Effects of forming process on composite mode I interlaminar fracture toughness

  • Xingyi Chen
  • , Zengshan Li*
  • , Xiao Huang
  • , Zhejun Kou
  • *Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

Abstract

In order to compare and analyse the effect of two different kinds of forming process on composite mode I interlaminar fracture toughness, the DCB specimens were tested by using hypothesis inspeetion method. A finite element model was also used to simulate the crack propagation process. The results demonstrate that the average of mode I interlaminar fracture toughness from silicon rubber flexible mold forming is a bit higher than that from metal rigid mold forming. Howevers the variance of mode I interlaminar fracture toughness from the two groups shows no significant difference. The crack propagation process of the two forming process is similar. The established finite element model, which is identical to the test results, can predict the process of the crack expansion effectively.

Original languageEnglish
Pages (from-to)58-63
Number of pages6
JournalJournal of Aeronautical Materials
Volume36
Issue number5
DOIs
StatePublished - 1 Sep 2016

Keywords

  • Composite
  • Forming process
  • Interface
  • Mode I interlaminar fracture toughness

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