Title of article :
Reaching the betz limit experimentally and numerically
Author/Authors :
Ranjbar, Mohammad Hassan Faculty of Engineering - University of Tehran, Tehran , Nasrazadani, Abolfazl Faculty of Engineering - University of Tehran, Tehran , Zanganeh Kia, Hadi Faculty of Engineering - University of Tehran, Tehran , Gharali, Kobra Faculty of Engineering - University of Tehran, Tehran
Pages :
8
From page :
271
To page :
278
Abstract :
The Betz theory expresses that no horizontal axis wind turbine can extract more than 16/27 (59.3%) of the kinetic energy of the wind. The factor 16/27 (0.593) is known as the Betz limit. Horizontal Axis wind turbine designers try to improve the power performance to reach the Betz limit. Modern operational wind turbines achieve at peak 75% to 80% of the Betz limit. In 1919, Albert Betz used an analytical method to derive the Betz limit. He derived momentum equations of an Actuator Disc (AD) in the stream. In this research, an experimental and a numerical setup based on the Actuator Disc (AD) have been designed and tested to reach the Betz limit. A Plexiglass screen with the porosity of 0.5 mimics the wind turbine rotor. For the numerical study, a 2D 􀏔low 􀏔iled is considered. The results of both experimental and numerical methods agree well with the analytical results of the Betz theory. From the experimental and numerical results, the relative errors in comparison with the Betz limit (which is 16/27) are 0.16% and 1.27%, respectively. The small amount of errors shows the possibility of reaching the Betz limit using either experimental or numerical methods. This approach can be used for modeling ideal wind turbines, ideal rotating devices or ideal wind farms either numerically or experimentally and gives the maximum possible power extractions; thus, any improvement to the performance of a system can be made by this method.
Keywords :
Betz Limit , Actuator Disc , Wind Turbine , CFD , Experiment , Porosity
Journal title :
Astroparticle Physics
Serial Year :
2019
Record number :
2466204
Link To Document :
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