Figure 4. Velocity contours (m/s) at the middle span of the rectangular wing at h/c= 0.15 at two angles of attack (α=4, 6 deg)

From

Numerical Aerodynamic of the Rectangular Wing Concerning to Ground Effect

Alireza Heidarian, Hassan Ghassemi, Pengfei Liu

American Journal of Mechanical Engineering. 2018, 6(2), 43-47 doi:10.12691/ajme-6-2-1