English  |  正體中文  |  简体中文  |  Items with full text/Total items : 64305/97157 (66%)
Visitors : 7079140      Online Users : 347
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


    Citation Infomation
    javax.net.ssl.SSLException: Received fatal alert: protocol_version
    Loading...
    Please use this identifier to cite or link to this item: https://tkuir.lib.tku.edu.tw/dspace/handle/987654321/44813


    Title: Partial Hybrid Stress Element for Mindlin Laminated Plates Theory
    Authors: Tseng, Yi-ping;Wu, Tzu-chiang
    Contributors: 淡江大學土木工程學系
    Date: 1991-05
    Issue Date: 2010-03-26 17:08:27 (UTC+8)
    Publisher: Hoboken, NJ: Wiley-Blackwell
    Abstract: The partial hybrid stress method is applied to the Mindlin plate theory for orthotropic composite plates. The displacement formulation is adopted in the flexurel part and the hybrid formulation in the transverse shear part. Since the interface traction discontinuity is overcome, the present element performs much better than the displacement-based method. Although only the stress parameters in transverse shear part are required, the accuracy approaches that of the conventional hybrid method, The governing equations of plate are also derived from the modified Hellinger-Reissner variational principle.
    Relation: Microcomputers in Civil Engineering 6(3), pp.217-227
    DOI: 10.1111/j.1467-8667.1991.tb00405.x
    Appears in Collections:[土木工程學系暨研究所] 期刊論文

    Files in This Item:

    File Description SizeFormat
    index.html0KbHTML270View/Open
    index.html0KbHTML82View/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 ©  2006-2025  - Feedback