随机函数的几乎处处中心极限定理

设{X_n,n≥1}是独立同分布随机变量序列,EX_1=0,EX_1~2=1．设S_n=∑_i~n=1 X_i,T_N=T_N(X_1,…,X_n)是随机函数且T_N=AS_N+R_n．我们证明若supE|R_n|＜∞,R_n=o n~(1/2)a．s．或R_n=O(n~(1／2-2γ))a．s．(0＜γ＜1／8),则对随机函数T_n几乎处处中心极限定理(简记为ASCLT)和函数型几乎处处中心极限定理(简记为FASCLT)成立．由此作为推论,可得对U统计量、Von-Mises统计量、线性过程、移动平均过程、线性模型中误差方差估计、功率和、连续分布函数的乘积极限估计和分位点函数的乘积极限估计等均成立着ASCLT和FASCLT．     

NEW WAVELET BASES FOR NON－HOMOGENEOUS SYMBOLIC SPACE OpS1,1^m AND RELATED KERNEL－DISTRIBUTION SPACES

This paper constructs several classes of new wavelet bases, which are unconditional bases for related operator spaces. Using these bases, the author analyzes non-homogeneous symbolic space OpSm1,1 and two related kernel-distribution spaces, and characterizes them in two wavelet coefficients spaces. Besides, some properties for singular integral operators are studied.     

催化剂薄层内甲烷水蒸气重整反应强化管内对流换热的数值模拟

本文以竖直圆管内壁催化剂薄层内发生甲烷水蒸气重整反应强化对流换热作为研究对象,对其进行了数值模拟．结果发现,催化剂薄层内的吸热化学反应可以有效地强化对流换热,降低流体和壁面温度,从而对壁面起到保护作用;极限热流密度的大小与流体的入口温度有关,存在最佳入口温度使极限热流密度最大．     

时变线性系统特征根判稳的推广

本文研究了二维时变线性系统零解的稳定性，给出了一些允许系数矩阵主对角元变号，系数矩阵特征根变号的判定稳定性的充分条件。     

模糊对向传播网络数据融合目标识别方法

重点研究了模糊对向传播网络 (FCPN)模型。针对数据融合和目标识别的特点 ,提出了基于模糊对向传播网络的融合目标识别方法和改进的模糊对向传播网络 (MFCPN)融合结构。利用仿真数据对网络的训练算法和融合结构进行了实验研究。结果表明 ,模糊对向传播网络较误差后向传播网络 (BPN)能够有效地实现融合识别 ;改进的模糊对向传播网络融合结构是可行的。同时还对FCPN和MFCPN应用于前视红外 (FLIR)和可见光摄像机目标跟踪系统进行了应用研究。     

A Facile Synthesis of α-Phenylthio-α,β-Unsatuated Esters

α-phenylthio-α，β-unsaturated esters 6 were synthesized by Witting reaction of 3.which were prepared by a phenylsulfenyllation-trans-ylidation reaction.     

稀土甘氨酸咪唑配合物[RE(Gly)4(Im)(H2O)](ClO4)3的热化学研究

采用溶解-反应量热法在具有恒温环境的溶解-反应热量计内,测定了[Gd(Gly)4(Im)(H2O)](ClO4)3和[Y(Gly)4(Im)(H2O)](ClO4)3两种稀土甘氨酸咪唑配合物的标准生成焓分别为(-3 461.46 ±0.22) kJ·mol-1 和(-3 926.6±0.90) kJ·mol-1.     

矩阵法拟定化学反应机理软件

本软件是根据Happel和Sellers提出的矩阵法编制的。用户只需输入基元反应方程式及其系数矩阵,即可得出全部动力学上有意义的反应路线。本软件不但可用于单一总反应的物系,也可用于多个总反应的物系,既适于均相反应,也适于非均相反应。它是拟定化学反应机理的有力工具。本软件用BASIC语言编写,由DOS3.3以上版本支持,可在APPLE-Ⅱ及其兼容机上运行,使用十分方便。     

ON THE ASYMPTOTIC BEHAVIOUR OF THE STEADY SUPERSONIC FLOWS AT INFINITY

This paper studies the asymptotic behaviour of steady supersonic flow past a piece-wise smooth corner or bend. Under the hypothese that both vertex angle and the total variation of tangent along the boundary are small, it is shown that the solution can be obtained by a modified Glimm scheme, and that the asymptotic behaviour of the solution is determined by the velocity of incoming flow and the limit of the tangent of the boundary at infinity.     

BOUNDEDNESS OF MAXIMAL SINGULAR INTEGRALS

The authors study the singular integrals under the Hormander condition and the measure not satisfying the doubling condition. At first, if the corresponding singular integral is bounded from L2 to itself, it is proved that the maximal singular integral is bounded from L∞to RBMO except that it is infinite μ-a.e. on Rd. A sufficient condition and a necessary condition such that the maximal singular integral is bounded from L2 to itself are also obtained. There is a small gap between the two conditions.