流动氩气放电系统中条纹斑图形成的实验研究

采用双水电极介质阻挡放电装置, 在大气压下流动氩气中产生了稳定的条纹斑图, 并采用拍照和电学方法对其产生机理进行了研究. 研究发现, 条纹斑图仅出现在外加电压较低的情况下, 在较高电压下放电会过渡到均匀模式. 低电压下的条纹斑图是由于放电丝沿着气流方向定向移动形成的, 该定向移动速度几乎与电压无关, 主要由气体流量决定. 分析发现放电空间中活性粒子的记忆效应对条纹斑图的形成起决定作用. 电学测量发现放电电流和放电的气隙起始电压都随着气流的增加而减小, 本文对这一现象进行了定性解释. 本文结果对斑图动力学研究和介质阻挡放电的工业应用都具有很重要的意义.     

离心泵叶轮内气液两相三维流动数值研究

本文采用欧拉模型对离心泵叶轮内气液两相泡状流动进行了数值模拟。分析了叶轮内压力、速度等的分布规律,发现在靠近轮盖侧吸力面入口附近压力较低,气液两相速度较大,气泡容易凝聚而导致含气率较高;靠近轮盘处含气率较低。分析了不同进口截面含气率对叶轮内部两相流动的影响机理,建立了进口截面含气率对内部相态分离及泵外特性的影响关系。     

多间隙轨道式气体开关自击穿特性

介绍了一种多间隙轨道式气体开关的结构及其自击穿实验研究结果。通过对开关放电的理论分析,并结合实验数据,获得一个适合该开关自击穿工作特性的表达式。研究结果发现, 在高气压条件下,开关静态特性曲线与空气击穿的经验式曲线存在较大的差别,并且击穿电压随气压增加并不完全呈线性变化。经过对实验条件和数据的分析,认为在高气压、高电压条件下,电极表面形成的电晕可能是导致该开关静态特性曲线出现此现象的原因。由于开关的特殊结构,电极电晕不仅未起到均压的作用,反而减小了电极之间有效的绝缘距离,从而导致开关自击穿电压实验值与经验理论值的偏离。     

锥形纳米孔内的电压整流及流体流动

文章以生物纳米通道及纳米孔中的离子传输及化学反应为背景,以离子流整流、电渗流整流、离子积累耗散模型为理论基础,使用有限元数值计算方法研究压力及电场交互作用下的锥形纳米孔孔内离子浓度分布及速度场分布现象.分析了不同电压下压力和电场的交互作用对锥形纳米孔中速度场、流场及浓度分布的影响.结果表明纳米孔孔内氢离子运动方向主要受电场方向影响.由于静电吸附效应,沿着孔壁流动的电渗流中的氢离子浓度会高于体溶液中的氢离子浓度.当电压较小时,流场方向主要受压力流的影响,当电压较大时,流场流动方向由电渗流带动的流体流动和压力驱动的流体流动共同决定.      

大气压氩气射流等离子体的光谱特性研究

等离子体喷枪是一种重要的等离子体源,已成为近几年低温等离子体研究的一个重要课题。本文利用钨针-钨丝网电极制作了直流喷枪装置,在大气压空气中产生了稳定的等离子体羽,并采用发射光谱的方法,对等离子体羽的等离子体参数进行了研究。在钨针电极与钨丝网电极之间放出耀眼的白光,钨丝网电极出口的气流下游有火苗形状的等离子体羽喷出。在电压保持不变的条件下(13.5 kV),等离子体羽长度随气体流量增加而增大;在气体流量保持不变的条件下(10 L·min-1),羽长度随外加电压的增大而增大。在气体流量一定的条件下,放电电压和放电电流呈反比例关系,即电压随着电流的增大而减小,说明放电属于辉光放电。采集了该喷枪在300～800 nm范围内的放电发射光谱,通过玻尔兹曼方法对放电等离子体电子激发温度进行了测量。结果表明,电子的激发温度随外加电压的增大而降低,随着工作气体流量的减小而升高。利用放电的基本理论对上述现象做了解释。这些研究结果对大气压均匀放电等离子体源的研制和工业应用具有重要意义。     

