淡江大學機構典藏:Item 987654321/38206
English  |  正體中文  |  简体中文  |  全文筆數/總筆數 : 62819/95882 (66%)
造訪人次 : 4006633      線上人數 : 558
RC Version 7.0 © Powered By DSPACE, MIT. Enhanced by NTU Library & TKU Library IR team.
搜尋範圍 查詢小技巧:
  • 您可在西文檢索詞彙前後加上"雙引號",以獲取較精準的檢索結果
  • 若欲以作者姓名搜尋,建議至進階搜尋限定作者欄位,可獲得較完整資料
  • 進階搜尋
    請使用永久網址來引用或連結此文件: https://tkuir.lib.tku.edu.tw/dspace/handle/987654321/38206


    題名: Numerical Studies of Curved-walled Micro Nozzle/Diffuser
    作者: Chen, Yu-tang;Hsu, Chin-chun;Chang, Ming-cheng;Kang, Shung-wen
    貢獻者: 淡江大學機械與機電工程學系;淡江大學水資源及環境工程學系
    關鍵詞: Nozzle;Diffuser;Pressure loss coefficient;Reynolds number
    日期: 2006-01-18
    上傳時間: 2010-04-15 10:31:30 (UTC+8)
    出版者: Institute of Electrical and Electronics Engineers (IEEE)
    摘要: In this study, commercially available software CFD was adopted for analyzing the performance of straight-walled and curved-walled micro nozzle/diffuser. Such nozzle/diffuser was used in valve-less micro-pumps. This model tested different types of nozzle/diffuser and the results showed that the pressure loss coefficient for nozzle/diffuser decreases with the increase of Reynolds number. At the same Reynolds number, the pressure loss coefficient for nozzle is higher than that of the diffuser. At a given volumetric flow rate, the pressure loss coefficient and ratio of pressure loss coefficient for curved-walled nozzle/diffuser are slightly higher than that of the straight-walled nozzle/diffuser. In this study, the numerical data was found good agreement with previous analytic solution and experimental results.
    關聯: Nano/Micro Engineered and Molecular Systems, 2006. NEMS '06. 1st IEEE International Conference on, pp.841-845
    DOI: 10.1109/NEMS.2006.334908
    顯示於類別:[水資源及環境工程學系暨研究所] 會議論文
    [機械與機電工程學系暨研究所] 會議論文

    文件中的檔案:

    檔案 描述 大小格式瀏覽次數
    1424401399_p841-845.pdf4196KbAdobe PDF701檢視/開啟
    index.html0KbHTML284檢視/開啟

    在機構典藏中所有的資料項目都受到原著作權保護.

    TAIR相關文章

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