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1.
用Matlab软件对大气压均匀辉光放电等离子体(OAUGDP)激励器系统的电特性进行了仿真。在仿真模型中,等离子体放电被建模成一个电压控制的电流源:当加在气隙上的电压超过等离子体产生电压时,该受控电流源接通;电流源的输出电流和所加电压之间遵循幂律。建立了一个OAUGDP激励器系统中等离子体放电的电路模型。仿真结果与实际激励器系统的实验数据很吻合。仿真结果表明,在不同的运行条件下,放电电流与电压之间遵循不同的指数幂律,仿真放电电流波形也不同。  相似文献   

2.
袁野  张岩  赵青  黄小平  郭成 《强激光与粒子束》2022,34(6):065003-1-065003-9
为了在高超声速飞行器减阻中达到更好的减阻效果,设计了一种电弧射流等离子体激励器。采用有限元法求解非线性多物理方程,对此电弧射流等离子体激励器的工作特性进行了数值模拟,得到了激励器内部的电势、压力、温度和速度分布,综合分析了进气口气体速度、放电电流、激励器管道半径对电势、压力、温度和速度分布的影响。获得了全面的影响规律,通过仿真结果还得到:电弧射流等离子体激励器可产生最高温度为8638 K、最高速度为655 m/s的等离子体射流。当电流20 A,进气速度0.5 m/s,管道半径2.5 mm时,所需功率最小;当电流20 A,入口气体流速5 m/s,管道半径2.5 mm时,出口处平均温度最高;当电流20 A,进口气体速度10 m/s,管道半径2.5 mm时,出口处平均速度最大。并对仿真得到的放电电压进行了实验验证,在等离子体参数相似的情况下,实验结果与仿真结果吻合较好。  相似文献   

3.
王磊  章程  罗振兵  王林  严萍  邵涛 《强激光与粒子束》2016,28(4):045013-145
为了产生高能等离子体合成射流,设计了一台面向等离子体合成射流应用的微秒脉冲源,输出电压为10 kV,重复频率为100 Hz,可承受高达250 A的放电电流。详细介绍了微秒脉冲源的工作原理,比较了不同放电电容对脉冲变压器原边电流及输出电压的影响。进一步将所设计的微秒脉冲源成功应用于等离子体合成射流实验中,研究了不同间距对等离子体合成射流的影响,比较了有无放电电容条件下的能量消耗率。实验结果表明:不同放电电容在相同激励器间距的条件下,击穿电压基本相同;击穿电压随激励器间距增大而增大。有放电电容能产生较大的放电电流,且电流值随电容值的增大而增大。有放电电容条件下的能量消耗率比无放电电容要高,易于产生高能的等离子体合成射流。  相似文献   

4.
两电极等离子体合成射流激励器工作特性研究   总被引:4,自引:0,他引:4       下载免费PDF全文
王林  夏智勋  罗振兵  周岩  张宇 《物理学报》2014,63(19):194702-194702
采用放电测量和高速阴影技术对两电极等离子体合成射流激励器工作特性进行了系统实验研究.实验表明:激励器工作击穿电压和放电峰值电流随激励器所处环境压强的降低和放电频率的增大而减小,激励器腔体内的放电过程为火花电弧放电.典型的等离子体合成射流流场包含有一道前驱激波和一股呈蘑菇状的高速射流.在整个射流发展过程中,前驱激波以当地声速恒速传播,不随激励器条件的改变而变化,波的强度则随着激励器出口直径的减小、腔体体积的增大、环境压强的降低和放电频率的升高而减小.激励器腔体体积和放电频率的增加会降低腔内气体的加热效果,并减小射流速度.激励器出口直径和环境压强对射流速度的影响按规律变化且存在最佳值.本文实各验条件下激励器都产生了明显的前驱激波和高速射流,具有实现高速流场主动流动控制的应用潜能.  相似文献   

