平面弹性理论的周期接触问题

对于平面弹性理论的经典接触问题,即弹性体(作为占有下半平面)上压着有限个压头的情况,和曾先后应用复变函数理论,得到了一些有效的解答,对于平面弹性理论的周期接触问题,即弹性体(作为占有下半平面)压着无限个按周期排列的压头,在所指弹性体为各向同性体的情况,路见可教授同样得到了     

复合材料弹性平面的周期接触问题

对于平面弹性理论的经典接触问题,即弹性体(作为占有下半平面)上压着有限个压头的情况,曾应用复变函数理论,得到了一些有效的解答。对于平面弹性理论的周期接触问题,即弹性体上压着无限个按周期排列的压头,在所指弹性体为各向同性体的情况,路见可和蔡海涛同样应用复变函数理论,得到了一些有效解答。     

广义 Eady 模型的非线性稳定性

对于广义 Eady 模型, 分别讨论了密度函数是常数函数与指数函数两种情形, 利用变分原理, 考虑到动量守恒的约束条件, 得到了优化的 Poincaré不等式, 从而得到了新的非线性稳定性定理, 并且得到了在径向长度分别不大于纬向长度的0.84402倍 及 0.86068 倍时(这对于地球的实际情况是成立的), 非线性稳定性判据与线性稳定性判据是一致的.     

非线性加工时间单机排序问题

讨论工件加工时间是等待时间的非线性增加函数的单机排序问题,目标函数为极小化完工时间和与极小化最大延误.基于对问题的分析,对于一般非线性函数的情况,给出了工件间的优势关系.对于某些特殊情况,利用工件间的优势关系得到了求解最优排序的多项式算法.推广了文献中的结论.     

广义Eady模型的非线性稳定性

对于广义Eady模型，分别讨论了密度函数是常数函数与指数函数两种情形，利用变分原理，考虑到动量守恒的约束条件，得到了优化的Poincare不等式，从而得到了新的非线性稳定性定理，并且得到了在径向长度分别不大于纬向长度的0．84402倍及0．86068倍时（这对于地球的实际情况是成立的），非线性稳定性判据与线性稳定性判据是一致的．     

Hilbert空间中的非严格凸情况的Uzawa算法

无穷维空间中目标泛函为严格凸时的Uzawa算法已由Bensoussan等提出.一般说来,对于普通凸泛函,这种算法无效.这是因为在非严格凸情况时,对偶泛函一般是不可微的.本文提出Hilbert空间中的非严格凸情况的Uzawa算法.对于可分离问题,我们就得到了价格分解方法.考虑问题这里,     

一类四阶微分方程解的有界性和稳定性

本文分两种情况研究方程(1):(i)P≡0,(ii)P(≠0)满足|P(t,x,y,z,ω)|≤(A+|y|+|z|+|ω|)q(t),这里,q(t)是t的非负函数.对于第一种情况研究了零解的全局渐近稳定性,对于第二种情况得到了方程(1)的有界性结果.这些结果改进并包含了一些已知的结果.     

关于“截断切割”的最优设计

针对 1 997年全国大学生数学建模竟赛 B题 ,对于换刀费用 e=0的情况 ,本文设计了一种异常简捷的切割厚度排序法来寻找最优切割方案 ,同时在数学上给出了严格的证明 .对于换刀费用 e≠ 0的情况 ,以 e=0时得到的最优切割方案为基础 ,先通过简单的调整原则寻找出限定不同换刀次数时各自的最优切割方案 ,再通过费用比较便可简捷地得到随 e值的大小而变化的最优切割方案 .本文构造的模型在求解时无须用计算机编程 ,只用手算即可简捷地得到答案     

一类四阶超线性奇异微分方程边值问题的正解

该文研究了一类包含二阶导数项的四阶超线性奇异微分方程边值问题,得到正解的存在性及有关性质.然后,对于不含有二阶导数项的情况,得到其C2[0,1]正解、C3[0,1]正解存在的充分必要条件.     

关于弹性半无限体表面的稳定性

本文综合报道有关弹性半无限体表面稳定性的若干工作.对于不可压缩弹性半无限体,概述在双向受载下自由表面的失稳分析,给出失稳的临界条件.对于可压缩弹性材料情况,分析了由标准材料组成的半无限体的表面轴对称失稳,得到失稳临界参数对于材料参数的依赖关系.     

Slow flow between concentric cones

This paper considers the low-Reynolds-number flow of an incompressiblefluid contained in the gap between two coaxial cones with coincidentapices and bounded by a spherical lid. The two cones and thelid are allowed to rotate independently about their common axis,generating a swirling motion. The swirl induces a secondary,meridional circulation through inertial effects. For specificconfigurations complex eigenmodes representing an infinite sequenceof eddies, analogous to those found in two-dimensional cornerflows and some three-dimensional geometries, form a componentof this secondary circulation. When the cones rotate these eigenmodes,arising from the geometry, compete with the forced modes todetermine the flow near the apex. This paper studies the relative dominance of these two effectsand maps out regions of parameter space, with attention to howshear and overall rotation can destroy the infinite sequenceof eddies that may be present when only the lid is rotated.A qualitative picture of the number of eddies visible in themeridional circulation is obtained as a function of the rotationrates of cones and lid, for various choices of angles. The resultsare discussed in the context of previous work, including theirsignificance for applications to the mixing of viscous fluidsin this geometry.     

