Verification of a CFD solver in near ground effect for aerodynamic behavior of airfoil NACA 0015

hasan sajjadi; S. F. Hosseinizadeh; Y. Vazifehshenas

Volume 8, Issue 1 , March 2011, , Pages 1-10

Abstract
  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 ...  Read More