Blade Wake Interaction Noise for a BO-105 Model Main Rotor
Burley, C.L. and Brooks, T.F. and Splettstößer, W.R. and Schultz, K.-J. and Kube, R, and Buchholz, H. and Wagner, W. and Weitemeier, W. (1997) Blade Wake Interaction Noise for a BO-105 Model Main Rotor. AHS Technical Specialists' Meeting for Rotorcraft Acoustics and Aerodynamics, Williamsburg, VA, USA, 28.-30.10.97.
Full text not available from this repository.
Fundamental characteristics of Blade Wake Interaction (BWI) noise are determinated, and a prediction method is developed, using acoustic and blade pressure data from a 4-bladed BO-105 model helicopter main rotor. BWI is a broadband noise source caused by the blade interactions with turbulence in the rotor wake, particularly about the tip vortices. The data are from the rotor aeroacoustic test program called HART which was jointly conducted by European and American government agencies in the German-Dutch Wind Tunnel, DNW. The test datainclude simultaneous measurements of instantaneous blade pressures and acoustic time histories as well as averaged data. The statistical character of the BWI is determined from the instantaneous surface pressures. A BWI noise metric is developed and BWI noise directivity contours (similar to those typically presented for BVI noise) are presented and shown to be a function of rotor tip-path-plane angle. Similarly, BWI.
|Document Type:||Conference or Workshop Item (Paper)|
|Title:||Blade Wake Interaction Noise for a BO-105 Model Main Rotor|
|Keywords:||Helicopter noise, rotor broadband noise, blade-wake interaction (BVI) noise|
|Event Title:||AHS Technical Specialists' Meeting for Rotorcraft Acoustics and Aerodynamics, Williamsburg, VA, USA, 28.-30.10.97|
|HGF - Research field:||Aeronautics, Space and Transport|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||L - no assignement|
|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|
Institute of Flight Systems > Institut für Flugmechanik
Institute of Aeroelasticity
|Deposited By:||elib DLR-Beauftragter|
|Deposited On:||03 Apr 2006|
|Last Modified:||27 Apr 2009 10:06|
Repository Staff Only: item control page