2017
DOI: 10.11648/j.ajme.20170302.12
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Aerodynamic Design and Blade Angle Analysis of a Small Horizontal–Axis Wind Turbine

Abstract: The wind turbine blades are the main part of the rotor. Extraction of energy from wind depends on the design of the blade. In this paper, a design method based on Blade Element Momentum (BEM) theory is explained for small horizontalaxis wind turbine model (HAWT) blades. The method was used to optimize the chord and twist distributions of the wind turbine blades to enhance the aerodynamic performance of the wind turbine and consequently, increasing the generated power. A Fortran program was developed to use (BE… Show more

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Cited by 20 publications
(12 citation statements)
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“…The selected small wind turbine was designed using Blade Element Momentum theory [35]. The blade has NACA-4412 airfoil section with a hub radius, rh, of 0.02 m, tip radius, rt, of 0.2 m and three blades, as shown in Figure 14(a).…”
Section: Performance Of Obtained Diffuser Shape With Wind Turbinementioning
confidence: 99%
“…The selected small wind turbine was designed using Blade Element Momentum theory [35]. The blade has NACA-4412 airfoil section with a hub radius, rh, of 0.02 m, tip radius, rt, of 0.2 m and three blades, as shown in Figure 14(a).…”
Section: Performance Of Obtained Diffuser Shape With Wind Turbinementioning
confidence: 99%
“…Hendriana et al optimized the wind turbine by changing the blade width and the pitch angle of the inner and outer ends, 35 and Zhu et al proposed a multi‐objective aerodynamic and structural optimization method to reduce the energy cost and improve the overall performance of the blade 36 . Mohamed et al proposed a design method for small HAWT blades, and the method was used to optimize the chord and twist distributions of the wind turbine blades to enhance the aerodynamic performance of the wind turbine and consequently increasing the generated power 37 …”
Section: Development Status Of Offshore Wind Energy Devicementioning
confidence: 99%
“…The following airfoils are used: NACA 4415, 4418, 4421, 4424, 4430 and 4436 (Fuglsang et al, 2004;Khaled et al, 2017;Mamadaminov, 2013;Manwell et al, 2009). These are located in the blade according to defined considerations used by (Mohammadi et al, 2016) and (Adaramola, 2014).…”
Section: Variation Of the Power Coefficient In Terms Of Tsrmentioning
confidence: 99%