系統識別號 | U0002-0309201214462900 |
---|---|
DOI | 10.6846/TKU.2012.00115 |
論文名稱(中文) | 大雨影響下圓柱體流場之數值模擬 |
論文名稱(英文) | Numerical Simulation of Circular Cylinder Vortex Flow under Heavy Rain Effects |
第三語言論文名稱 | |
校院名稱 | 淡江大學 |
系所名稱(中文) | 航空太空工程學系碩士班 |
系所名稱(英文) | Department of Aerospace Engineering |
外國學位學校名稱 | |
外國學位學院名稱 | |
外國學位研究所名稱 | |
學年度 | 100 |
學期 | 2 |
出版年 | 101 |
研究生(中文) | 陳柏禕 |
研究生(英文) | Po-Yi Chen |
學號 | 699430145 |
學位類別 | 碩士 |
語言別 | 英文 |
第二語言別 | 繁體中文 |
口試日期 | 2012-07-17 |
論文頁數 | 68頁 |
口試委員 |
指導教授
-
宛同
委員 - 洪勵吾 委員 - 湯敬民 |
關鍵字(中) |
圓柱 大雨 二相流 表面粗糙度 空氣動力學 |
關鍵字(英) |
Circular cylinder Heavy Rain Two Phase Flow Surface Roughness Aerodynamics |
第三語言關鍵字 | |
學科別分類 | |
中文摘要 |
近年來,由於氣候變化的影響,極端氣候的現象比過去更為頻繁,如:暴雨、強風、颱風...等,由於考慮到圓柱結構放置在戶外的情況下,我們在設計外型的階段時必須將惡劣氣候的條件考慮進去。因此,對於在大雨影響下柱體尾流情形的數值模擬更為重要且不可忽視。利用商用軟體FLUENT於不同數量和外型的柱體和大雨機制的模擬。 在此篇論文中,我們首先對於在雷諾數為100和200流體流經單一圓柱後的尾流分離做數值模擬。接下來,在對於雷諾數為200的情況下兩個相同直徑前後串聯的圓柱做模擬。透過成功的模擬前面3個不同的情況,我們對於接下來的研究更有信心。模擬雷諾數為2.5×104~1.0×105的LP-810纜線在大雨下的情形,則是採用FLUENT內二相流(Two-Phase Flow)的DPM模組(Discrete Phase Model)和改變圓柱的表面出糙度來計算空氣動力特性。雖然模擬出的結果和實驗值不完全相同,但是我們成功的模擬出LP-810在晴空狀態及大雨影響下阻力係數的變化趨勢。本研究在對於工業用纜線在側風及大雨影響條件下的空氣動力特性分析是非常有用的。 |
英文摘要 |
In recent years, due to the impact of climate changing, the phenomenon of extreme weather is more frequently compared to the past, such as heavy rain, strong wind, typhoon-weather conditions etc. For the cylindrical structure being located outdoors, we must put these severe weather influences into considerations in the stage of geometry design. Therefore, the importance of numerical simulation for circular cylinder vortex flow under the heavy rain effects can never be neglected. In this work, we first investigated the vortex shedding behind a circular cylinder at Re=100 and 200. Secondly, two circular cylinders in tandem arrangement at Re=200 are simulated also. Through the simulation of these three cases successfully, we will be more confident for the following research. For the heavy rain simulations, the two-phase flow approach plus the wall film mechanism on the body surface are implemented for LP-810 cable and at Re=2.5×104 to 1.0×105. Although the numerical results for the cable under the heavy rain effects show that aerodynamic degradation was not perfectly match to the experimental data, the correct tendency of the cable aerodynamic performance under both the clear weather and heavy rain situations are simulated successfully. The proposed simulation results will be quite useful to understand the industrial suspension cable’s behavior in cross wind and heavy rain conditions. |
第三語言摘要 | |
論文目次 |
Contents Abstract I Contents III List of Tables IV List of Figures V Nomenclatures VII Chapter 1 Introduction 1 Chapter 2 Research Background 4 Chapter 3 Characteristics of Rain 9 Chapter 4 Numerical Modeling 13 4-1 Geometry Model Construction 13 4-2 Grid Generation 16 4-3 Flow Solver 20 4-4 Turbulence Modeling 23 4-5 Discrete Phase Model 25 4-6 Surface Roughness 29 4-7 Heavy Rain Physics 31 Chapter 5 Results and Discussion 34 Chapter 6 Conclusions 55 References 57 List of Tables Table 5-1 The average drag coefficients and Strouhal number for a single circular cylinder at Re=100 and Re=200 [9] 38 Table 5-2 Numerical results for a single circular of pressure and viscous drag coefficient