脉冲高功率离子二极管的动力学模拟

基于等离子体的爆炸发射模型,利用自洽的2.5维的胞中粒子（PIC）模拟程序MAGIC模拟了平板型磁绝缘离子二极管中电子和质子的动力学特性。给出了电压为300kV,外加磁场为2倍临界磁场情况下的二极管特性,阴阳极间隙中带电粒子的空间和相空间分布,以及净电荷密度分布和电场分布,结果表明,引出束流密度比单离子Child-Langmuir公式计算的结果大5倍;外加磁场导致在阴极附近形成虚阴极。空间电荷使得阴阳极间隙中电场扰动和增强。     

光阴极注入器型能量回收射频加速器

光阴极注入器型能量回收射频加速器（PERL）是新一代加速器,在高平均功率自由电子激光和下一代高亮度光源等研究中有很好的应用前景。分析了PERL的强流与高平均功率特性,对注入器输出束流品质的要求及光阴极注入器、超导加速腔等关键技术进行了研究,设计分析了一种特殊结构的高压DC Gun光阴极注入器,能有效地提高DC加速腔中的加速场强,当高压为1MV和加速场达到10MV/m时,产生的电子束流能够基本满足PERL应用要求。同一超导加速段中的束流加速和能量回收的数值模拟计算结果表明,能获得高效率电子束流能量回收效果。     

预脉冲对相对论磁控管工作性能的影响分析

在阐述预脉冲产生的基础上,分析了预脉冲带来的一系列影响,包括工和电压波形变化,提前生成等离子体,以及预脉冲阶段放大竞争模式等,这些影响与相对论磁控管起振工作频率相联系,从而直接造成了相对论磁控管的基本性能参数,如脉宽、工作频率及输出功率等变化。结合具体实验,对比了有、无预脉冲条件下相对论磁控管工作性能的差异,对预脉冲的影响因素与相对论磁控管性能之间的联系进行了详细的分析。     

DF/HF化学激光器HYLTE喷管的副喷管质量流量系数

对DF/HF化学激光器HYLTE喷管的副喷管质量流量进行了数值和理论计算,得出入口滞止压力在0.01~0.4MPa之间、喉道半高度在0.1~0.9mm之间的喷管的氘气,氢气和氦气质量流量系数,总结出质量流量系数随入口滞止压力和喉道高度的变化规律,并给出拟合公式,为副喷管的设计提供依据。     

柱几何Rayleigh-Taylor不稳定性的数值模拟

给出了柱几何中流体力学方程组及其在数值模拟中采用的计算方法。对二维柱几何Rayleigh-Taylor不稳定性进行数值模拟,在线性阶段与线性理论符合得很好;不稳定性增长进入非线性区域的阈值依赖于界面的位置,并且明显不同于平面情况。     

Subsurface layers with degenerate hole gas arising in germanium immersed into liquid helium under 60Co-gamma irradiation

Abstract

The subsurface layers with quasi-metal hole conductivity have been observed in n- and p-Ge immersed into liquid He under the ⁶⁰Co-gamma-irradiation. three conditions are to be fulfilled simultaneously for the production of the layers: low temperature, direct contact between helium and germanium and gammairradiation.     

Size-dependent ignition temperature of metallic compounds fabricated by self-propagating high-temperature synthesis

Considering the diffusion reaction at solid interfaces, the ignition temperature of compounds fabricated by self-propagating high-temperature synthesis (SHS) is modelled with the help of size-dependent activation energy. As reactant size decreases, ignition temperature also decreases. This is because of increased contact areas between the reactants and the lowered diffusion barrier, both of which must be calculated specifically for reactants in nanoscale. The model predictions and experimental results are consistent for some metallic compounds.     

Air Flow Computation around an Automated Guided Vehicle

An upwind finite element scheme for the incompressible viscous flow at a high Reynolds number was proposed by the fourth and fifth authors. The scheme has the potential to approximate the advection term in third-order accuracy. We apply it to a two-dimensional non-stationary analysis of airflows around an Automated Guided Vehicle (AGV), which starts with constant acceleration, runs at a constant speed and stops with constant deceleration. The results are at least qualitatively good and compatible with experimental ones.     

Numerical study on combustion of H2—O2 in a supersonic reactive expansion in a nozzle

A study on expansion flow inside a nozzle considering full mechanism chemistry of hydrogen and oxygen was carried out. In this study, a full implicit scheme for turbulent reactive flow was obtained by combining the second order TVD scheme of Yee and Harten (1987, Implicit TVD schemes for hyperbolic conservation laws in curvilinear coordinates. American Institute of Aeronautics and Astronautics Journal, 25(2), 266–274) with the efficient implicit lower-upper scheme of Shuen and Yoon (1989, Numerical study of chemically reacting flows using a lower-upper symmetric successive overrelaxation scheme. American Institute of Aeronautics and Astronautics Journal, 27(12), 1752–1756). The species equations, Navier–Stokes equations and turbulence model were implemented in the numerical scheme and solved in conjunction with full detailed finite rate chemistry. The numerical scheme is verified by comparison with experimental results of a converging–diverging nozzle. Effects of inlet pressure, temperature and fuel-oxidant mass ratio on nozzle flow field were studied. Variation of chemical species under different conditions was investigated by considering a chemical mechanism. Results show that increasing inlet pressure increases the rate of reactions due to increasing the concentration of reactants. For lower inlet pressure the radical H increases slightly in the diverging part of the nozzle, while for higher pressures it decreases along the nozzle. Inlet fuel–oxidant mass ratio affects the variation of all species with a greater effect for a near stoichiometric ratio. It was also shown that a higher inlet temperature provides a more enhanced reaction zone in the diverging part of the nozzle.     

Wavespeed analysis: Approximating Arrhenius kinetics with step-function kinetics

The accuracy of using step-function approximations to the Arrhenius exponential in computing the wavespeed in combustion wave propagation is investigated. Gaseous and gasless combustion, and first- and second-order reactions are included in the study. The theoretical analysis is based on Melnikov theory from dynamical systems. The error is shown to be small in most instances. The analytical results are supported with numerical simulations.