Numerical Study of Heat Transfer Mechanism in Turbulent Supercritical CO2 Channel Flow

Direct numerical simulation (DNS) of supercritical CO2 turbulent channel flow has been performed to investigate the heat transfer mechanism of supercritical fluid. In the present DNS, full compressible Navier-Stokes equations and Peng-Robison state equation are solved. Due to effects of the mean density variation in the wall normal direction, mean velocity in the cooling region becomes high compared with that in the heating region. The mean width between high-and low-speed streaks near the wall decreases in the cooling region, which means that turbulence in the cooling region is enhanced and lots of fine scale eddies are created due to the local high Reynolds number effects. From the turbulent kinetic energy budget, it is found that compressibility effects related with pressure fluctuation and dilatation of velocity fluctuation can be ignored even for supercritical condition. However, the effect of density fluctuation on turbulent kinetic energy cannot be ignored. In the cooling region, low kinematic viscosity and high thermal conductivity in the low speed streaks modify fine scale structure and turbulent transport of temperature, which results in high Nusselt number in the cooling condition of the supercritical CO2.

Single curved fiber sedimentation under gravity

Dynamics of single curved fiber sedimentation under gravity are simulated by using the lattice Boltzmann method. The results of migration and rotation of the curved fiber at different Reynolds numbers are reported. The results show that the rotation and migration processes are sensitive to the curvature of the fiber. (c) 2007 Elsevier Ltd. All rights reserved.

DNS and LES of turbulent channel flow with hydrophobic surface

Hydrophobic surface benefits for drag reduction. Min and Kim[1] do the first Direct Numerical Simulation on drag reduction in turbulent channel flow. And Fukagata and Kasagi[2] make some theoretical analysis based on Dean[3]'s formula and some observations in the DNS results. Using their theory, they conclude that drag reduction is possible in large Reynolds number. Both Direct Numerical Simulation (DNS) and Large Eddy Simulation (LES) are performed in our research. How the LES behaving in the turbulent channel flow with hydrophobic surface is examined. Original Smagorinsky model and its Dynamical model are used in LES. The slip velocities predicted by LES using Dynamical model are in good agreement with DNS as shown in the Figure. Although the percentage of drag reduction predicted by LES shows some discrepancies, it is in the error limit for industrial flow. First order and second order moments of LES are also examined and compared with DNS's results. The first-order moments is calculated well by LES. But there are some discrepancies of second-order moments between LES and DNS. [GRAPHICS]

湍流研究最近半世纪的一些发展

<正>内容一、绪言(Ⅰ)研究湍流的意义(Ⅱ)国外开展湍流研究的情况二、湍流理论的进展(Ⅰ)先把流体动力学方程组平均的理论(a)1950年以前发展情况简述(1)Reynolds方程和混合长度理论(2)各向同性湍流的统计理论(3)具有剪应力的普通湍流理论(b)最近的剪切湍流的半经验理论(c)最近的湍流统计理论(1)E.Hopf理论(2)R.H.Kraichnan直接相互作用理论(8)Lewis等人的分子运动理论(4)Meecham理论。(5)S.Grossmann重正化群法(8)陈善谟统计动力学重复级串法

Coral Disease and Health Workshop: Coral Histopathology II

The health and continued existence of coral reef ecosystems are threatened by an increasing array of environmental and anthropogenic impacts. Coral disease is one of the prominent causes of increased mortality among reefs globally, particularly in the Caribbean. Although over 40 different coral diseases and syndromes have been reported worldwide, only a few etiological agents have been confirmed; most pathogens remain unknown and the dynamics of disease transmission, pathogenicity and mortality are not understood. Causal relationships have been documented for only a few of the coral diseases, while new syndromes continue to emerge. Extensive field observations by coral biologists have provided substantial documentation of a plethora of new pathologies, but our understanding, however, has been limited to descriptions of gross lesions with names reflecting these observations (e.g., black band, white band, dark spot). To determine etiology, we must equip coral diseases scientists with basic biomedical knowledge and specialized training in areas such as histology, cell biology and pathology. Only through combining descriptive science with mechanistic science and employing the synthesis epizootiology provides will we be able to gain insight into causation and become equipped to handle the pending crisis. One of the critical challenges faced by coral disease researchers is to establish a framework to systematically study coral pathologies drawing from the field of diagnostic medicine and pathology and using generally accepted nomenclature. This process began in April 2004, with a workshop titled Coral Disease and Health Workshop: Developing Diagnostic Criteria co-convened by the Coral Disease and Health Consortium (CDHC), a working group organized under the auspices of the U.S. Coral Reef Task Force, and the International Registry for Coral Pathology (IRCP). The workshop was hosted by the U.S. Geological Survey, National Wildlife Health Center (NWHC) in Madison, Wisconsin and was focused on gross morphology and disease signs observed in the field. A resounding recommendation from the histopathologists participating in the workshop was the urgent need to develop diagnostic criteria that are suitable to move from gross observations to morphological diagnoses based on evaluation of microscopic anatomy. (PDF contains 92 pages)

