Proceedings of the workshop on conclusions and lessons learnt from the livelihood study. Phnom Penh, Cambodia, 26-27 September 2002

This workshop is to follow-up the study on livelihoods of farmers and fishers in Kandal, Kampong Chhnang and Kratie provinces in Cambodia. It was the fourth workshop, part of an ongoing series of activities that will inform the Community Fisheries Development (CFD) Office of the Department of Fisheries (DOF), of the development of and changes in the fisheries law as it affects poor users of aquatic resources.(41 p.)

Numerical Investigation of Toroidal Shock Wave Focusing

In this paper,focusing of a toroidal shock wave propagating from a shock tube of an- nular cross-section into a cylindrical chamber was investigated numerically with the dispersion- controlled scheme. For CFD validation, the numerical code was rst applied to calculate both viscous and inviscid ows at a low Mach number of 1.5, which was compared with the experi- ment results and got better consistency. Then the validated code was used to calculate several cases for high Mach numbers. From the result, several major factors that in uent the ow, such as the Mach number and the viscosity, were analyzed detailedly and along with the high Mach number some unusual ow structure was observed and explained theoretically

Computation of flow over a rotating body on unstructured Chimera mesh

Flow around moving boundary is ubiquitous in engineering applications. To increse the efficienly of the algorithm to handle moving boundaries is still a major challenge in Computational Fluid Dynamics (CFD). The Chimera grid method is one type of method to handle moving boundaries. A concept of domain de-composition has been proposed in this paper. In this method, sub-domains are meshed independently and governing equations are also solved separately on them. The Chimera grid method was originally used only on structured (curvilinear) meshes. However, in a problem which involves both moving boundary and complex geometry, the number of sub-domains required in a traditional (structured) Chimera method becomes fairly large. Thus the time required in the interior boundary locating, link-building and data exchanging also increases. The use of unstructured Chimera grid can reduce the time consumption significantly by the reduction of domain(block) number. Generally speaking, unstructured Chimera grid method has not been developed. In this paper, a well-known pressure correction scheme - SIMPLEC is modified and implemented on unstructured Chimera mesh. A new interpolation scheme regarding the pressure correction is proposed to prevent the possible decoupling of pressure. A moving-mesh finite volume approach is implemented in an inertial reference frame. This approach is then used to compute incompressible flow around a rotating circular and elliptic cylinder. These numerical examples demonstrate the capability of the proposed scheme in handling moving boundaries. The numerical results are in good agreement with other experimental and computational data in literature. The method proposed in this paper can be efficiently applied to more challenge cases such as free-falling objects or heavy particles in fluid.

Improving turbomachinery design process management

It is widely acknowledged that a company's ability to aquire market share, and hence its profitability, is very closely linked to the speed with which it can produce a new design. Indeed, a study by the U.K. Department of Trade and Industry has shown that the critical factor which determines profitability is the timely delivery of the new product. Late entry to market or high production costs dramatically reduce profits whilst an overrun on development cost has little significant effect. This paper describes a method which aims to assist the designer in producing higher performance turbomachinery designs more quickly by accelerating the process by which they are produced. The adopted approach combines an enhanced version of the 'Signposting' design process management methodology with industry-standard analysis codes and Computational Fluid Dynamics (CFD). It has been specifically configured to enable process-wide iteration, near instantaneous generation of guidance data for the designer and fully automatic data handling. A successful laboratory experiment based on the design of a large High Pressure Steam Turbine is described and this leads on to current work which incorporates the extension of the proven concept to a full industrial application for the design of Aeroengine Compressors with Rolls-Royce plc.

