煤油燃料超燃发动机燃烧室温度测量与计算分析

为获得超燃冲压发动机燃烧室流场温度分布特性，深入分析发动机工作特性，对马赫数为2.0，总温为1100K，总压为1.0MPa的来流，利用可调谐的相干反斯托克斯拉曼散射（CARS）技术完成了直连式燃烧室流场温度测量；同时对实验状态进行了三维并行数值模拟，对比分析了计算和实验结果的差异。结果表明，隔离段温度的实验测量值与计算结果的最大相对误差约为0.8%；在燃烧室核心流区域，当量比为0.6和0.8两个状态下，实验测量值分别比计算值偏低约40K和150K，相对差异为4.2%和13%；在凹槽回流区内，当量比为0.6和0.8时实验值则分别比计算值偏低约140K和170K，相对差异为11.7%和7.5%。主喷油位置喷入当量比为0.2的燃料对燃烧室区域的温度和压力分布会产生较大影响，但对扩张段及后部区域的推力性能不会产生显著的改变。      

激光深熔焊接等离子体发射光谱诊断研究

综述了激光等离子体发射光谱诊断的基本假设;介绍了电子温度、密度光谱计算最常用的方法;同时综述了国内外激光焊接等离子体光谱诊断的研究进展.旨在对激光焊接等离子体光谱诊断基本理论和当前的研究进展进行全面的梳理,并对开展激光焊接等离子体光谱试验工作提供理论支持和技术参考.     

载机武器舱盖表面压力计算研究

对带有内埋武器舱盖的载机,采用结构重叠网格方法保证各舱盖与载机网格质量,通过求解三维定常、非定常Navier-Stokes方程,得到内埋武器舱盖开启过程的静态、动态复杂流场,分析了内埋舱盖开启过程中其内外壁的气动特性,通过分析发现内外壁分布压力变化各有特点,动态压力分布居于静态压力分布包络中,舱盖结构强度设计宜采取"动-静结合"方式。     

E region electric fields at the dip equator and anomalous conductivity effects

Zonal and vertical electric fields were estimated at E region heights in the Brazilian sector. Zonal electric fields are obtained from the vertical electric fields based on their relation through the Hall-to-Pedersen ionospheric conductivities ratio. The technique for obtaining the vertical electric field is based on its proportionality to the Doppler velocities of type 2 irregularities as detected by coherent radars. The 50 MHz backscatter coherent (RESCO) radar was used to estimate the Doppler velocities of the type 2 irregularities embedded in the equatorial electrojet. A magnetic field-line integrated conductivity model was developed to provide the conductivities. It considers a multi-species ionosphere and a multi-species neutral atmosphere, and uses the IRI 2007, the MISIS 2000 and the IGRF 10 models as input parameters for ionosphere, neutral atmosphere and Earth’s magnetic field, respectively. The ion-neutral collision frequencies of all the species are combined through the momentum transfer collision frequency equation, and different percentages of electron-neutral collisions were artificially included for studying the implication of such increase in the zonal electric field, which resulted ranging from 0.13 to 0.49 mV/m between the 8 and 18 h (LT), under quiet magnetic conditions.     

降低CC50汽轮机推力瓦运行温度研究

针对4#机组汽轮机出现正推力瓦运行金属温度偏高的状况,在深入调查4#机组汽轮机现状的基础上,通过与现有标准相比较,确定目标为正推力瓦运行金属温度≤95℃;在具体分析其影响因素的基础上,确定了5个主要影响因素,并针对其采取了相应措施,改造结果表明确实使4#机组汽轮机组正推力瓦运行金属温度低于95℃,达到了预期目标,为汽轮机的改造提供了技术指导。     

Effect of surface roughness on microwave brightness temperature from lunar surface: Numerical analysis with a hybrid method

A hybrid method, combining the radiative transfer theory and the method of moments (MoM), is proposed to study the potential effect of the lunar surface roughness on the microwave brightness temperature. The total upward emission reaching the lunar surface from below media is calculated by the radiative transfer theory, and then the brightness temperature is obtained by weighting the bidirectional transmission coefficients which is computed using the MoM. The method is validated by both flat and rough surface models with analytic solutions. With the hybrid method, brightness temperatures from simulated lunar model are calculated and compared to those from a flat layered model. The comparisons show that the effect of rough surface on brightness temperature cannot be ignored and also depends on many other factors, such as observation angle and polarizations. For vertical polarization, an optimal observation angle may exist to reduce the effect of surface roughness. These results indicate that the knowledge of lunar surface roughness is important in microwave remote sensing to the Moon and may probably provide a guide to lunar projects in future.     

热变形参数对镁合金力学性能及微观组织的影响

基于热模拟机GLEEBLE1500,以AZ31为研究对象进行热压缩实验,获得材料的应力-应变曲线。用金相显微镜对不同温度及应变速率下的金相进行观察分析,并对比分析热压缩前后的微观组织。同时分析了不同温度及应变速率下材料的力学行为,其行为属于典型的动态再结晶型。当热压缩温度为350℃和400℃时,材料强度随应变速率增大而增大,且加工硬化也增大。当应变速率为0.01和0.1/s时,随着变形温度的升高,材料的应力逐渐降低。在不同温度下,应变速率为0.01/s时的应力比应变速率为0.1/s时的应力要低。     

双锋角钻头钻削碳纤维增强树脂基复合材料研究

采用双锋角钻头和普通麻花钻对T700碳纤维复合材料(CFRP)进行钻削试验,从钻削轴向力、制孔出口质量和表面粗糙度等方面分析双锋角钻头在不同加工参数下制孔特点,并与普通麻花钻进行对比。试验结果表明:与普通麻花钻对比,双锋角钻头钻削CFRP时钻削轴向力减小约20%,制孔出口质量更好,孔壁的表面粗糙度值减小,体现优异的切削性能更适合CFRP的制孔加工。     

基于动态人工势场法的多机改航路径规划研究

在危险天气条件下,需要研究航班改航路径规划的问题。对传统人工势场法中的斥力势函数进行修正,将目标点与障碍物的距离以及航空器与受限区的运动速度考虑在内,建立了动态人工势场法的多机改航路径规划模型。模型解决了障碍物附近目标不可达问题,并且适应动态运行环境。算例验证了模型的有效性和可行性。     

圆排波瓣圆柱混合管的气动特性实验研究

建立了实验装置，对圆排波瓣喷管与８只圆柱混合管相配合，进行了冷热态实验。得出了它们引射混合的引射流量比随主次流温度比、混合管截面比、次流进口截面比的变化关系曲线。另外，还对不同温度下修正流量比的温度指数进行了研究，得出圆排波瓣圆柱混合管引射混合器的修正流量比温度指数ｎ＝０．４。