2005
DOI: 10.1002/we.153
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Tip loss corrections for wind turbine computations

Abstract: As an essential ingredient in the blade element momentum theory, the tip loss effect of rotors plays an important role in the prediction of wind turbine performance. Various tip loss corrections based on the Prandtl tip loss function are analysed in the article. Comparisons with measurements and theoretical analyses show that existing tip loss correction models are inconsistent and fail to predict correctly the physical behaviour in the proximity of the tip. A new tip loss correction model is proposed that rem… Show more

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Cited by 368 publications
(277 citation statements)
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“…The relative velocity U rel is defined from the velocity triangle, as sketched in Figure 3, that is a function of the axial velocity Ux, the rotational velocity U θ , the angular rotational speed Ω in radians per second and the radial coordinate r. ϕ is the angle between U rel and the rotor plane that, together with the local pitch angle γ (sum of the blade pitch angle and local twist), defines the local angle of attack α. To account for a finite number of the blades, the tip correction of Shen et al [21,22] used, in which λ is the tip speed ratio, R is the blade radius and ci are empirical constants. Shen et al determined the constants ci from a calibration with two small experimental wind turbine rotors that have a relatively blunt tip, leading to c2 = 21.…”
Section: Methods Iii: Ad Airfoil Methods (With Torque Calibration)mentioning
confidence: 99%
“…The relative velocity U rel is defined from the velocity triangle, as sketched in Figure 3, that is a function of the axial velocity Ux, the rotational velocity U θ , the angular rotational speed Ω in radians per second and the radial coordinate r. ϕ is the angle between U rel and the rotor plane that, together with the local pitch angle γ (sum of the blade pitch angle and local twist), defines the local angle of attack α. To account for a finite number of the blades, the tip correction of Shen et al [21,22] used, in which λ is the tip speed ratio, R is the blade radius and ci are empirical constants. Shen et al determined the constants ci from a calibration with two small experimental wind turbine rotors that have a relatively blunt tip, leading to c2 = 21.…”
Section: Methods Iii: Ad Airfoil Methods (With Torque Calibration)mentioning
confidence: 99%
“…Therefore, this study considers the blade surface pressure distribution, for the initial topology optimization design of wind turbine blade. Combined with the aerodynamic data calculated by RFOIL software and the theory of momentum leaf [7], the pressure distribution data of each airfoil section under normal operating conditions can be obtained. The aerodynamic pressure acting on the blade can be obtained according to equation (1):…”
Section: Aerodynamic Load and Boundary Conditionsmentioning
confidence: 99%
“…It is thus not surprising that Blade Element Momentum methods (simply, BEM) originally developed for wind turbines are extensively used for analysis and design of tidal and ocean current turbines, see e.g., [1]. BEM provides fast and reliable estimates of turbine performance if suitable tuning is applied to overcome important methodology weaknesses [2,3]. Specifically, blade loading is derived by prescribed lift and drag properties of two-dimensional profiles and semi-empirical three-dimensional flow corrections are necessary to account for blade tip effects, blade/hub interaction, number of blades.…”
Section: Introductionmentioning
confidence: 99%