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A Numerical Study on Cavitation Suppression Using Local Cooling

机译:局部冷却抑制气蚀的数值研究

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This study strives to develop an effective strategy to inhibit cavitation inception on hydrofoils by using local cooling technique. By setting up a temperature boundary condition and cooling a small area on the upper surface of a hydrofoil, the fluid temperature around the cooling surface will be decreased and thereby the corresponding liquid saturation pressure will drop below the lowest absolute pressure within the flow field. Hence, cavitation can never occur. In this paper, a NACA0015 hydrofoil at 4° angle of attack was numerically investigated to verify the effectiveness of the proposed technique. The CFD results indicate that the cooling temperature and the cooling surface roughness are the critical factors affecting the success of such technique used for cavitation suppression.
机译:这项研究致力于通过使用局部冷却技术来开发一种有效的策略来抑制水翼上的气蚀现象。通过设置温度边界条件并冷却水翼上表面的一小块区域,冷却表面周围的流体温度将降低,因此相应的液体饱和压力将降至流场内的最低绝对压力以下。因此,空化永远不会发生。在本文中,对攻角为4°的NACA0015水翼进行了数值研究,以验证所提出技术的有效性。 CFD结果表明,冷却温度和冷却表面粗糙度是影响这种用于抑制气蚀的技术成功与否的关键因素。

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