5.
等离子体流动控制激励器由于其响应速度快、激励频带宽、能量损耗低、可靠性强的优势,在航空航天领域的主动流动控制等方面得到了广泛应用.文章提出了一种新型的等离子体气动激励器——三电极共面介质阻挡放电激励器,研究了该激励器电极结构对放电特性和诱导气流速度的影响,并与传统共面介质阻挡放电和沿面介质阻挡放电激励器进行了比较.结果表明:(1)随着激励电压的提高,高压电极和地电极之间先出现了丝状放电并逐渐延伸到第三电极;(2)随着第三电极与高压电极之间的距离增大,诱导气流速率从2.4 m/s下降到0 m/s,而第三电极宽度的变动对诱导气流速度影响可忽略不计;(3)相同外部条件下,该激励器诱导的气流速度小于沿面介质阻挡放电激励器,但高于共面介质阻挡放电激励器.   相似文献   

6.
 等离子体激励器电极组相位不同便产生多相等离子体气动激励,建立了粒子图像测速仪流场参数测试系统,利用粒子图像测速仪技术,研究了非对称布局等离子体气动激励诱导空气流动特性,分析了多相等离子体气动激励对诱导空气流动速度的影响。结果表明:粒子图像测速仪流场测试系统能够准确地反映等离子体气动激励诱导空气流动的流场空间结构,等离子体气动激励诱导空气流动是平行于激励器的近壁面射流,多相等离子体气动激励能够增大等离子体气动激励诱导气流速度,或者使等离子体气动激励影响流场区域增大。粒子图像测速仪系统是深入研究等离子体气动激励的流场结构最佳的方式之一。  相似文献   

7.
为了增强等离子体激励器的扰动能力、提升等离子体气动激励的控制效果,采用高压探针、烟流显示和PIV流场测试等多种研究手段,开展了磁场加速等离子体激励器特性研究,获得了激励器不同时刻的放电图像,分析了磁场强度对激励器电学特性与诱导流场特性的影响规律.结果表明,(1)放电等离子体的定向运动速度与磁场强度成正比,磁加速等离子体的最大移动速度达到了6 m/s;(2)通过对不同剖面的诱导流场进行研究发现,磁场加速等离子体激励器能够在近壁区产生一系列涡结构.此外,该诱导流场具有显著的三维特征与非定常特性.研究结果为开展基于磁加速等离子体气动激励的流动控制奠定了基础.   相似文献   

8.
沈苑  王瑞雪  章程  方志  邵涛 《强激光与粒子束》2016,28(5):055001-112
研究了不同电极结构以及放电参数对微秒脉冲激励的氦等离子体射流放电特性的影响。实验中采用不同管内径、不同电极形状、不同重复频率等参数,通过采集放电阶段的电流电压图、发光图像以及发射光谱等,对等离子体射流的电学特性和光学特性进行诊断。实验结果表明,随着管内直径的增大,氦等离子体射流的长度减小;管内径为8mm时,等离子体射流的击穿电压与放电电流最小,同时,其发射光谱中第二正带系N2,N+2和O等高能活性粒子的强度最高;管内径为5mm的等离子体射流的放电电流、功率及消耗的能量最大;在相同实验条件下,针尖电极结构中的放电电流、消耗的功率还有发射光谱强度都较大;随着重复频率的增加,氦等离子体射流的长度会增加,但击穿电压减小。  相似文献   

9.
氩气/空气等离子体助燃激励器的实验研究   总被引:3,自引:0,他引:3  
为了获得氩气/空气等离子体助燃激励器的特性,首先在空气中加入少量氩气的条件下,对条状、王状和网状三种不同电极形状的等离子体助燃激励器的放电特性进行对比,实验结果表明电极形状对激励器放电特性影响不大。然后对条形电极在纯空气和10%氩气/90%空气两种条件下的放电特性和发射光谱进行研究,发现加入氩气后,放电参数变化趋势与纯空气相似,但电流脉冲增多,放电均匀度增加,起始放电电压由27kV降低到24kV,并且介质阻挡放电发射光谱增强。  相似文献   

10.
本文通过2D PIV及其CCD相机获取锯齿电极等离子体激励器在静态环境下诱导的流场结构以及放电图像。CCD相机拍摄的放电图像显示该激励器在锯齿中间存在一暗带区域,而不同截面的流场结果则验证了该型激励器能够诱导出带涡对三维射流结构,涡对贴近壁面向下游发展,并在激励器壁面上方诱导出下洗流。文中结合各拍摄截面的流场结构以及放电结构,分析了该型激励器诱导的流场结构特性,涡对发展规律和形成原因,以及锯齿电极激励器的放电特性,最后提出了其流场诱导机理模型。  相似文献   

