气泡破裂及其诱发射流液滴释放过程的实验研究

本文基于实验方法,通过高速摄像的方法捕捉不同直径下的气泡破裂过程及射流液滴的释放过程,获得了气泡破裂后气泡空腔的演变过程,捕捉了射流液滴的速度,探究了气泡直径和气泡表面寿命对射流液滴释放过程的影响规律。实验结果表明,气泡表面寿命对气泡破裂产生射流液滴的过程有着重要影响。随气泡表面寿命的增加,破裂气泡产生的射流液滴的速度也随之增加。当气泡直径较小时,气泡表面寿命呈现Rayleigh分布的特征,射流液滴的释放概率也较高。随气泡直径的增加,气泡表面寿命逐渐转变为指数衰减分布的特征,射流液滴的释放概率也随之下降。基于现有实验数据给出了一个精度更高的射流液滴速度与气泡直径关系式。

CO_2激光诱导液滴射流等离子体的实验研究

为了研究激光诱导射流等离子体特性,了解激光诱导液滴等离子体的发展过程,基于脉冲激光-液滴同步作用系统,采用阴影法,观测了激光作用液滴的阴影图像,取得了液滴在CO_2脉冲激光作用下的演化过程数据。对图像进行处理获得了激光诱导液滴等离子体冲击波膨胀范围随时间的变化,并估算出了产生冲击波的激光能量。结果表明,空气冲击波的膨胀半径在当前观测时间范围内线性膨胀,约32%的激光能量用于产生冲击波。空气冲击波的变化规律对激光诱导液态燃料点火的研究提供了一定的参考依据。

液滴半径与其侧向散射光通量关系的实验

为开发基于侧向散射光通量的喷雾液滴直径全场测量方法,搭建了均匀液滴射流发生器和侧向散射光通量测试装置。基于微粒几何散射理论,利用均匀液滴射流发生器实验研究了液滴半径与其侧向散射光通量之间的关系。在不同的侧向散射角下,用数字相机测量了水和0#柴油的单粒径液滴射流在不同粒径下的侧向散射光通量,并分析了它们之间的关系。实验结果表明:液滴半径与其侧向散射光通量之间存在明显的二次函数关系,拟合的相关系数大于0.98;侧向散射角的大小以及液体的种类均不会改变两者之间的二次函数关系,仅影响该关系式系数的大小。结果为基于侧向散射光通量实现喷雾雾滴直径的全场测量提供了重要依据。

Experimental evaluation and modeling of liquid jet penetration to estimate droplet size in a three-phase riser reactor

In this work, the effects of injecting an evaporating liquid jet into solid-gas flow are experimentally investigated. A new model （SHED model） and a supplementary model （spray model） have also been proposed to investigate some flow-field characteristics in three-phase fluidized bed with the mean relative error 4.3% between model and measured results. Some experiments were conducted to study the influences of flow-field parameters such as liquid volumetric flow rate, injection velocity, jet angle and gas superficial velocity as well as solid mass flux on the jet penetration depth （JPD）. In addition, independent variables were experimentally employed to propose two empirical correlations for JPD by using multiple regression method and spray cone angle （SCA） by using dimensional analysis technique. The mean relative errors between the JPD and SCA correlations versus ex- perimental data were 7.5% and 3.9%, respectively. In addition, in order to identify the variable effect, a parametric study was carried out. Applying the proposed model can avoid direct use of expensive devices to measureJPD and to nredict dronlet size.

Experimental investigation on heat transfer enhancement of mist/air impingement jet

The heat transfer performance of a mist/air jet impingement on a constant-heat flux surface was experimentally investigated.Two objectives were outlined in the current study.The first objective is to assess the effects of mist/air volumetric flow rate ratio,impinging mode and heat flux on the heat transfer characteristics of free mist/air jet impingement.The second objective is to assess the effect of swirl flow induced by the spinning grinding wheel on the mist/air jet impingement,simulating the heat transfer process on a grinding work-piece surface subjected to the mist/air jet impingement.The results show that the addition of dilute water droplets to air flow results in significant heat transfer enhancement.Once the mist/air ratio is increased to a certain value,the increase of heat transfer with the mist/air ratio becomes slow.For a given mist/air ratio,as the increase of heat flux,the contribution of droplet evaporation to the overall heat transfer is weakened relatively,resulting in a decrease of heat transfer enhancement in comparison to the lower heat flux case.The heat transfer coefficient in the stagnation region for the oblique jet is much lower than the normal mist/air jet impingement,while in the region away from the stagnation,the local heat transfer coefficient for the oblique jet is higher than the normal jet.As regards as the mist/air jet impingement in the vicinity of grinding zone is concerned,when the jet impinging direction is consistent with the rotating direction of rotating disk,the swirl flow induced by the rotating disk could entrain more droplets to enter the jet impinging stagnation zone,which is beneficial to convective heat transfer enhancement.Furthermore,as the rotational speed of disk increases,the temperature deceases in impinging jet stagnation zone.