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Fuselage-Rotor Mutual Interference: a Step Towards Interactional Aerodynamics in Comprehensive Codes

van der Wall, Berend G. and Bauknecht, Andre and Jung, Sung N. and You, Young H. (2014) Fuselage-Rotor Mutual Interference: a Step Towards Interactional Aerodynamics in Comprehensive Codes. 5th Decennial AHS Aeromechanics Specialists' Conference, 22.-24. Jan. 2014, San Francisco, CA, USA.

Full text not available from this repository.

Abstract

An analytical formulation of the induced velocities caused by the fuselage shell of the HART II wind tunnel model in the vicinity of the rotor is derived from computational fluid dynamics (CFD) velocity data. The analytical induced velocity model can directly be used to account for the inflow at the blade elements and also allows for analytical integration to compute the associated displacements of rotor blade tip vortices convecting downstream through this velocity field. The implementation is demonstrated at the example of the rotor simulation program S4 of the German Aerospace Center (DLR) in Braunschweig. The model’s influence on the major flow field variables around the rotor disk and the wake trajectory is demonstrated. Since the method is generic it is anticipated that the effect of any kind of fuselage can be accounted for this way and it may be used within any comprehensive code, prescribed wake code, and even free-wake codes.

Item URL in elib:https://elib.dlr.de/83016/
Document Type:Conference or Workshop Item (Speech)
Title:Fuselage-Rotor Mutual Interference: a Step Towards Interactional Aerodynamics in Comprehensive Codes
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
van der Wall, Berend G.Berend.vanderWall (at) dlr.deUNSPECIFIED
Bauknecht, Andreandre.bauknecht (at) dlr.deUNSPECIFIED
Jung, Sung N.Konkuk UniversityUNSPECIFIED
You, Young H.Konkuk UniversityUNSPECIFIED
Date:January 2014
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:pp. 1-14
Status:Published
Keywords:Rotor-fuselage interference, interactional aerodynamics, fuselage flow, rotor simulation
Event Title:5th Decennial AHS Aeromechanics Specialists' Conference
Event Location:San Francisco, CA, USA
Event Type:international Conference
Event Dates:22.-24. Jan. 2014
Organizer:American Helicopter Society International (AHS)
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 , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Helicopters
Institute of Flight Systems > Rotorcraft
Deposited By: van der Wall, Prof. Dr. Berend G.
Deposited On:28 Jan 2014 09:30
Last Modified:20 Oct 2014 09:37

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