2018 Wind Energy Symposium 2018
DOI: 10.2514/6.2018-0991
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Wind Turbine Aerodynamics from an Aerospace Perspective

Abstract: The current challenges in wind turbine aerodynamics simulations share a number of similarities with the challenges that the aerospace industry has faced in the past. Some of the current challenges in the aerospace aerodynamics community are also relevant for today's wind turbine aerodynamics community and vice versa. This paper sketches these similarities in broad strokes and points out the possibilities to revive solutions from the aerospace aerodynamics community from the 1960's onward that, with some modifi… Show more

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Cited by 20 publications
(30 citation statements)
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“…This tool is an appealing alternative in the early stages of wind turbine design due to its simplicity of use and satisfactory accuracy provided at a lower computational cost than CFD tools. [18][19][20][21] A turbulent, viscous potential flow field around the wind turbine is resolved by QBlade. The Non-Linear Lifting Lines Free Vortex Wake (NLLFVW) method, in contrast to BEM techniques, relies on fewer assumptions and experimental corrections to resolve 3D flow structure around the blades.…”
Section: Methodsmentioning
confidence: 99%
“…This tool is an appealing alternative in the early stages of wind turbine design due to its simplicity of use and satisfactory accuracy provided at a lower computational cost than CFD tools. [18][19][20][21] A turbulent, viscous potential flow field around the wind turbine is resolved by QBlade. The Non-Linear Lifting Lines Free Vortex Wake (NLLFVW) method, in contrast to BEM techniques, relies on fewer assumptions and experimental corrections to resolve 3D flow structure around the blades.…”
Section: Methodsmentioning
confidence: 99%
“…Rotational effects were already included in the airfoil polar data thus no additional 3D correction was applied in AM. Snel's first-order model [11] was used to account for dynamic stall effects in both BEM and AWSM (AM's FVW model [12]) simulations. To compare with the experiment, the ensemble-averaged individual blade pitch and rotor speed time histories obtained from the wind tunnel measurements were prescribed in the simulations.…”
Section: Simulation Modelsmentioning
confidence: 99%
“…The optimization technique that will be used to this end is Multi-objective Bayesian Optimization (MOBO). MOBO builds a probabilistic model of the objective function, where the objective function is the aerodynamic performance evaluated by the aerodynamic analysis tool, for which the lifting line code AWSM [11] is used. AWSM's free wake model is used where the wake length is set to three diameters.…”
Section: Optimization Setupmentioning
confidence: 99%