空中交通管制商业化的利与弊

自新西兰率先使其空中交通管制服务(ATS)商业化,即公司化以来,8年已经过去了.在这期间世界上出现了几种类型的空管商业化形式.空管商业化已成为全球90年代和20世纪初的发展趋势.空管的效率可能会由于商业化而得到提高.然而,它对用户收费的长远影响却很难推测,因为商业化使一些国家中的收费减少,但使另一些国家中的收费大为增加.安全性也是一个值得注意的问题.而且,人们普     

因子分析方法在商业银行经营效率评价中的应用

应用因子分析方法对我国13家商业银行的经营效率进行了实证研究，通过因子评分，测度了商业银行的经营效率，指出各商业银行由于内部控制能力不高和风险承担能力较低而导致经营效率不理想，各商业银行应努力优化资源配置和不断进行金融创新，以应对激烈的国内外竞争。     

我国上市商业银行财务竞争力评价

为了对我国上市商业银行财务竞争力进行系统的综合评价,建立了包括资本状况、资产质量、盈利能力以及流动性在内的四个方面的指标体系。采用因子分析的方法,对我国18家上市商业银行财务竞争力进行了实证分析,并对其进行了排名,最后结合分析结果提出了提高银行财务竞争力的应对措施。     

浅谈基层商业银行企业文化的构建

在我国商业银行加快与国际接轨的今天，如何用先进的金融企业文化来助推经营工作快速发展，并实现可持续发展目标，是基层商业银行目前必须考虑的问题。从我国基层商业银行企业文化建设中存在的问题入手。有的放矢地提出了如何构建基层商业银行企业文化的对策。     

我国商业银行拆入资金业务内部控制体系研究

资金拆入是指商业银行因资金周转需要而在金融机构之间借入资金的行为，是商业银行的一项常规性业务，拆入资金业务内部控制是我国商业银行内部控制体系中的一个重要组成部分。拆入资金业务内部控制体系可以为我国商业银行加强拆入资金业务管理、提高拆入资金业务的运作效率提供可靠的理论借鉴。我国商业银行拆入资金业务内部控制体系的设计必须密切联系我国商业银行拆入资金业务的运作实践。因子分析可以为理论模型提供现实性检验，从而展现我国商业银行拆入资金业务内部控制的现实性微观机理。     

辽宁高校科技资源的状况及潜力分析

针对高等院校作为国家技术创新体系的重要组成部分，在区域经济发展中占有重要地位这一实际，立足于辽宁高校对地方经济发展的重要作用，对辽宁高校科技资源的规模、分布等现状进行了分析研究，明确辽宁高校具有明显的人才优势、雄厚的科研资源与科研成果资源，集合优势明显、产业化能力强等丰富的资源潜力，提出了建立先进的高等教育信息化平台，实现教育、科技资源共享，对科技成果资源的转化采用商业化运作模式，加强政府积极引导以及建立与完善共享科技资源的配套服务等几点设想。     

管理会计在我国商业银行应用中的问题及对策

随着国际金融自由化影响的加剧和我国金融管制的逐步解除,商业银行由于产品的趋同面临着巨大的竞争压力。而管理水平的高低是评价银行有无发展潜力的重要标尺。管理会计作为银行经营管理中极其重要的工具之一,其水平的高低往往决定着银行内部经营管理的质量。从我国商业银行应用管理会计的现状出发,详述商业银行管理会计的价值、应用的必要性,并指出面临的问题及解决的对策。     

用扩散连接法连接不同的金属

用扩散连接法连接不同的金属有些不同的金属依靠常规手段（如焊接）不能连接在一起，美国核金属公司（ＮＭＩ）正在把连接两种个同金属无缝管的独特方法推向商业化。例如在低温燃料系统中，几个用不同材料制成的的罐，必须尽可能以无缝方式连接。两种不同金属，如钛和不锈...     

