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研究生: 高義明
Kao, Yi-Ming
論文名稱: 內政部建研所環境風洞校驗及二維鈍形體空氣動力流場實驗研究
Calibration of the ABRI Environment Wind Tunnel and Experimental Study of 2-D Bluff-Body Aerodynamic Flows
指導教授: 苗君易
Miau, Jiun-Jih
學位類別: 碩士
Master
系所名稱: 工學院 - 航空太空工程學系
Department of Aeronautics & Astronautics
論文出版年: 2005
畢業學年度: 93
語文別: 中文
論文頁數: 141
中文關鍵詞: 風洞校驗紊流強度流場均勻度流場偏向角平均分離點
外文關鍵詞: wind tunnel calibration, turbulent intensity, flow uniformity, flow angularity, time-mean separation point
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  • 本文之首要目的在於校驗內政部建研所之低速循環式環境風洞(Environment Wind Tunnel),該風洞設有兩測試區,第一測試區截面積為4m×2.6m,長度為36.5m,校驗後流速最高可達36m/s;第二測試區之截面積6m×2.6m,長21m,流速最高為22m/s。流場品質方面主要針對第一測試區進行校驗,經由初步測試並與相關文獻比較後,大致上得到令人滿意的流場品質:入口截面之速度均勻度在低中高三組流速下平均約0.37%,截面中心之紊流強度則低於0.3%,空風洞之邊界層厚度在入口處(x=2m)約60mm。速度20m/s時氣流偏向角α角(pitch angle)與β角
    (yaw angle)分別落在±0.415度及±0.97度之範圍。另外,在入口速度為30m/s時,風洞之全壓損失為576.8pa,能量比為0.939。
    本文另一目的為研究二維圓柱體之空氣動力流場特性,以建立本風洞實驗室所需之實驗量測能量,實驗所設定之雷諾數範圍在176000~548000之間,屬於邊界層轉換區之範圍。所得阻力係數從1.23降低至0.39,此範圍內雷諾數愈大阻力係數愈低,結果與文獻相符合。並利用表面壓力量測結果進一步探討臨界雷諾數下,二維圓柱體之平均分離點與非定常分離特性。

    The main purpose of the study is to calibrate the ABRI wind tunnel that is of closed circuit type with two rectangular test sections. The first test section is 36.5m long and it has a cross section area of 4m×2.6m with maximum speed is approximately 36m/s, the second test section is 20m long and it has a cross section area of 6m×2.6m with maximum speed about 22m/s. The calibration performed included the structural vibration, temperature stability, flow uniformity, turbulent intensity, flow angularity and boundary layer thickness at the inlet of first test section. The results obtained show the flow quality meets design requirements. For instance, at three different velocities measured the mean flow uniformity is less than 0.37%, turbulent intensity is less than 0.35%, boundary layer thickness about 60mm thick at the inlet cross section. At 20m/s, the pitch angle α falls within ±0.415 in degree and yaw angle β falls within ±0.97 in degree. At 30m/s, the total pressure loss and energy ratio are 576.8pa and 0.939, respectively.
    The other purpose of this work is to study the aerodynamic flow around a 2-D circular cylinder. For Reynolds numbers 176000 increased to 548000, the drag coefficient were reduced form 1.23 to 0.39 The drag coefficients found show a good agreement with the results reported in the literature. The pressure measurement results allow one to further investigate the time-mean separation point and the characteristic of unsteadiness of flow separation on the 2-D circular cylinder.

    目 錄 頁次 中文摘要.......................................................Ⅰ 英文摘要.......................................................Ⅱ 誌謝...........................................................Ⅲ 目錄...........................................................Ⅳ 表目錄.........................................................Ⅶ 圖目錄.........................................................Ⅷ 符號說明.......................................................XⅢ 第一章 序論..................................................1 1.1研究動機與目的.............................................1 1.2國內外風洞發展回顧.........................................3 1.3風洞種類介紹...............................................7 1.4風洞校驗之文獻回顧.........................................9 1.5二維圓柱空氣動力流場文獻回顧..............................14 第二章 環境風洞與實驗設備.....................................19 2.1內政部建研所環境風洞介紹..................................19 2.2皮托靜壓管及三孔壓力管....................................22 2.3壓力轉換器................................................22 2.4熱線測速儀量測系統........................................23 2.5資料擷取系統..............................................23 2.6圓柱模型..................................................24 2.7輔助儀器設備..............................................24 第三章 實驗方法與步驟.........................................26 3.1風洞實驗之參數分析........................................26 3.2校驗項目與實驗方法........................................27 3.2.1風洞運轉之穩定性.......................................27 3.2.2流場均勻度.............................................28 3.2.3紊流強度...............................................30 3.2.4流場偏向角.............................................31 3.2.5風洞壓損與能量比(energy ratio).........................32 3.3二維圓柱空氣動力流場量測..................................34 3.3.1表面流場量測...........................................34 3.3.2阻力及阻力係數.........................................35 第四章 結果與討論.............................................37 4.1風洞基本性能校驗結果......................................37 4.1.1風洞運轉穩定性測試.....................................37 4.1.2流場均勻度初步量測.....................................39 4.1.3移動機構干擾效應測試...................................40 4.1.4流場均勻度修正結果.....................................43 4.1.5空風洞邊界層量測.......................................43 4.1.6紊流強度分佈...........................................45 4.1.8流場偏向角量測結果.....................................49 4.1.7風洞壓損及能量比評估...................................48 4.2二維圓柱空氣動力流場量測..................................50 4.2.1圓柱平均壓力分佈與阻力係數量測結果.....................51 4.2.2擾動壓力係數與非定常分離特性探討.......................52 第五章 結論...................................................56 5.1風洞校驗結果..............................................56 5.2高雷諾數下二維圓柱流場量測結果............................58 5.3未來建議..................................................59 參考文獻......................................................61

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