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Advanced landing gear noise reduction - Test data analysis and assessment of results

Dobrzynski, W. and Holthusen, H. (2004) Advanced landing gear noise reduction - Test data analysis and assessment of results. DLR-Interner Bericht. 124-04/902, 115 S.

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Abstract

Future landing gear designs must account for aeroacoustics requirements at design stage. The development of such advanced low noise landing gears for future aircraft application was performed in Silencer WP 1.5.4, taking production costs, maintenance aspects and acoustic benefits into account. In SILENCER WP 2.3.3 full scale low noise gear mock ups were built and noise tested in the DNW-LLF. The noise test results were compared against those obtained for the baseline A340 landing gears in the RAIN project. For both the nose and the main landing gears each one reference configuration (as designed in WP 1.5.4) and selected configuration modifications were tested. Farfield noise spectra turned out to scale on a Strouhal number basis, with sound intensities increasing with wind speed to the power of 6. In terms of overall A-weighted noise levels the advanced low noise NLG is up to - 7 dB quieter compared to the A340 baseline gear for forward arc radiation directions. The advanced low noise MLG is up to about -5 dB quieter compared to the A340 baseline gear.

Document Type:Monograph (DLR-Interner Bericht)
Additional Information: LIDO-Berichtsjahr=2005,
Title:Advanced landing gear noise reduction - Test data analysis and assessment of results
Authors:
AuthorsInstitution or Email of Authors
Dobrzynski, W.UNSPECIFIED
Holthusen, H.NLR
Date:2004
Number of Pages:115
Status:Published
Keywords:Airframe noise, landing gear noise
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:L VU - Air Traffic and Environment (old)
DLR - Research area:Aeronautics
DLR - Program:L VU - Air Traffic and Environment
DLR - Research theme (Project):L - Quiet Air Traffic (old)
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology
Deposited By: Claudia Grant
Deposited On:31 Jan 2006
Last Modified:14 Jan 2010 19:42

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