高焓湍流边界层壁面摩阻产生机制分析

高超飞行器在中低空以极高马赫数飞行时,飞行器表面会遇到湍流与高温非平衡效应耦合作用的新问题.这种高焓湍流边界层壁面摩阻产生机制是新型高超声速飞行器所关注的基础科学问题,厘清此产生机制可以为减阻方法的设计提供指导,具有重要的工程实用价值.本文选取高超声速飞行时楔形体头部斜激波后的高焓流动状态,开展了考虑高温非平衡效应的湍流边界层直接数值模拟研究,并设置同等边界层参数下的低焓完全气体湍流边界层流动作为对比,采用RD (Renard&Deck)分解技术研究了高焓湍流边界层摩阻的主要产生机制,对摩阻产生的主要贡献项积分函数分布进行了详细分析,研究了高温非平衡效应对摩阻产生的影响规律;采用象限分析技术,研究了摩阻分解湍动能生成项的主导流动事件.计算结果表明,高温非平衡效应会使得壁面摩阻脉动条带的流向和展向尺寸均减小.分子黏性耗散项和湍动能生成项是高焓湍流边界层摩阻生成的主要流动过程.分子黏性耗散项主要作用在近壁区,高焓流动的分布与低焓流动存在差异.象限分析表明,上抛和下扫运动是影响摩阻分解中湍动能生成项的主导事件.     

基于滑移网格与RNG湍流模型计算泵内的动静干扰

本文利用三维Navier-Stockes方程和RNG湍流模型,在转动与静止部件间采用滑移网格技术建立交互界面,对泵内动静干扰引起的三维非定常湍流进行了计算,得到了旋转叶轮与固定导叶间流体的湍流特征。从计算结果可知,静叶与动叶间各点的压力脉动频率成分一致,且幅值沿周向呈正弦变化规律。这说明利用滑移网格技术及RNG湍流模型,可以模拟三维非定常动静干扰流动问题。     

等厚薄板翼型的气动力特性研究

本文从吹风实验及数据分析两方面来研究等厚薄板翼型的气动力特性。在实验中对单园弧、双圆弧、抛物线三种类型的薄板翼型进行了孤立翼型的吹风试验，得出了各翼型升力系数，阻力系数随冲角变化的结果。然后利用非交错网格下的ＳＩＭＰＬＥ方法，计算了等厚薄板翼型流场，计算结果和实验结果吻合较好。     

激光传输模拟中基于衍射过程FFT算法的参量优化

为实现采用相位屏法正确模拟准直激光束经湍流大气的传输特性,根据湍流特性、抽样定理以及两屏间衍射过程FFT算法本身所决定的相邻两屏网格间距之间的关系,得出相位屏间距和网格间距确定网格数目最优取值的解析表达式,数值模拟高斯光束经自由空间和湍流大气传输的远场分布,网格数目取解析式求得的最优值848时,光束经自由空间传输的模拟结果与ABCD定律求得的解析结果完全一致;网格数目取836或860时,等效于光束通过偶数相位屏时被正透镜或负透镜阵列会聚或发散,削弱或夸大湍流大气对光束的影响,模拟结果出现严重偏差。     

Inflow conditions for spatial direct numerical simulation of turbulent boundary layers

The inflow conditions for spatial direct numerical simulation (SDNS) of turbulent boundary layers should reflect the characteristics of upstream turbulence, which is a puzzle. In this paper a new method is suggested, in which the flow field obtained by using temporal direct numerical simulation (TDNS) for fully developed turbulent flow (only flow field for a single moment is sufficient) can be used as the inflow of SDNS with a proper transformation. The calculation results confirm that this method is feasible and effective. It is also found that, under a proper time-space transformation, all statistics of the fully developed turbulence obtained by both temporal mode and spatial mode DNS are in excellent agreement with each other, not only qualitatively, but also quantitatively. The normal-wise distributions of mean flow profile, turbulent Mach number and the root mean square (RMS) of the fluctuations of various variables, as well as the Reynolds stresses of the fully developed turbulence obtained by using SDNS, bear similarity in nature. Supported by the National Natural Science Foundation of China (Grant No. 90205021), the China Postdoctoral Science Foundation (Grant No. 20060400707), and the Foundation for the Author of National Excellent Doctoral Dissertation of China (Grant No. 200328), and partially supported by Liu-Hui Center of Applied Mathematics, Nankai University and Tianjin University     

e~(ax+bx~2)(a,b∈R)参数平面上的骚动区域

本文将参数（ａ，ｂ）平面分为七个区域，然后讨论在每一个区域中ｅａｘ＋ｂｘ２的不动点分布（§１）．在§２中，我们得到一个定理：在Ｄ∞１∪Ｄ∞Ｃ中ｅａｘ＋ｂｘ２是骚动的（在扩充意义下）．     

Schlieren measurement of turbulent structure in a diffusion flame

The regular and random mixing structures in a turbulent diffusion flame were investigated using the quantitative, dynamic crossed-beam schlieren method. Evidence was found close to the nozzle relating to the vortexlike structure of eddies surrounding the central fuel jet flow. The observations also make possible resolution of turbulent intensity, scales, convection, and spectra within the diffusion flame without the use of seeding or intrusion of measuring probes. It is found that length scales and other turbulence parameters in the diffusion flame progressively revert to values similar to those expected and observed in scalar passive mixing as the combustion reaction intensity reduces with axial distance from the nozzle system.     

Preparation of Zirconia Nanocrystals from Concentrated Zirconium Aqueous Solutions

A high concentration (0.8 M) zirconium solution turned into a stable aqueous colloid of about 60 nm in size upon low temperature (96^°C) incubation. Changing the acid concentration did not affect the colloidal growth rate nor the final colloid size much. However, the induction time before the rapid growth of colloidal particle could be altered. By limiting the incubation to just before the rapid growth of colloidal zirconia, and the addition of organic acids as surface modifiers, non-agglomerated primary crystallites (10 nm) of m-ZrO₂ could be recovered. These modified primary crystallites could then be repeatedly flocculated and redispersed in water by adjusting the pH.     

二次风率对分级进风燃烧室内湍流燃烧与NOx生成的影响

本文在分级进风燃烧室的热态实验装置上,测量了燃烧室内湍流燃烧的温度场和组分浓度场,研究了分级进风的流量比率即二次风率对燃烧及NOx生成的影响.得到了四组不同二次风率下燃烧室内气体温度和O2、CO2、CO与NO浓度的分布.     

Hydrothermal synthesis and magnetic properties of CuSb<Subscript>2</Subscript>O<Subscript>6</Subscript> nanoparticles and nanorods

Nanoparticles and nanorods of CuSb₂O₆ are prepared by hydrothermal method and its high temperature α-phase is stabilized at room temperature. The average size of the nanoparticles is ca. 13.7 nm. The nanorods, with a width of ca. 20 nm and an aspect ratio of ca. 5, are the agglomerates composing of smaller nanoparticles with an average size of ca. 8.3 nm. Compared with the high temperature α-phase of bulk sample at 400 K, the lattice of nanophases elongated in ab plane and compressed along c direction. The CuSb₂O₆ nanoparticles exhibit predominant paramagnetic phenomenon. The difference in magnetic properties of the nanoparticles and nanorods indicates the interfacial interaction of agglomerated nanoparticles.