research-article

The impact response of composite laminates based on fracture toughness stiffness degradation

Authors:

Xiaoyu ZhaoAuthors Info & Claims

RICAI '19: Proceedings of the 2019 International Conference on Robotics, Intelligent Control and Artificial Intelligence

Pages 316 - 323

https://doi.org/10.1145/3366194.3366250

Published: 20 September 2019 Publication History

Abstract

Based on ABAQUS, a 3D finite element analysis model of damage of composite laminates under low-speed impact was established. By writing VUMAT subroutine, this paper uses strain-based 3d Hashin failure criterion to judge fiber failure. The bilinear stiffness degradation scheme based on fracture toughness of fiber constitutive model is adopted for stiffness reduction. This paper uses cohesive element to simulate the area between the layers. Traditional stress failure criterion and strain energy release rate was used to analyze the initiation and evolution of delamination damage. The effects of different stiffness degradation schemes on the response of laminated plates under low velocity impact are analyzed in this paper.

References

[1]

DS Li, MR Wisnom (1994). Modelling damage initiation and propagation in composites using interface elements. Computer Aided Design in Composite Material Technology IV, (4), 213--220.

[2]

Lo D C (1993). Modelling of damage evolution in thick laminates subjected to low veloeity impact. Mechanics of Thick Composites, 162(2), 137--150.

[3]

Lammerant L, VerPoest (1996). Modelling of the interaction between matrix Cracks and delaminations during impact of composite plates. Composite Science and Tech, 56(10), 1171--1178

[4]

Zhihua Cui, 1996, Fatigue characteristics of composite laminates. Aviation industry press, Beijing, China.

[5]

Hou J P, Petrinic N, Ruiz C (2000). Prediction of impact damage in composite plates. Composite Science and Technology, 60(2), 273--281.

[6]

De Moura M F S F, Marques A T (2002). Prediction of low velocity impact damage in carbon-epoxy laminates. Composite Part A, 33(3), 361--368.

[7]

Yuepeng Yi, Zhefeng Yu, Hai Wang (2012). Study on simulation scheme of low-speed impact stiffness degradation of composite laminates. Chinese Quarterly of Mechanics, 33(3), 469--475.

[8]

Chen Li, Huanhuan Xu, Xingjin Gu (2017). Prediction of tensile strength of interlaminar hybrid composite plates. Acta Materiae Compositae Sinica, 34(4), 795--800.

[9]

Weiyao Zhu, Xiwu Xu (2010). Finite element simulation of low-velocity impact damage of composite laminates. Acta Materiae Compositae Sinica, 27(6), 200--207.

[10]

Shicheng Zhao, Zhenqing Wang, Jianming Guo (2015). Effect of hybrid mode on low-speed impact performance of CF/GF/epoxy hybrid composites. Journal of Harbin Engineering University, 36(11), 1476--1480.

[11]

Bin Yang, Jifeng Zhang, Limin Zhou (2015). Preparation and low - speed impact properties of hybrid glass - carbon fiber reinforced PCBT composite laminates. Acta Materiae Compositae Sinica, 32(2), 435--443.

[12]

Chengcheng Zhang, Jianjun Wang (2016). Research Advances in Damage of Composite Structures on Stiffness Degradation. Materials Reports, 30(11), 8--13.

[13]

Y. Shi, T. Swait, C. Soutis (2012). Modelling damage evolution in composite laminates subjected to low velocity impact. Composite Structures, 94(9), 2902.

[14]

Volnei Tita, Jonas de Carvalho, Dirk Vandepitte (2008). Failure analysis of low velocity impact on thin composite laminates: Experimental and numerical approaches. Composite Structures, 83(4), 413--428.

[15]

Yufen Wu, Boming Zhang (2012). Experimental research of carbon fiber filament's fracture toughness based on focus iron beam. Acta Materiae Compositae Sinica, 29(2), 228--232.

[16]

Da Tian, Hongjun Fu (2018). Finite Elements Simulation Of GI Fracture Toughness Of Toughened Composites. Fiber Reinforced Plastics/Composites, (1), 18--23.

