论刘勰诗本体论诗体的规范与进化观

既强调诗体的规范又强调诗体的进化的诗的进化论，是刘勰诗本体论的重要组成部分，刘勰在诗歌的形式本体上的思想是既保守又激进的，他很重视文体，语言，体验和想象，刘勰诗的形式本体论的主要学说是“诗有恒裁”说：强调诗歌有体，诗人应该有自觉的文体意识，甚至认为四言为正体；又不反对诗体进化，主张“随性适分”、“质文代变”。     

Application of nonsmooth transformations to analyze a vibroimpact duffing system

The forced vibrations of an impact Duffing oscillator with one degree of freedom are studied using Zhuravlev's nonsmooth transformation and the multiple-scales method. Detailed consideration is given to the forced vibrations in the domain of resonance family. The stability and bifurcations of periodic vibrations are analyzed Translated from Prikladnaya Mekhanika, Vol. 44, No. 10, pp. 114–121, October 2008.     

Monodromy and nonintegrability in complex Hamiltonian systems

This paper investigates the monodromy representation of the normal variational equation along a phase curve of a two-dimensional complex analytic Hamiltonian system. Geometrical conditions are presented which guarantee reducibility, together with additional hypotheses to ensure complete reducibility. Symmetries in the equations are treated in detail. Applications to establishing the nonintegrability of specific systems are presented.     

Qualitative Theory and Identification of Dynamic System with One Degree of Freedom

Dynamic systems described by nonlinear differential equations of the second order are studied. It is assumed that certain preliminary information on the dissipative or elastic characteristics of systems is known. A new approach is demonstrated to obtaining full information on unknown or partially known characteristics of a system from measurements of not only displacements but also velocities and accelerations __________ Published in Prikladnaya Mekhanika, Vol. 41, No. 6, pp. 139–143, June 2005.     

一类多自由度强非线性振动系统主共振的渐近解法

提出一种渐近方法用来处理一类多自由度强非线性自治振动系统，它是新渐近方法￣［１］的推广。本方法适用于主共振情形，我们建立了振幅和相位所满足的方程。文末用两个例子说明本方法的有效性。     

含面内转动自由度的广义协调曲面矩形扁壳元

扁壳单元中引入结点转角自由度可以在不增加结点的情况下,增加位移场的阶次,提高计算精度,从而显著地提高单元性能。同时在单元中引入泡状位移场,能有效地扩大了单元位移场的解空间,所构造的单元具有计算精度高、对计算网格畸变不敏感的优良特性。本文利用广义协调薄板单元RGC-12的位移函数作为扁壳元的法向位移,利广义协调矩形膜元的位移函数作为扁壳面的切向位移,通过附加面内转动自由度构造了一个具有24个自由度的4结点广义协调曲面矩形扁壳元GRC-S24。在此基础上再增加一个广义泡状位移,又构造了一个具有更高计算精度的曲面矩形扁壳元GRC-S24M。并通过实例分析对这两个单元的收敛性和精度进行了验证。     

一类指数型间断函数的嵌入非连续等参有限元法

在嵌入非连续有限元的基本思想下,提出一类附加位移形函数———指数型间断函数,来模拟由于非连续结构,如裂纹和节理,所导致的位移不连续规律,该附加函数是以到间断处的垂直距离为自变量,且随距离的增大而呈指数衰减的函数.指数型间断函数具有在数学上的便于积分和求导的优点,且比阶梯间断函数更能反映实际破裂后的变形情况.本文用弱解形式推导了嵌入非连续有限元格式,编制了二维4节点和三维8节点的嵌入非连续等参有限元程序,并分别给出了算例.算例表明在模拟裂纹追踪时,指数型间断函数的嵌入非连续等参有限元法可行且有效.     

Limit cycle oscillation behavior of transonic control surface buzz considering free-play nonlinearity

The limit cycle oscillation (LCO) behaviors of control surface buzz in transonic flow are studied. Euler equations are employed to obtain the unsteady aerodynamic forces for Type B and Type C buzz analyses, and an all-movable control surface model, a wing/control surface model and a three-dimensional wing with a full-span control surface are adopted in the study. Aerodynamic and structural describing functions are used to deal with aerodynamic and structural nonlinearities, respectively. Then the buzz speed and buzz frequency are obtained by V-g method. The LCO behavior of the transonic control surface buzz system with linear structure exhibits subcritical or supercritical bifurcation at different Mach numbers. For nonlinear structural model with a free-play nonlinearity in the control surface deflection stiffness, the double LCO phenomenon is observed in certain range of flutter speed. The free-play nonlinearity changes the stability of LCOs at small amplitudes and turns the unstable LCO into a stable one. The LCO behavior is dominated by the aerodynamic nonlinearity for the case with large control surface oscillation amplitude but by the structural nonlinearity for the case with small amplitude. Good agreements between LCO behaviors obtained by the present method and available experimental data show that our study may help to explain the experimental observation in wind tunnel tests and to understand the physical mechanism of transonic control surface buzz.     

基于MEMS惯性技术的鞋式个人导航系统

研究了低精度鞋式个人惯性导航系统的导航修正算法.该系统由低精度MEMS惯性IMU单元组成,固联在步行者的鞋上.导航算法在传统捷联惯性导航算法基础上,引入了零速修正技术,根据人行走时脚部运动的加速度统计特性,设计了一种比力模值+滑动方差检测算法,用以检测行走过程中的静止时间段.然后通过设计的改良卡尔曼滤波器在静止时间段内滤波估计导航姿态、速度和位置的计算误差,通过反馈校正可以提高原系统的导航精度.最后通过两组MEMS实物实验验证了导航修正算法的有效性和可行性,并指出了进一步的研究方向.     

爆炸冲击载荷作用下车辆和人员的损伤与防护

在当前反恐战争和地区武装冲突迫切形势下,如何提高车辆及人员的防护能力是诸多学科工作者面临的共同挑战。综述了威胁车辆安全的常见爆炸物、其作用原理和影响爆炸物作用载荷的因素,阐述了爆炸物爆炸冲击对车辆的破坏和人员损伤的各类不同形式。在此基础上分析了相关的实验、表征和模拟技术的研究进展,总结了国内外车辆爆炸防护结构的研究现状,包括轻质防护材料和结构的研发趋势,展望了车辆爆炸防护结构设计的研究趋势。