首页> 外文期刊>Journal of Engineering for Gas Turbines and Power >Trajectory of a Liquid Jet in a High Temperature and Pressure Gaseous Cross Flow
【24h】

Trajectory of a Liquid Jet in a High Temperature and Pressure Gaseous Cross Flow

机译:高温高压气态横流中液体射流的轨迹

获取原文
获取原文并翻译 | 示例
           

摘要

An experimental study of liquid jet injection into subsonic air crossflow is presented. The aim of this study was to relate the jet trajectory to flow parameters, including jet and air velocities, pressure and temperature, as well as a set of nondimensional variables. For this purpose, an experimental setup was developed, which could withstand high temperatures and pressures. Images were captured using a laser-based shadowgraphy system. A total of 209 different conditions were tested and over 72,000 images were captured and processed. The crossflow air temperatures were 25 degrees C, 200 degrees C, and 300 degrees C; absolute crossflow air pressures were 2.1, 3.8, and 5.2 bars, and various liquid and gas velocities were tested for each given temperature and pressure. The results indicate that the trajectory and atomization change when the air and jet velocities are changed while keeping the momentum flux ratio constant. Therefore, it is beneficial to describe the trajectory based on air and jet Weber numbers or momentum flux ratio in combination with one of the Weber numbers. Also, examples are given where both Weber numbers are kept constant but the atomization is changed, and therefore, other terms beyond inertia terms are required to describe the spray behavior. It is also shown that the gas viscosity has to be considered when developing correlations. The correlations that include this term are generally better in predicting the trajectory. Therefore, Ohnesorge numbers in combination with the Weber numbers is used in the present correlations to describe the trajectories.
机译:提出了向亚音速横流喷射液体的实验研究。这项研究的目的是将射流轨迹与流量参数相关联,包括射流和空气速度,压力和温度以及一组无量纲变量。为此目的,开发了可以承受高温和高压的实验装置。使用基于激光的阴影照相系统捕获图像。总共测试了209种不同条件,并捕获并处理了72,000张图像。横流空气温度分别为25℃,200℃和300℃。横流空气的绝对压力分别为2.1、3.8和5.2巴,并且针对每个给定的温度和压力测试了各种液体和气体的速度。结果表明,在保持动量通量比不变的情况下,当空气和喷气速度改变时,轨迹和雾化也会改变。因此,有益的是基于空气和射流韦伯数或动量通量比结合韦伯数之一来描述轨迹。此外,给出了两个韦伯数均保持不变但雾化发生变化的示例,因此,需要使用惯性项以外的其他项来描述喷涂行为。还表明在建立相关性时必须考虑气体粘度。包含该术语的相关性通常可以更好地预测轨迹。因此,在本发明的相关中使用欧姆尼佐夫数与韦伯数的组合来描述轨迹。

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