有反应的双流体模型中两相流量守恒问题的研究

在单相流动CFD数值模拟中,对计算域出口进行流量守恒的修正是保证程序稳定和计算结果合理的有效手段。本文结合作者实际的模拟工作,探讨了在复杂的湍流两相流动,湍流两相反应流动中出口流量修正问题,给出了基于双流体模型的出流边界条件,为复杂反应流动的CFD模拟提供了有益的经验。

Rayleigh-Taylor不稳定的物理模型和数值模拟

界面不稳定是自然界和工业中流动的普遍现象。本文以Rayleigh-Taylor不稳定性为范例,说明基于物理思想的CFD方法在流动问题研究中的应用。为了确定自由面,以往的Lagrange坐标法、阵面跟踪法在界面发生大变形时都会失效。同时,因流动不稳定从层流发展到湍流要经历若干阶段。因此,如何追踪演化过程的界面变形和如何确定湍流模型是R-T不稳定性研究中的主要困难。本文将溶质浓度差异视为导致介质轻重不同的原因,在不稳定发展过程中发生对流和混合。我们提出采用被动标量的大涡模拟方法来模拟R-T不稳定。鉴于该物理模型考虑了流体粘性和物质扩散的影响,可以自动确定阵面,完整描述不稳定从线性小扰动阶段、经过非线性变形阶段、剪切不稳定阶段到湍流混合阶段,真实重现了现象的物理过程,所以更为优越。通过比较尖钉和气泡阵面前进速度和计算亚格子分量的份

扩散抛物化(DP)NS方程组的意义及其在计算流体力学中的应用

本文首先讨论扩散抛物化(DP)NS方程组的早期研究工作:它的提出、数学性质、意义和在CFD中的应用,然后讨论扩散抛物化理论的一些新发展。这些新发展是对NS方程组数值计算进行物理分析的基础上得到的,其中包括NS方程组差分计算时,粘性剪切流对网格间距和格式精度的要求;粘性项只保留剪切粘性项的广义扩散抛物化(GDP)NS方程组,它的性质和应用。由于高Re数流动在NS方程组的差分计算中,网格Re数彼此相差悬殊的特点,产生了计算离散单元守恒方程组的新的算法思路,即离散流体力学(DFD)算法。在DFD算法中需要同时计算三种不同的守恒方程组(Euler,DPNS和NS方程组)。本文讨论了DFD格式的构造、它的优点和应用。并以超声速绕前后台阶流动为算例,来说明GDPNS方程组的用处和DFD算法的优点。DPNS方程组、GDPNS方程组、DFD算法是高智提出的,对这些问题他和合作者从

Optimización del Uso de Hormigones Autocompactantes Reforzados con Fibras de Acero en Aplicaciones Convencionales de Resistencias Moderadas

El objetivo de la presente tesis doctoral, se centra en plantear las posibilidades estructurales de fibras cortas de acero como refuerzo de la matriz de hormigón, habitualmente denominado HRFA, junto con la posibilidad de proporcionarle propiedades autocompactantes, que mejoren ciertos aspectos del material, formando el denominado Hormigón Autocompactante Reforzado con Fibras de Acero (HACRFA), en determinadas condiciones, gracias a las propiedades y características que se han atestiguado en este documento. Para tal fin y a diferencia de la mayoría de las experiencias anteriores que conocemos, se construye y analiza un tramo de muro de gran envergadura (3 metros de alto y 6 metros de largo). Este planteamiento permite estudiar la disposición de las fibras de acero dentro de un elemento estructural de gran tamaño y ejecutado en condiciones reales de obra, para determinar el comportamiento del material teniendo en cuenta todos los condicionantes posibles, algunos de los cuales no están presentes en las investigaciones de laboratorio. La exhaustiva caracterización del material que compone la estructura, conlleva la división del muro en 380 probetas de diversos tamaños que se someten a prometedores ensayos no destructivos y a los habituales ensayos destructivos. Las correlaciones establecidas entre ambos campos, posibilitan la determinación de aspectos resistentes de forma indirecta y sin dañar el material, estableciendo nuevas vías para un interesante control de calidad sobre la propia estructura. Para complementar el análisis a posteriori, se establece una metodología para determinar de manera previa a la ejecución de los trabajos la orientación de las fibras dentro de la masa de hormigón. Las simulaciones realizadas por medio de la Dinámica Computacional de Fluídos, permiten además establecer una serie de estimaciones de las resistencias residuales del material a partir de la orientación de las fibras prevista, detectando a priori puntos débiles o inadecuados procesos de hormigonado. Como colofón se realiza una comparativa económica y sostenibilidad medioambiental entre la aplicación a depósitos de contención cilíndricos propuesta, ejecutada por un lado mediante un hormigón convencional y el HACRFA por el otro. Cada sistema presenta sus ventajas y desventajas pero se concluye que el HACRFA puede resultar igual o más económico y sostenible, que un diseño estructural convencional. Estos trabajos se enmarcan dentro de las investigaciones desarrolladas por el Área de Conocimiento de Ingeniería de la Construcción adscrito al Departamento de Ingeniería Mecánica de la Universidad del País Vasco / Euskal Herriko Unibertsitatea (UPV/EHU).