Measurement of pressure distribution from PIV experiments

In this study, a non-staggered grid SIMPLER pressure solution algorithm, which is able to produce correct pressure distribution directly if correct velocities are given, is proposed to solve the pressure distribution for PIV experiments. The cell face pseudo velocity required in the pressure equation is approximated by a simple linear average of the adjacent nodal pseudo velocities so that the velocity and pressure are collocated without causing the checkerboard pressure distribution problem. In addition, the proposed pressure solution algorithm has the features that upwind effects of the convective terms are considered, boundary conditions are not required, and the pressure distribution obtained can be used to correct the velocity field so that the continuity equation is satisfied. These features make the present algorithm a superior method to calculate the pressure distribution for PIV experiments. The pressure field solved is realistic and accurate. The proposed pressure equation solver is first calibrated with a two-dimensional cavity flow. It is found that the results are almost identical to the exact solution of the test flow. The algorithm is then applied to analyze a uniform flow past two side-by-side circular cylinders in a soap film channel. With the velocity and pressure distributions successfully measured, the structures of the complex shedding flow patterns are clearly manifested.     

小功率等离子体射流的流特性

采用焓探针对小功率(5kW)热喷涂等离子体射流的焓、温度和速度进行了测量和计算。研究了气体成分、流量、电弧电压和电流对等离子流体的焓、温度和速度分布的影响。结果表明,对于单一氩气等离子体,当使用新喷嘴时,增大氩气流量能够使喷嘴内部电弧弧根向出口方向移动,从而增加等离子体射流的焓、温度和速度。对于Ar-N2等离子体,增加气体中氮气的含量,会提高等离子电弧电压,在同样的输入功率下,改变等离子电流和电压对等离子体的焓、温度和速度影响较小。对于Ar-N2等离子体,增加氢气含量会明显地提高等离子射流的速度和热传递。     

“绿色”液体激光介质的热流场特性研究

选取掺钕四氟化钆钠(Nd3+: NaGdF4)纳米晶分散到二甲基亚砜作为绿色液体介质,构建单侧抽运和液体横流系统,使用ANSYS软件对液体介质稳定热流场分布进行模拟分析。结果表明：当流道形状、流动状态、壁面相同时,液体流场分布基本相同,泵浦光的频率对流场分布影响很小;液体介质入口的流速会影响流线分布,流速越快,流线越密;泵浦区域中,介质沿着液体流动方向温度逐渐升高;在液体流向变化小的区域,可获得较为均匀的温度分布。     

“绿色”液体激光介质的热流场特性研究

选取掺钕四氟化钆钠(Nd3+:NaGdF4)纳米晶分散到二甲基亚砜作为"绿色"液体介质,构建单侧抽运和液体横流系统,使用ANSYS软件对液体介质稳定热流场分布进行模拟分析。结果表明:当流道形状、流动状态、壁面相同时,液体流场分布基本相同,泵浦光的频率对流场分布影响很小;液体介质入口的流速会影响流线分布,流速越快,流线越密;泵浦区域中,介质沿着液体流动方向温度逐渐升高;在液体流向变化小的区域,可获得较为均匀的温度分布。     

Study on high voltage generation using flame column and DC power supply

A theory for generating an ultra-high voltage using a flame column (weakly ionized plasma) and a normal high-voltage (HV) power supply is presented. A high-voltage generator adapted based on this theory was fabricated, and experiments on high voltage generation were carried out. As a result, high voltages were observed between an electron cloud in front of the flame column and the positive electrode in the experiment, and highly positive charges were stored efficiently on the large positive electrode. The experimental results proved that the output voltage is three times higher than that of the output voltage of the HV power supply whenever the gas flow velocity is close to 0. A maximum output voltage was obtained for the output voltage of the HV power supply, which was 15 times higher than the output voltage of the HV power supply. The generated voltage and the output current for the output voltage of the HV power supply were investigated, and the temporal dependence of the charging current was also measured. The use of this method made it possible to obtain a high voltage and high electric field in a large space. Furthermore, the realistic possibility of achieving a 10-MV using this method was shown.     

