螺旋弹簧应力松驰实验研究

对导弹弹体及发动机中常用的压缩螺旋弹簧进行应力松驰实验研究，得到了这种弹簧在常温下长期贮在职的应力松驰方程，为导弹武器系统的质量评判和延寿提供了可靠的实验依据。     

阵风缓和系统的组合控制规律

 本文给出具有阵风缓和和其他主动控制功能的组合控制规律。阵风缓和用测量阵风方法的开环控制。当缓和输出量时,闭环控制用以稳定阵风缓和系统并满足其他主动控制要求。本文用一组合的二次型性能指标,得到最优反馈控制规律与测量阵风的组合的控制规律。文末并附有算例。     

电磁轴承及其应用 第二部分 电磁轴承工作原理和设计要点

第一部分简述了电磁轴承及电传动技术在国内外的发展及其在航空领域的应用前景.第二部分介绍了燃气涡轮发动机用电磁轴承的设计要求和主要设计问题及其解决方法.     

管流转捩对比态定律的讨论：层,紊流并存流态转捩现象

转捩对管内流动和换热有很大影响，Ｎ．Ｔ．Ｏｂｏｔ曾在总结归纳圆管、矩形管、三角形管和环形管实验结果的基础上提出对比态定律，并断言：对任意截面管道，只要知道临界摩擦因子和临界雷诺数，根据对比态定律，就可以计算其流动和平均换热特性。本文通过对复杂截面通道流动的研究，指出管流转捩的对比态定律只适用于单一流态管流，而不适用于层、紊流并存管流，文中还分析了层、紊流并存现象及其产生的原因，它的起始点和终止点的判定，以及流动和换热特性计算的处理方法。     

New VF-power system architecture and evaluation for future aircraft

Conventional aircraft power system is a constant-frequency (CF) supply based on mechanical-regulated constant-speed mechanism that has relatively low efficiency. Replacing the CF system with variable-frequency (VF) power improves overall efficiency, and reduce the system's weight and volume. However, this creates a new tier of requirements and design challenges. Novel VF-power architecture is developed with minimization of the power losses throughout the stages of power conversions. Optimal partitioning and grouping of onboard AC loads has been discussed with specific system data. New VF-input multi-functional power converters are also briefly discussed.     

全顺汽车车身涂装底漆线投槽工艺

从配方、操作方法、原理等方面介绍了全顺汽车车身涂装底漆线的投槽工艺。较为详细的介绍了涂装前处理工艺和电泳工艺部分的清洗工序。本文对水质的影响也做了简要的分析。     

区域空中交通流量控制研究

运用排队论思想，结合区域控制的特点建立了区域流量控制模型，分析了郑州区域管制中心实施流量控制的实际效果，研究结果表明，仅考虑单独区域流量控制，将使航班延误的不利影响逐级放大，理想的流量控制应该全面考虑所有受影响的区域，合理地选择控制时段和控制间隔，最大限度地利用空域资源，减少航班延误，保证空中交通的安全畅通。     

粗糙表面偏振二向反射分布函数的影响参数及其反演

针对目标偏振二向反射特性研究中模型参数难以准确确定的问题,分析了粗糙表面偏振二向反射分布函数的影响参数,并通过理论推导和仿真计算,研究了各参数对粗糙表面散射特性的作用机理。总结分析了现有参数反演方法,针对现有方法存在的理论缺陷,在P-G(Preist-Germer)模型的基础上,提出了利用"相对偏振分量-角度"的相关关系进行参数反演的方法,设计了参数反演算法,进行了标准反射板和绿漆表面的偏振二向反射特性测试实验,并根据实验数据进行了参数反演和模型验证。实验结果表明,改进的参数反演方法可准确反演所有模型参数。利用反演参数进行模型验证,结果显示模型预测数据与实验数据具有较好的吻合度,验证了模型的准确性。     

基于AFAS 软件的机翼壁板耐久性分析及试验验证

随着航空工业的发展,对机翼壁板耐久性分析的精确性及计算速度的要求日益提高,必须考虑从手工计算到程序计算的转变。飞机结构耐久性分析软件系统(AFAS)是为了满足飞机结构耐久性分析的工程实际使用要求而编制的。本文介绍采用该软件中包含的DFR方法计算程序对机翼壁板结构进行耐久性分析的过程,并进行试验验证,分析得到的机翼壁板结构具有95%置信度、95%可靠度的可靠性寿命与试验统计结果非常相近,证明AFAS是一个可以进行耐久性分析的快速准确的计算工具。     

Complexity,Forced and/or Self-Organized Criticality,and Topological Phase Transitions in Space Plasmas

The first definitive observation that provided convincing evidence indicating certain turbulent space plasma processes are in states of ‘complexity’ was the discovery of the apparent power-law probability distribution of solar flare intensities. Recent statistical studies of complexity in space plasmas came from the AE index, UVI auroral imagery, and in-situ measurements related to the dynamics of the plasma sheet in the Earth's magnetotail and the auroral zone. In this review, we describe a theory of dynamical ‘complexity’ for space plasma systems far from equilibrium. We demonstrate that the sporadic and localized interactions of magnetic coherent structures are the origin of ‘complexity’ in space plasmas. Such interactions generate the anomalous diffusion, transport, acceleration, and evolution of the macroscopic states of the overall dynamical systems. Several illustrative examples are considered. These include: the dynamical multi- and cross-scale interactions of the macro-and kinetic coherent structures in a sheared magnetic field geometry, the preferential acceleration of the bursty bulk flows in the plasma sheet, and the onset of ‘fluctuation induced nonlinear instabilities’ that can lead to magnetic reconfigurations. The technique of dynamical renormalization group is introduced and applied to the study of two-dimensional intermittent MHD fluctuations and an analogous modified forest-fire model exhibiting forced and/or self-organized criticality [FSOC] and other types of topological phase transitions. This revised version was published online in August 2006 with corrections to the Cover Date.