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Enhancement of Prescribed Wake Codes with a CFD-Based Model of the Fuselage-Induced Velocities

van der Wall, Berend G. and Bauknecht, Andre and Jung, Sung N. and You, Young H. (2013) Enhancement of Prescribed Wake Codes with a CFD-Based Model of the Fuselage-Induced Velocities. 39th European Rotorcraft Forum, 2013-09-03 - 2013-09-06, Moscow, Russia.

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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/81309/
Document Type:Conference or Workshop Item (Speech)
Title:Enhancement of Prescribed Wake Codes with a CFD-Based Model of the Fuselage-Induced Velocities
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
van der Wall, Berend G.UNSPECIFIEDhttps://orcid.org/0000-0001-6144-0921UNSPECIFIED
Bauknecht, AndreUNSPECIFIEDhttps://orcid.org/0000-0002-4076-780XUNSPECIFIED
Jung, Sung N.Konkuk UniversityUNSPECIFIEDUNSPECIFIED
You, Young H.Konkuk UniversityUNSPECIFIEDUNSPECIFIED
Date:September 2013
Refereed publication:No
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:39th European Rotorcraft Forum
Event Location:Moscow, Russia
Event Type:international Conference
Event Start Date:3 September 2013
Event End Date:6 September 2013
Organizer:Russian Helicopters, Moscow
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 , 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:09 Sep 2013 15:14
Last Modified:24 Apr 2024 19:47

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  • Enhancement of Prescribed Wake Codes with a CFD-Based Model of the Fuselage-Induced Velocities. (deposited 09 Sep 2013 15:14) [Currently Displayed]

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