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Takao Maeda

Researcher at Mie University

Publications -  89
Citations -  1782

Takao Maeda is an academic researcher from Mie University. The author has contributed to research in topics: Wind tunnel & Turbine. The author has an hindex of 21, co-authored 89 publications receiving 1396 citations. Previous affiliations of Takao Maeda include Chinese Academy of Sciences.

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Effect of number of blades on aerodynamic forces on a straight-bladed Vertical Axis Wind Turbine

TL;DR: In this article, the authors evaluated the aerodynamic forces depending on several numbers of blades in wind tunnel experiment and found that the power consumption of a straight-bladed VAWT decreases with the increase of number of blades.
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Study on power performance for straight-bladed vertical axis wind turbine by field and wind tunnel test

TL;DR: In this article, the power and torque performance of a straight-bladed VAWT is investigated by wind tunnel experiment and field test, and the relationship between operating conditions and wind velocity is verified.
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A straight-bladed vertical axis wind turbine with a directed guide vane row — Effect of guide vane geometry on the performance —

TL;DR: In this article, a straight-bladed vertical axis wind turbine (S-VAWT) with a directed guide vane row has been proposed and tested by the authors, and the experimental study of the proposed wind turbine was carried out by a wind tunnel.
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Wind tunnel and numerical study of a straight-bladed vertical axis wind turbine in three-dimensional analysis (Part I: For predicting aerodynamic loads and performance)

TL;DR: In this paper, a straight-bladed VAWT (Vertical Axis Wind Turbine) with two straight blades was analyzed and compared in wind tunnel experiments and numerical analysis.
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Effect of solidity on aerodynamic forces around straight-bladed vertical axis wind turbine by wind tunnel experiments (depending on number of blades)

TL;DR: In this paper, the authors focused on evaluating the aerodynamic forces acting on a single blade, depending on the different numbers of blades in wind tunnel experiments, and the cross-sectional shape of the tested airfoil was a NACA0021.