A mixed explicit-implicit antidiffusive method of navier-stokes equations for supersonic and hypersonic separated flows

The supersonic and hypersonic.laminar and turbulent vi-scous separated flows over two and three-dimensional com-pression corners are solved by the antidissipative explicit-implicit difference scheme presented in this paper.The re-sults obtained show that a high accuracy has been achieved bythis method and the time needed for computation is greatlyreduced.     

Dynamical fluctuations in fragmentation reactions in a Boltzmann–Langevin approach

Based on the isospin-dependent Boltzmann–Langevin model, the dynamical fluctuations in the fragmentation reaction of ¹¹²Sn+¹¹²Sn are investigated. The quadrupole moment and octupole moment with zero magnetic quantum number have large fluctuations in the early time of the collisions. The dynamical fluctuations in momentum space show a strong dependence on the incident energy. The effects of using different fluctuations on the fragment cross sections are also studied in the fragmentation reactions. The results by using Q₂₀ + Q₃₀ fluctuation have a better agreement with the experimental data. Calculations using Q₂₀ + Q₃₀ fluctuation produce more proton-rich and neutron-rich nuclei than those using Q₂₀ fluctuation only. Besides, the difference between the production cross sections of fragments calculated by using Q₂₀ and Q₂₀ + Q₃₀ fluctuations is larger in the vicinity of the projectile. These results present that the dynamical fluctuations may affect the whole dynamical process of fragmentation reactions including the production of fragments, due to the nonlinear nature of the Boltzmann–Langevin equation.     

船用加筋板架爆炸载荷下动态响应数值分析

针对船用加筋板架复杂结构在爆炸冲击波作用下的动态响应 ,采用商用高动态非线性有限元程序MSC/Dytran ,讨论了大尺寸加强结构板架迎爆承载问题 ,提出了复杂板架结构爆炸冲击波作用下动态响应的有限元计算方法 ,并进行了模型试验。试验结果与计算结果吻合较好 ,验证了应用程序及计算模型参数的稳定性和可靠性。对加筋板架两种承载形式 (大尺寸加强构件迎爆或背爆设置 )在爆炸冲击波作用下的动态响应 (板架中心挠度和塑性分布 )差异的分析研究表明 ,大尺寸骨架 (纵骨和肋骨 )背向爆炸冲击波设置将分散爆炸冲击波的冲击作用、减小板架变形、增强其抵抗爆炸冲击波冲击的能力 ,使结构偏于安全。     

时滞非线性动力吸振器的减振机理

对一个带有时滞非线性动力吸振器的两自由度结构,采用多尺度法研究了时滞非线性动力吸振器对主系统的减振性能,得到了主系统的振幅-时滞响应曲线.研究结果表明,对时滞非线性动力吸振器,可以通过调节反馈增益系数和时滞控制主系统的振动. 研究还发现,对确定的反馈增益系数,可以存在时滞的一些调节区域,时滞非线性动力吸振器可以减小主系统的振动. 并且在时滞的这些可调区域里,存在一个``最大减振点'对应这一反馈增益系数下主系统振幅的最小值.对不同的反馈增益系数,``最大减振点'对应的主系统的振幅也不同.因此能够找到一组反馈增益系数和时滞量的最佳值,最大程度地减小主系统的振动.研究结果表明,当反馈增益系数和时滞量调到最佳值时,主系统的振动较无时滞非线性动力吸振器可以减少90{\%}左右, 数值模拟也证实了解析结果的正确性.      

Exact traveling wave solutions to 2D-generalized Benney-Luke equation

By using the dynamical system method to study the 2D-generalized Benney- Luke equation, the existence of kink wave solutions and uncountably infinite many smooth periodic wave solutions is shown. Explicit exact parametric representations for solutions of kink wave, periodic wave and unbounded traveling wave are obtained.     

