Aerodynamics of indirect thrust measurement by the impulse method

The aerodynamic aspects of indirect thrust measurement by the impulse method have been studied both experimentally and numerically. The underlying basic aerodynamic principle is outlined, the phenomena in subsonic, supersonic and arc-heated jets are explored, and factors affecting the accuracy of the method are studied and discussed. Results show that the impulse method is reliable for indirect thrust measurement if certain basic requirements are met, and a simple guideline for its proper application is given.     

Test analysis of detection of damage to a complicated spatial model structure

A two-stage damage detection approach is proposed and experimentally demonstrated on a complicated spatial model structure with a limited number of measurements. In the experiment,five known damage patterns,including 3 brace damage cases and 2 joint damage cases,were simulated by removing braces and weakening beam-column connections in the structure. The limited acceleration response data generated by hammer impact were used for system identification,and modal parameters were extracted by using the eigensystem realization algorithm. In the first stage,the possible damaged locations are determined by using the damage index and the characteristics of the analytical model itself,and the extent of damage for those substructures identified at stage I is estimated in the second stage by using a second-order eigen-sensitivity approximation method. The main contribution of this paper is to test the two-stage method by using the real dynamic data of a complicated spatial model structure with limited sensors. The analysis results indicate that the two-stage approach is ableto detect the location of both damage cases,only the severity of brace damage cases can be assessed,and the reasonable analytical model is critical for successful damage detection.     

M/M/1算子的其它特征值

证明对一切θ∈（0,1）,θ（2（λμ）~（1/2）-λ-μ）都是偏微分方程形式的M/M/1排队模型主算子的几何重数为1的特征值.     

含分布时滞递归神经网络的一般衰减同步

对具有分布时滞的递归神经网络模型进行了研究,并通过构造适当的Lyapunov-Krasovskii函数和非线性控制函数,采用不等式估计方法,得到了所研究模型一般衰减同步的充分条件.最后给出了一个例子,进一步说明了所得结论的正确性.     

超导微电子学

本文巧妙地借助于摆的类比对超导微电子学的基础──约瑟夫森效应作了描述和说明．在此基础上讨论了单约瑟夫森结以及超导量子干涉器件的工作原理和应用，论述了超导微电子器件在灵敏度和速度上的巨大优越性及其在制作超高速超导计算机方面的应用前景．     

论光滑粒子流体动力学(SPH)方法

“光滑粒子流体动力学(SPH-SmoothedParticleHydrodynamics)”是近20多年来发展起来的一种新的纯Lagrange方法.SPH是一种质点方法,有点类似质点网格法,但根本的不同点在于SPH方法中计算空间导数时不需要使用任何网格,而被插值公式中的解析微分式子所替代,从而避免了高维拉氏差分网格法中网格缠结和扭曲等最令人头痛的问题.这种方法另一个突出的优点是表现在对缺乏对称性和内含真空的三维系统的计算特别有效.因为利用网格建立的所有传统的差分方法,随着网格数目的增加,到了三维情形变得难以招架,真空区域的网格剖分造成内存储量的大量浪费又实在令人可惜,而SPH恰能克服上述的缺点.本论文重点介绍了该方法的理论基础和SPH执行过程等有关问题.     

H∞分散控制系统范数计算的模态综合法(Ⅱ)

在大系统控制中，H∞分散控制方法将整个系统划分成一系列子系统分别研究，然后综合设计大系统的分散控制器，这与结构力学中的子结构分析技术类似．本着这一思想建立了分散H∞控制与子结构振动分析的模拟关系、分散控制系统的最优H∞范数与整体结构一阶本征值之间的对应关系，进而利用结构力学中的模态综合法和扩展Wittriek-Williams算法计算这一参数．论的第(Ⅰ)部分主要介绍系统H∞控制及其本征函数的正交性和展开定理；第(Ⅱ)部分介绍分散控制系统最优H∞范数计算的模态综合法及数值算例。     

Φ-INEQUALITIES AND LAWS OF LARGE NUMBERS OF HARDY MARTINGALETRANSFORMS

In[101,GarlinghasintroducedtheAUMDpropertyofComplexBanachspaceusinginequalityofmartingaletransforms,somefactsshowwhichdiffersfromUMDpropertyofrealBanachspaceintroducedbyBurkholder[6].GarlingalsoprovedthatAUMDpropertyimpliessuperreflexivityandARNP.In[13],XuprovedHMT.isequivalenttoAMT.thatistheBanachspacesforwhicllHardymartingalesconvergeunconditiollallyarethoseforwhichanalyticmartingalesconvergeunconditionally.Hardymartingalesandanalyticmartingalesformaspecialclassofmartingalesforwh…     

平面运动学位似运动Steiner公式的推广

对单参数闭平面复意义位似运动，给出了Muller提出的Steiner公式和混合面公式的表达式。利用推广的Steiner公式得到了位似运动的Holditch定理．作为特例，给出了Muller位似比h≡1时的结果。     

组合最优化中的布尔方法

本文旨在从NP-完全性理论的角度,以拟布尔函数最优化为典型实例介绍组合最优化问题的一些研究方法和取得的主要进展。并且也提出了一些有待解决的问题和可能的研究途径。