Aero-dynamical characteristics of the single rotor-blade in lower tip-speed ratio condition; a supplemental notee

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• The basic aero-dynamical characteristics of the rotating single-blade was investigated utilizing the lifting-line theory.<BR>The fundamental integral equation was solved numerically by Runge-Kutta method, equipped in the computer aided design tool named MATLAB&SIMULINK system.<BR>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.

• 一般社団法人 日本風力エネルギー学会の論文

一般社団法人 日本風力エネルギー学会 | 論文

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