Application of hot-film anemometry to resolve the unsteady boundary layer transition of a laminar airfoil experiencing limit cycle oscillations
Crossref DOI link: https://doi.org/10.1007/s00348-020-2907-y
Published Online: 2020-02-13
Published Print: 2020-02
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Braune, Marc
Koch, Stefan
Text and Data Mining valid from 2020-02-01
Version of Record valid from 2020-02-13
Article History
Received: 17 October 2019
Revised: 6 January 2020
Accepted: 29 January 2020
First Online: 13 February 2020