三层流体中斜入射波作用下半无限板的水弹性响应

解析地研究了在三层流体中斜入射波浪与半无限弹性板的相互作用引起的波散射和板的水弹性响应. 三层流体在界面处的密度发生阶跃, 各层为一常数. 假设流体不可压缩、无黏、流体运动无旋. 在线性势流理论框架下, 使用本征函数展开法和内积式给出波板相互作用的半解析解. 根据色散关系分析, 得到了表面波模态和界面波模态入射时的临界入射角. 随着物理参数的变化, 临界角将随之发生变化. 临界角决定了当由开阔水域向板覆盖水域传播的表面波或界面波的存在性: (1)板覆盖水域入射界面上, 透射波能否存在; (2)入射界面之上界面中, 板覆盖水域中的透射波以及开阔水域中的反射波能否存在. 当下界面波入射时并且入射角足够大时, 开阔水域中的下界面波模态是整个流体域中唯一存在的模态.      

光子晶体全反射贯穿偏振滤波器的理论研究

为了研究1维光子晶体中光的全反射贯穿效应及其偏振滤波特性,利用传输矩阵法计算了TE波和TM波在大于全反射角入射1维光子晶体的透射率,发现在透射波中出现了全反射贯穿效应。研究了TE波和TM波的全反射贯穿效应随介质光学厚度和周期数的变化特征,表明：全反射贯穿峰的频率随介质光学厚度的增加而减少,全反射贯穿峰数与周期数相等。且全反射贯穿效应具有优良的偏振滤波特性,利用这些特性可以设计出结构简单、控制方便的1维光子晶体的偏振滤波器。     

Domain wall motion in ferromagnets modelled by a quintic complex Ginzburg-Landau equation

A quintic complex Ginzburg-Landau equation is derived from a Landau-Lifshitz-Gilbert equation and is used to describe the magnetization dynamics in a one-dimensional uni-axial ferromagnet. Trough the use of suitable approximations, we derive the magnetic solitary wave excitations solutions which have pulse-like shapes. Subsequent numerical simulations reveal domain wall propagation.     

Gene delivery to cells on a miniaturized multiwell plate for high-throughput gene function analysis

The transfectional microarray is a promising tool to conduct high-throughput analysis of gene function. In this study, a miniaturized multiwell plate was prepared by applying a silicone rubber sheet with holes on a gold electrode. The combination of electroporation and a miniaturized multiwell plate successfully achieved spatially controlled gene delivery with absence of cross-contamination between genes. Furthermore, we found that gene delivery efficiency was not dependent on conditions such as plasmid loading, electric field strength, and pulse duration.     

On Boundary Damping for a Weakly Nonlinear Wave Equation

In this paper an initial-boundary value problem for a weakly nonlinear string(or wave) equation with non-classical boundary conditions is considered. Oneend of the string is assumed to be fixed and the other end of the string isattached to a spring-mass-dashpot system, where the damping generated by thedashpot is assumed to be small. This problem can be regarded as a rather simple model describing oscillationsof flexible structures such as suspension bridges or overhead transmission lines in a windfield. A multiple-timescales perturbation method will be usedto construct formal asymptotic approximations of the solution. It will also beshown that all solutions tend to zero for a sufficiently large value of thedamping parameter. For smaller values of the damping parameter it will be shownhow the string-system eventually will oscillate.     

一类带时滞和全局反应项生物模型的行波解

研究了带时滞的微分方程异宿轨解的存在条件,并通过时滞微分系统和反应扩散系统解之间的关联性,得到了一类带全局反应项的生物反应扩散模型的行波解.     

Recent results on light hadron spectroscopy from BES Ⅱ

We reported the observation of Y(2175) in φf0(980) mass spectrum in J/ψ→ηφf0(980) with f0(980)→π+π- and the observation of a broad 1-- resonance of K+K-mass in J/ψ→K+K-π0. The results from the partial wave analyses of Jψ→γπ+π- and γπ0π0, as well as J/ψ→pK-∧. are also presented.     

受限亚音速气流中倒置悬臂壁板静气弹稳定性的理论及实验研究

板壳结构在航空航天、高速列车、能量采集等诸多工程领域已经得到了广泛应用.将悬臂壁板倒置于轴向气流中并在壁板周围流场中设置刚性壁面可有效地调控壁板的失稳速度,是俘能器优化设计的重要措施之一.但针对刚性壁面作用下亚音速气流中倒置悬臂壁板的失稳机制仍需要开展深入研究.本文以受限亚音速气流中倒置的二维悬臂壁板为对象,以理论分析及风洞实验为手段,研究了单侧刚性壁面效应对倒置悬臂壁板静态失稳特性的影响规律.在理论分析中,首先应用镜像函数法来处理壁面约束条件,基于算子理论研究获得了以Possio积分方程为表征的壁板气动力,壁面效应实际表征为一包含移位Tricomi算子的复合算子;然后将壁板失稳方程的求解问题转化为定区间上的函数逼近问题;最后,依据Wererstrass定理并利用最小二乘法求解该最优函数,以获得系统的失稳临界参数.在试验研究中依据压杆稳定原理设计了壁板静态失稳的测试方法并完成了风洞实验.理论分析结果表明,壁板会发生发散(静气动弹性)失稳,临界动压随壁板与壁面间距的增加而增大并最终趋于稳定(无壁面情况);通过理论与风洞实验结果的对比分析,验证了本文气动力及理论分析的适用性及准确性.针对倒...     

Effect of Localization of Pulsed Energy Addition on the Wave Drag of an Airfoil in a Transonic Flow

The possibility of controlling the aerodynamic characteristics of airfoils with the help of local pulsed-periodic energy addition into the flow near the airfoil contour at transonic flight regimes is considered. By means of the numerical solution of two-dimensional unsteady equations of gas dynamics, changes in the flow structure and wave drag of a symmetric airfoil due to changes in localization and shape of energy-addition zones are examined. It is shown that the considered method of controlling airfoil characteristics in transonic flow regimes is rather promising. For a zero angle of attack, the greatest decrease in wave drag is obtained with energy addition at the trailing edge of the airfoil.__________Translated from Prikladnaya Mekhanika i Tekhnicheskaya Fizika, Vol. 46, No. 5, pp. 60–67, September–October, 2005.     

Newman-Penrose Formalism and Gravitational Impulsive and Shock Waves

Vacuum spacetimes endowed with two commuting spacelike Killing vector fields are considered. Subject to the hypothesis that there exists a shearfree null geodesic congruence orthogonal to the two-surface generated by the two commuting spacelike Killing vector fields,it is shown that, with a specific choice of null tetrad, the Newman-Penrose equations are reduced to an ordinary differential equation of Riccati type. fiom the consideration of this differential equation, exact solutions of the vacuum Einstein field equations with distribution valued Weyl curvature describing the propagation of gravitational impulsive and shock wave of variable polarization are then constructed.