剪切水-气界面下的湍流特征

利用氢气泡技术测量了剪切水-气界面下二维瞬时流速的分布,根据从流动显示图像获得的流速剖面样本,考察水面附近湍流场的平均特性,重点分析猝发事件的信号特征。氢气泡方法较为准确地测定了水流中平均流速、湍流脉动强度以及Reynolds切应力的分布,更重要的是,它能将流动显示图像中观察到猝发事件与定量的信号特征直接联系起来.在猝发过程中,水面近区的流向和垂向瞬时速度以及Reynolds切应力出现较大幅度的脉动,它们与低速流体条带的喷射行为对应;大幅度脉动在时间和空间垂直方向上表现出高度的相干性,这是猝发事件的一个显著特征。

高速剪切层线性稳定性空间模式参数分析

用一类高精度对称紧致差分格式数值离散一阶改型三维可压粘性扰动方程,对导出的非线性离散特征值问题采用二阶修正Newton-Raphson边值迭代局部解法,实现了超声速剪切流的线性空间稳定性分析。基于对流Mach数、Reynolds数、速度比、密度比等参数研究,讨论了压缩性效应、粘性效应、超声速扰动快/慢模态等,结果显示超声速粘性剪切流的弱不稳定性同多种影响因素密切相关。

微重力流体力学

目录

前言
第一章 微重力流体科学概论
一、微重力科学与微重力流体科学
1、微重力环境
2、重力的影响
3、微重力流体科学的发展
二、微重力流体力学概述
1、对流
2、扩散及输运现象
3、液滴和气泡动力学
4、多相流过程
5、残余重力效应
6、其他流体力学问题
三、微重力物理化学概述
1、临界现象
2、燃烧
3、分散体悬浮系统
4、晶体生长的物理化学问题
四、微重力流体科学的研究途径
1、微重力研究的一般途径
2、微重力实验手段
参考文献
第二章 基本方程组和流体运动特性
一、引言
二、连续性方程和迁移方程
三、动量方程
1、流体的粘性——Reynolds应力
2、动量守恒定律
3、Navier-Stokes方程
四、能量方程
1、总能量方程
2、动能方程
3、内能方程
4、粘性耗散函数
5、Fourier定律及另外二种形式的能量方程
6、不可压流体的导热方程
五、Newton流体的运动方程组及定解条件
1、基本方程组和适定性
2、定解条件
六、Boussinesq近似及适用范围
七、相似律和无量纲参数
1、利用Buckinghan〓定理导出相似参数
2、微重力流体力学的有关物理量和无量纲参数
参考文献
第三章 毛细现象以及界面的平衡和稳定
一、引言
二、表面张力的物理描述
三、液体射流的表面不稳定
1、基本方程组和基态
2、小扰动的线性化方程
3、本征值方程及其解
四、等温条件下液桥的平衡位型和稳定
1、表面张力作用下的平衡条件
2、毛细稳定性
3、旋转稳定性
第五章 液桥的流体动力学稳定理论
1、基本假设和液桥的平衡条件
2、稳定问题的数学提法
3、液桥的Liapunov稳定理论
4、特殊情形（Ω〓=μ=0）以及纯半波不稳定（n=1，m=1）
5、小扰动方程的变分方程
6、小Weber数和大Reynolds数情形的不稳定发展率
7、液桥微重力实验的结果的分析
8、讨论和结论
参考文献
第四章 对流和扩散
一、Pearson对流
1、自由面不变形时的小扰动分析
2、自由面可变形情形
3、非线性理论
4、多层不混溶液体系统
二、热毛细对流
1、矩形容器中的热毛细对流
2、柱形液桥的热毛细对流
3、半浮区液桥热毛细对流的数值模拟
4、薄层液体的热毛细对流
三、热毛细振荡对流的实验研究
1、液桥内部的温度振荡
2、热毛细对流的表面振荡
3、综合测量
四、热毛细对流的振荡机理
1、热流体波不稳定性
2、表面波不稳定性
3、有限高度液桥的线性不稳定性
4、三维不定常数值模拟
5、重力的影响
6、一种非稳定性理论
7、关于振荡的激发机制
参考文献
第五章 液滴动力学
一、等温液滴动力学
1、球形液滴的振荡
2、不混溶液体中球形液滴的振荡
3、弱非线性理论
4、实验模拟
二、非等温液滴的Marangoni迁移
1、定常线性化理论（小Reynolds数，小Marangoni数）
2、非线性理论
3、实验结果
三、液滴和气泡的相互作用
1、双气泡的轴对称理论
2、多液滴的轴对称理论
四、旋转液滴的演化序列和分叉理论
1、旋转液滴的演化
2、旋转液滴的Thomson-Tait稳定准则
3、长期稳定性和动力稳定性
4、长期稳定性真实性的实验证明
5、结论
参考文献
第六章 微重力材料流体力学
一、晶体生长过程
二、纯扩散过程
1、一维扩散过程
2、二维扩散过程
3、固-液界面弯曲对径向分凝的影响
三、浮区晶体生长
1、浮区的热毛细对流
2、浮区的熔质毛细对流
3、浮区对流的振荡特征（小Prandtl数对流）
4、耦合过程
四、溶液晶体生长
1、溶液晶体生长的相变界面过程
2、一维纯扩散过程
3、准定常溶液晶体生长过程
4、不定常溶液生长过程
五、气相晶体生长
1、气相晶体生长过程
2、一维模型
3、物理气相输运中的对流效应
4、化学气相沉积（CVD）过程
参考文献

