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研究生: 張馨云
Chang, Hsin-Yun
論文名稱: 小型垂直軸風機尾流於開放式風洞中實驗量測與模擬分析比較
Comparison of Experimental Measurements and Numerical Simulations for Vertical Axis Wind Turbine Wakes in an Open-Jet Wind Tunnel
指導教授: 吳毓庭
Wu, Yu-Ting
學位類別: 碩士
Master
系所名稱: 工學院 - 工程科學系
Department of Engineering Science
論文出版年: 2018
畢業學年度: 106
語文別: 英文
論文頁數: 74
中文關鍵詞: 垂直軸風機風機尾流分析風洞實驗量測動態皮托管熱線測 速CFD 模擬
外文關鍵詞: Vertical axis wind turbine, Wind-turbine wake analysis, Wind tunnel experiment, Cobra probe, Hot-wire anemometer, CFD simulation
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  • 能源的使用使人類生活更加地進步,科技發展的進步也促使著能源的消耗增加。發展再生能源成為我們解決能源匱乏問題的方法,其中風力發電更是世界各國所關注的重點。風力發電機依據結構分為垂直軸式與水平軸式,水平軸式風機常見應用於空曠的空間其高風速時發電效率高,但在發電潛力上垂直軸式風機也不惶多讓,有著不受使用場所及來流風向的限制。相關垂直軸風機的研究中多關於其性能特性的分析比較,但了解垂直軸風機的尾流特徵對於風能開發也相當重要。
    本研究利用實驗測量和CFD模擬兩種方式來探討小型垂直軸風機尾流於開放式風洞的流場特性,風機模型為一翼型為NACA9412的小型四葉垂直軸式風機。在實驗部份我們分別使用眼鏡蛇探針與熱線風速計做為實驗測量的儀器,比較量測儀器間的不同的量測特性。在CFD模擬部分,使用大渦旋模擬法求解暫態的Navier-Stokes方程式。我們使用分離求解器中的SIMPLE算法與耦合求解器中的coupled算法分別求解並比較尾流特徵。我們將分析無因次化平均時間流向速度與垂直流向速度、流向速度與垂直流向速度的紊流強度、水平剖面的動量通量,並用頻譜分析結果對此實驗所量測到的資料提供可靠度。通過比較垂直軸風機尾流的實驗測量和CFD模擬有助於了解垂直軸風機後尾流特性幫助風力能源的發展。

    Energy made human life progress, and science technology advanced faces an issue which the energy consumption increased. Using the renewable energy is a method for solving the problem of energy scarcity, the wind power generation has more interest in the countries around the world. The wind turbines are according to their structures divided into vertical axis wind turbine (VAWT) and horizontal axis wind turbine (HAWT). The HAWT has commonly applied in open space and that the high efficiency at high wind speed. However, the VAWT has unlimited potential in power generation which the advantage is not a lot of restrictions on the site and the flow direction. The research relevant the VAWT is mostly about the analysis and comparison of its performance characteristics. The wake characteristics are also important for wind energy development.
    In this study, comparison of experimental measurements and numerical simulations for vertical axis wind turbine wakes in an open-jet wind tunnel which the wind turbine model is an airfoil NACA9412 four-blade VAWT. The two kinds of experimental measuring instruments in the experiment which are the cobra probe and the hot wire probe for comparing the result between different measurement instruments. In the CFD simulation part, the transient Navier-Stokes equations are solved using the Large Eddy Simulation (LES). We use the SIMPLE algorithm in the split solver and the coupled algorithm in the coupled solver for solve and compare the wake characteristics. The results were analyzed normalized time-averaged velocity of streamwise and spanwise, the turbulence intensity for streamwise and spanwise, and momentum flux at the horizontal plane. The spectrum analysis with data collected using the cobra probe and the hot-wire probe shows the expected slope of -5/3 to indicate the inertial subrange, which increases the reliability of the data measured in this experiment. In order to develop the wind energy and accurate VAWT models that though the VAWT wake compaction of the measuring experiment and the CFD simulation.

    中文摘要 I ABSTRACT II ACKNOWLEDGMENTS IV CONTENTS VI LIST OF TABLES VIII LIST OF FIGURES IX NOMENCLATURE XV CHAPTER I INTRODUCTION 1 1-1 Background Information 3 1-2 Literature Review 3 1-3 Content of Research 7 CHAPTER II EXPERIMENTAL EQUIPMENT 8 2-1 Open-jet wind tunnel 8 2-2 Experiment model of vertical axis wind turbine 11 2-3 Hot-wire probe and constant temperature anemometer 14 2-4 Cobra probe 19 2-5 Laser Tachometer 21 2-6 Experimental set-up 23 CHAPTER III SIMULATION SET-UP 26 3-1. Geometry model and mesh generation 28 3-2. Boundary conditions 33 3-3. ANSYS FLUENT calculation framework 36 3-4. Simulation method 38 CHAPTER IV RESULTS AND DISCUSSION 42 4-1 Normalized time-averaged streamwise velocity 43 4-2 Normalized time-averaged spanwise velocity 44 4-3 Turbulence intensity of the streamwise and the spanwise 45 4-4 Normalized lateral momentum flux 46 4-5 Power spectrum analysis 47 4-6 The turbulence intensity on boundary condition 62 CHAPTER V CONCLUSIONS 69 REFERENCES 71

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