Abstract
Measuring parameters related to each damage mode of composites subjected to impact is very challenging because of the complex damage phenomenology. Here, we developed an experimental methodology for evaluating the micro-scale fracture characteristics of two principal damage modes, i.e., transverse crack and delamination, and providing the corresponding fracture toughness. We demonstrated the capability of the method by comparing and providing additional insights about two materials, namely homopolymer-based (ductile) and copolymer-based (less-ductile) glass/polypropylene thermoplastic composites. We found that (i) transverse crack behavior of both composites is similar as indicated by a small difference in their fracture toughness, (ii) delamination growth in copolymer-based composites is slower than in homopolymer-based composites, (iii) the fibrillation induced by rubber particles in copolymer-based composites is responsible for decelerating the delamination growth and improving its fracture toughness during delamination. This method is deemed useful and quick for determining the micro-scale fracture behavior of composite laminates under impact in order to support the material selection process.
Recommended Citation
H. Wafai et al., "In Situ Micro-Scale High-Speed Imaging for Evaluation of Fracture Propagation and Fracture Toughness of Thermoplastic Laminates Subjected to Impact," Composite Structures, vol. 210, pp. 747 - 754, Elsevier, Feb 2019.
The definitive version is available at https://doi.org/10.1016/j.compstruct.2018.11.092
Department(s)
Mechanical and Aerospace Engineering
Publication Status
Full Text Access
Keywords and Phrases
Damage behavior; High-speed imaging; Impact test; Thermoplastic composites
International Standard Serial Number (ISSN)
0263-8223
Document Type
Article - Journal
Document Version
Citation
File Type
text
Language(s)
English
Rights
© 2025 Elsevier, All rights reserved.
Publication Date
15 Feb 2019

Comments
King Abdullah University of Science and Technology, Grant BAS/1/1315-01-01