郭永怀文集

Marine Mammal Strandings in the United States: Proceedings of the Second Marine Mammal Stranding Workshop, Miami, Florida, December 3-5, 1987

Over a decade ago, in August 1977, the First Marine Mammal Stranding Workshop was convened in Athens, Georgia. That workshop, organized by j.R. Geraci and D.J. St. Aubin, not only considered biology and pathology of stranded marine mammals, but it also served as a springboard for the formation of regional marine mammal stranding networks in the United States. The ramifications have been extremely important to the field of marine mammalogy since, for some species, examination or rehabilitation of stranded specimens serves as virtually the only source of information on distribution, anatomy, physiology, reproduction, and pathology. The First Marine Mammal Stranding Workshop led to increased awareness of the marine mammals themselves, as well as the logistic and legal factors associated with effective handling of the animals. A number of individuals indicated that they felt that a Second Marine Mammal Stranding Workshop held prior to the Seventh Biennial Conference on the Biology of Marine Mammals (Miami, Florida; December 1987) would be both timely and productive. Accordingly, we organized the workshop and scheduled it to occur on 3-5 December. Our goals for the workshop were several, including 1) providing descriptions of some research, especially new techniques, regarding stranded marine mammals; 2) providing a forum where scientists could interact and possibly initiate cooperative research activities; 3) presenting information regarding procedures used effectively to handle stranded animals; 4) assessing ways to standardize data and specimen collection, archiving, and retrieval; and 5) providing a forum for assessing accomplishments and status of regional stranding networks to date, as well as for making recommendations regarding future activities of the networks. Nearly 100 individuals representing Federal and State governments, academic institutions, the oceanarium industry, consulting groups, conservation organizations, and the private sector attended the workshop (see Workshop Participants, this volume). (PDF file contains 166 pages.)

