Application of computational fluid dynamics models to aerodynamic design and optimization of wind turbine airfoils

In this work, the capability of simple numerical models with coarse grids to predict performance coefficients in wind turbine airfoils is explored. A wide range of simulations were performed for a typical wind turbine profile, under the main criteria of design simplicity and low calculation time. Th...

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Detalles Bibliográficos
Autores: Castiñeira Martínez, Esther, Solís Gallego, Irene|||0000-0002-1130-614X, González Pérez, José|||0000-0002-5195-3229, Fernández Oro, Jesús Manuel, Argüelles Díaz, Katia María|||0000-0003-1641-637X, Velarde Suárez, Sandra|||0000-0002-4967-4642
Tipo de recurso: artículo
Fecha de publicación:2014
País:España
Institución:Universidad de Oviedo (UNIOVI)
Repositorio:RUO. Repositorio Institucional de la Universidad de Oviedo
Idioma:inglés
OAI Identifier:oai:digibuo.uniovi.es:10651/72409
Acceso en línea:https://hdl.handle.net/10651/72409
https://dx.doi.org/10.24084/REPQJ12.342
Access Level:acceso abierto
Palabra clave:Wind turbine airfoils
CFD
2D-RANS
Numerical models
Turbulence models
Descripción
Sumario:In this work, the capability of simple numerical models with coarse grids to predict performance coefficients in wind turbine airfoils is explored. A wide range of simulations were performed for a typical wind turbine profile, under the main criteria of design simplicity and low calculation time. The solutions were computed over different mesh sizes using a two-dimensional Reynolds-Average Navier-Stockes (2D-RANS) approach. Spalart-Allmaras, k-ε and k- turbulence models were run in the simulations. Lift, drag and momentum coefficients were computed for four incident angles, ranging from -2.5 to 12.5, for each mesh size and turbulence model, comparing them later with experimental data. Results show a useful model which gives a good agreement between numerical and experimental results and can indeed be used as a first approximation previous to a more detailed and expensive study.