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

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 stag...

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Veröffentlicht in:Wind energy (Chichester, England) Jg. 26; H. 1; S. 5 - 22
Hauptverfasser: Horcas, Sergio González, Ramos‐García, Néstor, Li, Ang, Pirrung, Georg, Barlas, Thanasis
Format: Journal Article
Sprache:Englisch
Veröffentlicht: Bognor Regis John Wiley & Sons, Inc 01.01.2023
Wiley
Schlagworte:
Aerodynamics
Blade Element Momentum
Computational aerodynamics
Computational aeroelasticity
Computational Fluid Dynamics
Computer applications
Design optimization
Dihedral angle
Fluid flow
Geometry
Horizontal Axis Wind Turbines
IEA 10 MW RWT
Lifting Line
Load
Near wake
Numerical analysis
Proprietary
Simulation
Solvers
Stalling
Sweep angle
Turbine blades
Turbines
Wind power
ISSN:1095-4244, 1099-1824
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Zusammenfassung: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.
Bibliographie:Funding information
Innovationsfonden, Grant/Award Number: 7046‐00023B
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ISSN:1095-4244
1099-1824
DOI:10.1002/we.2780