2018
DOI: 10.1115/1.4038811
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Inverse Design of Single- and Multi-Rotor Horizontal Axis Wind Turbine Blades Using Computational Fluid Dynamics

Abstract: A method for inverse design of horizontal axis wind turbines (HAWTs) is presented in this paper. The direct solver for aerodynamic analysis solves the Reynolds Averaged Navier Stokes (RANS) equations, where the effect of the turbine rotor is modeled as momentum sources using the actuator disk model (ADM); this approach is referred to as RANS/ADM. The inverse problem is posed as follows: for a given selection of airfoils, the objective is to find the blade geometry (described as blade twist and chord distributi… Show more

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Cited by 13 publications
(6 citation statements)
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“…In aerodynamic evaluated processing, Selig and Tangler [3] use the blade element momentum (BEM) theory as for a method for aerodynamic analysis. Lee [4] used the vortex line method (VLM) and Moghadassian and Sharma [5] resolved Reynolds-averaged Navier-Stokes (RANS) equations using an actuator disk model (ADM) to emulate the rotor as a body force. These extensions permit analysis of unconventional rotor-and blade geometries, e.g., multi-rotor turbine configurations and rotor blades with dihedral and/or sweep.…”
Section: Introductionmentioning
confidence: 99%
“…In aerodynamic evaluated processing, Selig and Tangler [3] use the blade element momentum (BEM) theory as for a method for aerodynamic analysis. Lee [4] used the vortex line method (VLM) and Moghadassian and Sharma [5] resolved Reynolds-averaged Navier-Stokes (RANS) equations using an actuator disk model (ADM) to emulate the rotor as a body force. These extensions permit analysis of unconventional rotor-and blade geometries, e.g., multi-rotor turbine configurations and rotor blades with dihedral and/or sweep.…”
Section: Introductionmentioning
confidence: 99%
“…In order to account for the advantages of both the CFD and BEM methods, some researchers conducted wind turbine optimization by combining these two methods. In this way, the design accuracy and flexibility were improved while maintaining the low computational cost [31,32]. Another approach to reduce the computational cost of a CFD solution to a level as low as that of a BEM solution is to use a surrogate model such as the response surface method.…”
Section: Introductionmentioning
confidence: 99%
“…They declared that the method was rather robust and capable of recovering the blade shape corresponding to the prescribed target pressure distribution. Mileshin et al and Moghadassian and Sharma further applied their inverse design methods to improve the performance of multi‐stage compressors and wind turbine blades. Regarding the description of the blade shape, Lane, and Marshall developed an inverse design method by employing Class/Shape Transformation (CST) parameters to pursue better accuracy of the blade geometry .…”
Section: Introductionmentioning
confidence: 99%