CLVD 法制备C/C复合材料工艺探索研究

研究了采用化学液气相沉积法制备C／C复合材料的工艺过程，分析了不同预制件、温度、浸泡时间等工艺参数对致密速度、效果的影响，并总结出了一套快速高效的致密方法。     

The Primordial Helium-4 Abundance from Observations of a Large Sample of Blue Compact Dwarf Galaxies

We use a sample of 45 low-metallicity H II regions in blue compact dwarf (BCD) galaxies to determine the primordial helium abundance YP with a precision better than 5%. We have carefully investigated the physical effects which may make the He I line intensities deviate from their recombination values such as collisional and fluorescent enhancements, underlying He I stellar absorption and absorption by Galactic interstellar Na I. By extrapolating the Y vs. O/H and Y vs. N/H linear regressions to O/H = N/H = 0, we obtain YP = 0.244±0.002 and 0.245±0.001, respectively, higher than previous determinations (YP = 0.230 - 0.234). Part of the difference comes from the fact that previous investigators have not taken into account underlying He I stellar absorption, especially in the NW component of the BCD I Zw 18 which, because of its extremely low metallicity plays a key role in the determination of YP. We derive a slope dY/dZ = 2.3±1.0, considerably smaller than those derived before. With this smaller slope and taking into account the errors, chemical evolution models with an outflow of well-mixed material can be built for star-forming dwarf galaxies which satisfy all the observational constraints. Our YP gives _bh ₅₀ ² = 0.058±0.007,f consistent with the lower limit set by dynamical measurements and X-ray observations of clusters of galaxies. It is also consistent, within the framework of standard big bang nucleosynthesis theory, with measurements of primordial 7Li in galactic halo stars and with the D/H abundance measured in absorption systems toward quasars by Burles and Tytler (1997).     

小不对称物体配平性能风洞实验研究

用阶跃响应法,在风洞中测量小不对称物体配平性能的实验原理、实验装置、数据处理及部分实验结果。 模型支承于空气静压轴承。在模型内部设有电磁机构,在一次吹风中,可以阶跃方式多次提供不对称量。由高精度、非接触的感应同步器数字测量模型俯仰角变化历程。用修正Newton-Raphson法处理数据,求出小不对称量引起的配平角δ_o、俯仰力矩C_mo和气动刚度C_ma、气动阻尼C_mq等参数。 对11°斜切锥,钝度比分别为0.06及0.16的模型进行了风洞实验。实验M数为33.5和4。实验结果表明,所采用的实验原理、设备及方法可提供较好的精度及分辨率。实验还求出了配平性能(δ_o,C_mo)以及C_ma,C_mq随M数的变化。     

弹道跟踪数据野值剔除方法性能分析

弹道跟踪数据中的野值会影响导弹目标定位精度。对用于弹道跟踪数据的野值剔除方法进行了综述。结合事后和实时两大类处理模式,分析了各野值剔除方法在理论和工程应用上的优缺点,给出了实际应用时的限制因素,建立了野值判决准则和相应的野值剔除实现步骤。仿真结果表明:野值剔除方法可以有效提高弹道跟踪数据的精度。事后处理模式中,基于格拉布斯准则的野值剔除效果最佳;实时处理模式中,基于自适应门限的五点线性预报法野值剔除效果相对较好,且时间复杂度相对较低,适合实时处理。     

Investigations into sensing characteristics of circular thin-plate electrostatic sensors for gas path monitoring

Circular thin-plate electrostatic sensors are promising in gas path monitoring due to their advantages of non-intrusiveness and easy installation. The spatial sensitivity and filtering effect are two important performance parameters. In this paper, an analytically mathematical model of induced charge on a circular thin-plate electrode is first derived. Then the spatial sensitivity and filtering effect of the circular electrostatic sensor are investigated by numerical calculations. Finally,experimental studies are performed to testify the theoretical results. Both theoretical and experimental results demonstrate that circular thin-plate electrostatic sensors act as a low-pass filter in the spatial frequency domain, and both the spatial filtering effect and the temporal frequency response characteristics depend strongly on the spatial position and velocity of the charged particle. These conclusions can provide guidelines for the optimal design of circular thin-plate electrostatic sensors.     

基于面板数据模型的中西部地区加工贸易升级研究

我国经济高速发展,劳动力、土地等要素随之发生转变,加工贸易从东部地区向中西部地区转移,中西部地区加工贸易急需升级以适应发展。利用2001-2011年中西部地区部分省份的面板数据建立计量模型,通过检验对混合估计模型、固定效应模型和随机效应模型进行选择,并对选定模型的估计结果进行具体分析,提出中西部地区加工贸易升级的对策及建议。     

民航安全经济学研究的基本架构和意义

从一般经济学的投入、成本和效益的基本思路进行探讨，阐述了民航安全经济学研究的基本内容、研究方法，指出了民航安全经济学的基本特点，分析了研究民航安全经济学的意义与价值，勾勒了民航安全经济学研究的基本框架。     

经营多角化的结合效应与度量

经营多角化多年来一直是产业经济学家和政策制定者关注的焦点之一。本文对如何取得多角化经营的结合效应作了分析,并给出了经营多角化的度量方法。     

化学气相沉积/渗透技术综述

综述了化学气相沉积技术的最新发展，包括金属有机化合物化学气相沉积，等离子辅助化学气相沉积，激光化学气相沉积；同时介绍了三种用于制备工程材料的快速致密化化学气相渗透技术，包括强迫流动热梯度化学气相渗透，化学液相沉积，感应加热热梯度快速致密化技术。     

民机高速风洞试验的阻力雷诺数效应修正

在飞机设计阶段,获得准确的气动特性数据对设计者是十分重要的,采用缩比模型的风洞试验是主要途径之一。但是风洞条件限制了试验的Re数,从而影响了对跨音速巡航阻力的评估,因此需要对风洞试验结果的阻力进行Re数效应修正。分析了风洞试验结果阻力的误差构成,提出了Re数效应修正的风洞试验数据基础;进一步就跨音速巡航阻力的构成进行分析,论述了对最小阻力和升致阻力分项修正的方法,并对修正结果进行了验证,得到了一种可靠的工程方法。