Comparison of aerodynamic models for horizontal axis wind turbine blades accounting for curved tip shapes

Abstract Curved tip extensions are among the rotor innovation concepts that can contribute to the higher performance and lower cost of horizontal axis wind turbines. One of the key drivers to exploit their advantages is the use of accurate and efficient computational aerodynamic models during the de...

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Main Authors: Sergio González Horcas, Néstor Ramos‐García, Ang Li, Georg Pirrung, Thanasis Barlas
Format: Article
Language:English
Published: Wiley 2023-01-01
Series:Wind Energy
Subjects:
Online Access:https://doi.org/10.1002/we.2780
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author Sergio González Horcas
Néstor Ramos‐García
Ang Li
Georg Pirrung
Thanasis Barlas
author_facet Sergio González Horcas
Néstor Ramos‐García
Ang Li
Georg Pirrung
Thanasis Barlas
author_sort Sergio González Horcas
collection DOAJ
description Abstract Curved tip extensions are among the rotor innovation concepts that can contribute to the higher performance and lower cost of horizontal axis wind turbines. One of the key drivers to exploit their advantages is the use of accurate and efficient computational aerodynamic models during the design stage. The present work gives an overview of the performance of different state‐of‐the‐art models. The following tools were employed, in descending order of complexity: (i) a blade‐resolved Navier Stokes solver, (ii) a lifting line model, (iii) a vortex‐based method coupling a near‐wake model with a far‐wake model, and (iv) two implementations of the widely used blade element momentum method (BEM), with and without radial induction. The predictions of the codes were compared when simulating the baseline geometry of a reference wind turbine and different tip extension designs with relatively large sweep angle and/or dihedral angle. Four load cases were selected for this comparison, to cover several aspects of the aerodynamic modeling: steady power curve, pitch step, extreme operating gust impact, and standstill in deep stall. The present study highlighted the limitations of the BEM‐based formulations to capture the trends attributed to the introduction of curvature at the tip. This was true even when using the radial induction submodel. The rest of the computational methods showed relatively good agreement in most of the studied load cases. An exception to this was the standstill configuration, as the blade‐resolved Navier‐Stokes solver was the only code able to capture the highly unsteady effects of deep stall.
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spelling doaj.art-eb40e9bf602848a5a73c3980ec3ff31c2022-12-22T04:22:59ZengWileyWind Energy1095-42441099-18242023-01-0126152210.1002/we.2780Comparison of aerodynamic models for horizontal axis wind turbine blades accounting for curved tip shapesSergio González Horcas0Néstor Ramos‐García1Ang Li2Georg Pirrung3Thanasis Barlas4Department of Wind Energy Technical University of Denmark (DTU) Roskilde DenmarkDepartment of Wind Energy Technical University of Denmark (DTU) Roskilde DenmarkDepartment of Wind Energy Technical University of Denmark (DTU) Roskilde DenmarkDepartment of Wind Energy Technical University of Denmark (DTU) Roskilde DenmarkDepartment of Wind Energy Technical University of Denmark (DTU) Roskilde DenmarkAbstract Curved tip extensions are among the rotor innovation concepts that can contribute to the higher performance and lower cost of horizontal axis wind turbines. One of the key drivers to exploit their advantages is the use of accurate and efficient computational aerodynamic models during the design stage. The present work gives an overview of the performance of different state‐of‐the‐art models. The following tools were employed, in descending order of complexity: (i) a blade‐resolved Navier Stokes solver, (ii) a lifting line model, (iii) a vortex‐based method coupling a near‐wake model with a far‐wake model, and (iv) two implementations of the widely used blade element momentum method (BEM), with and without radial induction. The predictions of the codes were compared when simulating the baseline geometry of a reference wind turbine and different tip extension designs with relatively large sweep angle and/or dihedral angle. Four load cases were selected for this comparison, to cover several aspects of the aerodynamic modeling: steady power curve, pitch step, extreme operating gust impact, and standstill in deep stall. The present study highlighted the limitations of the BEM‐based formulations to capture the trends attributed to the introduction of curvature at the tip. This was true even when using the radial induction submodel. The rest of the computational methods showed relatively good agreement in most of the studied load cases. An exception to this was the standstill configuration, as the blade‐resolved Navier‐Stokes solver was the only code able to capture the highly unsteady effects of deep stall.https://doi.org/10.1002/we.2780IEA 10 MW RWTComputational aerodynamicsComputational aeroelasticityComputational Fluid DynamicsBlade Element MomentumLifting Line
spellingShingle Sergio González Horcas
Néstor Ramos‐García
Ang Li
Georg Pirrung
Thanasis Barlas
Comparison of aerodynamic models for horizontal axis wind turbine blades accounting for curved tip shapes
Wind Energy
IEA 10 MW RWT
Computational aerodynamics
Computational aeroelasticity
Computational Fluid Dynamics
Blade Element Momentum
Lifting Line
title Comparison of aerodynamic models for horizontal axis wind turbine blades accounting for curved tip shapes
title_full Comparison of aerodynamic models for horizontal axis wind turbine blades accounting for curved tip shapes
title_fullStr Comparison of aerodynamic models for horizontal axis wind turbine blades accounting for curved tip shapes
title_full_unstemmed Comparison of aerodynamic models for horizontal axis wind turbine blades accounting for curved tip shapes
title_short Comparison of aerodynamic models for horizontal axis wind turbine blades accounting for curved tip shapes
title_sort comparison of aerodynamic models for horizontal axis wind turbine blades accounting for curved tip shapes
topic IEA 10 MW RWT
Computational aerodynamics
Computational aeroelasticity
Computational Fluid Dynamics
Blade Element Momentum
Lifting Line
url https://doi.org/10.1002/we.2780
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