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Fuselage-Rotor Aerodynamic Interaction: Modeling, Simulation and Results Obtained

van der Wall, Berend G. (2014) Fuselage-Rotor Aerodynamic Interaction: Modeling, Simulation and Results Obtained. [Other]

Full text not available from this repository.

Abstract

Dr. van der Wall joins NASA Ames on a Research Sabbatical from August 13 to Nov. 21, focusing on the modeling of the isolated fuselage-induced flow in the air volume of the main rotor operation above it. He will provide a brief sketch of the CFD computations to obtain the flow field data. Then, the underlying principles and assumptions for reduced-order semi-empirical modeling are addressed. Three different fuselages have been modeled during the sabbatical: LRTA as used for UH-60 airloads and IBC programs; RTA as used for Bo105 wind tunnel validation and IBC programs; HART as used for B015 model-scale wind tunnel validation and HHC programs. Many examples about the comparison between CFD data and the results obtained with the model will be given both within the volume modeled and outside. Finally, the model has been used in a comprehensive rotor simulation program for comparison of isolated rotor results versus including the fuselage. The fuselage influence on rotor trim controls, thrust and power will be shown.

Item URL in elib:https://elib.dlr.de/94184/
Document Type:Other
Title:Fuselage-Rotor Aerodynamic Interaction: Modeling, Simulation and Results Obtained
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
van der Wall, Berend G.Berend.vanderWall (at) dlr.deUNSPECIFIED
Date:19 November 2014
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Helicopter, interactional aerodynamics, fuselage-rotor interaction
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:rotorcraft
DLR - Research area:Aeronautics
DLR - Program:L RR - Rotorcraft Research
DLR - Research theme (Project):L - The Innovative Rotorcraft
Location: Braunschweig
Institutes and Institutions:Institute of Flight Systems > Rotorcraft
Deposited By: van der Wall, Prof. Dr. Berend G.
Deposited On:06 Jan 2015 11:36
Last Modified:06 Jan 2015 11:36

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