Comparison of turbulence models in simulating swirling pipe flows

Swirling flow is a common phenomenon in engineering applications. A numerical study of the swirling flow inside a straight pipe was carried out in the present work with the aid of the commercial CFD code fluent. Two-dimensional simulations were performed, and two turbulence models were used, namely, the RNG k–ε model and the Reynolds stress model. Results at various swirl numbers were obtained and compared with available experimental data to determine if the numerical method is valid when modeling swirling flows. It has been shown that the RNG k–ε model is in better agreement with experimental velocity profiles for low swirl, while the Reynolds stress model becomes more appropriate as the swirl is increased. However, both turbulence models predict an unrealistic decay of the turbulence quantities for the flows considered here, indicating the inadequacy of such models in simulating developing pipe flows with swirl.     

On the Stability of Compressible Swirling Flow

The linear stability to axisymmetric perturbations of compressible non-dissipative swirling flow is shown to be insured if a suitably defined “Richardson number” depending on the basic velocity, temperature and density fields everywhere exceeds 1/4. This result combines and generalizes in a natural way some known results for incompressible swirling flow and stratified parallel flow.     

涡旋流动的空间不稳定性分析

本文研究无粘、不可压缩流体的涡旋流动的空间不稳定性,假定扰动波的波数k=k_r+ik_i是一复数,而它的频率ω为一给定的实数。这一假定意味着扰动沿涡旋流动的轴向随距离的增长而增长,但不随时间而增长。这种扰动的产生称之为空间不稳定性;与之相对应的是时间不稳定性,扰动波的波数k为一实数,而频率ω=ω_r+iω_i是一复数。本文的结果表明空间不稳定性分析是全面认识涡旋流动不稳定性的一种有用的工具。     

慢扩张旋转流的稳定性分析（Ⅰ）—理论研究

本文研究了无粘不可压慢扩张旋转流的稳定性问题，采用多重尺度展开法对有慢扩张的旋转流的非对称扰动进行浅化稳定性研究，导出了零阶及一阶扰动模所应满足的微分方程及由于慢扩张引起振幅变化的控制方程，将Ｐｌａｓｃｈｋｏ关于慢扩张喷流的结果推广到具有慢扩张的旋转流情况。     

Theoretical model for swirling thin film flows inside nozzles with converging-diverging shapes

A quasi-one-dimensional model was developed to describe a swirling, thin, liquid film inside nozzles with different wall profiles. The model quantifies the effects of swirl strength, initial film thickness, and Reynolds and Weber numbers on the film thickness along the nozzle surface. Moreover, the model allows for a rapid (at least, qualitative) evaluation of different effects, e.g. of the swirl strength and nozzle geometry, and can serve as a benchmark case for the subsequent more involved numerical simulations. Steady-state solutions are presented as a function of various parameters. The effect of the nozzle geometry on film thickness is explored. As swirling flow entered the expanding (diverging) section of the nozzle, film thickness decreased to satisfy continuity (to conserve mass). Conversely, film thickness increased upon entering the contracting (converging) region of the nozzle. Geometric effects controlled film thicknesses much more than other flow parameters. This quasi-one-dimensional model for a swirling thin film can be useful for designing a swirl jet used in various industrial applications.     

同心圆管间无粘可压缩旋转流动的稳定性研究

本文主要研究了两个同心圆管之间无粘可压缩旋转流动的稳定性问题.首先推导出了关于径向扰动速度分量的可压缩线化微分方程.利用类似于Ludwieg的分析方法,推导了可压缩旋转流的两个稳定性准则.然后用有限差分方法数值求解了本征值问题,给出了时间增长率,并验证了稳定性准则的正确性.最后讨论了压缩性对稳定性的影响.     

The limiting vortex in the similarity solution for a swirling flow

It is known that the similarity solution for a viscous swirling flow over a stationary disk does not exist if the driving vortex far away from the disk is a potential vortex, while the solution exists for a rigid body vortex. Previously, the breakdown has been determined to occur if the azimuthal velocity of the driving vortex decreases faster than a certain power of the radial distance from the axis of symmetry. The decay parameter at which the similarity solution ceases to exist is computed here by a more direct method, and the reason for the breakdown becomes apparent. The analysis confirms (and slightly improves) the known value of the parameter. The case where the fluid, now assumed to be conducting, is subject to an axial magnetic field and the asymptotic behavior of the solution far away from the axis are also briefly discussed.     

激波在异种气体中传播及诱导的剪切混合研究

利用二阶迎风TVD格式求解多组分,层流全N－S方程,针对直通道和突扩直通道,研究了马赫数为2和4的激波在H2和空气界面上的传播及诱导的燃料剪切混合,计算结果表明：（1）直通道中,剪切层中的激波阵面要发生畸变,存在对混合起主要作用的卷吸涡,激波马赫数不同,卷吸涡结构和横向混合的尺寸也不同,激波马赫数低,剪切混合效果好,（2）在突扩直通道中,马赫数为2和4的激波在H2中产生不同强度激波,在剪切层中都能产生顺时针,尺度较大的卷吸涡,后台阶增强了剪切层的混合。