Author:
Bruno M.,Esposito L.,Papa I.,Viscusi A.
Abstract
AbstractIn the present work, the response of composite hybrid laminates made of carbon and glass fibers in different stacking configurations was tested under low-velocity impact loads. Experimental drop impact tests were conducted on three different stacking sequences and three rising impact energy levels. The results from the tests were assumed for the development and validation of a numerical impact model reproducing for each stacking sequence and all the impact energy levels, the laminates impact response. The validated model investigated the occurred damage mechanisms, their distribution in the panel thickness and their extension on the plane of the laminate. Depending on the stacking sequence and the impact energy level, the energy absorption capacity was related to the dominant damage mechanism. The percentage contribution of interlaminar and intralaminar damages was presented and conclusions were drawn about the influence of stacking sequences on energy absorption and damage characteristics.
Funder
Università degli Studi di Napoli Federico II
Publisher
Springer Science and Business Media LLC
Subject
Mechanical Engineering,Mechanics of Materials,General Materials Science
Reference22 articles.
1. A. Hallal, R. Younes, and F. Fardoun, Review and Comparative Study of Analytical Modeling for the Elastic Properties of Textile Composites, Compos. B Eng., 2013, 50, p 22–31.
2. F. Paris and K.E. Jackson, A Study of Failure Criteria of Fibrous Composite Materials, Office., 2001, 76, p 1–10.
3. G. Zhou, Q. Sun, D. Li et al., Meso-Scale Modeling and Damage Analysis of Carbon/Epoxy Woven Fabric Composite Under In-plane Tension and Compression Loadings, Int. J. Mechan. Sci., 2021, 190, p 105980. https://doi.org/10.1016/j.ijmecsci.2020.105980
4. M.A. Wahab, T. Jabbour, and P. Davies, Prediction of Impact Damage in Composite Sandwich Plates, Mater. Tech., 2019, 107(2), p 273–281.
5. A. Riccio, G. Di Felice, S. Saputo et al., Stacking Sequence Effects on Damage Onset in Composite Laminate Subjected to Low Velocity Impact, Proced. Eng., 2014, 88, p 222–229. https://doi.org/10.1016/j.proeng.2014.11.148
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