Rate-Dependent Cohesive Models for Dynamic Mode I Interfacial Propagation and Failure of Unidirectional Composite Laminates
With the increasing application of composite materials in anti-impact structure, the development of reliable rate-dependent interlaminar constitutive model becomes necessary. This study aims to assess and evaluate the applicability of three types of rate-dependent cohesive models (logarithmic, expon...
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doaj-73ec92def40c4b9fbd16c1bec2be116f2021-02-08T00:01:34ZengMDPI AGCoatings2079-64122021-02-011119119110.3390/coatings11020191Rate-Dependent Cohesive Models for Dynamic Mode I Interfacial Propagation and Failure of Unidirectional Composite LaminatesChenxu Zhang0Huifang Liu1Junchao Cao2Chao Zhang3Department of Aeronautical Structure Engineering, Northwestern Polytechnical University, Xi’an 710072, ChinaDepartment of Aeronautical Structure Engineering, Northwestern Polytechnical University, Xi’an 710072, ChinaDepartment of Aeronautical Structure Engineering, Northwestern Polytechnical University, Xi’an 710072, ChinaDepartment of Aeronautical Structure Engineering, Northwestern Polytechnical University, Xi’an 710072, ChinaWith the increasing application of composite materials in anti-impact structure, the development of reliable rate-dependent interlaminar constitutive model becomes necessary. This study aims to assess and evaluate the applicability of three types of rate-dependent cohesive models (logarithmic, exponential and power) in numerical delamination simulation, through comparison with dynamic test results of double cantilever beam (DCB) specimens made from T700/MTM28-1 composite laminate. Crack propagation length history profiles are extracted to calibrate the numerical models. Crack propagation contours and fracture toughness data are predicted, extracted and compared to investigate the difference of the three different rate-dependent cohesive models. The variation of cohesive zone length and force profiles with the implemented models is also investigated. The results suggest that the crack propagation length can be better predicted by logarithmic and power models. Although crack propagation length profiles are well predicted, the numerical calculated dynamic fracture toughness tends to be higher than that of experimental measured results. The three models also show differences in the prediction of maximum loading forces. The results of this work provide useful guidance for the development of more efficient cohesive models and more reliable interface failure simulation of impact problems.https://www.mdpi.com/2079-6412/11/2/191composite laminatescohesive zone modelingrate dependencyfinite element analysis (FEA)delaminationcrack propagation |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
Chenxu Zhang Huifang Liu Junchao Cao Chao Zhang |
spellingShingle |
Chenxu Zhang Huifang Liu Junchao Cao Chao Zhang Rate-Dependent Cohesive Models for Dynamic Mode I Interfacial Propagation and Failure of Unidirectional Composite Laminates Coatings composite laminates cohesive zone modeling rate dependency finite element analysis (FEA) delamination crack propagation |
author_facet |
Chenxu Zhang Huifang Liu Junchao Cao Chao Zhang |
author_sort |
Chenxu Zhang |
title |
Rate-Dependent Cohesive Models for Dynamic Mode I Interfacial Propagation and Failure of Unidirectional Composite Laminates |
title_short |
Rate-Dependent Cohesive Models for Dynamic Mode I Interfacial Propagation and Failure of Unidirectional Composite Laminates |
title_full |
Rate-Dependent Cohesive Models for Dynamic Mode I Interfacial Propagation and Failure of Unidirectional Composite Laminates |
title_fullStr |
Rate-Dependent Cohesive Models for Dynamic Mode I Interfacial Propagation and Failure of Unidirectional Composite Laminates |
title_full_unstemmed |
Rate-Dependent Cohesive Models for Dynamic Mode I Interfacial Propagation and Failure of Unidirectional Composite Laminates |
title_sort |
rate-dependent cohesive models for dynamic mode i interfacial propagation and failure of unidirectional composite laminates |
publisher |
MDPI AG |
series |
Coatings |
issn |
2079-6412 |
publishDate |
2021-02-01 |
description |
With the increasing application of composite materials in anti-impact structure, the development of reliable rate-dependent interlaminar constitutive model becomes necessary. This study aims to assess and evaluate the applicability of three types of rate-dependent cohesive models (logarithmic, exponential and power) in numerical delamination simulation, through comparison with dynamic test results of double cantilever beam (DCB) specimens made from T700/MTM28-1 composite laminate. Crack propagation length history profiles are extracted to calibrate the numerical models. Crack propagation contours and fracture toughness data are predicted, extracted and compared to investigate the difference of the three different rate-dependent cohesive models. The variation of cohesive zone length and force profiles with the implemented models is also investigated. The results suggest that the crack propagation length can be better predicted by logarithmic and power models. Although crack propagation length profiles are well predicted, the numerical calculated dynamic fracture toughness tends to be higher than that of experimental measured results. The three models also show differences in the prediction of maximum loading forces. The results of this work provide useful guidance for the development of more efficient cohesive models and more reliable interface failure simulation of impact problems. |
topic |
composite laminates cohesive zone modeling rate dependency finite element analysis (FEA) delamination crack propagation |
url |
https://www.mdpi.com/2079-6412/11/2/191 |
work_keys_str_mv |
AT chenxuzhang ratedependentcohesivemodelsfordynamicmodeiinterfacialpropagationandfailureofunidirectionalcompositelaminates AT huifangliu ratedependentcohesivemodelsfordynamicmodeiinterfacialpropagationandfailureofunidirectionalcompositelaminates AT junchaocao ratedependentcohesivemodelsfordynamicmodeiinterfacialpropagationandfailureofunidirectionalcompositelaminates AT chaozhang ratedependentcohesivemodelsfordynamicmodeiinterfacialpropagationandfailureofunidirectionalcompositelaminates |
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1724280472801902592 |