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Study on fiber-reinforced laminated composite textile tearing behavior and strength prediction

  • Yun Chao Gu*
  • , Long Bin Liu
  • , Shuai Cao
  • , Hou Di Xiao
  • , Ming Yun Lv
  • *Corresponding author for this work
  • Beihang University

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

The tearing behavior of fiber-reinforced laminated composite textile plays the key role in the decision of mechanics performance of high altitude airship envelop material, even directly deciding its safety and stability. This paper, based on typical woven fabricated fiber yarns’ characteristics of geometry and mechanics, adopts Euler-displacement deformation analysis to explore yarn bundles deformation effects on tearing behavior and strength of envelope material with prefabricated damage and crack. Also, models with prefabricated crack with different size and textile density are respectively built to find factors that affect tearing behavior and strength of envelope material. From tests, it can be observed that the built models for predicting its tearing strength are in conformity with the experimental data. Nonlinear relationship is reflected between the initial crack width or yarn bundles density with tearing strength. Conclusively, the methods and models adopted in this paper provide an effective and innovative mind on tearing behavior and strength of fiber reinforced envelope material and make the foundation for its engineering application.

Original languageEnglish
Title of host publicationMaterial Science, Civil Engineering and Architecture Science, Mechanical Engineering and Manufacturing Technology II
EditorsH.W. Liu, G. Wang, G.W. Zhang
PublisherTrans Tech Publications Ltd
Pages1370-1373
Number of pages4
ISBN (Electronic)9783038352679
DOIs
StatePublished - 2014
Event3rd International Conference on Advanced Engineering Materials and Architecture Science, ICAEMAS 2014 - Huhhot, China
Duration: 26 Jul 201427 Jul 2014

Publication series

NameApplied Mechanics and Materials
Volume651-653
ISSN (Print)1660-9336
ISSN (Electronic)1662-7482

Conference

Conference3rd International Conference on Advanced Engineering Materials and Architecture Science, ICAEMAS 2014
Country/TerritoryChina
CityHuhhot
Period26/07/1427/07/14

Keywords

  • Initial Crack Length
  • Laminated Composite
  • Mechanics Characteristics
  • Strength Prediction
  • Tear Damage
  • Tearing Behavio

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