2012
DOI: 10.1115/1.4007798
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A Continuum Based Three-Dimensional Modeling of Wind Turbine Blades

Abstract: Accurate modeling of large wind turbine blades is an extremely challenging problem. This is due to their tremendous geometric complexity and the turbulent and unpredictable conditions in which they operate. In this paper, a continuum based three dimensional finite element model of an elastic wind turbine blade is derived using the absolute nodal coordinates formulation (ANCF). This formulation is very suitable for modeling of largedeformation, large-rotation structures like wind turbine blades. An efficient mo… Show more

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Cited by 22 publications
(17 citation statements)
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“…In general, most studies on ANCF shell elements have been based on purely academic models that are usually rectangular. One practical application of initially curved ANCF shell elements has been the analysis of large deflection wind turbine blades [1,2,11]. The focus in these studies has been on the discretization of the complex blade geometry into an ANCF finite element mesh rather than the computational performance of the discretized model.…”
Section: Introductionmentioning
confidence: 99%
“…In general, most studies on ANCF shell elements have been based on purely academic models that are usually rectangular. One practical application of initially curved ANCF shell elements has been the analysis of large deflection wind turbine blades [1,2,11]. The focus in these studies has been on the discretization of the complex blade geometry into an ANCF finite element mesh rather than the computational performance of the discretized model.…”
Section: Introductionmentioning
confidence: 99%
“…Under the umbrella of the multibody system dynamics, efficient procedure was developed for mapping airfoils geometry of wind turbine blades into flexible models using absolute nodal coordinate formulation (ANCF) [4,5]. This procedure is extended to involve the complete aerodynamical and structural behavior of blades with the nonuniform and twisted configuration [6].…”
Section: Introductionmentioning
confidence: 99%
“…In Nada, 8 the ANCF is used for constructing a continuum model of blade-span with uniform structure, in this model, Bspline surface is used to approximate airfoil structures. In Bayoumy et al, 18 the ANCF is used in modeling the blade-span for non-uniform and twisted structure; in this model, an analytical and explicit procedure is established for calculating the ANCF positions and gradients of NACA (National Advisory Committee for Aeronautics airfoils). Both models concern the ANCF thin plate element for modeling the blade-span structure due to its aerodynamical nature.…”
Section: Introductionmentioning
confidence: 99%