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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 (2020) Application of hot‑film anemometry to resolve the unsteady boundary layer transition of a laminar airfoil experiencing limit cycle oscillations. Experiments in Fluids, 61 (68), pp. 1-15. Springer. doi: 10.1007/s00348-020-2907-y. ISSN 0723-4864.

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Official URL: https://doi.org/10.1007/s00348-020-2907-y


Item URL in elib:https://elib.dlr.de/135745/
Document Type:Article
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 AuthorsAuthor's ORCID iD
Braune, MarcMarc.Braune (at) dlr.deUNSPECIFIED
Koch, StefanStefan.Koch (at) dlr.deUNSPECIFIED
Date:13 February 2020
Journal or Publication Title:Experiments in Fluids
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:61
DOI :10.1007/s00348-020-2907-y
Page Range:pp. 1-15
Editors:
EditorsEmailEditor's ORCID iD
UNSPECIFIEDSpringerUNSPECIFIED
Publisher:Springer
ISSN:0723-4864
Status:Published
Keywords:hot-film anemometry, laminar airfoil, boundary layer transition, limit cycle oscillation
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 (old)
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity
Institute for Aerodynamics and Flow Technology > High Speed Configurations, GO
Deposited By: Braune, Marc
Deposited On:20 Aug 2020 09:21
Last Modified:04 Nov 2020 23:33

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