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Representation of Yaw Angle Influence on the Fuselage-Induced Velocities in the Rotor Disk

van der Wall, Berend G. (2013) Representation of Yaw Angle Influence on the Fuselage-Induced Velocities in the Rotor Disk. DLR-Interner Bericht. DLR-IB 111-2013/31, 42 S.

Full text not available from this repository.

Abstract

An analytical mathematical model is developed to compute fuselage-induced velocities in the volume of a helicopter rotor operation for use in comprehensive rotor codes, prescribed and free-wake codes.

Item URL in elib:https://elib.dlr.de/83902/
Document Type:Monograph (DLR-Interner Bericht)
Title:Representation of Yaw Angle Influence on the Fuselage-Induced Velocities in the Rotor Disk
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
van der Wall, Berend G.Berend.vanderWall (at) dlr.deUNSPECIFIED
Date:30 August 2013
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:42
Status:Published
Keywords:helicopter simulation, helicotper aerodynamics, interactional aerodynamics, rotor-fuselage interaction
Institution:DLR Institut für Flugsystemtechnik
Department:Hubschrauber
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Rotorcraft (old)
DLR - Research area:Aeronautics
DLR - Program:L RR - Rotorcraft Research
DLR - Research theme (Project):L - The Innovative Rotorcraft (old)
Location: Braunschweig
Institutes and Institutions:Institute of Flight Systems > Rotorcraft
Deposited By: van der Wall, Prof. Dr. Berend G.
Deposited On:09 Sep 2013 15:01
Last Modified:09 Sep 2013 15:01

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