混合气体燃烧中压力对爆震波特性参数影响研究

采用平衡常数法对烃一空气混合气体燃烧中爆震燃烧产物的平衡温度、平衡压力及爆震波速进行了计算与分析。在此基础上研究了混合气压力对爆震波特性参数的影响。研究结果表明：在同一混气余气系数下，平衡温度和爆震波速随混气压力的增大而增大，而平衡压力则随混气压力呈线性增大。同时，对于不同燃料，分子量越大，其平衡温度、平衡压力就越高。     

Experimental Investigation of Hypersonic Flow and Plasma Aerodynamic Actuation Interaction

For hypersonic flow,it was found that the most efective plasma actuator is derived from an electromagnetic perturbation.An experimental study was performed between hypersonic flow and plasma aerodynamic actuation interaction in a hypersonic shock tunnel,in which a Mach number of 7 was reached.The plasma discharging characteristic was acquired in static flows.In a hypersonic flow,the flow field can afect the plasma discharging characteristics.DC discharging without magnetic force is unstable,and the discharge channel cannot be maintained.When there is a magnetic field,the energy consumption of the plasma source is approximately three to four times larger than that without a magnetic field,and at the same time plasma discharge can also afect the hypersonic flow field.Through schlieren pictures and pressure measurement,it was found that plasma discharging could induce shockwaves and change the total pressure and wall pressure of the flow field.     

Experimental Investigation on Airfoil Shock Control by Plasma Aerodynamic Actuation

An experimental investigation on airfoil （NACA64-215） shock control is performed by plasma aerodynamic actuation in a supersonic tunnel （Ma -= 2）. The results of schlieren and pressure measurement show that when plasma aerodynamic actuation is applied, the position moves forward and the intensity of shock at the head of the airfoil weakens. With the increase in actuating voltage, the total pressure measured at the head of the airfoil increases, which means that the shock intensity decreases and the control effect increases. The best actuation effect is caused by upwind-direction actuation with a magnetic field, and then downwind-direction actuation with a magnetic field, while the control effect of aerodynamic actuation without a magnetic field is the most inconspicuous. The mean intensity of the normal shock at the head of the airfoil is relatively decreased by 16.33%, and the normal shock intensity is relatively reduced by 27.5% when 1000 V actuating voltage and upwind-direction actuation are applied with a magnetic field. This paper theoretically analyzes the Joule heating effect generated by DC discharge and the Lorentz force effect caused by the magnetic field. The discharge characteristics are compared for all kinds of actuation conditions to reveal the mechanism of shock control by plasma aerodynamic actuation.     

高压脉冲直流等离子体电源的研制及其放电特性

为满足高超声速磁流体流动控制实验研究的需要,采用同步高压脉冲电离和直流维持放电技术,研制了一种适用于高超声速激波风洞实验系统的高压脉冲直流等离子体电源。首先进行了静止低气压条件下的放电特性研究。通过高速电荷耦合器件(charge coupled device,CCD)可以发现:初始时刻直流放电强烈,放电电流达到16A;随着电容储存能量的消耗,放电电流逐渐减小,放电强度缓慢减弱,直至完全消失,放电形状近似为一圆形。然后进行了高超声速气流中无磁场激励、磁流体(magnetohydrodynamics,MHD)逆气流减速激励和MHD顺气流加速激励条件下的放电特性研究,提出了用于高超声速激波风洞实验系统的MHD激励强度判定标准。研究结果表明:高超声速气流中施加磁场能够起到稳弧的作用,有磁场激励条件下的电源能量消耗约是无磁场激励条件下的3～4倍;MHD加速激励同MHD减速激励的功率相等,而MHD加速激励的电源能量消耗高于MHD减速激励的电源能量消耗。     

铌欠缺对掺镧PZN基陶瓷的有序微区和介电性能的影响

研究了铌欠缺对掺镧 PZN基陶瓷相结构、有序微区以及介电性能的影响。铌欠缺消除了掺镧所产生的焦绿石相 ,使陶瓷试样恢复为百分之百的钙钛矿相结构。 Ram an散射光谱分析表明 ,铌欠缺使掺镧 PZN基陶瓷的有序微区增大 ,同时铌欠缺也提高了掺镧 PZN基陶瓷的介电常数。铌欠缺使介电常数增大的原因归结于焦绿石相的消除和“有效有序微区”尺寸的扩大     

一维理想磁控等离子体激波管流动仿真

推导了磁场作用下等离子体流动的控制方程,采用加入人工粘性项的MacCormack二阶格式对方程进行了离散.计算了在不同磁场作用下,一维理想磁控等离子体在激波管内的流动情况.计算结果表明,在施加磁场作用后,激波管内的波系结构发生了明显的改变,磁场强度在激波的影响下发生了重新分布.