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The Effects of Leading-edge Suction on Hydrodynamic Performance and Cavitation Performance of Hydrofoil

机译:前缘吸力对水翼流体动力性能和空化性能的影响

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In order to study the effects of leading-edge suction on hydrodynamic performance and cavitation performance of hydrofoil,this paper applied FLUENT software for the system factors analysis.The variational conditions of lift and drag coefficients,and lift drag ratio were analyzed while suction inlet was added at leading-edge of hydrofoil.The effect on stalling angle was also studied.The results have shown that the suction inlet can increase the stalling angle,enlarge the stable working angle limit,enhance lift drag ratio,and improve the efficiency of the hydrofoil.This paper also calculated NACA0012 airfoil and its leading-edge suction hydrofoil while considering both steady and unsteady cavitating flow.The results have shown that the suction inlet can make the cavitation bubble size decrease,and reduce the influence area of cavitation.
机译:为了研究前缘吸附对水翼水动性能和空化性能的效果,本文应用了系统因素分析的流畅软件。分析了升力和拖曳系数的变分条件,以及吸入入口的同时分析了升力牵伸比率在水翼的前缘添加。研究了对失速角的影响。结果表明,吸入入口可以增加失速角,扩大稳定的工作角度限制,增强升力阻力比,提高水翼效率本文还计算了NaCA0012翼型及其前缘吸水机,同时考虑稳定和不稳定的空化流动。结果表明,吸入入口可以使空化气泡尺寸降低,并减少空化的影响面积。

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