@inproceedings{b32a6c479dd8457fbae6e381ba762044,
title = "Demonstration of a Crack arresting Concept in Composite Bonded Joints: Testing and Simulation of Carbon Z-Pin Reinforcement Applied to Post-Cured Carbon/Epoxy Laminates",
abstract = "In innovative crack arresting solution based on inserting and bonding z-pins into a cured carbon-epoxy laminate is presented. The crack arresting solution is investigated experimentally under mode-I loading conditions and simulated numerically using homogenized as well as high fidelity modelling approaches. For the interface tested, it was shown that the mode-I fracture toughness of the interface can be increased by a seven fold factor. Numerical results gave reasonable agreement with the experimental findings.",
author = "M. Grimberg and I. Simon and Y. Poleg and O. Shor and P. Knoth and S. Clay and W. Ault and T. Rev and D. Rittel and N. Shemesh",
note = "Publisher Copyright: {\textcopyright} 2022, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.; AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022 ; Conference date: 03-01-2022 Through 07-01-2022",
year = "2022",
doi = "10.2514/6.2022-0106",
language = "אנגלית",
isbn = "9781624106316",
series = "AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
pages = "1--18",
booktitle = "AIAA SciTech Forum 2022",
}