English  |  正體中文  |  简体中文  |  Items with full text/Total items : 56562/90363 (63%)
Visitors : 11855832      Online Users : 82
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/987654321/85646

    Title: A Tutorial on Finite Element Analysis of Journal Gas Bearings
    Authors: Tyan, Feng;Tu, Shun-Hsu
    Contributors: 淡江大學航空太空工程學系
    Keywords: Gas bearing;Galerkin method;Finite element method
    Date: 2006-12
    Issue Date: 2013-04-09 11:49:19 (UTC+8)
    Abstract: Although Finite element method has been a matured technique and has been implemented to the analysis of gas bearing by numerous researchers. While very few of the literature provided a detail and thorough derivation on the procedure of forming the matrix equation to be solved for pressure distribution. This is the aim of this work. To this end, a weak form of Reynolds equation is derived using Galerkin's weighted residue method. Then a finite element method is illustrated via a linear shape function with three nodes triangular element. The upshot of the above procedure is a nonlinear quadratic matrix equation. Finally a under relaxation method is adopted for solving this resulted nonlinear matrix equation.
    Relation: 中華民國力學學會第三十屆年會暨全國力學會議論文集, 8p.
    Appears in Collections:[Graduate Institute & Department of Aerospace Engineering] Proceeding

    Files in This Item:

    File SizeFormat
    A Tutorial on Finite Element Analysis of Journal Gas Bearings _西文摘要.docx15KbMicrosoft Word103View/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