Abstract
The basic aero-dynamical characteristics of the rotating single-blade was investigated utilizing the lifting-line theory.
The fundamental integral equation was solved numerically by Runge-Kutta method, equipped in the computer aided design tool named MATLAB&SIMULINK system.
This note emphasizes the feasibility of the method, providing the results of parametric research according to several main parameters like an aspect ratio, sweepback angle, taper-ratio and asymmetry of the rotor-blade.
