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.
5054-5068
Powell, Stephen
17ca31b3-10bf-4054-b6f2-bc746ccd75cc
Sobester, Andras
096857b0-cad6-45ae-9ae6-e66b8cc5d81b
Joseph, Phillip F.
9c30491e-8464-4c9a-8723-2abc62bdf75d
November 2012
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), .
(doi:10.1016/j.jsv.2012.06.012).
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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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
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Date deposited: 14 Aug 2012 14:08
Last modified: 15 Mar 2024 03:13
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Author:
Stephen Powell
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