Abstract:
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.
Keywords:pulling propeller, high aspect ratio wing, side slip angle, circulation of the wing, inductive drag References.