涡流阀流量调节特性数值模拟

用数值模拟研究了涡流阀的流量调节特性。在来流总压恒定的条件下,用时间相关法求解了雷诺平均的Ｎａｖｉｅｒ—Ｓｔｏｋｅｓ方程。计算了无控制流和有控制流两种情况,得到了流动参数在流场中的分布和控制流量与喷管流量的关系。计算表明,涡流阀有良好的流量调节特性。     

基于LES的三维桅杆绕流的数值实验研究

以舰船棱柱形的全封闭桅杆为研究对象,利用计算流体力学软件ANSYS ICEMCFD和ANSYSCFX对模型进行数值实验。在雷诺数为5.74×105和7.66×105,桅杆的攻角从0°变化到90°,以15°为间隔的条件下,研究了表面倾斜且前后不对称的四边形棱柱状结构在均匀流场中所受的流体载荷。通过对桅杆绕流进行数值模拟,得到了漩涡发放随时间的变化规律;发现模型由于表面倾斜的原因,除了受到阻力和升力外,还受到垂直方向上的垂向力,这在以往的柱状结构中是没有的;同时分析了模型所受的定常力和脉动力系数随雷诺数和攻角的变化规律。     

Aerodynamics analysis of a hypersonic electromagnetic gun launched projectile

A hypersonic aerodynamics analysis of an electromagnetic gun (EM gun) launched projectile configuration is undertaken in order to ameliorate the basic aerodynamic characteristics in comparison with the regular projectile layout. Static margin and pendulum motion analysis models have been applied to evaluate the flight stability of a new airframe configuration. With a steady state computational fluid dynamics (CFD) simulation, the basic density, pressure and velocity contours of the EM gun projectile flow field at Mach number 5.0, 6.0 and 7.0 (angle of attack = 0°) have been analyzed. Furthermore, the static margin values are enhanced dramatically for the EM gun projectile with configuration optimization. Drag, lift and pitch property variations are all illustrated with the changes of Mach number and angle of attack. A particle ballistic calculation was completed for the pendulum analysis. The results show that the configuration optimized projectile, launched from the EM gun at Mach number 5.0 to 7.0, acts in a much more stable way than the projectiles with regular aerodynamic layout.     

展向局部加热与圆柱尾流的绝对不稳定性

采用对圆柱展向局部电加热的方式,在水槽中实验研究了临界/亚临界雷诺数圆柱尾流的绝对不稳定性.利用可控电加热改变圆柱表面温度分布,对二维圆柱绕流引入局部三维扰动,观察其对于临界/亚临界雷诺数圆柱尾流稳定性的影响.研究表明,在临界雷诺数状态,圆柱绕流尾流具有绝对不稳定性;在亚临界雷诺数状态,圆柱绕流尾流则是对流不稳定的.加热圆柱展向局部涡脱落存在锁频现象.     

小水线面四体船的阻力特点分析

从粘性阻力、兴波阻力和旋涡阻力3个方面分析小水线面四体船(以SLICE为代表)的阻力特点,讨论了浮体横向错位、支柱和潜体形状、航速和吃水对兴波阻力的影响.结果表明,在浅水中一定航速范围内,与等排水量的小水线面双体船(SWATH)相比,SLICE有一定优势.     

基于FDTD方法的电波在等离子体中传输特性研究

根据时域有限差分法(Finite Difference Time Domain, FDTD)的基本原理,本文首先分析了等离子体的物理场特性及数值计算,然后介绍了飞行器再入时等离子鞘的形成以及等离子体相对介电常数对波的衰减,最后通过三维FDTD和二维FDTD模拟了电磁波在等离子体中的传播情况,证明了FDTD方法是解决电磁波在复杂媒质中传播的一种有效方法,并探究了飞行器再入段黑障区通信的理论和方法。     

Influence of high frequency pulse on electrode wear in micro-EDM

An electromagnetic coupling mathematical model is established by finite element method and is verified by the contrastive experiments of copper matrix Ni–TiN cylindrical coating electrode, copper electrode and Cu50W electrode. The wear mechanism of Ni–TiN/Cu composite electrode in the case of high-frequency pulse current is studied, and the influence of the fluctuation frequency of discharge current on electrode wear in micro-EDM is found out. Compared with the electrode made from homogeneous material, the high frequency electromagnetic properties of Ni–TiN composite layer can be used effectively to inhibit the effect of high frequency pulse on the electrode and improve the distribution trend of current density.     

电子设备的克星--电磁脉冲炸弹

随着高能电磁脉冲产生技术和高能微波技术的发展,应用于信息战的电磁脉冲炸弹在技术上已经成熟.讨论了电磁脉冲炸弹的发展动态及其技术.     

人工免疫系统的战场异态电磁信号检测模型

分析了复杂电磁信号环境下电磁信号监测的现实需求,抽象出"异态电磁信号"的概念。结合人工免疫系统建立起基于人工免疫系统的适用于复杂电磁环境下异态电磁信号检测模型,初步的信号检测实验表明该模型在信号检测准确性、检测时间等方面具有一定优势。     

梢涡空泡初生预报方法

应用气泡动力学方程和气泡运动微分方程研究了梢涡空泡的初生问题.建立了球形气泡平均压力模型,通过模拟梢涡流场中的球形气泡形态对梢涡空泡的初生进行预报.应用平均压力模型分别计算了三种尺度水翼梢涡流场中不同初始尺寸气泡在一定时间内的半径和辐射声压,梢涡用轴向梢涡尺寸不变的兰金涡代替.计算结果表明:从光学法和声学法角度选取空化...