分段式固体火箭发动机内部流动不稳定性数值分析

采用大涡模拟技术,针对某分段式固体火箭发动机开展了发动机燃面退移0mm,160mm和280mm三个时刻下发动机燃烧室内部流动不稳定现象的数值分析,获得了三个典型时刻燃烧室内压强可能的振荡特性.计算结果表明,在发动机点火初期燃烧室内流动不稳定性主要由表面涡脱落导致;随着燃面的退移,端面限燃层暴露在燃气中,由于端面包覆结构残余的影响,燃烧室内流动不稳定性主要由障碍涡脱落决定,且与点火初期相比,压强振荡的频率逐步减小.     

加肋板结构中弹性波一维局部问题的研究

分析研究了失谐周期多跨加肋板结构中的弹性波一维局部化问题。采用传递矩阵方法给出了系统的传递矩阵 ,并采用 Wolf提出的计算连续型动力系统中 Lyapunov指数的方法 ,给出了局部化因子的计算表达式。作为算例 ,给出了失谐加肋板结构中局部化因子的数值结果 ,并分析了跨长的失谐程度及结构参数对弹性波局部化的影响     

一种梁板复合结构的设计

对某卫星主结构中应用的一种新型的复合材料结构形式——梁板复合结构进行了设计、分析与试验。首先通过整星分析,设计了梁板复合结构,并为其设计了试验件进行研制试验。同时,利用有限元软件PATRAN和NASTRAN建立了三种模型:二维板壳模型、三维板壳模型和三维实体模型,通过比较试验结果与分析结果,修正了分析模型,并找出了合理的分析方法。试验结果表明,设计的梁板复合结构满足了既定的强度要求。     

Calculation of an unsteady jet flow around the plate cascade

In the framework of the general theory for unsteady weakly disturbed fluid flows with free boundaries, a problem is solved to calculate a jet flow around the cascade of plates executing the harmonic oscillations. We developed a program that enables us for the first time to carry out systematic calculations of flow characteristics depending on arbitrary values of determining parameters.     

Acceleration sensors based modal identification and active vibration control of flexible smart cantilever plate

Some flexible appendages of spacecrafts, such as solar panels, are cantilever plate structures. Thus, vibration problem is unavoidable when there is slewing maneuver or external disturbance excitation. Vibration of such cantilever plate structures includes coupled bending and torsional motion. Furthermore, the low amplitude vibration near the equilibrium point is very difficult to be quickly suppressed due to nonlinear factors of the hardware in the system, which is harmful to stability and attitude control accuracy. To solve these problems, acceleration sensor-based modal identification and active vibration control methods are presented for the first two bending and the first two torsional modes vibration of the cantilever plate. Optimal placements of three acceleration sensors and PZT patches actuators are performed to decouple the bending and torsional vibration of such cantilever plate for sensing and actuating, and identifications are achieved by experiments. A nonlinear control method is presented to suppress both high and low amplitude vibrations of flexible smart cantilever plate significantly. Experimental comparison researches are conducted by using acceleration proportional feedback and the presented nonlinear control algorithms. The experimental results demonstrate that the presented acceleration sensor-based methods can suppress the vibration of cantilever plate effectively.     

基于主动约束层阻尼控制的大型挠性航天器动力学模型

以大型挠性航天器简化模型——中心刚体和固接板混合系统为对象,同时考虑板表面粘贴的主动约束层阻尼结构,根据拟坐标拉格朗日方程,建立了包含所有高阶小量的完整动力学模型。建模时,采用混合坐标描述中心刚体和主动约束阻尼板的运动,用Golla-Hughes-Mctavish模型描述阻尼材料的复模量。基于该动力学模型可进行空间柔性板振动的主动约束阻尼控制器设计和大型挠性航天器的姿态动力学研究。     

基于改进Sobel算子的边缘检测车牌定位方法

车牌定位是自动识别的关键步骤,而在整个车牌定位过程中,边缘检测是其中的一项重要环节和关键技术。文中在分析了目前常用的边缘检测方法后,给出了一种基于Sobel算子的改进边缘检测方法。实验结果证明具有较好的检测效果。     

脉冲干扰下交错与FEC编码扩频系统性能的研究

推导了在脉冲干扰下无人机扩频遥测系统的误码率公式。提出了用吉尔伯特信道 ( Gi信道 )描述脉冲干扰下无交错编码的扩频系统的信道,用离散无记忆信道 ( DMC)描述脉冲干扰下的有交错扩频系统的信道。对比分析了脉冲干扰下的扩频系统采用 FEC前向纠错和不采用 FEC,以及采用 FEC与交错技术相结合3种情况时的系统误码率性能。最后通过数值计算分析,得到了一些有用的结论。所得公式和结论同样适用于部分频带干扰。     

Flow field characteristics,mixing and emissions performance of a lab-scale rich-quench-lean trapped-vortex combustor utilizing a quench orifice plate combined with a bluff-body

In this study, the low emission combustion technology of Rich-Quench-Lean (RQL) has been applied in Trapped-Vortex Combustor (TVC), and the combinative RQL-TVC shows a promising low emissions performance. By utilizing a quench orifice plate combined with a bluff-body, a lab-scale RQL-TVC was designed. The flow fields of RQL-TVC were measured by 2-D PIV and predicted by 3-D numerical simulation. Flow structures, radial profiles of normalized mean axial velocity, turbulence intensity and mixing level of the quench zone were analyzed. Results reveal that the dual-vortex and the single-vortex flow patterns both exist in cavities and quench zone of RQL-TVC, and the turbulence intensity is strong in the quench zone with some reverse flows. The spiral vortex was discussed by 3-D streamlines and the detail flow structures of the quench zone were analyzed based on the numerical results. The mixing level of the quench zone was determined, and results show that the quench device enhances the mixing level compared with TVC. Combustion efficiency and emissions performance were investigated experimentally, and results demonstrate that RQL-TVC has relatively higher combustion efficiency and lower emission index of CO, UHC and NO_x than the same size lab-scale TVC in present work.     

冷却介质在层板内流动特性研究(第二部分 数值模拟复杂结构内流场)

用商业软件模拟复杂层板中冷却介质流动特性,以粒子图像速度(PIV)测量技术获得的实验数据,验证所选择的数学模型和数值方法.实验是在确定的径高比1及入口雷诺数4.1×104下进行的.用验证的数学模型及数值方法,向上下扩展雷诺数至2.05×104及8.2×104,改变层板径高比至0.5及2.0, 模拟这两个参数变化对层板内冷却介质流场的影响.模拟结果指出:在相同的径高比下,入口雷诺数的改变对层板内冷却介质流动特性影响很小;相反在相同的入口雷诺数下,径高比改变对层板内冷却介质流动特性有明显的影响.