Effect of micropillar electrode spacing on the performance of electrohydrodynamic micropumps

Electrohydrodynamic (EHD) micropumps with three-dimensional 50 μm × 50 μm micropillar electrodes were fabricated and tested in this study. Two basic electrode configurations were investigated: (i) micropillar emitter and collector electrodes (symmetric) and (ii) micropillar emitter and planar collector electrodes (asymmetric). The micropumps were fabricated by integrating chromium/gold planar electrodes with electroplated 3-D Nickel micropillars on a glass substrate with a 100 μm high PDMS microchannel. The effect of the spanwise micropillar spacing on the pump performance was determined. The pumps were tested using HFE-7100 as the working fluid for the maximum pressure generation under a no flow condition. The micropumps with the asymmetric electrode design generated a significantly higher pressure head than the corresponding micropumps with symmetric electrode configuration for the same applied voltage, with lower power consumption. A decrease in the spanwise spacing of the micropillar electrodes increased the pump performance for the symmetric configuration, while the performance decreased for the asymmetric configuration.     

高压氦气平行极板击穿电压实验研究

为获得高温气冷堆核电站电气设备绝缘设计所需基础数据, 本文设计了一套测量高压氦气绝缘性能的装置. 利用该装置进行了15-20 ℃, 0.1-7 MPa氦气, 间距0.25, 0.35, 0.5 mm平行极板击穿实验. 实验表明: 氦气的绝缘性能远低于空气; 气压越高, 氦气的击穿电压越大, 3.0 MPa氦气的击穿电压与常压空气基本一致; 根据低气压实验数据和巴申定律推导的公式, 在高气压下计算值偏大, 且偏差随着气压和间距乘积的增大不断增大; 提出了可计算0.1-7 MPa氦气击穿电压的简易公式, 同时修正了高气压氦气的巴申公式, 并进行了理论分析.     

高比转速离心压气机叶轮的设计及其三维流场分析

利用三维数值模拟计算(CFD)技术进行了100 kW微型燃气轮机的高比转速离心压气机叶轮的设计与内部流动的数值模拟与分析,得到了相应的特性曲线与主要气动参数分布。根据数值模拟分析,设计的100 kW微型燃气轮机高比转速离心压气机叶轮具有较高的效率和较宽广且平坦的工作特性,可以满足微燃机总体设计对压气机的要求。流道内存在复杂的跨音速流动现象。在下一步工作中,有必要优化设计叶轮几何型线,提高压气机效率。     

高频高效率混合型潘尼管的理论分析

对混合型潘尼管作了等离子体动力学分析和非线性粒子模拟。动力学的分析结果指出，混合型潘尼管是基于潘尼管工作机理的一种混合器件。非线性模拟验证了这一结论，并指出混合型潘尼管具有二个优点:高效率和高频率。     

电子束在气体中传输的最佳压强研究

推导得到了有外加磁场情况下强流相对论电子束在中性气体中产生的等离子体参数、等离子体电流和束产生电场的理论公式,通过编程计算得知最佳气体压强值随电子束峰值电流的增大而增大,电子束脉冲前沿上升越快最佳气体压强值就越高,当电子束的峰值电流为500kA、峰值电压为1.0MV、电流脉冲前沿上升时间为60ns时,氮气的最佳压强为332Pa,即当气压为332Pa时净电流和平均电场强度近似最低,有效传输的气压范围约为199~532Pa。实验结果与理论计算符合很好。     

随机填充增殖剂球床内载气流动特性数值模拟

固态氚增殖包层是聚变堆及聚变-裂变混合堆产氚包层的重要候选结构之一,其球床通道内载气流动特性将影响氚提取效率。利用离散元方法(DEM)生成随机填充增殖剂球床,通过径向孔隙率分布验证其合理性,计算流体力学(CFD)模拟计算其通道内气体流场特征。模拟得到:球床内吹扫氦气流速随孔隙率波动并随入口流速增大而均匀增大,通道内氦气流向及流速变化显著,Blake-Kozeny方程可良好预测该随机填充球床通道压降。     

