Unable to render {include} The included page could not be found.
A NACA 0012 Airfoil is placed in a wind tunnel with the following free stream conditions:
Reynolds Number : 2.88e6
x velocity: 1 m/s
viscosity: 3.4722e-7
A NACA 0012 Airfoil is placed in a wind tunnel with the following free stream conditions:
Reynolds Number : 2.88e6
x velocity: 1 m/s
viscosity: 3.4722e-7