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Crack damage and facture analysis of airship envelope material

  • Hou Di Xiao*
  • , Long Bin Liu
  • , Ming Yun Lv
  • *此作品的通讯作者
  • Beihang University

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

Original defects in the envelope material easily torn damage under overpressure, when the stratospheric airship in use. This paper based on linear elastic theory studied the tear strength of envelope material containing initial center crack and proposed theoretical model for this problem. Choose Vectran fiber as a reinforcing layer of stratospheric airship envelope material, Combined with digital speckle method measuring tear strength of envelope materials containing different initial center crack length. Comparative analysis found that the theoretical model applicable to estimate the tear strength of envelope material, that center initial crack width ratio is less than 50%.It estimation error within 5% .It satisfies the requirement of engineering application accuracy.

源语言英语
主期刊名Material Science, Civil Engineering and Architecture Science, Mechanical Engineering and Manufacturing Technology II
编辑H.W. Liu, G. Wang, G.W. Zhang
出版商Trans Tech Publications Ltd
7-10
页数4
ISBN(电子版)9783038352679
DOI
出版状态已出版 - 2014
活动3rd International Conference on Advanced Engineering Materials and Architecture Science, ICAEMAS 2014 - Huhhot, 中国
期限: 26 7月 201427 7月 2014

出版系列

姓名Applied Mechanics and Materials
651-653
ISSN(印刷版)1660-9336
ISSN(电子版)1662-7482

会议

会议3rd International Conference on Advanced Engineering Materials and Architecture Science, ICAEMAS 2014
国家/地区中国
Huhhot
时期26/07/1427/07/14

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