线性与非线性稳定性理论下液体射流空间发展的对比研究

分别基于线性和非线性稳定性理论,建立了描述同轴旋转可压缩气体中含空泡液体射流稳定性的一阶与二阶色散方程,并对色散方程进行验证分析;在此基础上,进行了射流表面一阶与二阶扰动及其发展的分析,线性与非线性稳定性理论下射流空间发展的对比研究.研究结果表明,二阶扰动波的波长和振幅明显小于一阶扰动波;沿射流方向,射流表面的扰动发展主要由一阶扰动波的发展所主导;随着轴向距离的增大,二阶扰动波才开始逐渐对扰动的发展起一定的作用.两种稳定性理论下射流表面的占优扰动模式不会发生改变;采用非线性稳定性理论时,可以反映一些实验中发现的射流表面出现"卫星液滴"的现象,由于考虑了射流表面的二阶扰动,射流界面振荡程度加剧.     

自由表面射流磁流体不稳定性分析(I)

利用微分解析方法分析了自由表面液态金属射流在非均匀的横向磁场中的稳定性行为，得出了在给定射流初始速度分布和磁场分布条件下，射流的速度空间分布表达式。在特定的条件下，射流存在固有稳定区，其稳定区长度与横向磁场的空间非均匀程度和射流的初始速度有关；但其向外溅射的位置与BT横向磁场的非均匀程度、射流的初始速度、液态金属粘滞系数和重力加速度有关。     

非均匀磁场中自由表面液态射流的MHD稳定性分析

基于在液态金属实验回路上的实验，对非均匀磁场中液态金属射流的MHD稳定性进行了研究，建立了一个描述射流性能的简化模型。由此简化模型所得的结果与从实验获得的结果相比较表明，它们相当吻合，并发现在此液态金属射流中存在一个固有稳定性区域。     

空心旋转液体射流初始阶段运动规律的研究

应用质量守恒定律和动量守恒定律,建立了描述空心旋转液体射流初始阶段运动的非线 性常微分方程组;该方程组可以用数值方法方便地求解。理论计算结果与实验拍摄到的射流照片吻 合很好。本结果表示射流受挑动失稳破碎成液滴前的最基本运动状态,是进一步从理论上研究空心 旋转射流破碎雾化机理的基础。     

大流量时多股射流静电雾化研究

为了使静电雾化在大流量时能够应用，本文研究了具有多股射流的某些喷咀。试验表明：多股射流中的每股射流仍然是圆锥体一射流模式，但是具有不稳定性。由此引起了ＰＤＡ（相位粒度分析仪）测量结果的畸变。同时试验还揭示，每股射流及其雾化依赖于喷咀不同部位的局部主要参数，使得均匀性受到影响。基于稳定性和均匀性之间很强的相互作用，本文提出了增加稳定性及改善均匀性的一些措施。     

粗糙表面对非定常冲击射流传热的影响

利用在射流驻点周围设置不同高度的圆环来模拟粗糙表面,进行非定常射流冲击换热的实验研究.非定常射流由一个特殊的质量流量控制装置产生,波形和频率可调.采用高度分别为1 mm,2 mm和3 mm的圆环,研究发现环高h=3 mm时,冲击射流流场发生了实质性的改变.对于流动形态没有发生实质改变的粗糙表面,在稳定射流冲击下,传热特性没有质的变化.然而,非定常射流冲击粗糙表面时,与其冲击光滑平板相比,传热特征有很大不同,传热强化系数总体上是削弱了,随着圆环高度的增加更为明显.     

旋转离心叶轮内部非定常流动实验研究

利用激光成像速度仪(PIV)测量了旋转离心叶轮内部的非定常流场,获得了旋转离心叶轮内部相对速度的非定常流场分布。详细分析了叶轮内部非定常流动现象和流动规律。通过实验研究发现旋转离心叶轮内部的流动是非定常,在叶轮出口处,叶片的吸力面与轮盖的夹角区存在一个低速区,并观察到了明显的射流/尾迹结构。射流区和尾流区的大小和范围在沿盘盖方向和跨叶片方向上是不同的。射流区和尾流区之间不存在明显的分界线。     

自由表面磁流体射流不稳定性分析(II)

用微分解析方法分析了自由表面磁流体射流在两个非均匀、相互垂直的横向磁场中的稳定性行为。获得了在给定射流初始速度分布和磁场分布条件下射流的速度空间分布表达式;分析了射流扭转及向外溅射的位置。     

自由表面磁流体射流不稳定性分析(Ⅱ)

用微分解析方法分析了自由表面磁流体射流在两个非均匀、相互垂直的横向磁场中的稳定性行为。获得了在给定射流初始速度分布和磁场分布条件下射流的速度空间分布表达式；分析了射流扭转及向外溅射的位置。     

旋转射流冲击换热液晶显示实验研究

采用热色液晶测温技术对以二氧化碳为工质的稳态射流冲击换热和管内插入扭转带方式的旋转射流冲击换热进行了实验研究。与普通射流相比,旋转射流导致驻点附近区域的换热趋于均匀化。其换热系数在大于某一半径之后高于普通射流,但在驻点附近相对较低。旋转射流对换热的此种影响随雷诺数的增大而减弱。     

