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EXPLORATION AND RESEARCH OF THE IMPACT OF HYDROFOIL SURFACE WATER INJECTION ON CAVITATION SUPPRESSION

机译:水翼表面注水对空化抑制作用影响的探索研究

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To explore the impact of hydrofoil surface water injection on cavitation suppression, the unsteady cavitation flow around the NACA0066 hydrofoil was simulated by the modified RNG k-ε turbulence model combined with the full-cavitation model. The influence of water injection position and jet angle on cavitation suppression were analyzed. A detailed analysis shows that cavitation suppression effect is closely related to water injection position and jet angle. It is noted that the optimal position is just the vertex position on the upper surface of hydrofoil. Water injection in an appropriate position will increase the velocity gradient in the boundary layer and enhanced the ability of anti reverse pressure gradient, thus weakening the intensity of separation flow. The recirculation zone thickness and the velocity of re-entrant jet are all significantly reduced. For the study of jet angle, the cavitation suppression effect is obvious with jet angles from 145° to 155°. This may due to the high pressure produced by the mixing of jet with the main flow, and the high-pressure zone limit the spread of low pressure from the leading edge to the trailing edge of hydrofoil. This can also explain why the suppression effect is significant at the vertex position on the upper surface.
机译:为了探索水翼地表注水对气蚀抑制的影响,通过改进的RNGk-ε湍流模型与全气蚀模型相结合,模拟了NACA0066水翼周围的非定常气蚀流。分析了注水位置和射流角度对气蚀抑制的影响。详细分析表明,气蚀抑制效果与注水位置和射流角密切相关。注意,最佳位置只是水翼上表面的顶点位置。在适当的位置注水将增加边界层的速度梯度,并增强了抗反向压力梯度的能力,从而削弱了分离流的强度。回流区的厚度和折返射流的速度均显着降低。对于射流角的研究,当射流角在145°至155°之间时,气蚀抑制效果很明显。这可能是由于射流与主流混合而产生的高压,而高压区限制了低压从水翼的前缘到后缘的扩散。这也可以解释为什么抑制效果在上表面的顶点位置处显着的原因。

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