首页> 外文会议>AIAA SciTech forum;AIAA Aerospace Sciences Meeting >Spray Droplet Impingement onto a Smooth Flat Surface
【24h】

Spray Droplet Impingement onto a Smooth Flat Surface

机译:雾滴撞击在光滑的平面上

获取原文

摘要

A series of experimental measurements are presented of the liquid film thickness for a dense water spray impacting onto an unheated, smooth, flat impact surface. These data have been acquired using a non-contacting confocal chromatic optical thickness probe originally developed to measure the central thicknesses of precision optics. The measured average liquid film thickness is approximately 160 μm. This local residual liquid layer thickness increases slightly versus radial location at each spray flow rate, and also decreases slightly as the spray flow rate is increased. Also, backlit high-speed video imaging through the glass impact plate from below is used to observe the time variation of the diameter of individual spray droplet impact cavities. The spray droplet impact cavity diameter results indicate a time variation that is proportional to (t)~(0.2) during the cavity growth phase, rather than the (t)~(0.5) behavior that is commonly observed for isolated single drop impacts into a static liquid film. Generally, the details of the cavity retraction phase could not be observed in the current experiments. Measured maximum cavity diameters ranged from around 0.4 mm to 1.6 mm. It is estimated that the corresponding impinging droplets had diameters of between 80 μm and 320 μm. This range of estimated droplet diameters is consistent with a series of Phase Doppler Particle Analyzer measurements that were made for the same spray nozzle and flow conditions. These results are found to be consistent with the predictions from simple time scale estimates of the cavity formation time and cavity lifetime. Based on these observations and the time scale analysis, it is reasoned that transient conduction to the sub-cavity liquid film beneath spray droplet impact cavities enhances the overall spray cooling heat transfer, but resulting dry out of these cavities could then contribute to onset of critical heat flux.
机译:给出了一系列实验测量结果,显示了浓水喷雾撞击到未加热,光滑,平坦的撞击表面上的液膜厚度。这些数据是使用非接触共焦彩色光学测厚仪获取的,该探头最初是为测量精密光学器件的中心厚度而开发的。测得的平均液膜厚度为约160μm。在每个喷雾流速下,该局部残余液体层的厚度相对于径向位置略有增加,并且随着喷雾流速的增加也略有减小。同样,从下方通过玻璃冲击板的背光高速视频成像用于观察各个液滴冲击腔直径的时间变化。液滴冲击腔直径的结果表明,在腔体生长阶段,时间变化与(t)〜(0.2)成正比,而不是通常的单个液滴冲击进入管腔时通常观察到的(t)〜(0.5)行为。静态液膜。通常,在当前实验中无法观察到腔缩回阶段的细节。测得的最大腔体直径范围约为0.4毫米至1.6毫米。据估计,相应的撞击液滴的直径在80μm和320μm之间。估计的液滴直径范围与在相同的喷嘴和流量条件下进行的一系列相多普勒颗粒分析仪测量结果一致。发现这些结果与根据简单的时标估计腔形成时间和腔寿命的预测是一致的。基于这些观察和时间尺度分析,可以认为,瞬态传导至喷雾冲击腔下方的子腔液膜会增强整体喷雾冷却传热,但导致这些腔变干可能会导致临界点的出现。热通量。

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