首页> 外文期刊>Marine Systems & Ocean Technology >Numerical and experimental evaluation of cavitation flow around axisymmetric cavitators
【24h】

Numerical and experimental evaluation of cavitation flow around axisymmetric cavitators

机译:轴对称空穴空穴空穴流动的数值和实验评价

获取原文
获取原文并翻译 | 示例
       

摘要

The primary objective of this research is to study the cavitating effects of fluid flow past different axisymmetric cavitator in the upper sub-critical flow regime, which corresponds to the Reynolds number (2 × 10~4 to 2 × 10~5). Experiments are conducted in a water tunnel with a fluid flow velocity of 30 to 60 m/s at a constant rate of injection. The commercial software tool, ANSYS Fluent 18.1, is used to simplify three dimensional Reynolds averaged Navier Stokes equation with the compressible fluid flow by considering the pressure-based solver with standard K- ω turbulence model. The transport equation-based Schnerr and Sauer cavitation model is employed to study the cavitation phenomena. The finite volume discretisation method is implemented to evaluate the cavity length and diameter, respectively. A comparison of the numerical and experimental results shows that the numerical method can predict accurately the shape parameters of the natural cavitation phenomena such as cavity length, cavity diameter, and cavity shape. Results reported that with an increase in velocity, the cavity length and diameter increased to 250 and 20%, respectively. With a decrease in the cavitator angle at constant Reynolds number, the drag coefficient decreases up to 40%. Also, for the 30° cavitator, the drag coefficient rises by 28% when cavitation number is increased from 0.25 to 0.32.
机译:本研究的主要目的是研究流体流过上部亚临界流动状态的流体流过的空化效应,这对应于雷诺数(2×10〜4至2×10〜5)。实验在水隧道中进行,流体流速,以恒定的注射速率为30至60m / s。商业软件工具,ANSYS流畅的18.1,用于简化三维雷诺通过考虑基于压力的求解器与标准k-ω湍流模型的压力基求解器来简化三维雷诺等方程。基于交通方程式的Schnerr和Sauer空化模型用于研究空化现象。实施有限体积分散方法分别评估腔长和直径。数值和实验结果的比较表明,数值方法可以准确地预测天然空化现象的形状参数,例如腔长,腔直径和腔形状。结果报告称,随着速度的增加,腔体长度和直径分别增加到250%和20%。在恒定雷诺数处的空穴角度下降,拖曳系数降低至40%。此外,对于30°空穴器,当空化数从0.25增加到0.32时,阻力系数将升高28%。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号