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Aeroelastic Behavior of a Laminar Wing in Transonic Flow

Fehrs, Michael and Helm, Sebastian and Kaiser, Christoph and Klimmek, Thomas (2021) Aeroelastic Behavior of a Laminar Wing in Transonic Flow. In: 22nd STAB/DGLR Symposium on New Results in Numerical and Experimental Fluid Mechanics XIII (151), pp. 164-173. Springer International Publishing. STAB 2020 - 22. DGLR-Fachsymposium der STAB, 2020, Göttingen, Deutschland. doi: 10.1007/978-3-030-79561-0. ISBN 978-3-030-79560-3. ISSN 1612-2909.

Full text not available from this repository.

Official URL: https://www.dlr.de/as/Portaldata/5/Resources/dokumente/veranstaltungen/stab_workshop/STAB-Jahresbericht-2020.pdf

Abstract

A laminar wing test case for the flutter behavior in transonic flow with free boundary layer transition is presented. The DLR-AE-L1 airfoil and wing are designed to serve as an aeroelastic testbed to develop a better understanding for the effect of boundary layer transition on flutter stability. Coupled CFD-CSM simulations are used to determine the flutter onset in a transitional and a fully turbulent flow. It is found that flutter occurs at lower stagnation pressures for the transitional flow, which is in accordance with earlier research on laminar airfoils.

Item URL in elib:https://elib.dlr.de/139471/
Document Type:Conference or Workshop Item (Other)
Additional Information:Weder Präsenz- noch Online-Veranstaltung auf Grund der Corona-Pandemie
Title:Aeroelastic Behavior of a Laminar Wing in Transonic Flow
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Fehrs, MichaelMichael.Fehrs (at) dlr.deUNSPECIFIED
Helm, SebastianSebastian.Helm (at) dlr.deUNSPECIFIED
Kaiser, ChristophChristoph.Kaiser (at) dlr.dehttps://orcid.org/0000-0001-9156-8352
Klimmek, ThomasThomas.Klimmek (at) dlr.dehttps://orcid.org/0000-0002-5573-7355
Date:2021
Journal or Publication Title:22nd STAB/DGLR Symposium on New Results in Numerical and Experimental Fluid Mechanics XIII
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
DOI :10.1007/978-3-030-79561-0
Page Range:pp. 164-173
Editors:
EditorsEmailEditor's ORCID iD
Dillmann, AndreasAndreas.Dillmann@dlr.deUNSPECIFIED
Heller, GerdAirbus BremenUNSPECIFIED
Krämer, EwaldInstitut für Aerodynamik und Gasdynamik, Universität StuttgartUNSPECIFIED
Wagner, ClausClaus.Wagner@dlr.deUNSPECIFIED
Publisher:Springer International Publishing
Series Name:Notes on Numerical Fluid Mechanics and Multidisciplinary Design
ISSN:1612-2909
ISBN:978-3-030-79560-3
Status:Published
Keywords:laminar wing, boundary layer transition, CFD-CSM coupling, transonic flutter
Event Title:STAB 2020 - 22. DGLR-Fachsymposium der STAB
Event Location:Göttingen, Deutschland
Event Type:national Conference
Event Dates:2020
Organizer:STAB - Deutsche Strömungsmechanische Arbeitsgemeinschaft
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 - VicToria (old)
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity > Aeroelastic Simulation
Institute of Aeroelasticity > Loads Analysis and Aeroelastic Design
Deposited By: Fehrs, Michael
Deposited On:18 Dec 2020 16:22
Last Modified:26 Aug 2021 14:33

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