Parametric Study of the Device Angle Dependency of a Single Vortex Generator on a Flat Plate

Ponencia presentada en el 10th World Congress on Computational Mechanics (WCCM 2012), Sao Paulo (Brazil).Publicados los abstracts en documento con ISBN: 978-85-86686-69-6.

Framework for the Shape Optimization of Aerodynamic Profiles Using Genetic Algorithms

This study developed a framework for the shape optimization of aerodynamics profiles using computational fluid dynamics (CFD) and genetic algorithms. Agenetic algorithm code and a commercial CFD code were integrated to develop a CFD shape optimization tool. The results obtained demonstrated the effectiveness of the developed tool. The shape optimization of airfoils was studied using different strategies to demonstrate the capacity of this tool with different GA parameter combinations.

基于神经网络技术的乘波体优化设计

乘波体是高超声速飞行器的主要组成部分,也是飞行器产生升力的主要部分.针对基于计算流体动力学(CFD)分析的乘波体优化设计问题,引入人工神经元网络响应面方法.选取一定数量的乘波体外形,进行气动性能分析后,利用乘波体的外形控制参数和气动参数做为训练样本对乘波体进行训练.利用这些训练样本对人工神经网络进行训练.在优化计算中以充分训练的神经网络替代CFD分析,发展了一种基于神经网络技术的乘波体优化设计方法.利用该方法在马赫数6、雷诺数7×10~6条件下,分别对乘波体进行了最大升阻比的单目标和综合考虑升阻比、容积及表面积的多目标优化.计算结果表明,采用神经网络响应面技术可在保证计算稳定性的条件下有效提高计算效率.

流量配比对Coil增益分布影响的数值研究

利用三维CFD技术,通过求解层流Navier-stokes方程与组分输运方程,对简化后的化学氧碘激光RADICL模型进行数值模拟与分析,结合10种组分和21个基元反应的化学反应模型,对COIL亚声速段横向射流情况下,不同的主副流流量配比对化学氧碘激光器性能的影响进行分析与比较.结果证明,过高或过低的碘分子浓度状态均不利于合理、可观的小信号增益系数产生.存在一个最佳流量配比范围,与之对应的工作状态下,COIL的小信号增益系数会得到显著提高.

Development of an efficient particle approach for micro-scale gas flow simulations

The micro-scale gas flows are usually low-speed flows and exhibit rarefied gas effects. It is challenging to simulate these flows because traditional CFD method is unable to capture the rarefied gas effects and the direct simulation Monte Carlo (DSMC) method is very inefficient for low-speed flows. In this study we combine two techniques to improve the efficiency of the DSMC method. The information preservation technique is used to reduce the statistical noise and the cell-size relaxed technique is employed to increase the effective cell size. The new cell-size relaxed IP method is found capable of simulating micro-scale gas flows as shown by the 2D lid-driven cavity flows.

超燃燃料和空气混合及燃烧的数值模拟

本文通过数值模拟中国科学院力学研究所高温气动实验室两组超燃燃烧室实验，来校核CFD程序和所用物理化学模型。实验分两组，第一组为冷流无燃烧实验，第二组为热流有燃烧室实验，每组分有燃料喷射和无燃料喷射两种工况。这四个实验中都对燃烧室侧壁中心线的压力进行了测量，计算结果和实验符合较好，初步验证了所用CFD程序和模型对于超燃燃烧室数值模拟的可行性。下一步科研计划是比较不同煤油反应机理对流场影响。