English  |  正體中文  |  简体中文  |  全文筆數/總筆數 : 49925/85107 (59%)
造訪人次 : 7780303      線上人數 : 25
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: http://tkuir.lib.tku.edu.tw:8080/dspace/handle/987654321/106060

    題名: A simulation of the fatigue life of light aircraft glass fibre-reinforced composites landing gear
    作者: P. W. Chen;W. T. Huang
    關鍵詞: Light aircraft;Landing gear;Glass fibre-reinforced composites;Fatigue;Finite element analysis
    日期: 2015/11/01
    上傳時間: 2016-04-22 13:17:40 (UTC+8)
    摘要: This study uses finite element analysis software to conduct simulations and compares the fatigue behaviour of the aluminium alloy and glass fibre-reinforced composite that is used in light aircraft landing gear. The maximum stress, maximum strain and deformation of landing gear of different shapes (plate and tube shapes) are also determined. The results show that the composite landing gear weighs 45% less than an aluminium equivalent. Of the samples tested, plate-shaped glass fibre-reinforced composite landing gear exhibits the lowest maximum stress under a static load. Regardless of whether the landing gear is plate- or tube-shaped, the maximum strain and deformation for the composite landing gear are more than four times those for the aluminium alloy landing gear. The results for dynamic load show that plate-shaped glass fibre-reinforced composite and tube-shaped aluminium landing gear have similar maximum alternating stress under cyclic loading.
    關聯: Materials Research Innovations 19(suppl. 9), pp.142-147
    DOI: 10.1179/1432891715Z.0000000001947
    顯示於類別:[航空太空工程學系暨研究所] 期刊論文


    檔案 描述 大小格式瀏覽次數



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