of Amiet’s theory have been validated against installed jet noise measurements with a low aspect ratio plate. The finite span implementation shows an improvement in spectra at low frequencies, however, it under-predicts at azimuthal observer angles near the plane of the plate. Finally, the OASPL directivity of a cranked wing has been calculated both using strip theory and assuming infinite span (both swept and unswept). Of the three, the strip theory model agrees best with the measured data.

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More information

Published date: 8 June 2020
Venue - Dates: AIAA 2020 Aviation Forum, Virtual, 2020-06-15 - 2020-06-19

Identifiers

Local EPrints ID: 476388
URI: http://eprints.soton.ac.uk/id/eprint/476388
PURE UUID: 64665bfd-bc15-4c93-95df-5832d42b2caf

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Date deposited: 19 Apr 2023 16:50
Last modified: 17 Mar 2024 01:57

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Contributors

Author: Martin Dawson
Author: Jack Lawrence
Author: Rodney Self
Author: Michael Kingan

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