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Effect of asymmetrical tip clearances on energy performance and cavitation characteristics of NACA0009 hydrofoil in tidal energy

机译:不对称尖端间隙对潮汐能NACA0009水翼能量性能及空化特性的影响

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Tidal energy is an important renewable energy that uses the potential energy created by the rising and falling of ocean tides to generate electricity. The tip leakage vortex (TLV) and cavitation caused by the tip leakage flow have adverse effects on the energy conversion efficiency and stable operation of the tubular turbine. The selection of the tip clearance shape is critical. Therefore, the effects of four different combinations of asymmetrical tip clearance shapes on the energy and cavitation characteristics of hydrofoils are studied in this paper. The results show that the TLV remains unchanged when tipwall and endwall are sinusoidal and cosine curve shaped, respectively. When tip clearance is the combination of a flat tipwall and a sinusoidal endwall, the lift-drag ratio decreases by 10.72 . The high shear stress region of tipwall near leading edge decreases. The flow resistance of the leakage flow decreases, and the leakage flow becomes more serious. The cavitation volume is 2.5 times that under the original flat tip clearance. When tip clearance is the combination of a flat tipwall and a cosine endwall, and the lift-drag ratio increases by 9.67 . The shear stress increases, the leakage flow decreases. The swirling strength around the center of the vortex core is weakened. The cavitation volume is 3.81, with a decrease of nearly 30 . A proper asymmetrical tip clearance can effectively improve the energy performance and cavitation characteristics of hydrofoils. This study provides theoretical support for the design and optimization of hydraulic machine with tip clearance.
机译:潮汐能是一种重要的可再生能源,它利用海洋潮汐涨落产生的势能来发电。尖端泄漏流引起的尖端泄漏涡流(TLV)和气蚀对管式涡轮机的能量转换效率和稳定运行产生不利影响。尖端间隙形状的选择至关重要。因此,本文研究了4种不同组合的不对称尖端间隙形状对水翼能量和空化特性的影响。结果表明:当顶壁和端壁分别呈正弦曲线和余弦曲线时,TLV保持不变;当尖端间隙为平坦的尖端壁和正弦端壁的组合时,升阻比降低了 10.72 %。前缘附近翻墙的高剪应力区域减小。泄漏流的流动阻力减小,泄漏流变得更加严重。气蚀体积是原始平头间隙下的2.5倍。当尖端间隙为平坦的尖端壁和余弦端壁的组合时,升阻比增加 9.67 %。剪切应力增加,泄漏流量减小。涡旋核心中心的漩涡强度减弱。空化体积为3.81,减少近30%。适当的不对称尖端间隙可以有效提高水翼的能源性能和气蚀特性。本研究为带叶尖间隙的液压机的设计与优化提供了理论支持。

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