首页> 外文学位 >Study of tip clearance flow in a turbomachinery cascade using large eddy simulation.
【24h】

Study of tip clearance flow in a turbomachinery cascade using large eddy simulation.

机译:利用大涡模拟研究涡轮机械叶栅中的叶尖间隙流。

获取原文
获取原文并翻译 | 示例

摘要

In liquid handling systems like pumps and ducted propulsors, low pressure events in the vicinity and downstream of the rotor tip gap can induce tip-leakage cavitation which leads to noise, vibration, performance loss, and erosions of blade and casing wall. In order to analyze the dynamics of the tip-clearance flow and determine the underlying mechanism for the low pressure events, a newly developed large-eddy simulation (LES) solver which combines an immersed-boundary method with a generalized curvilinear structured grid has been employed. An analysis of the LES results has been performed to understand the mean flow field, turbulence characteristics, vortex dynamics, and pressure fluctuations in the turbomachinery cascade with tip gap. In the cascade passage, the tip-leakage jet, which is generated by the pressure difference between the pressure and suction sides of the blade tip, is found to produce highly enhanced vorticity magnitude and significant levels of turbulent kinetic energy. Based on the understanding of the flow field, a guideline for reducing viscous loss in the cascade is provided. Analyses of the energy spectra and space-time correlations of the velocity fluctuations suggest that the tip-leakage vortex is subject to pitchwise wandering motion. The largest pressure drop and most intense pressure fluctuations due to the formation of the tip-leakage vortex are found at the location where the strongest portion of the tip-leakage vortex is found. Present study suggests that the tip-leakage vortex needs to be controlled in its origin to reduce cavitation in the present configuration. The effects of tip-gap size on the end-wall vortical structures and on the velocity and pressure fields have been investigated. The present analysis indicates that the mechanism for the generation of the vorticity and turbulent kinetic energy is mostly unchanged by the tip-gap size variation. However, larger tip-gap sizes are found to be more inductive to tip-leakage cavitation judged by the levels of negative mean pressure and pressure fluctuations.
机译:在诸如泵和管道推进器之类的液体处理系统中,转子尖端间隙附近和下游的低压事件会引起尖端泄漏空化,从而导致噪音,振动,性能损失以及叶片和壳体壁的腐蚀。为了分析叶尖间隙流动的动力学并确定低压事件的潜在机理,采用了一种新开发的大涡模拟(LES)求解器,该方法将浸入边界方法与广义曲线结构化网格相结合。对LES结果进行了分析,以了解具有尖端间隙的涡轮机叶栅中的平均流场,湍流特性,涡旋动力学和压力波动。在叶栅通道中,发现由叶尖的压力侧和吸力侧之间的压力差产生的叶尖泄漏射流会产生高度增强的涡度和显着水平的湍动能。基于对流场的理解,提供了减少级联中粘性损失的指南。能量谱的分析和速度波动的时空相关性表明,尖端泄漏涡流受到螺距的漂移运动的影响。在尖端泄漏涡旋最强的位置发现了最大的压降和最剧烈的压力波动,这是由尖端泄漏涡的形成引起的。目前的研究表明,在本构造中,需要控制尖端泄漏涡的起源,以减少空化现象。研究了尖端间隙尺寸对端壁涡旋结构以及速度场和压力场的影响。目前的分析表明,由于间隙间隙的大小变化,产生涡旋和湍动能的机理基本没有改变。然而,发现较大的尖端间隙尺寸对由负平均压力和压力波动水平判断的尖端泄漏空化具有更大的诱导作用。

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