Stability, Transition1

3:20 PM - 3:40 PM JST(6:20 AM - 6:40 AM UTC)

[1-61] Numerical simulations and Low-Density Wind Tunnel Tests of Compressible Flows over symmetric NACA 4-Digit Airfoils with different thickness at Re=10000

*Yuri Sato¹, Taku Nonomura¹, Takayuki Nagata¹, Tentaro Uchida¹ (1. Nagoya University, Graduate School of Engineering, Divisions of Mechanical and Aerospace Engineering, Fluid Dynamics Laboratory)

Keywords:

Compressible Low-Reynolds Flow,Wall-Resolved LES,Low-Density Wind Tunnel,Airfoil