一种弹性低密度耐高温隔热涂层

针对固体火箭发动机实际使用的热环境要求,研制了一种弹性低密度耐高温隔热涂层,通过石英 灯辐射和电弧风洞试验对其进行了防热性能考核。该涂层密度为0. 62 g/ cm3,伸长率为25%,热导率为0． 18 W/ (m·K);在401℃时DSC 失重率仅为6. 6%;验证考核表明,采用1. 0 mm 涂层时,壳体与涂层界面温度最高 为77. 3℃,壳体背温度最高为44. 5℃。     

启动过程推力器喷注管内推进剂流的温降

根据空间发动机的总体结构、环境特点和能量守恒原理,提出推进剂在推力器喷注管内流动降温的简化数理模型,研究启动时单元推进剂在推力器喷注管内的流动降温现象.耦合求解推进剂流和喷注管能量方程,可以获得单元推力器喷注管单推三流整体温度的沿程分布规律.用推进剂模拟液实际考察和验证推力器喷注管的流动特点和理论模型的计算结果,分析推进剂流速、喷注管长度和内径对推进剂流温度变化的影响,导出推进剂流前缘出口温度和这3个物理参量间的拟合关系式.研究结果对推力器的热控设计有参考价值.     

高低温箱运行及故障分析探讨

通过对高低温箱的运行记录进行整理，分析其运行状况及故障，判断故障产生的原因，有针对性地提出故障排除的方法和设备维护保养措施，以延长设备的使用寿命。     

测控装备机内测试设备计量校准技术研究

研究测控装备机内测试设备计量校准方法，获取机内测试设备技术状态的准确信息，是确保测控装备量值准确可靠的基础。以系统理论为指导，研究测控装备机内测试设备的工作运行机理和计量校准方法，选取某型测控装备，分析其技术要求、确定校准点、校准接口和校准设备，明确计量校准项目和参数，对提出的测控装备机内测试设备计量校准方法进行实验验证，为今后开展机内测试设备计量校准提供了方法和依据。     

Experimental study on NOx emission correlation of fuel staged combustion in a LPP combustor at high pressure based on NO-chemiluminescence

Experimental investigations on NO_x emissions of a single-cup, Lean Premixed Prevaporized (LPP), module combustor were carried out at elevated inlet temperature and pressure up to 810 K and 2.0 MPa, close to the real operating conditions of aero-engine combustors. This LPP combustor adopts centrally staged fuel injections which could produce separated stratified swirling spray flame. In the NO_x emissions measurements, the ranges of dome equivalence ratio and fuel stage ratio were from 0.55 to 0.58 and 8% to 24%, respectively. The optical diagnosis on separated stratified swirling spray flame were carried out with fuel stage ratio changing from 15% to 30%. Therefore, NO* and OH* chemiluminescence images were obtained. The results show that NO_x emissions increase with the increase of the fuel stage ratio. And from the chemiluminescence images, the main flame and pilot flame are found weakly coupled. The pilot flame plays a significant role in NO_x emission production because of its higher adiabatic flame temperature. Based on the results of chemiluminescence optical tests, a new NO_x emission prediction model is proposed based on the Lefebvre’s single flame model. The estimate of local equivalence ratio of the pilot stage’s non-premixed flame is modified considering the characteristics of spray combustion, and a “PLUS” emission prediction model suitable for separated stratified swirling spray flame is obtained. Compared to the experimental data, the “PLUS” model exhibits a good prediction in a range of ±13% of deviation.     

The northern and southern mid-latitude ionospheric trough using global IGS vTEC maps

The aim of this work is the analysis of the mid-latitude ionospheric trough (MIT) using the Global Ionospheric Maps from IGS (GIMs) during the solar minimum, year 2008. This study was performed for different local times, 22, 00, 02 and 04 LT on the Northern and Southern hemisphere simultaneously. In the two hemispheres the MIT show asymmetric pattern. The high-latitude troughs are clearly distinguished in autumn and winter. Another feature is the longitudinal development towards the west of the geomagnetic pole covering a wider area in the Northern Hemisphere. Five empirical reference models were tested and compared with the MIT minimum position obtained from GIMs at different local times for both hemisphere. The results show a better agreement with the observations for the Northern Hemisphere specially with the Köehnlein & Raitt model. Fluctuations of 9 days and 27 days of the MIT minimum position are found, which could be related with the solar wind oscillations, especially for 00 and 02 LT in both hemisphere, suggesting a link between them.     

时域中低阶等效系统方法及其应用

介绍了用低阶等效系统拟配高阶飞机时间反应的新方法，该方法利用飞行试验中收集的飞机输入和输出数据识别飞机动力学特性，以变稳飞机ＮＴ－３３Ａ飞行试验为例，预测和评定了不同构形情况下的有关飞行品质，并与带宽准则估计结果和实际驾驶员评定进行了比较，结果证明该方法适用于飞行试验中飞行品质的评定。     

典型散射体低频特性估计

本文探讨了几种典型金属物体的低频散射问题。介绍了低频散射截面的计算方法；对计算结果进行了分析；并就雷达目标低频散射特性提出了作者的观点。     

基于化学反应器网络模型法的预混气组分对NOx反应路径影响研究

摘 要：为探究预混气组分对不同反应路径下NOx生成影响,针对高压射流反应器,基于CFD流场特征等,构建优化了单PSR、2PSR、3PSR以及PSR+PFR四种化学反应器网络模型。在贫预混燃烧条件下,研究了纯CH4及其混合气燃烧时不同反应路径下NOx的生成情况,得出了燃烧室内不同反应区域每条反应路径NOx的生成量。结果表明,纯CH4燃烧产生的NOx主要来自于热力型、快速型和N2O-中间体型三条反应路径。绝热火焰温度的提高主要促进了热力型和N2O-中间体型NOx的生成。随着CH4或CO中加入H2摩尔分数的增加,NOx排放总量降低,快速型NOx生成速率降低,特别是火焰刷区域的。另外,混合气中CO摩尔分数的增加会导致NOx生成量增多。     

Latitude and solar-cycle dependence of radial IMF intensity

I describe a simple procedure for extrapolating the observed solar magnetic field into the heliosphere, which averages the asymptotic fields computed using the standard source surface and current sheet models. The resultant field is characterized by strong latitudinal gradients (maintained by volume currents outside the source surface) and by abrupt reversals in direction at the current sheets. The model yields good agreement with the observed long-term variation of the radial IMF component in the ecliptic, and is used to predict the variation of |B _r | along the latitudinal trajectory of Ulysses during 1990–1994. As found in earlier studies, the magnitude ofB _r at any latitude is determined largely by the strength and relative orientation of the Sun's dipole moment.