建立以贡献排序法为基本内容的职称评审制度--高校教师职称评审中实行贡献排序法的研究(二)

现行职称评审制度改革应当坚持公正性、可比性、科学性、导向性、易操作五个原则.应采用贡献排序法,建立多劳早晋、少劳晚晋的职称评审制度.贡献排序法量化考评体系主要包括思想政治表现、教学业绩、科研业绩、荣誉称号、其他项目五大方面.     

论学术腐败及其遏制措施

针对目前学术界,尤其是高等院校学术论文抄袭之风愈演愈烈的趋势,揭示了产生学术腐败的根源,提出高等教育的公共决策要符合中国的国情和科学发展的要求;改革现行的职称评审制度及学位评价标准.修正<著作权法>,对学术腐败者进行必要的法律制裁;加强舆论监督,加强知识分子的人格励炼,提高科技期刊编辑自身修养和拒腐能力,对上刊论文事前经学术不端文献检测系统的检测等遏制腐败的具体措施.     

国内外航空发动机研制过程中评审工作的对比分析

评审是航空发动机研制过程中一个必不可少,至关重要的阶段,组织缜密、有效地评审对于降低研制风险、缩短周期、减少反复将起到不可或缺的作用.本文分别介绍了罗罗公司对某高压压气机技术方案的评审,和国内某发动机技术设计的评审.通过对评审人员的组成、评审内容和资料的准备以及评审结论、跟踪检查的对比,分析了两次评审在评审过程、评审机制等方面的差异.     

浅谈课堂讲授艺术

目前,课堂讲授依然是教学的主要形式.因此,如何提高课堂讲授效果是提高教学质量的关键.众所周知,在教学中常有这种现象:有些知识水平较高的教师讲课却不受欢迎,而也有一些知识水平一般讲课却很受欢迎的教师,究其原因,主要是他们的教学方法及讲课艺术有差别.因此,要提高课堂讲授效果,教师必须重视教学方法及讲授艺术.本文仅就如何提高课堂讲授艺术,谈谈个人的看法.     

欧盟第七框架计划中航空项目的立项评审模式

本文就欧盟第七框架计划航空项目立项评审的专家遴选、保密要求、评审标准、评审系统、评审程序以及评审特点进行了详细说明和分析。其中一些不同于我国的立项评审模式尤其值得关注。     

上海交大——管理制度改革经验

中国高教会和北京市高教学会于4月2日举行报告会,邀请上海交大党委副书记刘克介绍该校管理制度改革的经验.刘克说:①改革要打破平均主义、吃“大锅饭”的局面,彻底解决“讲师不讲,教授不教”,人浮于事的问题.为进行必要的人员流动,要注意做好流动人员的工作,保证他们在提职、提薪、分房上不受影响.②从上到下,先机关后基层,进行定编、定员.③制定出各种教师工作规周和干部、以及教师职称晋升具体标准和各级干部的定级标准.④根据按劳分配的原则逐步进行工资制度的改革.⑤实行权力下放,扩大基层自     

关于改进提高设计评审有效性的思考

设计质量对产品质量的形成起到决定作用,而设计评审是对设计质量进行有效控制的重要手段,在实践中得到广泛应用,但实际上设计评审的贯彻实施却存在许多不足,致使执行效果大打折扣,亟待改进完善。基于此,分析当前设计评审存在的不足,给出了改进提高设计评审有效性的建议,供有关单位参考。     

歼八飞机外场可靠性信息质量问题研究

对歼八飞机外场可靠性工作作了总结。当前存在的主要问题是信息准确性差、不全面、反馈不及时、流失大等；造成这些问题的主要原因是领导重视不够、组织不健全以及信息表格不完善、信息不能及时处理、未能充分利用跟飞人员的有利条件。建议的改进途径和措施：健全可靠性信息网，制定可靠性信息标准，建立信息评审制度，实行信息计算机管理等。     

实行贡献排序法的相关建议与说明--高校教师职称评审中实行贡献排序法研究(四)

依据贡献排序法量化考评体系对高校职称参评者进行考评时,还要解决好贡献排序法的适应性问题、操作方便性问题、职称评审委员会的职责再定位问题、行政管理与党务工作者的分数补贴问题,贡献排序法本身也要不断完善.     

和谐师德传承理念——从中国传统文化看当代师德构建

当前高校师德建设中存在缺乏主流引导思想、教师职业道德的不均衡、不同步,以及师德评价指标体系不完善等问题.分析传统文化价值体系对高校师德构建的作用,并结合相应师德现状提出有关对策.     

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.