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CA9: Analysis of a Stall-Resistant Aerofoil in View of Wave Power Conversion

机译:CA9:鉴于波力转换的耐稳定性翼型分析

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Wave energy power take-off typically consists of a Wells turbine. This self-rectifying axial air turbine has shown to be constrained by severe stall at high angle of attack or in the supercritical range. This paper presents an experimental and numerical investigation of the CA9 aerofoil, which was optimised for stall resistance. Analysis was done for a 0.6m rotor and tests were carried out at Re = 5×10~5 and Ma = 0.2. Results showed that the CA9 profile was more resistant to stall and had a higher average efficiency than NACA0015; thus being more suitable for wave energy conversion systems. Numerical data was benchmarked using experimental ones and provided an insight in the separation mechanism of the flow. Guide vanes improved both starting and running characteristics of rotor.
机译:波浪能量输出通常由井涡轮​​机组成。这种自整流的轴向空气涡轮机表明,在高迎角或超临界范围内受到严重摊位的约束。本文介绍了CA9 Aerofoil的实验性和数值研究,其针对失速抗性进行了优化。为0.6M转子进行分析,并在RE = 5×10〜5和MA = 0.2处进行测试。结果表明,CA9型材更耐抵抗,比NACA0015更高的平均效率;因此更适合于波能量转换系统。数值数据使用实验数据基准测试,并在流动的分离机制中提供了洞察力。导向叶片改善了转子的起始和运行特性。

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