S. F. Hosseinizadeh

[ 1 ] - Verification of a CFD solver in near ground effect for aerodynamic behavior of airfoil NACA 0015

Numerical investigation was performed on NACA 0015 which is a symmetric airfoil. Pressure distribution and then lift and drag forces are verified. Changing of ground clearance was a considerable point. Also the angle of attack was changed from 0° to 10°. Pressure coefficient reaches its higher amounts on the wing lower surface when the ground clearance diminishes. Increment of the angle of atta...