English  |  正體中文  |  简体中文  |  全文笔数/总笔数 : 49064/83170 (59%)
造访人次 : 6963019      在线人数 : 50
RC Version 7.0 © Powered By DSPACE, MIT. Enhanced by NTU Library & TKU Library IR team.
搜寻范围 查询小技巧:
  • 您可在西文检索词汇前后加上"双引号",以获取较精准的检索结果
  • 若欲以作者姓名搜寻,建议至进阶搜寻限定作者字段,可获得较完整数据
  • 进阶搜寻


    jsp.display-item.identifier=請使用永久網址來引用或連結此文件: http://tkuir.lib.tku.edu.tw:8080/dspace/handle/987654321/46004


    题名: A Study of Viscous Air Damping in Laterally Oscillating Micro Comb Structures
    作者: 陳慶祥;Chen, Ching-shung;楊龍杰;Yang, Lung-jieh;Chou, C. F.
    贡献者: 淡江大學航空太空工程學系
    关键词: Accelerometer;Micro comb structure;Viscous damping
    日期: 2003-03
    上传时间: 2013-03-20 16:20:06 (UTC+8)
    出版者: 臺南市:中國航空太空學會
    摘要: This paper studies analytically as well as numerically viscous air damping in laterally oscillating micro comb structures. The analytical results demonstrate that the transient motion is damped out in less than one oscillating period of the comb structures studied. The Knudsen numbers in typical micro comb structures indicate part of the flow falling in the slip flow region. The slip effect is also studied. The predicted quality factors subject to the slip and the nonslip boundary conditions are both larger than the experimental data. The possible explanation for this discrepancy is that our solution procedure assumes that the structure is infinite, while an actual structure is finite and three-dimensional. The pumping and sucking motions at the edges of the comb fingers have significant effects on the flow field.
    關聯: 中國航空太空學會學刊=Transactions of the Aeronautical and Astronautical Society of the Republic of China 35(1),頁99-105
    DOI: 
    显示于类别:[機械與機電工程學系暨研究所] 期刊論文
    [航空太空工程學系暨研究所] 期刊論文

    文件中的档案:

    档案 大小格式浏览次数
    index.html0KbHTML181检视/开启

    在機構典藏中所有的数据项都受到原著作权保护.

    TAIR相关文章

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