The chaotic response of a fluttering panel: The influence of maneuvering

The influence of maneuvering on the chaotic response of a fluttering buckled plate on an aircraft has been studied. The governing equations, derived using Lagrangian mechanics, include geometric non-linearities associated with the occurrence of tensile stresses, as well as coupling between the angular velocity of the maneuver and the elastic degrees of freedom. Numerical simulation for periodic and chaotic responses are conducted in order to analyze the influence of the pull-up maneuver on the dynamic behavior of the panel. Long-time histories phase-plane plots, and power spectra of the responses are presented. As the maneuver (load factor) increases, the system exhibits complicated dynamic behavior including a direct and inverse cascade of subharmonic bifurcations, intermittency, and chaos. Beside these classical routes of transition from a periodic state to chaos, our calculations suggest amplitude modulation as a possible new mode of transition to chaos. Consequently this research contributes to the understanding of the mechanisms through which the transition between periodic and strange attractors occurs in, dissipative mechanical systems. In the case of a prescribed time dependent maneuver, a remarkable transition between the different types of limit cycles is presented.Nomenclature a plate length - a _r u _r /h - D plate bending stiffness - E modulus of elasticity - g acceleration due to gravity - h plate thickness - j₁,j₂,j₃ base vectors of the body frame of reference - K spring constant - M Mach number - n 1 + ₀/g - N ₁ applied in-plane force - p–p aerodynamic pressure - P pa ⁴/Dh - q ₀/2 - Q _r generalized Lagrangian forces - R rotation matrix - R ₄ N, a ²/D - t time - kinetic energy - u plate deflection - u displacement of the structure - u _r modal amplitude - v₀ velocity - x coordinates in the inertial frame of reference - z coordinates in the body frame of reference - Ka/(Ka+Eh) - - elastic energy - 2qa ³/D - a/_mh - Poisson's ratio - material coordinates - air density - _m plate density - - _r prescribed functions - _r sin(r z/a) - angular velocity - a/v₀ - skew-symmetric matrix form of the angular velocity     

单自由度磁浮陀螺寻北仪的控制及分析

提出了一种结构简单的新型磁悬浮寻北仪,建立了电磁轴承约束的单自由度陀螺罗盘的数学模型,讨论了陀螺框架轴在弹性约束下偏离铅垂方向对寻北精度及定向时间的影响。采用动态补偿器使磁浮轴承系统稳定工作,并通过适当选取控制策略,有效地降低了由于框架轴运动而造成的寻北误差,并解决了可能出现的转子轴轨迹发散的问题。仿真结果表明,该磁悬浮寻北仪具有明显优于现有寻北仪的性能,当寻北时间为40 s时,定向误差小于2.3081×10?11 rad。     

幂强化材料和超弹性材料组合球体中孔穴的动态生成

在简单加载条件下,研究幂强化材料和超弹性材料组合球体中的动态孔穴生成和增长问题.首先在有限变形动力学的框架下建立了相应的非线性数学模型,得到了应力的表达式,利用变量变换的方法求得了外加载荷和孔穴半径之间的一个精确的微分关系式.证明了当突加载荷超过其临界值时,球体内部有孔穴的突然生成,并随时间呈现非线性的周期振动.通过数值计算,分析了材料参数和球体的半径比对孔穴生成和增长的影响,并与相应的静态结果进行了比较.结果发现,惯性力的影响降低孔穴生成的临界载荷,而且材料的塑性对孔穴生成和增长有明显的影响.     

一维流体饱和粘弹性多孔介质层的动力响应

本文研究了不可压流体饱和粘弹性多孔介质层的一维动力响应问题。基于粘弹性理论和多孔介质理论,在流相和固相微观不可压、固相骨架服从粘弹性积分型本构关系和小变形的假定下,建立了不可压流体饱和粘弹性多孔介质层一维动力响应的数学模型,利用Laplace变换,求得了原初边值问题在变换空间中的解析解,并利用Laplace逆变换的Crump数值反演方法,得到原动力响应问题的数值解。数值研究了饱和标准线性粘弹性多孔介质层的动力响应,分析了固相位移、渗流速度、孔隙压力及固相有效应力等的响应特征。结果表明,与不可压流体饱和弹性多孔介质相同,不可压流体饱和粘弹性多孔介质中亦只存在一个纵波,并且固相骨架的粘性对动力行为有显著的影响。     

DYNAMICAL CHARACTER FOR A PERTURBED COUPLED NONLINEAR SCHRODINGER SYSTEM

The dynamical character for a perturbed coupled nonlinear Schrodinger system with periodic boundary condition was studied. First, the dynamical character of perturbed and unperturbed systems on the invariant plane was analyzed by the spectrum of the linear operator. Then the existence of the locally invariant manifolds was proved by the singular perturbation theory and the fixed-point argument.