11.
The influence of the electric signal shape applied to a surface dielectric barrier discharge (DBD) actuator is investigated in order to optimise the produced electric wind. This report also gives insights on the mechanisms involved in the electro-fluido-dynamic (EFD) operated by actuators based on atmospheric non-thermal discharges in air. The parameters of the electric signal that maximises the produced electric wind in quiescent air are investigated with a positive and negative sawtooth waveforms. The induced airflow properties are observed with a particle image velocimetry (PIV) set-up. The positive sawtooth waveform results in a more filamentary discharge and generates an electric wind with maximum velocities close to the active air exposed electrode. This contrasts with the negative sawtooth waveform that does not create as many filaments and induces electric wind velocities more homogeneously distributed along the dielectric surface. Even though the velocities values are of the same order, the shape of the vortex generated above the air exposed electrode is very dependant on the waveform.  相似文献   

12.
In this paper, a computational model was developed to model the potential of plasma actuators to reduce flow-induced noise. The model consisted of a viscous flow solver to compute the flow field and a Ffowcs Williams and Hawkings acoustic solver to predict the far-field noise radiation. A velocity-inlet boundary condition was used to model the induced velocity effect of plasma actuators applied to the surface of a bluff body. A test case of the noise radiation from a cylinder in fluid flow was used to validate the model. A comparison between the numerical results and previous experimental results was made. The results confirmed the noise-reduction potential of plasma actuators for bluff-body noise control. Good agreement was made between the numerical and experimental results. It was concluded that the model could be a useful tool to predict the effect of plasma actuation applied to aerodynamic, acoustic, and optimization problems.   相似文献   

13.
Plasma flow control is a new type of active flow control approach based on plasma pneumatic actuation.Dielectric barrier discharge(DBD) actuators have become a focus of international aerodynamic research.However,the practical applications of typical DBDs are largely restricted due to their limited discharge area and low relative-induced velocity.The further improvement of performance will be beneficial for engineering applications.In this paper,high-speed schlieren and high-speed particle image velocimetry(PIV) are employed to study the flow field induced by three kinds of plasma actuations in a static atmosphere,and the differences in induced flow field structure among typical DBD,extended DBD(EX-DBD),and tri-electrode sliding discharge(TED) are compared.The analyzing of the dynamic evolution of the maximum horizontal velocity over time,the velocity profile at a fixed horizontal position,and the momentum and body force in a control volume reveals that the induced velocity peak value and profile velocity height of EX-DBD are higher than those of the other two types of actuation,suggesting that EX-DBD actuation has the strongest temporal aerodynamic effect among the three types of actuations.The TED actuation not only can enlarge the plasma extension but also has the longest duration in the entire pulsed period and the greatest influence on the height and width of the airflow near the wall surface.Thus,the TED actuation has the ability to continuously influencing a larger three-dimensional space above the surface of the nlasma actuator.  相似文献   

14.
This paper reports the material characterization and performance evaluation of an AlN ceramic based dielectric barrier discharge(DBD) plasma actuator. A conventional Al_2O_3 ceramic is also investigated as a control. The plasma images,thermal characteristics and electrical properties of the two actuators are compared and studied. Then, with the same electrical operating parameters(12-kV applied voltage and 11-kHz power frequency), variations of the surface morphologies,consumed power and induced velocities are recorded and analyzed. The experimental results show that the AlN actuator can produce a more uniform discharge while the discharge of the Al_2O_3 actuator is easier to become filamentary. The later condition leads to higher power consumption and earlier failure due to electrode oxidation. In the plasma process,the power increment of the AlN actuator is higher than that of the Al_2O_3 actuator. The induced velocity is also influenced by this process. Prior to aging, the maximum induced velocity of the AlN actuator is 4.2 m/s, which is about 40% higher than that of the Al_2O_3 actuator. After 120-min plasma aging, the maximum velocity of the aged AlN actuator decreases by 27.8% while the Al_2O_3 actuator registers a decrease of 25%.  相似文献   

