Numerical studies of side slip and propeller on tips high aspect ratio wing effect on the inductive drag

The results of a numerical study of the influence of the angle are presented. sliding and operation of the propeller at the end of a high aspect ratio wing at circulation and inductive reactance. Numerical studies of the influence of angle slip (side wind) on the aerodynamic characteristics of the model aircraft with an ultra-high aspect ratio wing with working propellers at the wing tips were carried out using a program based on the solution Reynolds-averaged Navier–Stokes equations. Numerical studies showed that as the sliding angle increases, circulation decreases and inductive reactance of the wing.