Cited By

Yang XYao TLi DJiang L(2024)Theoretical prediction and validation of mechanical properties and damage of 3D orthogonal woven composites with different parametersComposites Science and Technology10.1016/j.compscitech.2024.110591(110591)Online publication date: Apr-2024
https://doi.org/10.1016/j.compscitech.2024.110591
Zhang MMirza HZhang YTabasum MLang HZou P(2022)Investigation into a comprehensive forming limit curve considering multi-parameters effects for semi-cured FMLs through uniform pressure loading testInternational Journal of Damage Mechanics10.1177/1056789522113505432:2(289-317)Online publication date: 4-Dec-2022
https://doi.org/10.1177/10567895221135054

Index Terms

The impact response of composite laminates based on fracture toughness stiffness degradation
1. Applied computing
  1. Operations research
    1. Computer-aided manufacturing

Recommendations

Influence of loading conditions on the impact damage resistance of composite panels

In this paper the onset of impact induced delaminations in stiffened composite panels is analysed by using an approach based on a threshold critical impact force. This approach is adopted in combination with geometrically non-linear finite element ...
Experimental and numerical analysis of low velocity impact on a preloaded composite plate

An experimental and numerical study on the influence of biaxial preloading on the low velocity impact performance of E-glass/epoxy-laminated composite plates was conducted. For this aim, an experimental device was developed to apply the load in two ...
Fatigue Life Methodology for Tapered Composite Flexbeam Laminates

Comments

Information & Contributors

Information

Published In

cover image ACM Other conferences

RICAI '19: Proceedings of the 2019 International Conference on Robotics, Intelligent Control and Artificial Intelligence

September 2019

803 pages

ISBN:9781450372985

DOI:10.1145/3366194

Copyright © 2019 ACM.

Permission to make digital or hard copies of all or part of this work for personal or classroom use is granted without fee provided that copies are not made or distributed for profit or commercial advantage and that copies bear this notice and the full citation on the first page. Copyrights for components of this work owned by others than ACM must be honored. Abstracting with credit is permitted. To copy otherwise, or republish, to post on servers or to redistribute to lists, requires prior specific permission and/or a fee. Request permissions from [email protected]

Publisher

Association for Computing Machinery

New York, NY, United States

Publication History

Published: 20 September 2019

Permissions

Request permissions for this article.

Request Permissions

Check for updates

Author Tags

Qualifiers

Research-article
Research
Refereed limited

Conference

RICAI 2019

RICAI 2019: 2019 International Conference on Robotics, Intelligent Control and Artificial Intelligence

September 20 - 22, 2019

Shanghai, China

Acceptance Rates

RICAI '19 Paper Acceptance Rate 140 of 294 submissions, 48%;

Overall Acceptance Rate 140 of 294 submissions, 48%

Contributors

Other Metrics

View Article Metrics

Bibliometrics & Citations

Bibliometrics

Article Metrics

2
Total Citations
View Citations
96
Total Downloads

Downloads (Last 12 months)12
Downloads (Last 6 weeks)1

Reflects downloads up to 18 Aug 2024

Other Metrics

View Author Metrics

Citations

Cited By

Yang XYao TLi DJiang L(2024)Theoretical prediction and validation of mechanical properties and damage of 3D orthogonal woven composites with different parametersComposites Science and Technology10.1016/j.compscitech.2024.110591(110591)Online publication date: Apr-2024
https://doi.org/10.1016/j.compscitech.2024.110591
Zhang MMirza HZhang YTabasum MLang HZou P(2022)Investigation into a comprehensive forming limit curve considering multi-parameters effects for semi-cured FMLs through uniform pressure loading testInternational Journal of Damage Mechanics10.1177/1056789522113505432:2(289-317)Online publication date: 4-Dec-2022
https://doi.org/10.1177/10567895221135054

View Options

Get Access

Login options

Check if you have access through your login credentials or your institution to get full access on this article.

Full Access

Get this Publication

View options

PDF

View or Download as a PDF file.

eReader

View online with eReader.

Media

Figures

Other

Tables

View Table of Contents