离心泵启动过程内部瞬态流动的二维数值模拟

为分析离心泵启动过程外部瞬态特性的内流机理,建立求解叶轮启动和加速过程泵内部非定常流动的数值模拟方法,以二维离心泵为模型进行启动过程内部流动的数值模拟研究.以绝对坐标系描述伞场流动,采用动网格方法实现离心泵启动过程中叶轮加速旋转引起的流场变形,选用人涡模拟(LES)描述湍流.分析了叶轮启动过程巾内部非定常流动结构和演化过程及其与外部瞬态特性的关系,并与准稳态假设下的流动模拟结果进行了对比分析,定性地分析了离心泵在启动过程中的瞬态效应,验证了采用动网格方法求解启动过程瞬态流动的可行性.     

弱旋湍流火焰合成纳米二氧化钛的机理研究

湍流效应在火焰合成纳米TiO2颗粒工业化规模放大中具有重要影响.本文基于一种内加环形旋流片的弱旋火焰开展了合成TiO2纳米颗粒的实验研究.对于内径12 mm管式燃烧器,加入旋片后火焰贫燃极限大幅度降低16%～33%,火焰高度也从9.0 cm减少到3.0 cm,焰区温度约减少20%～30%.研究表明,弱旋湍流火焰具有流速大、可燃当最比低和温度低的特点,使其相对无旋火焰可以合成粒径较小、烧结程度较低的TiO2纳米颗粒.     

“反胶团法”合成的CdS半导体纳米粒子的光谱性质研究

反相胶束是指由介于油和水界面的表面活性剂分子, 稳定、且均匀分散于连续油介质中的微液滴。它可以作为“微反应器”合成性能优良的CdS粒子。文章研究了反相胶束的W值(W=[水]/[表面活性剂])、[Cd2+]与[S2-]的比例和Cd2+和S2- 离子的起始浓度对CdS纳米粒子发光特性均有明显影响。回流处理可以对CdS纳米粒子的表面进行修饰,可以使CdS粒子的缺陷发光减弱并消失而显著增强激子发射,同时可增大粒径使激子发射峰位红移,体现了明显的量子限域效应; 所得材料的室温最大荧光量子效率高达11%。     

一种目标区域最佳椭圆描述方法

目标的最佳描述区域对于建立目标特征、目标跟踪、目标轮廓求取具有非常重要的意义。针对这类问题,提出了一种目标区域最佳椭圆描述确定方法。新方法首先根据目标和背景的差别确定出目标区域,然后利用尺度空间理论计算出目标的最佳椭圆描述。实验表明：新算法可以有效、准确地确定出目标包含区域的大小和方向。     

Non-Commutative Fock--Darwin System and Magnetic Field Limits

A Fock--Darwin system in noncommutative quantum mechanics is studied. By constructing Heisenberg algebra we obtain the levels on noncommutative space and noncommutative phase space, and give the corrections to the results in usual quantum mechanics. Moreover, to search the difference among the three spaces, the degeneracy is analysed by two ways, the valueof ω/ω_c and certain algebra realization (SU(2)and SU(1,1)), and some interesting properties in the magnetic field limit are exhibited, such as totally different degeneracy and magic number distribution for the given frequency or mass of a system in strong magnetic field.     

The Minimum Model for the Iron-Based Superconductors

A single band t-U-J₁-J₂ model is proposed as the minimum model to describe the superconductivity of the newly discovered iron-based superconductorsR(O_1-xF_x)FeAs and RO_1-xFeAs (R=La, Ce, Sm, Pr, Nd, Gd). With the mean-field approach, it is found that the pairing occurs in the d-wave channel. In the likely parameter region of the real materials, by lowering temperature, the system enters firstly the d_xy superconducting phase with D_4h-symmetryand then enters the time-reversal-symmetry-broken d^_xy+id_x²-y² superconducting phase with C_4h-symmetry.     

Finite-Difference Lattice Boltzmann Scheme for High-Speed Compressible Flow: Two-Dimensional Case

Lattice Boltzmann (LB) modeling of high-speed compressible flows has long been attempted by various authors. One common weakness of most of previous models is the instability problem when the Mach number of the flow is large. In this paper we present a finite-difference LB model, which works for flows with flexible ratios of specific heats and a wide range of Mach number, from $0$ to 30 or higher. Besides the discrete-velocity-model by Watari [Physica A 382 (2007) 502], a modified Lax--Wendroff finite difference scheme and an artificial viscosity are introduced. The combination of the finite-difference scheme and the adding of artificial viscosity must find a balance of numerical stability versus accuracy. The proposed model is validated by recovering results of some well-known benchmark tests: shock tubes and shock reflections. The new model may be used to track shock waves and/or to study the non-equilibrium procedure in the transition between the regular and Mach reflections of shock waves, etc.     

Squeezing for Entangled States of Two Entangled Particles with Different Masses

Using the technique of integration within an ordered product of operators we present a convenient approach for introducing the squeezing operator for the entangled states of two entangled particles with different masses. We also introduce one-sided squeezing operators.     

A straightforward method for wall impedance eduction in a flow duct

The development of the advanced liner technology for aeroengine noise control necessitates the impedance measurement method under realistic flow conditions. Currently, the methods for this need are mainly based on the inverse impedance eduction principle, confronting with the problems of initial guess, high computation cost, and low convergence. In view of this, a new strategy is developed that straightforwardly educes the impedance from the sound pressure information measured on the duct wall opposing to the test acoustic liner embedded in a flow duct. Here, the key insight is that the modal nature of the duct acoustic field renders a summed-exponential representation of the measured sound pressure; thus, the characterizing axial wave number can be readily extracted by means of Prony's method, and further the unknown impedance is calculated from the eigenvalue and dispersion relations based on the classical mode-decomposition analysis. This straightforward method is simple in its basic principle but remarkably has the advantages of ultimately overcoming the drawbacks inherent to the inverse methods, incorporating the realistic multimode nonprogressive wave effects, high computational efficiency, possibly reducing the measurement points, and even avoiding the necessity of the duct exit impedance that bothers perhaps all the existing waveguide methods.