随机填充增殖剂球床内载气流动特性数值模拟

固态氚增殖包层是聚变堆及聚变-裂变混合堆产氚包层的重要候选结构之一,其球床通道内载气流动特性将影响氚提取效率。利用离散元方法（DEM）生成随机填充增殖剂球床,通过径向孔隙率分布验证其合理性,计算流体力学（CFD）模拟计算其通道内气体流场特征。模拟得到：球床内吹扫氦气流速随孔隙率波动并随入口流速增大而均匀增大,通道内氦气流向及流速变化显著,Blake-Kozeny方程可良好预测该随机填充球床通道压降。     

Effect of staggered array structure on the flow field of micro gas chromatographic column

A new design of staggered array semi-packed micro gas chromatographic column was presented based on the micro electromechanical system(MEMS)technology.It was a sensor for gas sample analysis.The internal velocity fields of ten types of semi-packed micro gas chromatographic column were studied.The effects of array spacing and dislocation spacing on the flow field distribution were investigated.The results show that on the basis of ensuring the formation of virtual wall,with the increase of array spacing,the maximum velocity difference between the flow channels in the vertical direction decreases gradually,but the velocity difference in the flow channels a and b increases.When the inlet velocity was set to be 0.18 m/s,the maximum velocity difference in the channel of the staggered semi-packed micro gas chromatography column 3(CSAC3)was 0.05610 m/s.The maximum velocity difference in the channel a was 0.09160 m/s.The maximum velocity difference in the channel b was 0.02401 m/s.CSAC3 had a more uniform velocity field distribution,which can effectively suppress the laminar flow effect during chromatographic separation,and had a smaller pressure distribution,which puts forward lower requirements for carrier gas system.The staggered array semi-packed micro gas chromatography column proposed in this paper can effectively improve the velocity field distribution and pressure distribution in the channel,and provide a theoretical basis for the design of the new micro gas chromatography column structure.     

Momentengleichungen für Plasmen mit anisotropem Neutralgasdruck und anisotropem Ionendruck

Strongly non-Maxwellian and non-isotropic velocity distributions of the neutral atoms and of the ions occur in collisionless plasmas at high degrees of ionization, especially in gas discharges at low pressures and high current densities and in high temperature plasmas. The velocity distributions and the related velocity moments for the neutral gas and the ion gas are calculated. The influence of the magnetic fields on the ions is neglected. Especially, the pressure tensors and the heat flow tensors are investigated. The differential equations are given for the velocity moments of the velocity distribution. Additional terms occur in the equation of motion, if the pressure is non-isotropic and non-Cartesian coordinates are used. A heat flow tensor is evaluated that closes the system of differential equations for the neutral gas consistently and allows to rederive typical formulas of the molecular neutral gas flow. The heat flow tensor essentially determines the type of the differential equation system for the velocity moments. It is shown, that the neutral gas temperature is not constant across the plasma. Different statements deal with the heat flow tensor in the ion gas. In particular, non-vanishing ion temperature on the axis and a system of differential equations for the positive column under free-fall conditions are investigated. The inertia terms for the ion gas and the neutral gas must be taken into account in the pressure balance of the plasma.     

Subsonic non-steady-state gas flows in channels with inner cavities

A set of gasdynamic equations is given in the general form for matter with an arbitrary equation of state in the case when the entropy equation is used instead of the energy equation. In the ideal gas approximation in view of viscosity, a numerical investigation is performed of non-steady-state two-dimensional flows in a channel with a cavity. The calculation results have demonstrated that, given the flow velocity and the geometry of channel and cavity, pressure pulsations arise that are due to the departure of vortices from the cavity into the main flow. The values of the amplitude and frequency of pressure pulsations are determined. If measures are taken aimed at limiting the departure of vortices from the cavity, for example, a baffle is installed to restrict the interaction between the main flow and gas in the cavity, one can considerably increase the flow velocity in the channel, unaffected by the cavity. Such non-steady-state flows may be realized in MHD-generator channels, resonators of gas flow lasers, gas ducts for ventilation and gas transport systems, mufflers, whistles, etc.