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

机译:高温和压力气体交叉流动液射流的轨迹

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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:介绍了液喷射进入亚源射流的实验研究。本研究的目的是将喷射轨迹联系起来流动参数,包括喷射和空气速度,压力和温度,以及一组非潜能变量。为此目的,开发了一种实验装置,可以承受高温和压力。使用基于激光的太阳影像系统捕获图像。测试了209个不同的不同条件,捕获并处理了超过72,000张图像。十字流空气温度为25℃,200℃,300℃;绝对的十字流空气压力为2.1,3.8和5.2巴,对每个给定的温度和压力进行各种液体和气体速度。结果表明,当在保持动量磁通比恒定的同时改变空气和射流速度时,轨迹和雾化发生变化。因此,基于空气和喷射韦伯数或动量通量比与韦伯号组合的术语来描述轨迹是有益的。而且,给出了拍摄的次数保持恒定的示例,但是雾化被改变,因此,需要超出惯性术语的其他术语来描述喷射行为。还示出了在显影相关时必须考虑气体粘度。包括该术语的相关性通常更好地预测轨迹。因此,奥恩尼尔尤其与韦伯号组合的数字用于本相关性以描述轨迹。

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