at Re=100 and 200 39 Table 5-3 The Strouhal number and mean drag coefficients for two circular cylinders in tandem arrangement at Re=200 40 Table 5-4 Numerical results for two circulars of pressure and viscous drag coefficient at Re=200 41 Table 5-5 The drag coefficient of the LP-810 cable for different turbulence models 43 Table 5-6 The comparison of the drag coefficient for the cable and smooth circular cylinder with V=10 m/s and V=40 m/s 46 Table 5-7 Heavy rain conditions 47 Table 5-8 Numerical results for cable LP-810 of drag coefficients degradation percentage 49 Table 5-9 Experiment results for cable LP-810 of drag coefficients degradation percentage [19] 49 Table 5-10 Numerical results for cable LP-810 of viscous drag coefficients degradation percentage 51 Table 5-11 Numerical results for cable LP-810 of pressure drag coefficients degradation percentage 51 List of Figures Figure 2-1 Regimes of fluid flow over a circular cylinder [4] 7 Figure 2-2 Normalized distribution of the total data sample [16] 10 Figure 4-1 Computational domain of a single circular cylinder 14 Figure 4-2 Computational domain of two circular cylinders in tandem arrangement 14 Figure 4-3 The geometric model of cable compared to Kikuchi's Model [19]. (a) Kikuchi's Model (LP-810) and (b) present numerical model 15 Figure 4-4 Computational domain of cable LP-810 15 Figure 4-5 Mesh of the entire calculation domain for a single cylinder 17 Figure 4-6 Near mesh of a single circular cylinder 17 Figure 4-7 Mesh of the entire calculation domain for two cylinders 18 Figure 4-8 Near mesh of the downstream cylinder 18 Figure 4-9 Mesh of the entire calculation domain for cable LP-810 19 Figure 4-10 Near mesh of cable LP-810 19 Figure 4-11 Physics of splashing, momentum, heat, and mass transfer for the Wall-Film [20] 27 Figure 5-1 (a) Vorticity (b) Pressure field at Re=100 35 Figure 5-2 (a) Vorticity (b) Pressure field at Re=200 36 Figure 5-3 Lift and drag coefficient for a single cylinder at Re=100 37 Figure 5-4 Lift and drag coefficient for a single cylinder at Re=200 37 Figure 5-5 Pressure and viscous drag for a single cylinder at Re=100 and 200 38 Figure 5-6 (a) Vorticity and (b) Pressure contours for two circular cylinders in tandem arrangement 40 Figure 5-7 The averaged drag coefficient for LP-810 cable numerical and experimental results..................................................................................42 Figure 5-8 Drag coefficient for cable LP-810 numerical result comparing to experimental data 42 Figure 5-9 Pressure contours for different free stream velocities with LWC=0 g/m3 44 Figure 5-10 Vorticity contours for different free stream velocities with LWC=0 g/m3 45 Figure 5-11 Local view of rain droplets impingement 48 Figure 5-12 Drag coefficient for cable LP-810 numerical and experimental results 50 Figure 5-13 Viscous drag coefficient for different wind speed with LWC=0 g/m3 and LWC=9.23 g/m3 52 Figure 5-14 Pressure drag coefficient for different wind speed with LWC=0 g/m3 and LWC=9.23 g/m3 52 Figure 5-15 Pressure contours for different free stream velocity with LWC=9.23 g/m3 53 Figure 5-16 Vorticity contours for different free stream velocity with LWC=9.23 g/m3 54 |
參考文獻 |
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