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Coupled CAD-CFD automated optimization for leading and trailing edge of an axial impulse turbine blade

机译:耦合CAD-CFD自动优化轴向脉冲涡轮叶片的前缘和后缘

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摘要

A bidirectional impulse turbine with fixed guide vanes is used in an oscillating water column to extract wave energy. The turbine suffers from low aerodynamic efficiency, and it is required to improve performance. In the present study, coupled CAD-CFD automated optimization of the blade leading and trailing edge ratio was performed to maximize the efficiency. The design points were generated using a central composite design sampling technique and response surface optimization method estimated the optimum design. The optimization pipeline was automated using the Ansys Design Exploration module. Ansys Turbo Grid was used for generating structured hexahedral elements in the computational domain, and the problem was solved in Ansys CFX (R) v16.2. The results showed that the modified leading and trailing edge enhanced the performance compared to the reference blade by minimizing the pressure drop. The optimized design improved the relative peak efficiency and torque by 3.4% and 2% respectively. Additionally, a detailed flow analysis has been reported in this paper.
机译:具有固定导向叶片的双向脉冲涡轮机用于振荡水柱以提取波能量。涡轮机的空气动力学效率低,需要提高性能。在本研究中,执行刀片的耦合CAD-CFD自动优化,刀片引进和后缘比率以最大化效率。使用中央复合设计采样技术和响应面优化方法产生设计点,估计了最佳设计。使用ANSYS设计探索模块自动化优化管道。 ANSYS Turbo Grid用于在计算领域中生成结构化六面体元素,并且在ANSYS CFX(R)V16.2中解决了问题。结果表明,通过最小化压降,改进的前沿和后缘并增强了与参考刀片相比的性能。优化的设计分别提高了相对峰值效率和扭矩分别为3.4%和2%。另外,本文报道了详细的流动分析。

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