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.
Full text not available from this repository.
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.
|Document Type:||Conference or Workshop Item (Speech)|
|Title:||Landing Gear Airframe Noise Research Study|
|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|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||L VU - Air Traffic and Environment|
|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 19:10|
Repository Staff Only: item control page