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Landing Gear Airframe Noise Research Study

Chow, L.C. and Dobrzynski, W. (2002) Landing Gear Airframe Noise Research Study. 9th International Congress on Sound and Vibration, Orlando (usa), 8.-11.07.2002.

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This paper describes the landing gears airframe noise study research work in the EC co-financed "Significantly Lower Community Exposure to Aircraft Noise" (SILENCER) project. The landing gears airframe noise research include the study of gear-wake/gear interaction effects; the low noise landing gear design with add-on treatments and the advanced low noise landing gear design. Full scale optimized add-on treatments will be manufactured and flight tested on an Airbus A340 aircraft. Advanced low noise main and nose landing gear design of A340 size will be manufactured and wind tunnel tested in the German-Dutch Wind Tunnel (DNW-LLF). Together with other noise reduction treatment designs relating to engines and airframes conducted in the same project, it is expected that a total reduction margin of several EPNdB can be demonstrated through these large scale tests.

Item URL in elib:https://elib.dlr.de/12571/
Document Type:Conference or Workshop Item (Speech)
Additional Information: LIDO-Berichtsjahr=2003,
Title:Landing Gear Airframe Noise Research Study
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Keywords:Fahrwerkslärm, Aeroakustische Windkanalmessungen
Event Title:9th International Congress on Sound and Vibration, Orlando (usa), 8.-11.07.2002
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: Grant, Claudia
Deposited On:31 Jan 2006
Last Modified:14 Jan 2010 19:10

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