可压平面混合层稳定性分析及数值模拟

可压平面混合层是包含复杂多时空尺度运动的非定常流体力学部问题，具有深刻的理论意义和广泛的应用背景。针对该问题所涉及内容的多面性，本文的目的是，基于高精度、高分辨率数值算法的构造、发展和数值行为分析，采用线性稳定性分析和直接数值模拟方法。从理论和计算两方面集中研究压缩性效应、粘性效应、初值效应以及燃烧反应放热效应等对可压平面混合层早期稳定性行为和大尺度拟序涡结构非线性演化的影响。以混合层已有研究成果的分析和综述为开端，论文主体共包括四部分：第一部分是可压平面混合层时间/空间模式数值线性稳定性分析。实现了高精度对称紧致差分格式（SCD）对可压粘性扰动线性稳定性边值问题的求解，对导出的线性和非线性离散特征值问题，提出了两个高效局部解法。研究涉及二维/三维扰动波、无粘/粘性扰动波、特征函数和特征值谱、第一/第二模态、超声速快/慢模态、速度比和密度比等。验证了对流Mach数Mc为一个合理的压缩性参数。指出压缩性效应和粘性效应对最不稳定扰动波的波数（频率）和增长率呈相拟的抑制作用，且时间模式稳定性分析结果在许多方面是可信的。从随机和线性扰动场出发，采用高精度五阶迎风紧致和六阶对称紧致混合差分算法（UCD5/SCD6）对可压平面混合层的稳定性特征进行了直接数值模拟，揭示了初始主导线性扰动与一些实际涡结构非线性作用形态间的内在关联，印证了线性稳定性分析方法的合理性和有效性。第二部分是高精度迎风紧致差分格式（UCD）时空全离散数值行为分析。导出了其一维/二维一般色散表达式。研究表明，UCD格式在高波数区具有内在的全离散耗散和色散特性；其数值群速度的快/慢特征可因CFL数不同而改变；在稳定CFL数下简单附加人工粘性可强化UCD格式在高波数区的耗散量；提高时间精度可放宽稳定CFL数限制；UCD格式的二维全离散色散介质中存在三个不同性质的数值波，其全离散稳定性由数值声波主控。第三部分实现了高精度UCD5/SCD6差分算法对空间发展可压平面混合层的直接数值模拟。通过亚谐扰动波的个数和扰动频率的控制，捕捉到了基频涡的饱和、一次和二次对并等现象，显示了大尺度涡结构与入中初始扰动方式之间的内在联系。利用参数Mc观察了压缩性效应对大尺度涡空间演化及其相互作用的影响。第四部分实现了高精度UCD5/SCD6差分算法对非预混扩散火焰化学反应平面混合层的直接数值模拟。研究指出，放热效应可抑制和延迟涡的形成，使基频涡卷拉伸甚至丧失，混合层Reynolds 应力ρu'v'和流向速度波动关联项u'v'下降，以致涡结构与外流动量交换和标量输运减少，脉动输运能力被削弱，从而混合效率、产物生成率和混合层增长率下降，放热主要通过膨胀效应和斜压效应来抑制大尺度涡的演化。

Effects of geometric shape on the hydrodynamics of a self-propelled flapping foil

The hydrodynamics of a free flapping foil is studied numerically. The foil undergoes a forced vertical oscillation and is free to move horizontally. The effect of chord-thickness ratio is investigated by varying this parameter while fixing other ones such as the Reynolds number, the density ratio, and the flapping amplitude. Three different flow regimes have been identified when we increase the chord-thickness ratio, i.e., left-right symmetry, back-and-forth chaotic motion, and unidirectional motion with staggered vortex street. It is observed that the chord-thickness ratio can affect the symmetry-breaking bifurcation, the arrangement of vortices in the wake, and the terminal velocity of the foil. The similarity in the symmetry-breaking bifurcation of the present problem to that of a flapping body under constraint is discussed. A comparison between the dynamic behaviors of an elliptic foil and a rectangular foil at various chord-thickness ratios is also presented.

Numerical study on heavy rigid particle motion in a plane wake flow by spectral element method

Experimental particle dispersion patterns in a plane wake flow at a high Reynolds number have been predicted numerically by discrete vortex method (Phys. Fluids A 1992; 4:2244-2251; Int. J. Multiphase Flow 2000; 26:1583-1607). To address the particle motion at a moderate Reynolds number, spectral element method is employed to provide an instantaneous wake flow field for particle dynamics equations, which are solved to make a detail classification of the patterns in relation to the Stokes and Froude numbers. It is found that particle motion features only depend on the Stokes number at a high Froude number and depend on both numbers at a low Froude number. A ratio of the Stokes number to squared Froude number is introduced and threshold values of this parameter are evaluated that delineate the different regions of particle behavior. The parameter describes approximately the gravitational settling velocity divided by the characteristic velocity of wake flow. In order to present effects of particle density but preserve rigid sphere, hollow sphere particle dynamics in the plane wake flow is investigated. The evolution of hollow particle motion patterns for the increase of equivalent particle density corresponds to that of solid particle motion patterns for the decrease of particle size. Although the thresholds change a little, the parameter can still make a good qualitative classification of particle motion patterns as the inner diameter changes.

Generalization of the JTZ model to open plane wakes

The JTZ model [C. Jung, T. T¶el and E. Ziemniak, Chaos 3, (1993) 555], as a theoretical model of a plane wake behind a circular cylinder in a narrow channel at a moderate Reynolds number, has previously been employed to analyze phenomena of chaotic scattering. It is ex- tended here to describe an open plane wake without the con¯ned nar- row channel by incorporating a double row of shedding vortices into the intermediate and far wake. The extended JTZ model is found in qualitative agreement with both direct numerical simulations and ex- perimental results in describing streamlines and vorticity contours. To further validate its applications to particle transport processes, the in- teraction between small spherical particles and vortices in an extended JTZ model °ow is studied. It is shown that the particle size has signif- icant in°uences on the features of particle trajectories, which have two characteristic patterns: one is rotating around the vortex centers and the other accumulating in the exterior of vortices. Numerical results based on the extended JTZ model are found in qualitative agreement with experimental ones in the normal range of particle sizes.