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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。     

对称等离子体激励器系统电场仿真研究

采用电磁场数值计算的时域有限差分法，对用于产生等离子体的对称结构激励器系统进行了电场仿真，并对等离子体流动控制机理进行了分析.得出了与理论分析一致的用于蠕动加速的对称等离子体激励器的电场分布.这对于提高蠕动加速速度和激励器的结构优化具有一定的意义. 关键词： 蠕动加速 等离子体 时域有限差分 电流体动力     

ON f-EDGE COVER-COLOURING OF SIMPLE GRAPHS

An f-edge cover-colouring of a graph G = (V, E) is an assignment of colours to the edges of G such that every colour appears at each vertex υ∈ V at least f(υ) times.The maximum number of colours needed to f-edge cover colour G is called the f-edge cover chromatic index of G, denoted by χfc(G). This paper gives that min[d(ν)-1/f(ν)] ≤χfc(G) ≤min[d(υ)/f(υ)].     

Equivalent comparison and analysis between different nominal frequencies

We analyze the phenomena of phase group synchronization between the different nominal frequency signals and propose a new theory of the equivalent comparison between them. The exact expression of the equivalent comparison is deduced. High resolution frequency measurement and phase comparison can be realized using this theory with the divider. For avoiding the frequency mixing, multiplication and synthesis, the system phase noise is improved and the higher resolution comparison and measurement are achieved between the different nominal frequencies by theory.     

氩气/空气ICP放电现象研究和基于H_β光谱展宽的微波干涉电子密度诊断方法

闭式腔体ICP是解决飞行器等离子体局部隐身的可行方案,其电子密度Ne在电磁波入射方向上的分布是影响其电磁波衰减效果的关键因素。对此,开展了在30.8cm×30.8cm×5.8cm石英腔体内的ICP放电实验,通过实验研究了空气/氩气ICP的E-H模式跳变的物理现象,通过测量得到了空气/氩气环状ICP的宽度和覆盖面积比例随电源功率变化的规律,并给出了上述实验现象的理论解释。为了得到平面型ICP的电子密度在微波入射方向的分布,提出基于Hβ光谱展宽的微波干涉分布诊断法,分别对平面真空腔室内空气/氩气ICP的电子密度在电磁波入射方向上的分布进行了诊断,通过H_β(486.13nm)Stark展宽拟合和微波干涉过程分别获取电子密度分布函数的两项参数,得到了电子密度分布随放电功率变化的曲线。实验可得到电子密度范围为0.5×10~(11)~3.2×10~(11) cm~(-3)的环状ICP源,实验结果表明,ICP的电子密度受气体种类,射频功率影响较大,峰值电子密度接近ICP的中心位置,通过比较发现,氩气的电子密度较高,有效拟合区域较窄,空气的有效拟合区域较宽,覆盖面积较大。     

Experimental investigation of nanosecond discharge plasma aerodynamic actuation

In this paper we report on an experimental study of the characteristics of nanosecond pulsed discharge plasma aerodynamic actuation. The N 2 (C 3 Π u ) rotational and vibrational temperatures are around 430 K and 0.24 eV, respectively. The emission intensity ratio between the first negative system and the second positive system of N 2 , as a rough indicator of the temporally and spatially averaged electron energy, has a minor dependence on applied voltage amplitude. The induced flow direction is not parallel, but vertical to the dielectric layer surface, as shown by measurements of body force, velocity, and vorticity. Nanosecond discharge plasma aerodynamic actuation is effective in airfoil flow separation control at freestream speeds up to 100 m/s.     

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采用PSpice软件进行了等离子体流动控制实验系统的电特性仿真。将等离子体放电建模为分段非线性的电压控制电流源子模块,较好地解决了等离子体流动控制系统电特性仿真的关键问题。在此基础上,对等离子体流动控制实验系统进行了仿真。仿真结果证实了等离子体放电模型的有效性,可用于指导进一步仿真和流动控制实验系统的改进。     

高效液相色谱法测定酶转化液中D-苯丙氨酸

采用HPLC法测定了酶转化液中的D_苯丙氨酸、N_氨甲酰_D_苯丙氨酸和苄基海因。流动相为乙腈-20mmol·L-1 磷酸二氢钾(体积比25∶75), 用磷酸调pH为5.0, 利用DAD检测器, 检测波长为202 nm, 流速为1.0mL·min-1。用外标法进行定量分析, 三者的线性范围分别是1.82~466 mg·L-1(r=0.999)、2.01~516 mg·L-1(r=0.999)、1.94~496 mg·L-1(r=0.999), 回收率为99.9%~100.1%、99.8%~100.0%、99.5%~ 100.4%,RSD(n=6)分别为1.8%、1.6%、1.0%, 检出限为18.7、2.41、64.6 pg。实验结果表明该法简便、快速、结果可靠。     

边覆盖临界图的一些性质

设G是一个简单图,其顶点集为V(G)而边集为E(G),S∈E(G)称为 G的一个覆盖,如果由S导出的子图为G的一个生成子图. G的边覆盖色数χ'c(G)是E(G,)所能划分成的最大边覆盖数.已知δ-1 ≤χ'c(G)≤δ,由此将χ'c(G)=δ的图称为CI类图,否则称为CII类图.若G是连通CII类图,且G不是完全图,对任意的u,u∈V(G),e=uv( )E(G),都有χ'c(G+e)＞χ'c(G)成立,则称G为边覆盖临界的.本文研究了边覆盖临界图的一些性质.即若G为边覆盖临界图,则对任意的u,v∈V(G),若e=uv( )E(G),总存在w∈{u,v},有d(w)≤2δ-2,且w至少与max{d(w)-δ+1,3d(w)-4δ+4}个最小度顶点相邻.     

Influence of air pressure on the performance of plasma synthetic jet actuator

Plasma synthetic jet actuator(PSJA) has a wide application prospect in the high-speed flow control field for its high jet velocity.In this paper,the influence of the air pressure on the performance of a two-electrode PSJA is investigated by the schlieren method in a large range from 7 k Pa to 100 k Pa.The energy consumed by the PSJA is roughly the same for all the pressure levels.Traces of the precursor shock wave velocity and the jet front velocity vary a lot for different pressures.The precursor shock wave velocity first decreases gradually and then remains at 345 m/s as the air pressure increases.The peak jet front velocity always appears at the first appearance of a jet,and it decreases gradually with the increase of the air pressure.A maximum precursor shock wave velocity of 520 m/s and a maximum jet front velocity of 440 m/s are observed at the pressure of 7 k Pa.The averaged jet velocity in one period ranges from 44 m/s to 54 m/s for all air pressures,and it drops with the rising of the air pressure.High velocities of the precursor shock wave and the jet front indicate that this type of PSJA can still be used to influence the high-speed flow field at 7 k Pa.