Computational Modelling and Experimental Techniques for Fibre Metal Laminate Structural Analysis: A Comprehensive Review-Reference-Cited by-同舟云学术

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Computational Modelling and Experimental Techniques for Fibre Metal Laminate Structural Analysis: A Comprehensive Review

Published:2023-07-22 Issue:1 Volume:31 Page:351-369
ISSN:1134-3060
Container-title:Archives of Computational Methods in Engineering
language:en
Short-container-title:Arch Computat Methods Eng

Author:

Thomas Libin C.,Kumar Vikash,Gangwar Ankit,Pisupati Meghna,Gupta Chandan,Panda Subrata Kumar

Publisher

Springer Science and Business Media LLC

Subject

Applied Mathematics,Computer Science Applications

Link

https://link.springer.com/content/pdf/10.1007/s11831-023-09980-3.pdf

Reference167 articles.

1. Botelho EC, Silva RA, Pardini LC, Rezende MC (2006) A review on the development and properties of continuous fiber/epoxy/aluminum hybrid composites for aircraft structures. Mater Res 9:247–256. https://doi.org/10.1590/S1516-14392006000300002

2. Reyes VG, Cantwell WJ (2004) The high velocity impact response of composite and FML-reinforced sandwich structures. Compos Sci Technol 64:35–54. https://doi.org/10.1016/S0266-3538(03)00197-0

3. Alderliesten RC, Benedictus R (2008) Fiber/metal composite technology for future primary aircraft structures. J Aircr 45:1182–1189. https://doi.org/10.2514/1.33946

4. Vogelesang LB, Vlot A (2000) Development of fibre metal laminates for advanced aerospace structures. J Mater Process Technol 103:1–5. https://doi.org/10.1016/S0924-0136(00)00411-8

5. Cortés P, Cantwell WJ (2006) The prediction of tensile failure in titanium-based thermoplastic fibre-metal laminates. Compos Sci Technol 66:2306–2316. https://doi.org/10.1016/j.compscitech.2005.11.031

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