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Application of hot-film anemometry to resolve the unsteady boundary layer transition of a laminar airfoil experiencing limit cycle oscillations

Braune, Marc and Koch, Stefan (2019) Application of hot-film anemometry to resolve the unsteady boundary layer transition of a laminar airfoil experiencing limit cycle oscillations. FLUCOME 2019 - 15th International Conference on Fluid Control, Measurements and Visualization, 27.-30. Mai 2019, Neapel, Italien.

Full text not available from this repository.

Official URL: https://flucome2019.unina.it/e-book/web/papers/ID334.pdf


Item URL in elib:https://elib.dlr.de/128033/
Document Type:Conference or Workshop Item (Speech)
Title:Application of hot-film anemometry to resolve the unsteady boundary layer transition of a laminar airfoil experiencing limit cycle oscillations
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Braune, MarcMarc.Braune (at) dlr.deUNSPECIFIED
Koch, StefanStefan.Koch (at) dlr.deUNSPECIFIED
Date:27 May 2019
Refereed publication:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:hot-film anemometry, laminar airfoil, boundary layer transition, limit cycle oscillation
Event Title:FLUCOME 2019 - 15th International Conference on Fluid Control, Measurements and Visualization
Event Location:Neapel, Italien
Event Type:international Conference
Event Dates:27.-30. Mai 2019
Organizer:Università degli Studi di Napoli Federico II
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:09 Jul 2019 08:49
Last Modified:09 Jul 2019 08:49

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