Composites Theory and Practice > 2023 > R. 23, nr 2 > 97--103
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journal ISSN : | 2084-6096 |
journal e-ISSN : | 2299-128X |
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Bibliography
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[1] Cocchieri E., Almeida R., José S., Paulo S., A Review on the development and properties of continuous fiber/epoxy/aluminium hybrid composites for aircraft structures, Mater. Res. 2006, 9(3), 247-256.
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[2] Rao N.N., Rao P.M.V., Kumar S., A numerical approach to estimate first ply failure of fibre metal laminate. Revue des Composites et des Matériaux Avancés – Journal of Composite and Advanced Materials 2021, 31(1), 33-39, DOI: 10.18280/rcma.310105.
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[3] Morinière F.D., Alderliesten R.C., Benedictus R., Modelling of impact damage and dynamics in fibre-metal laminates – A review, Int. J. Impact Eng. 2014, 67, 27-38, DOI: 10.1016/j.ijimpeng.2014.01.004.