The current trend in the wind power market is to develop large diameter rotors in order to maximize the power extraction from the wind. Those rotors exhibit issues related to blade deflection and structural integrity that can be mitigated implementing design variations that were present on the early wind turbine designs, such as rotors with less than three blades located behind the tower in downwind configuration. This work assesses the aerodynamic performance of a downwind two-bladed wind turbine based on CFD simulations coupled with the Actuator Line Model (ALM). This design is compared with the MEXICO project upwind three-bladed wind turbine, for which experimental data is available. The simulations showed good agreement with measurements especially upstream the rotor and for higher inlet velocities. Furthermore, the downwind configuration was successfully modeled using ALM and the performance prediction of the turbines was physically accurate since realistic variations were obtained between the evaluated wind turbines and none of their performance coefficients exceeded Betz theoretical limit.
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ASME 2018 International Mechanical Engineering Congress and Exposition
November 9–15, 2018
Pittsburgh, Pennsylvania, USA
Conference Sponsors:
- ASME
ISBN:
978-0-7918-5210-1
PROCEEDINGS PAPER
Downwind Two-Bladed Wind Turbine Aerodynamic Performance Evaluation Implementing Actuator Line Model
Sebastian Henao,
Sebastian Henao
National University of Colombia, Medellín, Colombia
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Aldo G. Benavides,
Aldo G. Benavides
National University of Colombia, Medellín, Colombia
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Omar D. López
Omar D. López
Los Andes University, Bogotá, Colombia
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Sebastian Henao
National University of Colombia, Medellín, Colombia
Aldo G. Benavides
National University of Colombia, Medellín, Colombia
Omar D. López
Los Andes University, Bogotá, Colombia
Paper No:
IMECE2018-86549, V007T09A089; 11 pages
Published Online:
January 15, 2019
Citation
Henao, S, Benavides, AG, & López, OD. "Downwind Two-Bladed Wind Turbine Aerodynamic Performance Evaluation Implementing Actuator Line Model." Proceedings of the ASME 2018 International Mechanical Engineering Congress and Exposition. Volume 7: Fluids Engineering. Pittsburgh, Pennsylvania, USA. November 9–15, 2018. V007T09A089. ASME. https://doi.org/10.1115/IMECE2018-86549
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