Nonlinear electron-acoustic rogue waves in electron-beam plasma system with non-thermal hot electrons

The properties of nonlinear electron-acoustic rogue waves have been investigated in an unmagnetized collisionless four-component plasma system consisting of a cold electron fluid, non-thermal hot electrons obeying a non-thermal distribution, an electron beam and stationary ions. It is found that the basic set of fluid equations is reduced to a nonlinear Schrodinger equation. The dependence of rogue wave profiles on the electron beam and energetic population parameter are discussed. The results of the present investigation may be applicable in auroral zone plasma.     

进口斜激波、膨胀波干扰下等直隔离段内的激波串特性

 超燃冲压发动机的隔离段在实际工作中会受到进气道唇罩激波及肩部膨胀扇的显著干扰,本文针对这一特定问题进行了专门研究。提出了唇罩入射激波及肩部膨胀扇的模拟方法,并利用德国Achen的风洞试验对其进行了检验,而后以此研究了入射激波及肩部膨胀扇干扰下隔离段内激波串的基本形态,并分析了出口反压和激波入射位置的影响。仿真结果表明：当激波串在隔离段内不断前移时,受唇罩入射激波及其反射激波的干扰,其高速核心区交替地偏向上下壁面;与无激波入射的情况相比,此时激波串的耐反压能力显著降低,且入射点位置越高,降低幅度越大,管道内的沿程静压分布规律与Waltrup经验公式偏离程度也越来越大。该文结果可为进气道/隔离段的一体化设计提供依据。     

Oscillatory thermocapillary flows in simulated floating-zones with time-dependent temperature boundary conditions

This study deals with numerical simulations of the Maxus sounding rocket experiment on oscillatory Marangoni convection in liquid bridges. The problem is investigated through direct numerical solution of the non-linear, time-dependent, three-dimensional Navier-Stokes equations. In particular, a liquid bridge of silicon oil 2[cs] with a length L = 20 [mm] and a diameter D = 20 (mm) is considered. A temperature difference ΔT = 30 [K] is imposed between the supporting disks, by heating the top disk and cooling the bottom one with different rates of ramping. The results show that the oscillatory flow starts as an ‘axially running wave’, but after a transient time the instability is described by the dynamic model of a ‘standing wave’, with an azimuthal spatial distribution corresponding to m = 1 (where m is the critical wave number). After the transition, the disturbances become larger and the azimuthal velocity plays a more important role and the oscillatory field is characterized by a travelling wave. The characteristic times for the onset of the different flow regimes are computed for different rates of ramping.     

WEIGHTED COMPACT SCHEME FOR SHOCK CAPTURING

INTRODUCTIONRecently compact schemes have been widelyused in the simulation of complex flows,espe-cially in the directnumerical simulation of turbu-lent flows[1～ 2 ] . Standard finite differenceschemes have explicit forms and need to be atleastone pointwider than the desired approxima-tion order. It is also difficult to find suitable andstable boundary closure for high order schemes.Compared to the standard finite difference ap-proximations,the compact schemes can achievehigher order acc…     

声重波激发的ESF的波长效应

通过对赤道地区声重波激发的Ｓｐｒｅａｄ－Ｔ扰动的非线性制约方程的拓扑特性,在不同扰动波长和扰动振幅的条件一进行数值计算,以及对原始非线性方程组在不同参数范围内进行数值模拟,显示了声重波的垂直扰动分量对ＥＳＦ演化的影响,为赤道地区Ｓｐｒｅａｄ－Ｆ形态的多样性提供了一种非线性的解释。     

液晶显示方法研究管内马赫数4拟似冲击波流动

在一个压力-真空型超声速风洞中, 剪切应力敏感的液晶表面流动显示技术被用来研究方管内马赫数4拟似冲击波的超声速流动.实验是在日本室兰工业大学的超声速风洞中进行.它提供了关于测试表面流动结构的定性信息,诸如湍流边界层分离和再附, 以及边界层流动的维数等.液晶显示结果与纹影实验照片和油膜方法进行比较,证实了它是一种非常有效的表面流动显示工具.     

The Nonlinear Model of the Response of Airglow to Gravity Waves

In this paper, we develope a time-dependent, nonlinear, photochemical-dynamical 2-D model which is composed of 3 models: dynamical gravity wave model, middle atmospheric photochemical model, and airglow layer photochemical model. We use the model to study the effect of the gravity wave propagation on the airglow layer. The comparison between the effects of the different wavelength gravity wave on the airglow emission distributions is made. When the vertical wavelength of the gravity wave is close to or is shorter than the thickness of the airglow layer, the gravity wave can make complex structure of the airglow layer, such as the double and multi-peak structures of the airglow layers. However, the gravity wave that has long vertical wavelength can make large scale perturbation of the airglow emission distribution.     

应力波在变截面杆中传播的数值分析

 利用ＨＯＮＤＯ有限元程序对应力波在变截面杆中的传播进行了分析。根据分析结果提出采用有台阶的锥形调制器取代现有调制器可以解决手提式铆枪过重的问题。有台阶的调制器对应力透射波的放大效果不会有明显变化,但可减轻重量５０％以上。同时利用该程序对应力波在不同几何构形的调制器中的传播进行了对比分析,根据输出波形的质量对应力波调制器的几何尺寸进行了优化设计,提出了锥体的底角和直径范围。     

有等离子体层的导体圆柱空间散射特性的分析

分别给出平行极化和垂直极化平面波入射到圆柱体时产生的散射场通用公式及其散射参数定义式,对金属圆柱体带有不同厚度的欠密状态等离子体层,过密状态等离子层,有损耗介质层等条件下的RCS计算进行了全面的数值分析,分析了影响双站RCS的各种因素并给出了数值结果,获得一些有用的结论,为进一步研究再入体的散射机理提供有用的参考.     

在核爆炸冲击波环境中飞行飞机的结构动力响应分析

着重分析在核爆炸冲击波环境中飞机结构动力响应有关问题,推导了动力学基本方程,介绍了飞机在核爆炸冲击波中非定常气动载荷计算方法,给出了结构动力响应分析的思路和计算过程,提出了飞行飞机在核爆炸冲击波作用下总体结构安全边界值的估算方法,并对存在的问题进行了讨论。