Yu, Y.H. and Gmelin, B. and Splettstößer, W.R. and Philippe, J.J. and Prieur, J. and Brooks, T.F. (1997) Reduction of Helicopter Blade-Vortex Interaction Noise by Active Rotor Control Technology. Progress in Aerospace Science, 33 (1), pp. 647-687.
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Helicopter-blade-vortex interaction noise is one of the most severe noise sources and is very important both in community annoyance and military detection. Research over the decades has substantially improved basic physical understanding of the mechanisms generating rotor blade-vortex interaction noise and also of controlling techniques, particularly using active rotor control technology. This paper reviews active rotor control techniques currently available for rotor blade-vortex interaction noise reduction, including higher harmonic pitch control, individual blade control, and on-blade control technologies. Basic physical mechanisms of each active control technique are reviewed in terms of noise reduction mechanism and controlling aerodynamic or structural parameters of a blade. Active rotor control techniques using smart actuators to induce local torsional or flapping deformations.
|Title:||Reduction of Helicopter Blade-Vortex Interaction Noise by Active Rotor Control Technology|
|Journal or Publication Title:||Progress in Aerospace Science|
|In ISI Web of Science:||Yes|
|Page Range:||pp. 647-687|
|Keywords:||BVI Noise, Active Rotor Control, BVI Noise Reduction by HHC and IBC, Higher Harmonic Blade Control (HHC), Individual Blade Control (IBC), Smart Active Rotor Control|
|HGF - Research field:||Aeronautics, Space and Transport (old)|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||other|
|DLR - Research area:||Aeronautics|
|DLR - Program:||L DT - Drehflüglertechnologien|
|DLR - Research theme (Project):||L - The Quiet and Comfortable Rotorcraft|
|Location:||Köln-Porz , Braunschweig , Göttingen|
|Institutes and Institutions:||Institute of Aerodynamics and Flow Technology > Institut für Entwurfsaerodynamik|
|Deposited By:||Claudia Grant|
|Deposited On:||16 Sep 2005|
|Last Modified:||14 Jan 2010 19:58|
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