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Aeroelastic Simulations of High Reynolds Number Aero Structural Dynamics Wind Tunnel Model

Ritter, Markus and Neumann, Jens and Krüger, Wolf R. (2016) Aeroelastic Simulations of High Reynolds Number Aero Structural Dynamics Wind Tunnel Model. AIAA Journal, 54 (6), pp. 1962-1973. American Institute of Aeronautics and Astronautics (AIAA). DOI: 10.2514/1.J053384 ISSN 0001-1452

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Official URL: http://arc.aiaa.org

Abstract

This article presents results of numerical simulations of the HIRENASD High Reynolds Number Aero Structural Dynamics wind tunnel configuration. The activities consist of the selection of relevant transonic test cases, the set-up and simulation of the numerical models, as well as the comparison of computational and experimental results. Two steady (static coupling) and three unsteady (forced motion) test cases were selected, all in the transonic flow regime at Mach numbers up to 0.85 and Reynolds numbers up to 23 million. Good agreement between numerical and experimental data was obtained for both the steady and the unsteady test cases. It is shown that the consideration of the static elastic deformation of the wing is indispensable for both the steady and unsteady simulations. The unsteady simulations were executed in such a way that the elastic motion of the wing in a selected structural eigenmode was prescribed in a forced motion computational fluid dynamics simulation using grid deformation. This approach yields very satisfactory results in terms of the unsteady pressure distribution.

Item URL in elib:https://elib.dlr.de/109427/
Document Type:Article
Title:Aeroelastic Simulations of High Reynolds Number Aero Structural Dynamics Wind Tunnel Model
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Ritter, MarkusMarkus.Ritter (at) dlr.deUNSPECIFIED
Neumann, JensJens.Neumann (at) dlr.deUNSPECIFIED
Krüger, Wolf R.Wolf.Krueger (at) dlr.deUNSPECIFIED
Date:August 2016
Journal or Publication Title:AIAA Journal
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:54
DOI :10.2514/1.J053384
Page Range:pp. 1962-1973
Editors:
EditorsEmail
AIAA, AIAAUNSPECIFIED
Publisher:American Institute of Aeronautics and Astronautics (AIAA)
Series Name:AIAA Journal
ISSN:0001-1452
Status:Published
Keywords:aeroelasticity, CFD, fluid-structure-interaction
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Flight Physics
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity > Loads Analysis and Aeroelastic Design
Deposited By: Ritter, Markus Raimund
Deposited On:13 Dec 2016 08:28
Last Modified:08 Mar 2018 18:42

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