The University of Southampton
University of Southampton Institutional Repository

Measurements and control of aircraft's main landing gear broadband noise

Measurements and control of aircraft's main landing gear broadband noise
Measurements and control of aircraft's main landing gear broadband noise
Noise generated by aircraft landing gear is a major contributor to the overall airframe noise during landing approach of a commercial aircraft. Fairings covering geometrically complex areas of the gears have proved to be very effective in noise reduction, but in tests on an A340 main landing gear the overall benefits of the fairings were offset by an increase in low-frequency noise. In this study the measurement and control of broadband noise throughout the frequency range have been investigated using a 1/4 scale A340 main landing gear model that has been tested using a range of different measurement methods and wind facilities. Experiments were firstly conducted in a conventional closed-section wind tunnel using two phased microphone arrays mounted on the ceiling and sidewall of the tunnel respectively, and noise control strategies with modified fairings were developed. Noise tests were then performed in an open-jet aeroacoustic facility using far-field microphones to verify the wind-tunnel test results. Comparison between the two tests showed that the relatively smaller noise-reduction potential of the fairings measured in wind tunnel was due to the higher flow blockage of the tunnel. Nevertheless, the experiments indicated that the phased microphone arrays could be applied to measure the noise reductions achieved by noise control treatments with reasonable accuracy, especially in mid- and high-frequency range. The aeroacoustic facility test results were finally projected to full scale and compared to the full-scale model wind-tunnel test. Both results were shown to agree over a wide frequency range, indicating the validity of the tests on the 1/4 scale model.
landing gear noise, noise control, aeroacoustic measurements, beamforming technique
1270-9638
Li, Yong
ac705db5-b891-4d14-ac43-a87acd05cdd7
Smith, Malcolm
1bc8608d-0178-4793-8f73-46a6c6b9b279
Zhang, Xin
3056a795-80f7-4bbd-9c75-ecbc93085421
Li, Yong
ac705db5-b891-4d14-ac43-a87acd05cdd7
Smith, Malcolm
1bc8608d-0178-4793-8f73-46a6c6b9b279
Zhang, Xin
3056a795-80f7-4bbd-9c75-ecbc93085421

Li, Yong, Smith, Malcolm and Zhang, Xin (2011) Measurements and control of aircraft's main landing gear broadband noise. Aerospace Science and Technology. (doi:10.1016/j.ast.2011.07.009).

Record type: Article

Abstract

Noise generated by aircraft landing gear is a major contributor to the overall airframe noise during landing approach of a commercial aircraft. Fairings covering geometrically complex areas of the gears have proved to be very effective in noise reduction, but in tests on an A340 main landing gear the overall benefits of the fairings were offset by an increase in low-frequency noise. In this study the measurement and control of broadband noise throughout the frequency range have been investigated using a 1/4 scale A340 main landing gear model that has been tested using a range of different measurement methods and wind facilities. Experiments were firstly conducted in a conventional closed-section wind tunnel using two phased microphone arrays mounted on the ceiling and sidewall of the tunnel respectively, and noise control strategies with modified fairings were developed. Noise tests were then performed in an open-jet aeroacoustic facility using far-field microphones to verify the wind-tunnel test results. Comparison between the two tests showed that the relatively smaller noise-reduction potential of the fairings measured in wind tunnel was due to the higher flow blockage of the tunnel. Nevertheless, the experiments indicated that the phased microphone arrays could be applied to measure the noise reductions achieved by noise control treatments with reasonable accuracy, especially in mid- and high-frequency range. The aeroacoustic facility test results were finally projected to full scale and compared to the full-scale model wind-tunnel test. Both results were shown to agree over a wide frequency range, indicating the validity of the tests on the 1/4 scale model.

This record has no associated files available for download.

More information

Submitted date: 2011
e-pub ahead of print date: 27 July 2011
Keywords: landing gear noise, noise control, aeroacoustic measurements, beamforming technique
Organisations: Aerodynamics & Flight Mechanics

Identifiers

Local EPrints ID: 185839
URI: http://eprints.soton.ac.uk/id/eprint/185839
ISSN: 1270-9638
PURE UUID: 0c5284f7-1aa1-4391-8f95-7cae4ecd70a1

Catalogue record

Date deposited: 11 May 2011 10:27
Last modified: 14 Mar 2024 03:15

Export record

Altmetrics

Contributors

Author: Yong Li
Author: Malcolm Smith
Author: Xin Zhang

Download statistics

Downloads from ePrints over the past year. Other digital versions may also be available to download e.g. from the publisher's website.

View more statistics

Atom RSS 1.0 RSS 2.0

Contact ePrints Soton: eprints@soton.ac.uk

ePrints Soton supports OAI 2.0 with a base URL of http://eprints.soton.ac.uk/cgi/oai2

This repository has been built using EPrints software, developed at the University of Southampton, but available to everyone to use.

We use cookies to ensure that we give you the best experience on our website. If you continue without changing your settings, we will assume that you are happy to receive cookies on the University of Southampton website.

×