2019
DOI: 10.1016/j.renene.2018.08.040
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Design and optimization of airfoils and a 20 kW wind turbine using multi-objective genetic algorithm and HARP_Opt code

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Cited by 48 publications
(17 citation statements)
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“…For structural reasons, a thicker airfoil is typically used closer to the blade root, while a thinner airfoil is used along the tip area as it is distributed smoothly from the root to the tip. Krishnil et al [10] had applied a single airfoil, which differs from the large commercial blades currently in use; in general, large blades have 5 to 7 airfoil applications. In this paper, six types of airfoils are used, including the NACA and DU series, and especially, NACA 64-618 is considered as an airfoil at the tip.…”
Section: Initial Blade Designmentioning
confidence: 99%
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“…For structural reasons, a thicker airfoil is typically used closer to the blade root, while a thinner airfoil is used along the tip area as it is distributed smoothly from the root to the tip. Krishnil et al [10] had applied a single airfoil, which differs from the large commercial blades currently in use; in general, large blades have 5 to 7 airfoil applications. In this paper, six types of airfoils are used, including the NACA and DU series, and especially, NACA 64-618 is considered as an airfoil at the tip.…”
Section: Initial Blade Designmentioning
confidence: 99%
“…Wei et al [9] presented an integrated method for designing the airfoil families of large wind turbine blades. Krishnil et al [10] designed and optimized airfoils for a 20 kW wind turbine using a multi-objective genetic algorithm. In addition, in relation to the optimization of the blade design, many studies have already been conducted in helicopter and aeronautical engineering fields.…”
Section: Introductionmentioning
confidence: 99%
“…Zhu, Shen, and Sørensen (2014) presented an integrated method of designing the aerofoil families of large wind turbine blades using the BEMT. Krishnil et al (2018) designed and optimized the aerofoils for a 20 kW wind turbine using the multi-objective genetic algorithm. Vincent et al (2017) adopted the BEMT and the blade span to estimate the aerodynamic performance of the turbine and to optimize the horizontal axis wind turbine blade.…”
Section: Introductionmentioning
confidence: 99%
“…Wen et al (2019) designed an airfoil based on the S809 airfoil by using the artificial neural network to reduce the optimization time, and the calculated results indicated that the new airfoil has better lift force characteristics compared with the original airfoil. Ram et al (2019) generated airfoils for a 20kW wind turbine by using multi-objective genetic algorithm method, and an USP07-45xx family of airfoil was designed to achieve maximum lift/drag ratio from 4 to 10°angle of attack. Li et al (2020) proposed an optimization method to design wind turbine airfoil at low wind velocity.…”
Section: Introductionmentioning
confidence: 99%