径向圆跳动误差的最小二乘评定数学模型和微机数据处理

用传统的测量方法只能得到被测零件的径向圆跳动误差的近似值。为了得到该项误差的准确值，需要研究新的测量方法。建立了径向圆跳动误差最小二乘评定数学模型，并编制了高级语言数据处理程序。在万能工具显微镜上获得了采样数据，给出了计算结果。     

附加粘弹性阻尼齿轮结构的阻尼计算

本文结合模态应变能理论与20节点有限元方法,提出了一种附加粘弹性阻尼结构损耗因子的计算模型和方法。以某实际齿轮附加阻尼结构为例,进行阻尼计算,研究了如何提高阻尼处理的效率,并得到相应实验的验证。该方法克服了已有粘弹性阻尼结构计算方法只能对简单理想结构建模的局限性,能够简便有效地应用于实际粘弹性阻尼结构的阻尼预测和优化。这对阻尼的工程应用具有较大的理论和应用价值。      

细长旋成体大迎角绕流的背涡结构与压力脉动特性

在亚临界流动范围内,通过尖拱细长旋成体在无侧滑状态下的脉动压力测量,对大迎角下细长旋成体非对称背涡结构沿轴向的压力脉动特征进行了研究分析,揭示了压力的脉动幅度与频率沿旋成体轴向的变化规律及其与背涡结构之间的对应关系,并对压力脉动特征沿轴变化的原因进行了初步探讨.     

基于局部Neymark分解的混沌信号与噪声的分离方法

从动力系统和几何的观点出发,提出了基于局部Ｎｅｙｍａｒｋ分解的混沌信号与噪声的分离方法。该方法在一个局部的轨道空间内进行Ｎｅｙｍａｒｋ分解,重构时消除由噪声引起的在某些方向上的错误分量,接着进行反嵌入,使得这一由于噪声影响而发生畸变的局部轨道得以纠正,达到混沌信号与噪声分离（以下简称混沌滤波）的目的,并对其中的反嵌入问题作了较为深入的讨论,仿真实验表明了本方法的有效性。     

位相物体的三维非对称温度场的重建

采用卷积背抽影公式实现了位相物体的三维非对称温度场的重建,为光线偏／折测量三维非对称温度场提供了高精度分析和处理实验数据的方法。     

Time Sequence Change-Point Model of Electrostatic State Parameters of Aircraft Engine

Electrostatic monitoring technology of particle charging information can facilitate online monitoring of aero-engine,which effectively enhances engine fault diagnosis and health managements.Unlike traditional engine state monitoring technologies,aircraft engine monitoring by gas path electrostatic monitoring not only covers the predicted information source itself,but also detects the information that can provide an early warnings for initial fault states through gas path charging levels.This paper establishes a non-stationary time sequence change-point model for anomaly recognition of electrostatic signals based on change-point theory combined with difference method of non-stationary time series.Finally,electrostatic induction data were utilized by the engine life test for a particular aircraft to validate the proposed algorithm.The results indicate that the activity level and the event rate were0.5—0.8(nc)and 50%,respectively,which were far greater than 4—12(pc)and 0—4% under normal working conditions of the engine.     

Space experiments aboard the Lomonosov MSU satellite

At present, the Institute of Nuclear Physics of Moscow State University, in cooperation with other organizations, is preparing space experiments onboard the Lomonosov satellite. The main goal of this mission is to study extreme astrophysical phenomena such as cosmic gamma-ray bursts and ultra-high-energy cosmic rays. These phenomena are associated with the processes occurring in the early universe in very distant astrophysical objects, therefore, they can provide information on the first stages of the evolution of the universe. This paper considers the main characteristics of the scientific equipment aboard the Lomonosov satellite.     

Influence of Trapped Plasma on the Structure of Collisionless Thin Current Sheets

Using both analytical and numerical models of the collisionless anisotropic current sheet generated by the impinging flows of transient ions, we have studied the self-consistent solutions taking the plasma trapped in the sheet into account. It is demonstrated that there exists a limited window in the space of system parameters where self-consistent solutions can exist. When the density of the quasi-trapped plasma is sufficiently large, a redistribution of the total current can be a cause of the sheet decay, when the local current of the trapped particles compensate (totally or in part) the main current in the center and at the edges of the sheet, while the total current generated by ions on the trapped trajectories vanishes.