English  |  正體中文  |  简体中文  |  Items with full text/Total items : 49287/83828 (59%)
Visitors : 7155495      Online Users : 55
RC Version 7.0 © Powered By DSPACE, MIT. Enhanced by NTU Library & TKU Library IR team.
Scope Tips:
  • please add "double quotation mark" for query phrases to get precise results
  • please goto advance search for comprehansive author search
  • Adv. Search
    HomeLoginUploadHelpAboutAdminister Goto mobile version
    Please use this identifier to cite or link to this item: http://tkuir.lib.tku.edu.tw:8080/dspace/handle/987654321/38269


    Title: 直接甲醇燃料電池陽極流道設計與數值分析
    Other Titles: The Anode Flow Channel Design and Numerical Analysis of the Direct Methanol Fuel Cell
    Authors: 管衍德;李世鳴;張靜怡
    Contributors: 淡江大學機械與機電工程學系;淡江大學航空太空工程學系
    Keywords: 燃料電池;直接甲醇燃料電池;計算流體力學;Fuel Cell;DMFC;CFD
    Date: 2006-03
    Issue Date: 2010-01-11 15:00:12 (UTC+8)
    Publisher: 臺北縣淡水鎮:淡江大學
    Abstract: 本文主要是針對直接甲醇燃料電池之陽極流道,進行數值模擬分析與可視化實驗量測,並將兩者結果做一比對,進而進行電池性能量測。設計的目的在增進甲醇溶液補充至電池中的均勻性與一致性,較佳的流道設計能加強流體的擴散和對流能力,有助於提高電池效能。文中所使用的計算流體力學軟體,為美國FLUENT 公司的FLUENT 軟體。
    The objective of this paper is to make the numerical analysis and experimental visualization on the anode flow channel desing of the direct methanol fuel cell (DMFC). Both results are compared with each other;moreover, a DMFC was conducted the performance measurements under the different flow channels. The main design purpose is to increase the uniformity of the methanol solution supply. A better flow channel design could enhance the diffusion and convection phenomena and raise the DMFC performance. The CFD tools used in the study is FLUENT, by FLUENT Inc. USA.
    Relation: 第五屆海峽兩岸航空太空學術研討會論文集,頁149-154
    Appears in Collections:[機械與機電工程學系暨研究所] 會議論文
    [航空太空工程學系暨研究所] 會議論文

    Files in This Item:

    File SizeFormat
    index.html0KbHTML108View/Open

    All items in 機構典藏 are protected by copyright, with all rights reserved.


    DSpace Software Copyright © 2002-2004  MIT &  Hewlett-Packard  /   Enhanced by   NTU Library & TKU Library IR teams. Copyright ©   - Feedback