Dobrzynski, W. (2004) Quantified noise characteristics of the aircraft with control devices. Project Report, DLR-Interner Bericht. 124-04/11, 28 S.
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Novel wing designs will incorporate advanced wing-tip devices for a quick wake-vortex break down and an increased wing performance through different devices, e.g. differential spoiler setting, large wing-lets, mini trailing edge devices and sub-boundary layer vortex generators. Advanced wing configurations will enhance the aircraft's capability to perform noise abatement flight procedures, but may also generate excess aerodynamic noise. Therefore farfield noise measurements were conducted in the open test section of the DNW-LLF on a 1/10.6 scaled X408D (A340) model for all relevant aircraft configurations, to quantify the different devices' noise characteristics. All devices were tested individually by means of an out-of-flow traversing microphone boom. In comparison of measured noise directivities with and without devices installed only small effects on noise in the order of 1 dB were detected.
|Document Type:||Monograph (Project Report, DLR-Interner Bericht)|
|Title:||Quantified noise characteristics of the aircraft with control devices|
|Number of Pages:||28|
|Keywords:||Airframe noise, high lift 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 19:41|
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