液体横向射流在气膜作用下的破碎过程

为了研究液体横向射流在气膜作用下的破碎过程,采用背景光成像技术及VOF TO DPM方法进行了实验研究和仿真研究,模拟介质为水和空气.研究结果表明,液体射流在气膜作用下主要存在两种破碎过程:柱状破碎和表面破碎.Rayleigh-Taylor(R-T)不稳定性产生的表面波是液体射流发生柱状破碎的主要原因,气流穿透表面波的波谷导致射流柱破碎,破碎后的液丝沿流向逐渐发展呈带状分布.Kelvin-Helmholtz(K-H)不稳定性产生的表面波是液体射流发生表面破碎的主要原因,液丝和液滴从射流表面剥离.局部动量比对液体横向射流的破碎过程具有重要影响,当局部动量比较低时,液体射流的破碎由K-H不稳定性主导;随着局部动量比的增大液体射流的破碎逐渐由R-T不稳定性主导.液体射流的破碎长度及穿透深度均随局部动量比的增大而增大.     

影响空心旋转液体射流初始阶段运动的无量纲参数的分析

本文以描述空心旋转时流初始阶段运动规律的理论模型[1]为依据,重点讨论了影响射流运动的无量纲参数：韦伯数,液膜内外压力差,液膜初始内外环半径比,初始旋流度;初始径向速度等。从而进一步加深了对旋流喷嘴所产生的空心旋转射流初始阶段运动及发展规律的认识。     

Breakup and breakdown of bent kerosene jets in gas turbine conditions

Jet A-1 kerosene injection in air crossflow conditions has been studied for temperature up to 600 K and pressure up to 2 MPa. Thousand frames of jet shadowgraphs have been sampled for each of the 82 experimental conditions to determine statistical parameters characterizing the jet behavior. Among them the breakdown point, corresponding to the spatial position along the jet where the momentum jet looses its coherence, is the most relevant one. The axial coordinate of this point is strongly correlated with the liquid–gas momentum ratio while the breakdown position in gas stream direction mainly depends on the aerodynamic Weber number. This shows that the deformation of the liquid before and after its primary atomization is the most significant correction in respect to the ballistic, inviscid evolution of a bent cylindrical jet. The generalized profile equation, normalized to the breakdown coordinates, is invariant in respect of whatever external parameter and it predicts with high level of accuracy the measured profile upstream of the breakdown position.     

Three-dimensional electrohydrodynamic temporal instability of a moving dielectric liquid sheet emanated into a gas medium

A linear electrohydrodynamic instability analysis is presented for an inviscid dielectric liquid sheet emanated into an inviscid dielectric gas medium in the presence of a horizontal electric field. The influence of Weber number, gas-to-liquid density ratio, and the applied electric field on the evolution of two-, and three-dimensional disturbances of symmetrical and antisymmetrical types is studied. It is found, for antisymmetrical waves, that two-dimensional disturbances always prevail over three-dimensional disturbances, regardless of Weber number or gas-to-liquid density ratio values, especially for long waves; while for short waves, both two- and three-dimensional disturbances grow at approximately the same rate. It is also found, for symmetrical waves, that two-dimensional disturbances always dominate the instability process at low Weber number, and when the Weber number is large, symmetrical three-dimensional disturbances become more unstable than two-dimensional ones for long waves. The effect of increasing the gas-to-liquid density ratio is to promote the dominance of long three-dimensional symmetrical waves over their two-dimensional counterpart. Finally, the equilibrium Weber number at which the growth rates of two- and three-dimensional modes are equal is discussed for both symmetrical- and antisymmetrical-disturbances cases.-1     

空心旋转液体射流初始阶段特性的实验研究

以空心旋转射流的理论模型为基础［１］,通过实验对旋流喷嘴射流特性做进一步深入的研究,特别是实际射流形状的变化规律及喷嘴初始参数的变化规律．结果表明,旋流喷嘴的初始参数和空心射流内外表面压力差是决定射流形状的主要因素。     

Dispensing picoliter droplets on substrates using dielectrophoresis

Liquid dielectrophoresis is exploited to initiate rapid, transient flow of aqueous liquids along co-planar electrodes patterned on insulating substrates. The flow induced by the non-uniform electric field leads to a new electrostatic equilibrium. A reduced-order model predicts the transient motion of the rivulet. When the field is removed, capillary instability breaks up the rivulet into regularly spaced droplets. Periodic circular bumps patterned on the structure, when spaced according to the most unstable wavelength based on Rayleigh's inviscid theory for the cylindrical liquid jet, lead to uniformly spaced and sized droplets. A correction factor, based on the dimensionless Ohnesorge number, accounts successfully for the effect of viscosity.     

Cavitating vortex generation by a submerged jet

The surface geometry of a cavitating vortex is determined in the limit of inviscid incompressible flow. The limit surface is an ovaloid of revolution with an axis ratio of 5: 3. It is shown that a cavitating vortex ring cannot develop if the cavitation number is lower than a certain critical value. Experiments conducted at various liquid pressures and several jet exit velocities confirm the existence of a critical cavitation number close to 3. At cavitation numbers higher than the critical one, the cavitating vortex ring does not develop. At substantially lower cavitation numbers (k ? 0.1), an elongated asymmetric cavitation bubble is generated, with an axial reentrant jet whose length can exceed the initial jet length by several times. This flow structure is called an asymmetric cavitating vortex, even though steady motion of this structure has not been observed.