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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.

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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.

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 Authors
van der Wall, Berend G.Berend.vanderWall@dlr.de
Date:30 August 2013
Refereed publication: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
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: Dr.-Ing. Berend G. van der Wall
Deposited On:09 Sep 2013 15:01
Last Modified:09 Sep 2013 15:01

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