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Coupling of MBS and CFD: an oscillating aeroelastic wing model

Arnold, Jürgen and Krüger, Wolf and Einarsson, Gunnar (2010) Coupling of MBS and CFD: an oscillating aeroelastic wing model. SIMPACK News (September 2010), pp. 22-24. SIMPACK AG.

Full text not available from this repository.

Official URL: http://www.simpack.com

Abstract

Multi-body simulation has been shown to be a valuable software tool for virtual aircraft design. It is a standard approach for the analysis of landing gears, of aircraft on the ground, and for the design of high-lift systems. The medium level of complexity of typical multi-body models also makes it a suitable tool for the application of flight mechanics in combination with elastic deformations. The development of reliable aerodynamic models, in addition to the existing interface for complex elastic structures, has been a major activity in the DLR Institute of Aeroelasticity during the past several years. The coupling procedure of SIMPACK to CFD is shown in this article for the application of the Aeroelastic Model Programme (AMP) wind tunnel wing simulated with SIMPACK and the DLR TAU code.

Item URL in elib:https://elib.dlr.de/66083/
Document Type:Article
Title:Coupling of MBS and CFD: an oscillating aeroelastic wing model
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Arnold, JürgenUNSPECIFIEDUNSPECIFIED
Krüger, WolfUNSPECIFIEDUNSPECIFIED
Einarsson, GunnarInstitut für Aerodynamik und Strömungstechnik, BraunschweigUNSPECIFIED
Date:September 2010
Journal or Publication Title:SIMPACK News
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:pp. 22-24
Editors:
EditorsEmail
SIMPACK , AGFriedrichshafener Straße 1, 82205 Gilching
Publisher:SIMPACK AG
Series Name:SIMPACK News
Status:Published
Keywords:aeroelasticity, wing model, CFD, multibody simulation
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research (old)
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Flexible Aircraft (old)
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity
Deposited By: Erdmann, Daniela
Deposited On:12 Nov 2010 10:38
Last Modified:06 Sep 2019 15:29

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