Parametric evaluation on the curved part of composite T-joints based on numerical simulation

Hao Cui, Yulong Li, S. Koussios, A. Beukers

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

1 Scopus citations

Abstract

A detailed numerical model is presented to predict the failure process and the strength of composite T-joint subjected to pull-off loading. The Cohesive Zone Model (CZM) is employed to simulate the delamination and crack forming in the structure, including the stochastic crack in the filler. A series of simulations are carried out to evaluate the influence of matrix, adhesive, filler (placed in the T-joints) and the radius on the strength of T-joint. The numerical results show that the nominal stiffness of the whole structure can be affected by the filler. The strength of the matrix, adhesive and filler have great impact on the loading capability, and the failure modes of the structure may change with varying the matrix, adhesive and filler material properties. Increasing the filler radius will raise the pull-off strength of T-joints. The numerical results agree reasonably with experimental results.

Original languageEnglish
Title of host publication27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010
Pages2419-2428
Number of pages10
StatePublished - 2010
Event27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010 - Nice, France
Duration: 19 Sep 201024 Sep 2010

Publication series

Name27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010
Volume3

Conference

Conference27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010
Country/TerritoryFrance
CityNice
Period19/09/1024/09/10

Keywords

  • Cohesive zone model
  • Composites
  • Parametric evaluation
  • Stochastic crack

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