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Title: Transverse impact by RCCs on S-glass and Kevlar® FRC strips

Abstract

This study aims to isolate interactions between plies and tows and reveal fundamental physics involved in transverse impact on fiber-reinforced composite (FRC) structures. Composite strips were sectioned from large panels and characterized by optical photography, three-dimensional synchrotron X-ray computed tomography, and scanning electron microscopy (SEM). Each strip was impacted perpendicularly by a right circular cylinder (RCC) projectile at a velocity ranging from ~ 150 to 600 m/s. The global strip behavior, as well as localized deformation and failure of the strip near the projectile corner, were both captured by high-speed optical imaging. S-Glass FRC strips were observed to fail in tension ahead of the RCC projectiles’ flat surfaces while Kevlar® FRC strips fractured at the projectile corners. The concept of critical velocity region previously used for impact on yarns was introduced to define different failure modes of each composite strip type. The strip damage extent was found to increase with the impact velocity and reach the maximum at the upper limit of the critical velocity region. Above the critical velocity region, the damage extent decreased with impact velocity. Wave propagations and load histories in the composite strips during impact were quantified and compared with Smith’s theory. Finally, critical velocities ofmore » single fibers, yarns, and composite strips and ballistic limits of single-ply and multi-ply composite panels were compared to provide insight into the design of impact-resistant fabrics and composites.« less

Authors:
 [1];  [1];  [1]; ORCiD logo [1];  [1];  [2];  [1];  [1]; ORCiD logo [1];  [1];  [1];  [3];  [3];  [1];  [1];  [2];  [1]
  1. Purdue Univ., West Lafayette, IN (United States)
  2. Drexel Univ., Philadelphia, PA (United States)
  3. Argonne National Lab. (ANL), Argonne, IL (United States). Advanced Photon Source (APS)
Publication Date:
Research Org.:
Argonne National Laboratory (ANL), Argonne, IL (United States)
Sponsoring Org.:
USDOE Office of Science (SC), Basic Energy Sciences (BES). Scientific User Facilities Division; U.S. Army Research Laboratory
OSTI Identifier:
1869909
Alternate Identifier(s):
OSTI ID: 1780349
Grant/Contract Number:  
AC02-06CH11357; W911NF-12-2-0022; FA9550-16-1-0315
Resource Type:
Accepted Manuscript
Journal Name:
Composites. Part A, Applied Science and Manufacturing
Additional Journal Information:
Journal Volume: 146; Journal ID: ISSN 1359-835X
Publisher:
Elsevier
Country of Publication:
United States
Language:
English
Subject:
71 CLASSICAL AND QUANTUM MECHANICS, GENERAL PHYSICS; 42 ENGINEERING; Ballistic limit; Composite strips; Damage and fracture; Transverse impact; Wave propagation

Citation Formats

Gao, Jinling, Guo, Zherui, Hernandez, Julio Andres, Zhou, Fengfeng, Nie, Yizhou, Gao, Jian, Lim, Boon Him, Kedir, Nesredin, Zhai, Xuedong, Wang, Junyu, Tsai, Jung-Ting, De Carlo, Francesco, Shevchenko, Pavel D., Tallman, Tyler N., Byung-Guk Jun, Martin, Palmese, Giuseppe R., and Chen, Weinong. Transverse impact by RCCs on S-glass and Kevlar® FRC strips. United States: N. p., 2021. Web. doi:10.1016/j.compositesa.2021.106425.
Gao, Jinling, Guo, Zherui, Hernandez, Julio Andres, Zhou, Fengfeng, Nie, Yizhou, Gao, Jian, Lim, Boon Him, Kedir, Nesredin, Zhai, Xuedong, Wang, Junyu, Tsai, Jung-Ting, De Carlo, Francesco, Shevchenko, Pavel D., Tallman, Tyler N., Byung-Guk Jun, Martin, Palmese, Giuseppe R., & Chen, Weinong. Transverse impact by RCCs on S-glass and Kevlar® FRC strips. United States. https://doi.org/10.1016/j.compositesa.2021.106425
Gao, Jinling, Guo, Zherui, Hernandez, Julio Andres, Zhou, Fengfeng, Nie, Yizhou, Gao, Jian, Lim, Boon Him, Kedir, Nesredin, Zhai, Xuedong, Wang, Junyu, Tsai, Jung-Ting, De Carlo, Francesco, Shevchenko, Pavel D., Tallman, Tyler N., Byung-Guk Jun, Martin, Palmese, Giuseppe R., and Chen, Weinong. Sun . "Transverse impact by RCCs on S-glass and Kevlar® FRC strips". United States. https://doi.org/10.1016/j.compositesa.2021.106425. https://www.osti.gov/servlets/purl/1869909.
@article{osti_1869909,
title = {Transverse impact by RCCs on S-glass and Kevlar® FRC strips},
author = {Gao, Jinling and Guo, Zherui and Hernandez, Julio Andres and Zhou, Fengfeng and Nie, Yizhou and Gao, Jian and Lim, Boon Him and Kedir, Nesredin and Zhai, Xuedong and Wang, Junyu and Tsai, Jung-Ting and De Carlo, Francesco and Shevchenko, Pavel D. and Tallman, Tyler N. and Byung-Guk Jun, Martin and Palmese, Giuseppe R. and Chen, Weinong},
abstractNote = {This study aims to isolate interactions between plies and tows and reveal fundamental physics involved in transverse impact on fiber-reinforced composite (FRC) structures. Composite strips were sectioned from large panels and characterized by optical photography, three-dimensional synchrotron X-ray computed tomography, and scanning electron microscopy (SEM). Each strip was impacted perpendicularly by a right circular cylinder (RCC) projectile at a velocity ranging from ~ 150 to 600 m/s. The global strip behavior, as well as localized deformation and failure of the strip near the projectile corner, were both captured by high-speed optical imaging. S-Glass FRC strips were observed to fail in tension ahead of the RCC projectiles’ flat surfaces while Kevlar® FRC strips fractured at the projectile corners. The concept of critical velocity region previously used for impact on yarns was introduced to define different failure modes of each composite strip type. The strip damage extent was found to increase with the impact velocity and reach the maximum at the upper limit of the critical velocity region. Above the critical velocity region, the damage extent decreased with impact velocity. Wave propagations and load histories in the composite strips during impact were quantified and compared with Smith’s theory. Finally, critical velocities of single fibers, yarns, and composite strips and ballistic limits of single-ply and multi-ply composite panels were compared to provide insight into the design of impact-resistant fabrics and composites.},
doi = {10.1016/j.compositesa.2021.106425},
journal = {Composites. Part A, Applied Science and Manufacturing},
number = ,
volume = 146,
place = {United States},
year = {Sun Apr 18 00:00:00 EDT 2021},
month = {Sun Apr 18 00:00:00 EDT 2021}
}

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