2016
DOI: 10.1007/s12206-016-0731-3
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A multi-objective optimization for HAWT blades design by considering structural strength

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Cited by 17 publications
(6 citation statements)
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“…BEMT is a combination of momentum theory and blade element theory. It is an iterative process to compute the relative wind velocity induced at the rotor, axial, and tangential induction factors to determine the chord length with a defined TSR [17]. The model divides the blade into several sections from the root to the tip of the blade to determine the aerodynamic forces on each element.…”
Section: Introductionmentioning
confidence: 99%
“…BEMT is a combination of momentum theory and blade element theory. It is an iterative process to compute the relative wind velocity induced at the rotor, axial, and tangential induction factors to determine the chord length with a defined TSR [17]. The model divides the blade into several sections from the root to the tip of the blade to determine the aerodynamic forces on each element.…”
Section: Introductionmentioning
confidence: 99%
“…(3) and Eq. (4)[35]. dM are, respectively, the thrust and moment of the local blade element; ρ is the density of the inflow fluid; l C and d C are, respectively, the lift and drag coefficients of the sectional aerofoil; The Beddoes-Leishman dynamic stall model is used to correct the aerodynamic coefficients under unsteady conditions; c is the chord length of the blade element;…”
mentioning
confidence: 99%
“…In order to achieve the aerodynamic equivalence in the entire region between the cut-in and cut-out wind speeds, an innovative aerodynamic equivalent design methodology is proposed in this study, based on the genetic algorithm (GA). Based on previous investigations, the GA was extensively adopted for the performance optimization of wind turbines under the prototype scale to improve the power efficiency or reduce the structural mass and loads, which was validated to be effective [20][21][22]. In this paper, the scaling laws of wind tunnel real-time hybrid model tests and the aerodynamic equivalent design methodology are first introduced in Sections 2 and 3.…”
Section: Introductionmentioning
confidence: 99%