2016
DOI: 10.1016/j.renene.2016.03.027
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Aerodynamic wind-turbine rotor design using surrogate modeling and three-dimensional viscous–inviscid interaction technique

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Cited by 38 publications
(25 citation statements)
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“…The first and outer level is a surrogate-based optimization code developed by the authors [45,46] to solve Equation (5) in terms of blade chord, twist and relative thickness distributions. The second and inner level is the structural optimization routine described above which is performed for each candidate blade design from the first/outer level.…”
Section: Numerical Toolsmentioning
confidence: 99%
“…The first and outer level is a surrogate-based optimization code developed by the authors [45,46] to solve Equation (5) in terms of blade chord, twist and relative thickness distributions. The second and inner level is the structural optimization routine described above which is performed for each candidate blade design from the first/outer level.…”
Section: Numerical Toolsmentioning
confidence: 99%
“…Surrogate models have been used previously in wind turbine optimization. One surrogate optimization methodology implements a high‐fidelity viscous‐inviscid interaction code to evaluate the aerodynamic design . Another approach using a kriging fit to optimize the site‐specific aerodynamic design .…”
Section: Introductionmentioning
confidence: 99%
“…One surrogate optimization methodology implements a high-fidelity viscous-inviscid interaction code to evaluate the aerodynamic design. 15 Another approach using a kriging fit to optimize the site-specific aerodynamic design. 16 Our approach is unique in that our developed surrogate model that is used to predict the fatigue damage and extreme loads for a variety of design load cases can be extended (albeit on a limited extent) to wind turbines that were not originally included in the training of the data set.…”
mentioning
confidence: 99%
“…In the recent years, vortex methods have become an attractive tool for the analysis and design of wind turbine rotors . Combined with panel methods, the complete blade geometry is taken into account in the simulation after which a detailed aerodynamic description is obtained where sub‐chord flow scales are included.…”
Section: Introductionmentioning
confidence: 99%