Numerical Study on the Rebound of Low-Velocity Impact-Induced Indentation in Composite Laminate
Indentation is an effective indication of LVI damage in PMCs. However, indentation can rebound partly with time. Thus, a good understanding of the rebound behavior of the impacted pit is helpful in damage assessment for composites. In this paper, a transverse isotropic viscoelastic model and a visco...
Main Authors: | , |
---|---|
Format: | Article |
Language: | English |
Published: |
MDPI AG
2022-10-01
|
Series: | Aerospace |
Subjects: | |
Online Access: | https://www.mdpi.com/2226-4310/9/11/651 |
_version_ | 1827647691093442560 |
---|---|
author | Muhammad Yousaf Chuwei Zhou |
author_facet | Muhammad Yousaf Chuwei Zhou |
author_sort | Muhammad Yousaf |
collection | DOAJ |
description | Indentation is an effective indication of LVI damage in PMCs. However, indentation can rebound partly with time. Thus, a good understanding of the rebound behavior of the impacted pit is helpful in damage assessment for composites. In this paper, a transverse isotropic viscoelastic model and a viscoelastic cohesive interface model are proposed to represent the viscoelastic properties of ply and the interface between adjacent plies, respectively. In these models, we implement the in-plane 3D Hashin failure criterion to simulate ply level failures and the stress-based quadratic failure criterion and linear softening mixed-mode BK law to simulate cohesive interface failure initiation and propagation, respectively. LVI testing was performed on specimens at different impact energies (30 J, 40 J, and 50 J). Dents induced by impact will eventually rebound due to the viscoelastic behavior of plies and cohesive interfaces. This results in a decrease in depth with time. This indentation and its rebound phenomenon were simulated in ABAQUS by considering viscoelasticity with user-defined material subroutines. The simulation results show good agreement with the experimental observations and are validated accurately in terms of the indentation’s initial depth upon impact and its final rebound with time. From experiments, it was observed that the decrease in the original depth of indentation initially becomes faster with time after impact; then, it slows down with time and eventually stops due to viscoelasticity. While this decrease in the original depth of indentation remains invariable with time in simulation, it has a different rebound path. |
first_indexed | 2024-03-09T19:22:17Z |
format | Article |
id | doaj.art-c6ee9c3079d44f9fa296b9f347f9965f |
institution | Directory Open Access Journal |
issn | 2226-4310 |
language | English |
last_indexed | 2024-03-09T19:22:17Z |
publishDate | 2022-10-01 |
publisher | MDPI AG |
record_format | Article |
series | Aerospace |
spelling | doaj.art-c6ee9c3079d44f9fa296b9f347f9965f2023-11-24T03:15:13ZengMDPI AGAerospace2226-43102022-10-0191165110.3390/aerospace9110651Numerical Study on the Rebound of Low-Velocity Impact-Induced Indentation in Composite LaminateMuhammad Yousaf0Chuwei Zhou1Department of Engineering Mechanics, College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, ChinaDepartment of Engineering Mechanics, College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, ChinaIndentation is an effective indication of LVI damage in PMCs. However, indentation can rebound partly with time. Thus, a good understanding of the rebound behavior of the impacted pit is helpful in damage assessment for composites. In this paper, a transverse isotropic viscoelastic model and a viscoelastic cohesive interface model are proposed to represent the viscoelastic properties of ply and the interface between adjacent plies, respectively. In these models, we implement the in-plane 3D Hashin failure criterion to simulate ply level failures and the stress-based quadratic failure criterion and linear softening mixed-mode BK law to simulate cohesive interface failure initiation and propagation, respectively. LVI testing was performed on specimens at different impact energies (30 J, 40 J, and 50 J). Dents induced by impact will eventually rebound due to the viscoelastic behavior of plies and cohesive interfaces. This results in a decrease in depth with time. This indentation and its rebound phenomenon were simulated in ABAQUS by considering viscoelasticity with user-defined material subroutines. The simulation results show good agreement with the experimental observations and are validated accurately in terms of the indentation’s initial depth upon impact and its final rebound with time. From experiments, it was observed that the decrease in the original depth of indentation initially becomes faster with time after impact; then, it slows down with time and eventually stops due to viscoelasticity. While this decrease in the original depth of indentation remains invariable with time in simulation, it has a different rebound path.https://www.mdpi.com/2226-4310/9/11/651low-velocity impact (LVI)rebound of impact indentationfinite element simulationelement-based viscoelastic cohesive interfaceviscoelastic laminae model |
spellingShingle | Muhammad Yousaf Chuwei Zhou Numerical Study on the Rebound of Low-Velocity Impact-Induced Indentation in Composite Laminate Aerospace low-velocity impact (LVI) rebound of impact indentation finite element simulation element-based viscoelastic cohesive interface viscoelastic laminae model |
title | Numerical Study on the Rebound of Low-Velocity Impact-Induced Indentation in Composite Laminate |
title_full | Numerical Study on the Rebound of Low-Velocity Impact-Induced Indentation in Composite Laminate |
title_fullStr | Numerical Study on the Rebound of Low-Velocity Impact-Induced Indentation in Composite Laminate |
title_full_unstemmed | Numerical Study on the Rebound of Low-Velocity Impact-Induced Indentation in Composite Laminate |
title_short | Numerical Study on the Rebound of Low-Velocity Impact-Induced Indentation in Composite Laminate |
title_sort | numerical study on the rebound of low velocity impact induced indentation in composite laminate |
topic | low-velocity impact (LVI) rebound of impact indentation finite element simulation element-based viscoelastic cohesive interface viscoelastic laminae model |
url | https://www.mdpi.com/2226-4310/9/11/651 |
work_keys_str_mv | AT muhammadyousaf numericalstudyonthereboundoflowvelocityimpactinducedindentationincompositelaminate AT chuweizhou numericalstudyonthereboundoflowvelocityimpactinducedindentationincompositelaminate |