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Fan broadband noise shielding for over-wing engines

Fan broadband noise shielding for over-wing engines
Fan broadband noise shielding for over-wing engines
Increasingly demanding community noise targets are promoting noise performance ever higher on the list of airliner design drivers. In response, significant noise reductions are being made, though at a declining rate—it appears that a whole airframe approach is now needed to achieve significant further gains. As a possible step in this direction, over-wing engine installations are considered here, which use the airframe itself as a noise shield. The paper is the account of an experimental investigation of the comparative shielding performances of a range of relative engine positions on such a layout. Using the statistical modelling technique Kriging, we build an approximation of the noise shielding metric as a function of the position of the engines above the wing—this can serve as the input to multi-disciplinary design trade-off studies. We then compare the results found with the results of applying simple half-barrier diffraction theory to the same problem. We conclude that the latter could be considered as a first order, conceptual design tool, though it misses certain features of the design merit landscape identified by the experiment presented here.
0022-460X
5054-5068
Powell, Stephen
17ca31b3-10bf-4054-b6f2-bc746ccd75cc
Sobester, Andras
096857b0-cad6-45ae-9ae6-e66b8cc5d81b
Joseph, Phillip F.
9c30491e-8464-4c9a-8723-2abc62bdf75d
Powell, Stephen
17ca31b3-10bf-4054-b6f2-bc746ccd75cc
Sobester, Andras
096857b0-cad6-45ae-9ae6-e66b8cc5d81b
Joseph, Phillip F.
9c30491e-8464-4c9a-8723-2abc62bdf75d

Powell, Stephen, Sobester, Andras and Joseph, Phillip F. (2012) Fan broadband noise shielding for over-wing engines. Journal of Sound and Vibration, 331 (23), 5054-5068. (doi:10.1016/j.jsv.2012.06.012).

Record type: Article

Abstract

Increasingly demanding community noise targets are promoting noise performance ever higher on the list of airliner design drivers. In response, significant noise reductions are being made, though at a declining rate—it appears that a whole airframe approach is now needed to achieve significant further gains. As a possible step in this direction, over-wing engine installations are considered here, which use the airframe itself as a noise shield. The paper is the account of an experimental investigation of the comparative shielding performances of a range of relative engine positions on such a layout. Using the statistical modelling technique Kriging, we build an approximation of the noise shielding metric as a function of the position of the engines above the wing—this can serve as the input to multi-disciplinary design trade-off studies. We then compare the results found with the results of applying simple half-barrier diffraction theory to the same problem. We conclude that the latter could be considered as a first order, conceptual design tool, though it misses certain features of the design merit landscape identified by the experiment presented here.

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More information

Submitted date: 19 September 2011
Accepted/In Press date: 12 July 2012
Published date: November 2012
Organisations: Aeronautics, Astronautics & Comp. Eng

Identifiers

Local EPrints ID: 342179
URI: http://eprints.soton.ac.uk/id/eprint/342179
ISSN: 0022-460X
PURE UUID: 5d60467e-e50c-4241-b573-64d7852d2209
ORCID for Andras Sobester: ORCID iD orcid.org/0000-0002-8997-4375

Catalogue record

Date deposited: 14 Aug 2012 14:08
Last modified: 15 Mar 2024 03:13

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Contributors

Author: Stephen Powell
Author: Andras Sobester ORCID iD

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