Dynamic Stall Vortex Formation of OA-209 Airfoil at Low Reynolds Number

Article English OPEN
Aung Myo Thu; Sang Eon Jeon; Yung Hwan Byun; Soo Hyung Park;

The unsteady flow field around oscillating OA-209 airfoil at a Reynolds number of 3.5×105 were investigated. Three different reduced frequencies were tested in order to see how it affects the hysteresis loop of an airfoil. At a reduced frequency of 0.05 the deep dynamic... View more
Share - Bookmark

  • Download from
    ZENODO via ZENODO (Article, 2014)
  • Cite this publication