矩形移动荷载作用下饱和-非饱和土双层地基的动力响应分析

考虑地基为饱和-非饱和土双层半空间,利用连续介质力学和多相孔隙介质理论,构建双层地基的统一动力控制方程并进行耦合求解。利用Dirac-delta函数和Heaviside阶跃函数将矩形移动荷载作用描述为时间和空间坐标的解析函数,将荷载函数代入地基动力控制方程,采用三重Fourier变换以及降阶法进行求解,并对推导结果进行退化验证及对饱和-非饱和土双层地基的动力响应进行分析。研究表明,当荷载移动速度小于瑞利波速时,竖向振动峰值很小,振幅随速度的增大发生小幅增涨,但当荷载速度达到瑞利波速时,竖向振动发生激增;随着速度进一步增大,竖向位移多次出现峰点。非饱和土的饱和度及土层厚度也对地基振幅存在显著影响。     

阻尼对空爆荷载等效静载动力系数的影响

为考查阻尼参数对空爆荷载等效静载动力系数的影响,理论推导了空爆荷载下结构等效单自由体系弹塑性位移解及延性比解,设计并计算了阻尼比0.000 1～0.1、延性比1～4的20种典型工况的动力系数,并与现行抗爆设计规范动力系数公式结果进行了对比。结果表明:阻尼比小于0.000 1时可基本代表无阻尼状态,阻尼比0.01的动力系数比无阻尼的最大降低幅度为2.08%,数值差异很小,因此阻尼比为0.01以内时,可忽略阻尼对动力系数的影响;阻尼比0.05的动力系数比无阻尼的降低幅度约9.92%,数值差异较大,认为阻尼比0.05以上时将具有明显的经济效益;现行设计规范动力系数更适用于柔性结构体系,运用于刚性结构抗爆设计时,计算误差较大,对阻尼比较小的结构设计更不利。     

Pure Multiplicative Noises Induced Population Extinction in an Anti-tumor Model under Immune Surveillance

The dynamical characters of a theoretical anti-tumor model under immune surveillance subjected to a pure multiplicative noise are investigated. The effects of pure multiplicative noise on the stationary probability distribution （SPD） and the mean first passage time （MFPT） are analysed based on the approximate Fokker-Planck equation of the system in detail. For the anti-tumor model, with the multiplieative noise intensity D increasing, the tumor population move towards to extinction and the extinction rate can be enhanced. Numerical simulations are carried out to check the approximate theoretical results. Reasonably good agreement is obtained.     

Optimized transfer trajectories in the earth-moon system

Investigations of low energy transfer trajectories are important for both celestial mechanics and astronautics. Methodologies using the theories from dynamical systems are developed in recent years. This paper investigates the dynamics of the earth-moon system. Low energy transfer trajectories are solved numerically by employing a hybrid strategy： first, a genetic hide and seek method performs a search in large domain to confine the global minimum f（η） （objective function） region; then, a deterministic Nelder-Mead method is utilized to refine the minimum quickly. Some transfer trajectories of the spacecraft in the earth-moon system are successfully simulated which verify the desired efficiency and robustness of the method of this paper.     

Dynamical behaviour of Liu system with time delayed feedback

This paper investigates the dynamical behaviour of the Liu system with time delayed feedback. Two typical situations are considered and the effect of time-delay parameter on the dynamics of the system is discussed. It is shown that the Liu system with time delayed feedback may exhibit interesting and extremely rich dynamical behaviour. The evolution of the dynamics is shown to be complex with varying time-delay parameter. Moreover, the strange attractor like ‘wormhole＇ is detected via numerical simulations.     

用动力学法测杨氏模量实验及其实验装置的研制

介绍了新研制的用动力学法杨氏模量的实验装置,它具有功耗低,灵敏度高的特点;教学中测量悬线不同位置时的共振频率,用作图法拟合出其精确值,以减少由于悬线不在节点引起的系统性误差,测量精密度比传统的静态拉伸法高一个量级以上。     

ωN

从QHD-1场方程出发,用动力论的方法计算得到ωN强相互作用的核物质系统的介电函数,并具体分析了在高温下介电函数的特征及其物理背景.     

具有非比例阻尼的线性系统的动力响应

本文导出具有非比例阻尼的线性系统在一般激励下解的形式,给出了一种近似解法,並以简谐激励为例进行讨论。     

ωNN强相互作用的核物质系统在高温下的介电性质

从QHD-1场方程出发,用动力论的方法计算得到ωNN强相互作用的核物质系统的介电函数,并具体分析了在高温下介电函数的特征及其物理背景.     

HOMOCLINIC ORBITS FOR LAGRANGIAN SYSTEMS

The existence of at least two homoclinic orbits for Lagrangian system (LS) is proved, wherethe Lagrangian L(t,x,y) =1/2∑aij(x)yiyj-V(t, x), in which the potential V(t,x) is globallysurperquadratic in x and T-periodic in t. The Concentration-Compactness Lemma and Mini-max argument are used to prove the existences.