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  1. 40 大学院工学研究科・工学部
  2. 40D 学位論文
  3. 博士論文 本文
  4. 2023年度

Heat Transfer Mechanism and Thermal Performance of a Channel with Baffles having Open Wings

http://hdl.handle.net/10076/0002000818
http://hdl.handle.net/10076/0002000818
2fe12f47-060a-4319-b14f-55f1259c3477
名前 / ファイル ライセンス アクション
2023DE0308.pdf 2023DE0308.pdf (12.5 MB)
Item type 学位論文 / Thesis or Dissertation(1)
公開日 2024-06-10
タイトル
タイトル Heat Transfer Mechanism and Thermal Performance of a Channel with Baffles having Open Wings
言語 en
言語
言語 eng
資源タイプ
資源タイプ識別子 http://purl.org/coar/resource_type/c_db06
資源タイプ doctoral thesis
アクセス権
アクセス権 open access
アクセス権URI http://purl.org/coar/access_right/c_abf2
著者 Eiamsa-Ard, Smith

× Eiamsa-Ard, Smith

en Eiamsa-Ard, Smith

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著者(ヨミ)
姓名 イアムサード, スミス
言語 ja-Kana
抄録
内容記述タイプ Abstract
内容記述 For more than a century, heat exchangers have been widely used in cooling/heating systems in many commercial applications such as solar air heating, refrigeration, gas turbines, vehicle manufacturing, chemical engineering, and power plant industries. The major challenge in producing a heat exchanger is to intensify its heat transfer rate with a minimum friction loss penalty. Several heat transfer augmentation techniques have been applied and developed. One of the most widely used techniques is employing transverse baffles/ribs to alter flow structures by generating a recirculation and reattachment. The former separates the fluid from heat transfer surfaces while the latter facilitates the contact between fluid and heat transfer surfaces and thus the heat transfer rate. The thesis seeks ways to minimize the recirculation and intensify the flow reattachment by forming wings on the baffles.
In the first part of this thesis, heat transfer augmentation of newly designed perforated V-type baffles with semi-circular wings (SCW-PVBs) was examined. For a better understanding of the reasons behind the heat transfer by the baffles, a numerical analysis of the heat transfer mechanism and flow topology of channels was carried out. The effects of geometric parameters: pitch ratios (PR = 0.5, 1.0, 1.5 and 2.0), blockage ratios (BR = 0.1, 0.15 and 0.2), wing attack angles (θ = 5°, 10° and 15°) on heat transfer of air flow were studied in the turbulent region. The results of the channel installed with SCW-PVBs were compared with those of a smooth channel and the one with solid V-type baffles (VBs). The numerical results showed that the application of the SCW-PVBs having smaller pitch ratios and larger blockage ratios resulted in better heat transfer enhancement and higher pressure drop. The maximum heat transfer enhancement of 5.57 times over the smooth channel was found at a pitch ratio of 0.5, a blockage ratio of 0.2, wing attack angle of 10°. In addition, SCW-PVBs gave higher heat transfer and thermal performance factors (TPF) and lower pressure losses than VBs by around 1.73-8.98%, 5.41-26.84% and 4.51-15.22%, respectively depending on Reynolds number, blockage ratio, pitch ratio and wing attack angle. The maximum TPF of 2.6 was achieved by the SCW-PVBs having a blockage ratio of 0.1, a pitch ratio of 0.5 and wing attack angle of 10°.
The second part of the thesis aimed to experimentally investigate heat transfer enhancement in the channels installed with (1) perforated transverse baffles with square wings (SW-PBs) and (2) perforated V-type baffles with semi-oval/square/delta wings (SOW-PVBs/SW-PVBs/DW-PVBs). The effects of wing attack angles (θ = 0° (solid baffles), 22.5°, 45°, 67.5°, and 90°) and Reynolds numbers on the heat transfer performance characteristics were examined. All channels had an aspect ratio (W:H) of 3.75:1. All baffles had a width (w) of 150 mm and a perforated cross-sectional area of 64 mm2. During experiments, the lower walls of the channels were evenly heated, while the other walls were insulated. The temperature contours on the heated surface were acquired via a thermochromic liquid crystal (TLC) image-processing method. At the proper attack angles (θ = 22.5° and 45°), the modified baffles offered greater heat transfer rates and caused lower friction losses, resulting in higher TPFs than the solid baffles. In the current thesis, the greatest TPF was found at θ of 45°. The Nusselt number contours indicated that the modified baffles introduced multiple impinging jets which suppressed the size of the recirculation flow and allowed better contact between the fluid flow and the channel walls as compared to the solid ones. The jets impinged on the wall in different ways depending on the shapes of the wings and attack angles. Experimental results also suggested that the SW-PVBs gave TPF over those of the other modified baffles (SW-TBs/DW-PVBs/SOW-PVBs), owing to the higher heat transfer rate and lower pressure losses. The findings in this thesis are applicable to improving solar air heaters also other thermal systems.
言語 en
内容記述
内容記述タイプ Other
内容記述 本文/Division of System Engineering Graduate School of Engineering Mie University, Japan
内容記述
内容記述タイプ Other
内容記述 221p
書誌情報
発行日 2024-03-25
フォーマット
内容記述タイプ Other
内容記述 application/pdf
著者版フラグ
出版タイプ VoR
出版タイプResource http://purl.org/coar/version/c_970fb48d4fbd8a85
出版者
出版者 三重大学
出版者(ヨミ)
値 ミエダイガク
学位名
学位名 博士(工学)
学位授与機関
学位授与機関識別子Scheme kakenhi
学位授与機関識別子 14101
学位授与機関名 三重大学
学位授与年月日
学位授与年月日 2024-03-25
学位授与番号
学位授与番号 甲工学第2259号
資源タイプ(三重大)
値 Doctoral Dissertation / 博士論文
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