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Hysteretic response of a laminar airfoil undergoing single degree of freedom limit cycle oscillations in transonic flow

Braune, Marc and Hebler, Anne (2019) Hysteretic response of a laminar airfoil undergoing single degree of freedom limit cycle oscillations in transonic flow. IFASD 2019 - International Forum on Aeroelasticity and Structural Dynamics, 10.-13. Juni 2019, Savannah, GA (USA).

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Item URL in elib:https://elib.dlr.de/128036/
Document Type:Conference or Workshop Item (Speech)
Title:Hysteretic response of a laminar airfoil undergoing single degree of freedom limit cycle oscillations in transonic flow
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Braune, MarcMarc.Braune (at) dlr.deUNSPECIFIED
Hebler, Anneanne.hebler (at) dlr.dehttps://orcid.org/0000-0002-5450-9211
Date:9 June 2019
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:laminar airfoil, limit cycle oscillation, transonic flow, hysteresis, subcritical bifurcation, nonlinear system response
Event Title:IFASD 2019 - International Forum on Aeroelasticity and Structural Dynamics
Event Location:Savannah, GA (USA)
Event Type:international Conference
Event Dates:10.-13. Juni 2019
Organizer:AIAA
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:L - no assignment
DLR - Research theme (Project):L - no assignment
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity > Aeroelastic Experiments
Deposited By: Braune, Marc
Deposited On:26 Jun 2019 17:57
Last Modified:18 Nov 2019 11:42

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