Optimization of airfoil geometry using the NSGA-II method to improve the performance and efficiency of a very low head turbine
|更新时间:2026-06-24
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Optimization of airfoil geometry using the NSGA-II method to improve the performance and efficiency of a very low head turbine
Optimization of airfoil geometry using the NSGA-II method to improve the performance and efficiency of a very low head turbine
清洁能源(英文)2026年第3期
作者机构:
1. Department of Thermofluids, Faculty of Mechanical Engineering, Universiti Teknologi Malaysia
2. Research Center for Energy Conversion Technology, Research Organization for Energy and Manufacture, National Research and Innovation Agency (BRIN)
3. Department of Applied Mechanics and Design, Faculty of Mechanical Engineering, Universiti Teknologi Malaysia
4. Department of Aerospace Engineering, Faculty of Mechanical and Aerospace Engineering, Institut Teknologi Bandung
5. Research Center for Hydrodynamics Technology, Research Organization for Energy and Manufacture, National Research and Innovation Agency (BRIN)
作者简介:
基金信息:
This research was funded by National Research and Innovation Agency - Indonesia (Grant No. B-34521/III.3/TK.03.00/12/2024) and Universiti Teknologi Malaysia (Grant No. Q.J130000.3824.22H61) for funding this research and publication.
Ridwan Arief Subekti, Fazila Mohd-Zawawi, Kamarulafizam Ismail, 等. Optimization of airfoil geometry using the NSGA-II method to improve the performance and efficiency of a very low head turbine[J]. 清洁能源(英文), 2026,(3).
Ridwan Arief Subekti, Fazila Mohd-Zawawi, Kamarulafizam Ismail, Derren Audric Sudarto, Muhammad Lucky Witjaksono, Qidun Maulana Binu Soesanto, Anjar Susatyo, Henny Sudibyo, Ahmad Fudholi, Rudi Darussalam, Optimization of airfoil geometry using the NSGA-II method to improve the performance and efficiency of a very low head turbine, Clean Energy, Volume 10, Issue 3, June 2026, Pages 127–142, https://doi.org/10.1093/ce/zkag024
Ridwan Arief Subekti, Fazila Mohd-Zawawi, Kamarulafizam Ismail, 等. Optimization of airfoil geometry using the NSGA-II method to improve the performance and efficiency of a very low head turbine[J]. 清洁能源(英文), 2026,(3).DOI: 10.1093/ce/zkag024.
Ridwan Arief Subekti, Fazila Mohd-Zawawi, Kamarulafizam Ismail, Derren Audric Sudarto, Muhammad Lucky Witjaksono, Qidun Maulana Binu Soesanto, Anjar Susatyo, Henny Sudibyo, Ahmad Fudholi, Rudi Darussalam, Optimization of airfoil geometry using the NSGA-II method to improve the performance and efficiency of a very low head turbine, Clean Energy, Volume 10, Issue 3, June 2026, Pages 127–142, https://doi.org/10.1093/ce/zkag024DOI:
Optimization of airfoil geometry using the NSGA-II method to improve the performance and efficiency of a very low head turbine
摘要
Abstract
Research on the development of very low head turbines is becoming increasingly important for harnessing the potential of hydropower in flat-bottomed rivers. However
studies on very low head turbine runner optimization are generally limited to single-objective approaches or have not specifically integrated airfoil parameterization and aerodynamic evaluation within a multiobjective framework. This study proposed the optimization of the very low head propeller turbine runner airfoil geometry using the nondominated sorting genetic algorithm II multiobjective framework
which combines class shape transformation
genetic algorithm
and XFOIL. The turbine was designed for a net head of 2.07 m
a flow rate of 0.04 m3/s
and a rotational speed of 1700 rpm (high-speed micro-propeller turbine). Optimization was performed on five runner segments to improve the airfoil’s hydrodynamic characteristics
which were subsequently validated using three-dimensional computational fluid dynamics simulations. The results showed that optimization increased the lift-to-drag ratio to 27.67% over the low angle of attack range relevant to operating conditions. At the design point
the optimized runner achieved an efficiency of 86.8% and a power output of ∼573 W
which is 1.48% higher than the initial design. These results demonstrate that the nondominated sorting genetic algorithm II-based class shape transformation–genetic algorithm–XFOIL framework is effective for improving the performance of very low head turbine runners.