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Two- and Three-Bladed ONERA Model Rotors

Pahlke, K. and Sidès, J. and Wehr, D. (1997) Two- and Three-Bladed ONERA Model Rotors. In: Notes on Numerical Fluid Mechanics Vieweg Verlag Braunschweig. ISBN 3-528-06958-9.

Full text not available from this repository.

Abstract

Time-accurate 3D Euler solutions of DLR, ONERA and the University of Stuttgart are compared on common grids for a non-lifting 2-bladed and a lifting 3-bladed rotor in forward flight. For the lifting forward flight the wake and the downwash of the other blades are accounted for by an angle of attack correction. The computational results are compared with each other and with experimental data. The agreement of the inviscid computational results with the experimental data is good. A grid refinement was conducted for the lifting forward flight case. The computations agree well for the advancing blade but for the retreating blade with high angles of attack the three methods differ significantly. The grid refinement reduces but cannot eliminate these differences. The cpu-times for all computations are given.

Item URL in elib:https://elib.dlr.de/13167/
Document Type:Book Section
Additional Information: LIDO-Berichtsjahr=1999,
Title:Two- and Three-Bladed ONERA Model Rotors
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Pahlke, K.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Sidès, J.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Wehr, D.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:1997
Journal or Publication Title:Notes on Numerical Fluid Mechanics
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:Vol. 58
Publisher:Vieweg Verlag Braunschweig
ISBN:3-528-06958-9
Status:Published
Keywords:CFD, Euler Equations, rigid body motion, prescribed wake model, multibladed rotor, transonic flow, unsteady flows
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 Virtual Aerodynamic Rotorcraft (old)
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Institut für Entwurfsaerodynamik
Deposited By: Grant, Claudia
Deposited On:16 Sep 2005
Last Modified:14 Jan 2010 20:03

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