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Wake aerodynamics for 2D bluff bodies.

机译:二维钝体的空气动力学特性。

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摘要

Wake aerodynamics of bluff bodies is a vast and challenging domain and new theoretical, experimental or numerical approaches to this subject are expected to produce a great impact on a large palette of academic and practical topics.;A new description of the wake turbulent field is introduced in the present doctoral research. This wake model is further on applied to loading problems on isolated and buffeted structures.;Following a comprehensive review, a wake turbulence model is defined. Making use of a simple "variable filtering" eduction method, focusing on coherent turbulence rather than on random turbulence, and employing flow dimensions rather than body dimensions the similarity (self preservation) and universality (independence of constraint) of turbulence profiles is demonstrated for both smooth and turbulent flows. Longitudinal (downstream) variation of different wake parameters is introduced and used to demonstrate the validity of the vortex eduction method. CFD simulations by FLOW3D code are presented for different shapes for both steady and transient scenarios employing various turbulence models. Results are compared with present and other experimental data.;Direct applicability of the wake model for buffeting problems is found and tested. As a primary step an improvement of existing self-induced loading models for isolated structures is presented. A modified notched-hodograph theory is employed for drag and fluctuating lift modeling and comparison to experiment is provided. Based on vorticity-circulation calculations, the wake geometry for various 2D bluff bodies is analysed and the notched hodograph theory is completed with a r.m.s. lift model (L Model) with improved simulation qualities in terms of results and applicability.;A detailed investigation of the buffeting loading problem for sharp edged bluff bodies is addressed. Tandem and staggered configurations are studied in both smooth, large scale and small scale turbulent flows for various shapes and geometries. Characterisation and partition of the buffeting domain is provided. Semi-empirical models for force coefficients and Strouhal number are defined for the upstream wake inertial domain. The term 'inertial' is used somewhat loosely here but it defines the part of the wake field for which the body related turbulence production (close wake) and the dissipation effects (far wake) are in a certain equilibrium. This domain also corresponds to the similar and universal wake model previously defined (Chapter 2). Spectral modeling is also introduced and a new approach is proposed for drag loading so that wind-load linear dependence is extended. Collateral to this, an interesting centre-wake wind spectral analysis is provided and it is shown how transition from sub-inertial to inertial spectral behaviour is enhanced by free-stream turbulence. LASER flow visualisations are employed for a better understanding of critical interference regimes such as bi-stable flow situations.;Finally an original classification of 2D bluff bodies is proposed and this relies on both wake flow and wake loading aerodynamics.
机译:钝体的尾流空气动力学是一个广阔而具有挑战性的领域,该学科的新的理论,实验或数值方法有望对众多的学术和实践课题产生巨大的影响。在目前的博士研究中。该尾流模型将进一步应用于孤立的自助餐结构上的荷载问题。在全面审查之后,定义了尾流湍流模型。利用简单的“可变过滤”方法,重点关注相干湍流而不是随机湍流,并采用流量尺寸而非身体尺寸,对两种湍流分布图的相似性(自我保持)和通用性(约束的独立性)进行了证明。平稳而湍流。介绍了不同尾流参数的纵向(下游)变化,并用于证明涡旋消散方法的有效性。针对使用各种湍流模型的稳态和瞬态情况下的不同形状,提出了通过FLOW3D代码进行的CFD仿真。将结果与当前和其他实验数据进行比较。;发现并测试了唤醒模型对抖振问题的直接适用性。作为第一步,提出了一种针对隔离结构的现有自感应荷载模型的改进方法。提出了一种改进的刻痕波谱仪理论,对阻力和脉动升力进行了建模,并与实验进行了比较。根据涡流环流计算,分析了各种2D钝体的尾流几何形状,并用r.m.s完成了带缺口的全息图理论。提升模型(L模型),在结果和适用性方面具有改进的仿真质量。提出了对尖锐的钝形体的抖振载荷问题的详细研究。研究了在各种形状和几何形状的平滑,大比例和小比例湍流中的串联和交错构型。提供了抖抖域的特征和分区。为上游尾流惯性域定义了力系数和Strouhal数的半经验模型。术语“惯性”在这里有些宽松,但它定义了尾流场中与身体相关的湍流产生(近尾流)和耗散效应(远尾流)处于一定平衡的部分。该域还对应于先前定义的相似通用唤醒模型(第2章)。还介绍了频谱建模,并提出了一种新的阻力加载方法,从而扩展了风荷载线性相关性。与此相伴的是,提供了一个有趣的中心苏醒风频谱分析,它显示了如何通过自由流湍流来增强从次惯性到惯性频谱行为的转变。激光流动可视化用于更好地理解关键干扰机制,例如双稳态流动情况。最后,提出了二维钝体的原始分类,该分类依赖于尾流和尾流空气动力学。

著录项

  • 作者

    Hangan, Horia Mihai.;

  • 作者单位

    The University of Western Ontario (Canada).;

  • 授予单位 The University of Western Ontario (Canada).;
  • 学科 Engineering Aerospace.;Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 1996
  • 页码 299 p.
  • 总页数 299
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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