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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, Koch, StefanVolume:
61
Language:
english
Journal:
Experiments in Fluids
DOI:
10.1007/s00348-020-2907-y
Date:
February, 2020
File:
PDF, 4.23 MB
english, 2020