Khier, W. and Schwarz, T. and Raddatz, J. (2005) Time Accurate Simulation of the Flow Around the Complete BO105 Wind Tunnel Model. 31st European Rotorcraft Forum, Florenz (it), 13.-15.09.2005.
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Air flow past a reduced scale model of an Eurocopter BO-105 fuselage-main-rotor-tail rotor configuration was simulated by solving the time dependent Navier-Stokes equations. The computations correspond to wind tunnel measurements carried out under Mach 0.1578 forward flight conditions. Main and tail rotors' blades were considered rigid in the computations, and their motions were achieved by a moving overlapping grid technique (Chimera). The numerical results are judged against unsteady pressure measured on the fuselage and the blades. Apart from blade elasticity effects, good agreement with experiment was found.
|Document Type:||Conference or Workshop Item (Paper)|
|Title:||Time Accurate Simulation of the Flow Around the Complete BO105 Wind Tunnel Model|
|Keywords:||Helicopter Aerodynamics, Rotor-Fuselage interaction, Chimera, Overlapping grids, Time accurate RANS|
|Event Title:||31st European Rotorcraft Forum, Florenz (it), 13.-15.09.2005|
|HGF - Research field:||Aeronautics, Space and Transport (old)|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||Rotorcraft|
|DLR - Research area:||Aeronautics|
|DLR - Program:||L RR - Rotorcraft Research|
|DLR - Research theme (Project):||L - The Virtual Aerodynamic Rotorcraft|
|Location:||Köln-Porz , Braunschweig , Göttingen|
|Institutes and Institutions:||Institute of Aerodynamics and Flow Technology|
|Deposited By:||Claudia Grant|
|Deposited On:||09 Oct 2005|
|Last Modified:||14 Jan 2010 19:52|
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