研究生: |
曾睿正 Tseng, Jui-Cheng |
---|---|
論文名稱: |
百葉窗型擾流器扇葉攻角與截距對正方形雙通道紊動熱流特性之影響 Influences of Slat Attack Angle and Pitch Ratio on Turbulent Hydrothermal Characteristics in a Louvered Two-Pass Square Channel |
指導教授: |
劉通敏
Liou, Tong-Miin |
口試委員: |
吳興茂
黃柏文 |
學位類別: |
碩士 Master |
系所名稱: |
工學院 - 動力機械工程學系 Department of Power Mechanical Engineering |
論文出版年: | 2018 |
畢業學年度: | 107 |
語文別: | 英文 |
論文頁數: | 138 |
中文關鍵詞: | 百葉窗型擾流器 、扇葉攻角 、截距比 、雙通道熱傳 、質點影像測速儀 、紅外線測溫儀 |
外文關鍵詞: | Louver-Type Turbulator, Slat Attack Angle, Pitch Ratio |
相關次數: | 點閱:1 下載:0 |
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本研究基於 前人 肋條 (Rib)、折流版 (Baffle)以及 二維百葉窗型擾流器進一步 二維百葉窗型擾流器進一步 二維百葉窗型擾流器進一步 二維百葉窗型擾流器進一步 二維百葉窗型擾流器進一步 二維百葉窗型擾流器進一步 二維百葉窗型擾流器進一步 二維百葉窗型擾流器進一步 二維百葉窗型擾流器進一步 二維百葉窗型擾流器進一步 二維百葉窗型擾流器進一步 二維百葉窗型擾流器進一步 設計出一款新型的 三維百葉窗型擾流器, 三維百葉窗型擾流器, 並使用質點影像測速儀 、紅外線測溫儀 、紅外線測溫儀 與壓力傳感器 來量測 其在 正方形雙通道 中導引出 的紊流場結構、壁溫分布 紊流場結構、壁溫分布 紊流場結構、壁溫分布 紊流場結構、壁溫分布 紊流場結構、壁溫分布 紊流場結構、壁溫分布 紊流場結構、壁溫分布 紊流場結構、壁溫分布 紊流場結構、壁溫分布 與壓 損。 其中 百葉窗 型擾流器 扇葉攻角 扇葉攻角 扇葉攻角 扇葉攻角 (𝛼)與截距比 (Pi/DH)的變化範圍 分別為 -40°至 30°以及 1、2、3和∞。雷諾數 雷諾數 在量測紊流場結構時 定為 10,000,而在量測壁溫分布 ,而在量測壁溫分布 與壓 損時 從 5,000變化至 20,000。實驗結果 發現 新型 百葉窗型 擾流器 (Pi/DH = ∞)不僅可以擾動核心流體 消除後方迴旋死區 ,還能 ,還能 ,還能 導引出 四對類似迪恩渦漩的 反向 渦旋 ,並對流道上下壁面形成較強的衝擊冷卻 。相較於前人二維百葉 。相較於前人二維百葉 窗型擾流器 的結果 ,其基於全展紊流圓管的 基於全展紊流圓管的 平均紐賽數 比(𝑁𝑢̅̅̅̅/𝑁𝑢∞)提升 約 12%,而摩擦係 數比 (𝑓̅/𝑓∞)則降低 12%。在固定的 Pi/DH下,流道的𝑁𝑢̅̅̅̅/𝑁𝑢∞與𝑓̅/𝑓∞皆隨著 𝛼的 增加先下 降後 上升 ,其最大值分別為 ,其最大值分別為 3.0與 24.4。當𝛼固定時 ,隨著 ,隨著 Pi/DH減小 , 流道 𝑁𝑢̅̅̅̅/𝑁𝑢∞與𝑓̅/𝑓∞皆單調 增加 ,在 Pi/DH =1時,其最大值分別為 ,其最大值分別為 4.4與 58.9。 其中 𝑁𝑢̅̅̅̅/𝑁𝑢∞與前人結果接近,而 與前人結果接近,而 與前人結果接近,而 𝑓̅/𝑓∞則降低了 44.1%。綜合考慮 熱傳與壓損, 熱傳與壓損, 本研究 於定泵功率下的熱性能係數 泵功率下的熱性能係數 泵功率下的熱性能係數 泵功率下的熱性能係數 泵功率下的熱性能係數 泵功率下的熱性能係數 泵功率下的熱性能係數 泵功率下的熱性能係數 泵功率下的熱性能係數 泵功率下的熱性能係數 (TPF)均較 前人 在相同條件下的結果 相同條件下的結果 相同條件下的結果 相同條件下的結果 相同條件下的結果 相同條件下的結果 相同條件下的結果 相同條件下的結果 提升 2%至 26%。
This study reports an innovative design of 3-D louver-type turbulator based on previous ribs, baffles, and 2-D louver-type turbulators. The effect of the innovative turbulator on turbulent flow field, detailed temperature distribution and pressure drop in a two-pass square channel is investigated by Particle Image Velocimetry (PIV), Infrared Thermography (IRT), and pressure transducer. Four pitch ratios (Pi/DH), including 1, 2, 3, ∞, are examined and the slat attack angle (𝛼) of the louver-type turbulator ranges from -40° to 30°. The Reynolds number (Re) for PIV and IRT measurement is fixed at 10,000 and in the range of 5,000 to 20,000, respectively. It is found that the innovative louver-type turbulators (Pi/DH=∞) not only disturb the core flow and degenerate wake zone behind the turbulator but also induce four pairs of Dean-like counter-rotating vortices which result in strong impingement on the top and bottom walls. Consequently, the averaged Nusselt number ratio (𝑁𝑢̅̅̅̅/𝑁𝑢∞) and friction factor ratio (𝑓̅/𝑓∞) in the present study are respectively 12% higher and 12% lower than those in the previous study. For fixed Pi/DH, both 𝑁𝑢̅̅̅̅/𝑁𝑢∞ and 𝑓̅/𝑓∞ descend and then ascend with increasing 𝛼 with a maximum value of 3.0 and 24.4, respectively. As Pi/DH is varied from 1 to ∞, 𝑁𝑢̅̅̅̅/𝑁𝑢∞ and 𝑓̅/𝑓∞ decreases monotonously for fixed 𝛼. In particular, their maximum values occurring at Pi/DH =1 are respectively 4.4 and 58.9. The value of 𝑁𝑢̅̅̅̅/𝑁𝑢∞ is close to that of the previous data while the value of 𝑓̅/𝑓∞ is 44.1% lower. Considering both heat transfer enhancement and pressure drop, the thermal performance factors (TPF) in the present study are 2%-26% higher than those in previous research.
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