15.
In recent years, there has been an increase in the number of research papers on plasma and its use in active flow control applications. The main objective of this study is to assess the plasma actuator's position on a NACA0015 airfoil in terms of aerodynamic forces. In addition, optimization of the plasma actuator's position and its configuration are studied in order to identify the optimum configuration for improvement in lift coefficient. The experiments are conducted in an open-suction-type wind tunnel at Reynolds numbers of 48,000, 75,000, and 100,000. The plasma actuators are mounted on various positions (x/C) starting from the leading edge to trailing edge of the airfoil. The experimental results on aerodynamic force measurement are presented to illustrate the increasing lift effect of the generated plasma. It is also shown that the plasma actuators used as an active flow control device appears to shift the stall angle of the airfoil. The results of the experimental study suggest that the energy efficiency of airborne systems can be improved with the use of plasma actuators due to its increasing lift coefficient effect. This result becomes a vital finding considering that the same flight can be achieved with less fuel and less amount of environmental pollution for the same distance of journey. It is also worth mentioning that increasing lift effect would mean taking off from a shorter runway or allowing the airborne vehicle with the ability to fly with additional payload.  相似文献   

16.
在绝缘材料两侧交错布置电极的方式是航空领域所使用的等离子体激励器与众不同之处,因此航空等离子体激励器生成的等离子体具有沿弦向变化特点.利用光谱仪、红外热像仪、激光诱导荧光系统(LIF)对交错电极介质阻挡放电等离子体弦向特性进行了实验研究,并对介质阻挡放电等离子体流动控制机理作了初步的探讨.实验中发现等离子体发光强度和温度沿弦向的分布基本符合高斯分布;发射等离子体光谱强度随着电压升高而增大;等离子体弦向温度随激励电压的增大而增加;通过LIF系统直接检测到放电产生的NO.通过数值模拟得到电极附近的电势和电场强度分布进而对实验现象作了初步的解释,并在以上实验的基础上,将等离子体流动控制机理归纳为撞击效应、温升效应和化学反应效应.  相似文献   

17.
以NACA0012翼型为研究对象,采用动态测压及PIV测量技术,研究了AC-DBD等离子体激励器对翼型俯仰及耦合运动动态失速的控制作用和机理.研究表明,等离子体激励能够显著推迟失速迎角,抑制失速后的升力系数陡降,提前流动再附和升力系数回升,减小升力及俯仰力矩系数曲线迟滞环面积,改善翼型气动特性.研究了不同运动参数及激励器设置参数对控制效果的影响,结果表明翼型俯仰运动频率及激励器激励频率分别对激励器控制效果影响最大,为后续相关研究提供了数据基础.   相似文献   

18.
李雪辰  贾鹏英  袁宁  常媛媛 《中国物理 B》2012,21(4):45204-045204
A plasma column with a length of about 65 cm is generated in the upstream region of a plasma jet using dielectric barrier discharge configurations. The effects of experimental parameters such as the amplitude of the applied voltage and the driving frequency are investigated in aspects of the plasma column by the optical method. Results show that both the plasma length and the propagating velocity, as well as the discharge current, increase with the increase in the applied voltage or its frequency. The discharge mechanism is analysed qualitatively based on streamer theory, where photo-ionization is important. Furthermore, optical emission spectroscopy is used to investigate the electric field intensity of the upstream region.  相似文献   

19.
等离子体气动激励机理数值研究   总被引:4,自引:0,他引:4       下载免费PDF全文
程钰锋  聂万胜  李国强 《物理学报》2012,61(6):60509-060509
基于介质阻挡与准直流电弧放电的物理过程, 分析了它们的气动激励机理, 建立了各自的气动激励模型, 并分别研究了它们对低速和超声速流动的激励效果. 结果显示: 介质挡板放电等离子体气动激励机理是改变了连续流体中的三种力, 即由牛顿内摩擦引起的剪切应力、由电动力学引起的体积力及由压力突变引起的冲击力, 其中基于电动力学的体积力效应占主导地位; 临近空间环境中体积力的作用效果更强, 诱导速度更大; 超声速来流下准直流电弧放电气动激励机理主要是等离子体的热阻塞效应, 本文所建立的爆炸丝传热模型可以用于仿真其控制激波的过程; 热电弧对于超声速来流而言就像一个具有一定斜坡角度的虚拟突起, 可用于高超声速飞行器前体激波的控制.  相似文献   

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