2019
DOI: 10.1063/1.5115903
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Improvement in aerodynamic performance of NACA0021 airfoil using moving surface boundary layer: A computational study

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Cited by 1 publication
(1 citation statement)
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“…It possesses soft stall behaviour with a moderate maximum lift coefficient. It is commonly employed on low speed wind turbines and hydropower applications [11]. It is reported that the use of the NACA0021 leads to a relatively high performance, compared to other aerofoils with comparable thickness such as the DU91-W2-250 aerofoil [12].…”
Section: The Turbine Modelmentioning
confidence: 99%
“…It possesses soft stall behaviour with a moderate maximum lift coefficient. It is commonly employed on low speed wind turbines and hydropower applications [11]. It is reported that the use of the NACA0021 leads to a relatively high performance, compared to other aerofoils with comparable thickness such as the DU91-W2-250 aerofoil [12].…”
Section: The Turbine Modelmentioning
confidence: 99%