基于正外部性的我国农业保险问题透析

农业保险的准公共产品属性导致农业保险存在正外部性，以及由此而导致的近年来我国农业保险业务的萎缩，所以，完全商业化农业保险失灵，解决问题的根本出路在于建立“政府财政补贴推进，商业化运作”的模式，重点突出财政补贴方式，并伴随农业风险基金的建立，撑开农业保险这把大伞，保证农业经济稳定健康发展。     

机场的商业化管理

TheManagementoftheAirportBusiness所谓机场商业化管理，就是将机场由传统的以保障和服务为中心的管理，向以利润为中心的管理转化，从而建立高效、完善、科学的机场运营管理体系，增加融资渠道，提高投资回报率，以追求利润最大化做为机场的经营目标。根据我国目前机场的管理情况，笔者认为，机场在实施商业化管理过程中应从以下三个方面考虑。一、从机场资金来源考虑，要实行投资主体多元化目前，我国大部分机场仍然是政府单一投资行为，其弊端：一是加大了政府开支，增加了政府的财政压力，不利于机场的建设和发展ZH是因投资的一元化…     

The effect of inlet conditions on the flow and heat transfer in multiple rotating cavity with axial throughflow

This paper discusses experimental results from two different build configurations of a heated multiple rotating cavity test rig.Measurements of heat transfer from the discs and tangential velocities are presented.The test rig is a 70% full scale version of a high pressure compressor stack of an axial gas turbine engine.Of particular interest are the internal cylindrical cavities formed by adjacent discs and the interaction of these with a central axial throughflow of cooling air.Tests were carried out for a range of non-dimensional parameters representative of high pressure compressor internal air system flows(Re up to 5×106 and Rez up to 2×105).Two different builds have been tested.The most significant difference between these two build configurations is the size of the annular gap between the(non-rotating) drive shaft and the bores of the discs.The heat transfer data were obtained from thermocouple measurements of surface temperature and a conduction solution method.The velocity measurements were made using a two component,LDA system.The heat transfer results from the discs show differences between the two builds.This is attributed to the wider annular gap allowing more of the throughflow to penetrate into the cavity.There are also significant differences between the radial distributions of tangential velocity in the two builds of the test rig.For the narrow annular gap,there is an increase of non-dimensional tangential velocity V/Ωr with radial location to solid body rotation V/Ωr=1.For the wider annular gap,the non-dimensional velocities show a decrease with radial location to solid body rotation.      

Research on Auto-detection for Remainder Particles of Aerospace Relay Based on Wavelet Analysis

Aerospace relay is one kind of electronic components which is used widely in national defense system and aerospace system. The existence of remainder particles induces the reliability declining, which has become a severe problem in the development of aerospace relay. Traditional particle impact noise detection (PIND) method for remainder detection is ineffective for small particles, due to its low precision and involvement of subjective factors. An auto-detection method for PIND output signals is proposed in this paper, which is based on direct wavelet de-noising (DWD), cross-correlation analysis (CCA) and homo-filtering (HF), the method enhances the affectiv-ity of PIND test about the small particles. In the end, some practical PIND output signals are analysed, and the validity of this new method is proved.     

Preparation of Highly Dispersed Antimony-doped Tin Oxide Nano-powder via Ion-exchange Hydrolysis of SnCl4 and SbCl3 and Azeotropic Drying

Antimony-doped tin hydroxide colloid precipitates have been synthesized by hydrolysis of SnCl4 and SbCl3 using: (1) an ion-exchange hydrolysis to remove chlorine ions, and (2) isoamyl acetate as an azeotropic solvent to obviate water. The obtained dried powder is of high dispersivity without any need for further grinding. The size and dispersivity of the final particles are investigated with the aid of TG-DTA, BET, XRD and TEM. After having calcined, the antimony-doped tin oxide nanopowder possesses a tetragonal rutile structure with high dispersivity, uniform particles and low hard agglomeration.     

Effects of Mo on the Microstructure and Hydrogen Sorption Properties of Ti-Mo Getters

The effects of Mo on the microstructure evolution, porosity and hydrogen sorption properties of Ti-Mo getters are investigated in this work. The results show that the addition of Mo prolongs the densification process of Ti-Mo getters and results in a significant amount of sintered pores. With the Mo content increasing, the porosity of getters firstly increases reaching the maximum value as it at- tains about 7.5wt.%, and then drops. At the room temperature, the hydrogen sorption property of getters increases progressively with the Mo content increasing, but the tendency is not very clear before its content lies below 2.5wt.%. When the Mo content achieves about 7.5wt.%, the hydrogen sorption property proves to be the best. The discussion is made about the above mentioned phenomena inclusive of hydrogen sorption properties of getters under different activation conditions (from 500-750 ℃).     

