多目标多光谱辐射高速高温计的研制

固体火箭羽焰是一种特殊的火焰,固体火箭发动机喷管羽流沿径向和轴向的温度是研究固体推进剂燃烧状况和发动机燃烧流场的基本参数。针对固体火箭发动机尾喷焰温度及其空间分布测量的需要,继1999年采用多光谱辐射测温方法和技术实现航天某型号固体火箭发动机测量后,研制了新型的多目标多光谱辐射高速高温计用于固体火箭发动机地面搭载试验。仪器使用组合棱镜和光电二极管阵列实现目标0.4~1.1μm光谱的热辐射测量,在主光路设计中首次使用光纤技术,实现一台仪器同时测量空间分布6个目标点的温度和发射率,每个点的空间位置由光阑上的通光孔精确确定,且每个目标测点均有8个工作光谱,研制的同步高速数据采集系统完成48个测量通道的数据同步时间小于10 ns。     

迭代法分析圆环类微带行波天线的辐射特性

利用圆环类微带行波天线的辐射功率与等效行波磁流衰减常数之间的自洽关系,导出了计算衰减常数的迭代方程;为加快迭代速度,将辐射积分中的格林函数展开成柱面波函数,得到快速收敛的级数和.最后给出了方向图的计算曲线,与实验结果对比吻合良好,表明此方法模拟圆环类微带行波天线辐射特性的有效性.     

一种用于衍射光元件优化设计的快速算法的研究

讨论了傅里叶迭代算法对初始相位敏感的缺陷机理,提出用伪随机相位编码作为傅里叶迭代算法初始值的改进算法来克服相位敏感缺陷。改进算法具有加快迭代收敛速度、提高恢复图像强度准确性的优点。将该算法产生的任意期望图样的相位全息图写入纯相位液晶空间光调制器上,在远场成功地再现了期望图样。算法迭代10次可产生衍射效率接近85%的一幅相位全息图。作为一种快速相位恢复算法它在相控阵激光雷达以及光束敏捷偏转等领域有重要意义。     

Effects of Magnetic Nanofluid Fuel Combustion on the Performance and Emission Characteristics

Although the compression ignition engines are a significant source of power, their detrimental emissions create considerable problems to the environment as well as to humans. The objective of the present experimental investigation is to examine the effects of the magnetic nanofluid fuels on combustion performance characteristics and exhaust emissions. In this regard, the Fe₃O₄ nanoparticles dispersed in the diesel fuel with the nanoparticle concentrations of 0.4 and 0.8 vol% were employed for combustion in a single-cylinder, direct-injection diesel engine. After a series of experiments, it was demonstrated that the nanoparticle additives, even at very low concentrations, have considerable influence in diesel engine characteristics. Furthermore, the results indicated that the nanofluid fuel with nanoparticle concentration of 0.4 vol% shows better combustion characteristics in comparison with that of 0.8 vol%. Based on the experimental results, NO _x and SO₂ emissions dramatically reduce, while CO emissions and smoke opacity noticeably increase with increasing the dosing level of nanoparticles.     

ON THE STRUCTURE OF STEADY FLOW THROUGH DUAL-INTAKE ENGINE PORTS

The influence of intake port design on the flow field in a dual-intake valve engine was investigated using computational fluid dynamics, in order to study the effect of inlet port design on the in-cylinder flow. A detailed 3D computational grid incorporating all the features of the Ford Zetec production engine inlet ports, valves and cylinder head was initially created and the flow structure modelled at 5 and 10 mm valve lifts under steady flow conditions. Comparisons of computational results with experimental data obtained by laser Doppler anemometry indicate that the flow characteristics have been predicted well in most regions. Flow generated by different intake port designs was also simulated by introducing air into the cylinder at different directions to the inlet valve axes and the effects of port deactivation, throttling and exhaust gas recirculation were examined. The implications of the results for intake port design are discussed.     

MODELLING OF WAVE PROPAGATION IN THE NEARSHORE REGION USING THE MILD SLOPE EQUATION WITH GMRES-BASED ITERATIVE SOLVERS

The mild slope equation in its linear and non-linear forms is used for the modelling of nearshore wave propagation. The finite difference method is used to descretize the governing elliptic equations and the resulting system of equations is solved using GMRES-based iterative method. The original GMRES solution technique of Saad and Schultz is not directly applicable to the present case owing to the complex coefficient matrix. The simpler GMRES algorithm of Walker and Zhou is used as the core solver, making the upper Hessenberg factorization unneccessary when solving the least squares problem. Several preconditioning-based acceleration strategies are tested and the results show that the GMRES-based iteration scheme performs very well and leads to monotonic convergence for all the test-cases considered.     

风扇/增压级非设计工况特性分析

本文对某涡扇发动机风扇-外涵道-内涵道整体进行三维定常数值模拟,对内外涵道在设计转速下的流量特性和非设计工况下的气动性能进行了分析。得到内外涵道的稳定工作区域以及在内外涵道堵塞和近失速点的流场信息,为风扇／增压级整体结构的性能评估和优化设计提供了一定的依据。     

自由活塞斯特林发动机活塞位移测量

自由活塞斯特林发动机活塞往复振动位移对研究发动机特性具有重要意义,然而该类发动机活塞位于高压封闭腔体内且结构较为紧凑,其活塞往复振动位移难于直接进行测量。加速度传感器具有尺寸小、安装方便和工作稳定等特点,提出了采用加速度传感器测量活塞位移的方法。根据加速度传感器测量位移的原理,建立了一套加速度传感器测量自由活塞斯特林发动机活塞位移的标定试验系统,以位移传感器为基准测试并分析了不同活塞振幅和不同振动频率下加速度传感器测量位移的误差大小。实验结果表明,在活塞振幅小于8 mm,振动频率大于20 Hz条件下,加速度传感器测量位移的误差小于5%。因此加速度传感器可以用于测量自由活塞斯特林发动机的活塞往复运动位移。最后成功把加速度传感器测量的自由活塞斯特林发动机活塞振动位移用于发动机循环指示功的实验研究。     

增强型喷射器对爆轰波DDT过程的影响

在激波、火焰及射流同时存在的流场中,组织燃烧转爆轰过程是脉冲爆震发动机实现点火、起爆的关键问题。设计一类喷射器,采用C_2H_2/O_2/Ar反应,数值验证了该喷射器能增强爆震室燃料燃烧转爆轰的可行性,并讨论了流场中热点的点火机制。结果显示:该装置在流场中可激发不稳定性,产生漩涡,加速能量、质量的交换。流场产生热点,促进火焰速度加快,追赶前导激波。喷射器位置影响前导激波的运动速度。在一定范围内,前导激波速度越大,碰撞产生的热点越容易激发燃烧转爆轰过程。     

线性互补问题的异步并行多分裂松弛迭代算法

将求解线性方程组的异步并行多分裂松弛迭代算法推广到线性互补问题.当问题的系数矩阵为H-矩阵类时,证明了算法的全局收敛性.