ASME 2019 2nd International Offshore Wind Technical Conference 2019
DOI: 10.1115/iowtc2019-7540
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Lifting Line Free Wake Vortex Filament Method for the Evaluation of Floating Offshore Wind Turbines: First Step — Validation for Fixed Wind Turbines

Abstract: An in-house computational tool, called MIST, has been developed to improve the accuracy of the aerodynamic loads predictions of floating wind turbines. MIST has an aerodynamic module based on a Free Vortex filament Method (FVM) for the wake combined with a Lifting Line (LL) model for the blades. This aerodynamic model has been validated, in this first instance, for an onshore configuration against well known experimental data. Different options for the critical parameters of the code have been analyzed to get … Show more

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Cited by 5 publications
(7 citation statements)
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“…In this study, the INNWIND 10MW offshore wind turbine [9] supported by the SATH platform, designed by Saitec Offshore Technologies [10], have been used for the analysis. This wind turbine is a three bladed upwind system with 10 MW rated power.…”
Section: Floating Wind Turbinementioning
confidence: 99%
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“…In this study, the INNWIND 10MW offshore wind turbine [9] supported by the SATH platform, designed by Saitec Offshore Technologies [10], have been used for the analysis. This wind turbine is a three bladed upwind system with 10 MW rated power.…”
Section: Floating Wind Turbinementioning
confidence: 99%
“…The potential flow frequency domain solution was computed with WAMIT version 6.4 [16] and then transferred to time domain by HydroDyn. The viscous effects, that are neglected by the potential theory but can contribute to the system damping, were included using the Morison equation [10].…”
Section: Numerical Modelmentioning
confidence: 99%
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“…This happens because Blade Element Momentum Theory (BEMT) (Sørensen, 2016), which is the most widely aerodynamic model used in the wind energy industry, presents limitations when predicting loads in situations with large yaw or tilt misalignment between wind and rotor, mainly because the root vortex is not well modelled (Sant, 2007;Rahimi et al, 2016;Gupta and Leishman, 2005). The FVM model implemented in AeroVIEW has been validated previously in yaw misaligned conditions (Martín-San-Román et al, 2019 and allows an accurate inclusion of the effect of both the root vortex and the blade tip vortex in both aligned and misaligned conditions.…”
Section: Introductionmentioning
confidence: 99%