Stability, Transition3

9:00 AM - 9:20 AM JST(12:00 AM - 12:20 AM UTC)

[3-30] Experiment on secondary structure of a flat-plate wake at Reynolds numbers of 100 - 300

*Shota Ikejiri¹, Akihiro Wakabayashi¹, Takanori Uchida², Ao Takada², Katsuya Hirata¹ (1. Doshisha University, 2. Kyusyu University)

Keywords:

Aerodynamics,Airfoil,Wing,Very Low Reynolds Numbers,Drone