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 Nature. 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:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Braune, Marc	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Koch, Stefan	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED

Date:

13 February 2020

Journal or Publication Title:

Experiments in Fluids

Refereed publication:

Yes

Open Access:

Yes

Gold Open Access:

In SCOPUS:

Yes

In ISI Web of Science:

Yes

Volume:

DOI:

10.1007/s00348-020-2907-y

Page Range:

pp. 1-15

Editors:

Editors	Email	Editor's ORCID iD	ORCID Put Code
UNSPECIFIED	Springer	UNSPECIFIED	UNSPECIFIED

Publisher:

Springer Nature

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:

23 Oct 2023 12:39

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