超声速燃烧数值模拟中的湍流与化学反应相互作用模型

高精度数值模拟有助于理解超声速湍流燃烧中湍流与化学反应的相互作用,可为发动机燃烧室等工程应用设计提供可靠的预测模型。除直接数值模拟外,目前在湍流燃烧应用中使用的大涡模拟和雷诺平均Navier-Stokes模拟均需要借助模型模化发生在湍流小尺度上的流动与化学反应过程对湍流大尺度运动的影响。现有的湍流与化学反应相互作用模型大致可分为:火焰面类模型和概率密度函数类模型,2类模型在不同的应用中各自具有优势和局限性。此外,现有模型大都基于低马赫数燃烧,而超声速燃烧中通常会伴随快速混合、局部熄火和再着火以及激波等复杂过程,这为发展其中的湍流与化学反应相互作用模型提出了更多的挑战。     

适于低轨卫星IP网络的单核共享树组播算法(英文)

为了解决低轨卫星IP网络中现有典型源组播算法的信道资源浪费问题,本文提出了一套单核共享树组播算法,即核心群合并共享树(CCST)和加权核心群合并共享树(w-CCST)算法。CCST 算法包括动态近似中心(DAC)选核方法和核心群合并组播路径构建方法。DAC方法专为周期、规律运动的低轨卫星网络提出,不需要复杂的星上计算。在核心群合并方法中,以核节点作为初始核心群,通过核心群和剩余组成员的最短路径方法逐步扩展直至整棵组播树构建完成,从而使得组播树的树代价最小,大大提高了网络的带宽利用率和组播传输效率。w-CCST 算法中所提出的加权因子可以调整树代价和端到端传播时延之间的折衷程度,因此,可以通过调整加权因子来适度增大树代价、降低端到端传播时延以支持某些端到端时延要求苛刻的实时组播业务。最后,与低轨卫星 IP 网络中典型算法进行了性能比较,仿真结果说明,CCST 算法的平均树代价比其它算法显著降低,w-CCST 算法的平均端到端传播时延小于 CCST 算法。     

Jet Vectoring Control Using a Novel Synthetic Jet Actuator

A primary air jet vectoring control system with a novel synthetic jet actuator (SJA) is presented and simulated numerically. The results show that, in comparison with an existing traditional synthetic jet actuator, which is able to perform the duty of either “push” or “pull”, one novel synthetic jet actuator can fulfill both “push” and “pull” functions to vector the primary jet by shifting a slide block inside it. Therefore, because the new actuator possesses greater efficiency, it has potentiality to replace the existing one in various appli- cations, such as thrust vectoring and the reduction of thermal signature. Moreover, as the novel actuator can fulfill those functions that the existing one can not, it may well be expected to popularize it into more flow control systems.     

Nonlinear Adaptive Slewing Motion Control of Spacecraft Truss Driven by Synchronous V-gimbaled CMG Precession

The slewing motion control of a truss arm driven by a V-gimbaled control-moment-gyro (CMG) is a nonlinear control problem. The V-gimbaled CMG consists of a pair of gyros that must precess synchronously. The moment of inertia of the system, the angular momentum of the gyros and the external disturbances are not exactly known. With the help of feedback linearization and recursive Lyapunov design method, an adaptive nonlinear controller is designed to deal with the unknown items. Performance of the proposed controller is verified by simulation.     

An SOR Implicit Time-accurate Scheme in Calculating Unsteady Flows

A new time-accurate marching scheme for unsteady flow calculations is proposed in the present work. This method is the combination of classical Successive Over-Relaxation (SOR) iteration method and Jacobian matrix diagonally dominant splitting method of LUSGS. One advantage of this algorithm is the second-order accuracy because of no factorization error. Another advantage is the low computational cost because the Jacobian matrices and fluxes are only calculated once in each physical time step. And, the SOR algorithm has better convergence property than Gauss-Seidel. To investigate its accuracy and convergency, several unsteady flow computa- tional tests are carried out by using the proposed SOR algorithm. Roe’s FDS scheme is used to discritize the inviscid flux terms. Un- steady computational results of SOR are compared with the experiment results and those of Gauss-Seidel. Results reveal that the numerical results agree well with the experimental data and the second-order accuracy can be obtained as the Gauss-Seidel for unsteady flow computations. The impact of SOR factor is investigated for unsteady computations by using different SOR factors in this algorithm to simulate each computational test. Different numbers of inner iterations are needed to converge to the same criterion for different SOR factors and optimal choice of SOR factor can improve the computational efficiency greatly.