Fracture and Structural Integrity e-ISSN 1971-8993 Open access
Miscellanea Vol. 13, No. 49 (2019)

Experimental analysis of aluminium/carbon epoxy hybrid laminates under flexural load

Author and affiliation details
  • Costanzo Bellini Corresponding author University of Cassino and Southern Lazio ROR04nxkaq16 costanzo.bellini@unicas.it
  • Vittorio Di Cocco
  • Francesco Iacoviello
  • Luca Sorrentino
DOI
10.3221/IGF-ESIS.49.66
Pages
739-747
Published
Published inVol. 13, No. 49 (2019)Go to the issue

Abstract

Industry needs new materials that present very high structural characteristic, such as high strength, low weight and high damage tolerance. To obtain these characteristics a new class of materials has been introduced: Fibre Metal Laminate (FML); they consist in metal sheets alternated to composite material layers: in such manner, the good characteristics of each constituent material confer the utmost properties to the FMLs. However, the mechanical properties depend, among other factors, on the thickness and the numerousness of the layers constituting the FML, as well as the interface between metal and composite. Therefore, in this paper, the influence of the abovementioned factors on the material answer to flexural load was investigated. In particular, different kinds of laminates were produced varying the layers adhesion and the layers thickness, but maintaining unaltered the metal/composite volume ratio and the total laminate thickness. Then their structural behaviour was investigated through three-point bending test, and it was found that the flexural behaviour was affected by both the investigated factors; in fact, the maximum flexural load diminished incrementing the number of layers and inserting an adhesive layer at the metal/composite interface.

Keywords

Article history

  1. ReceivedUntil the next stage: 1 day
  2. AcceptedUntil the next stage: 15 days
  3. Published

How to cite

APA

Bellini, C., Di Cocco, V., Iacoviello, F., & Sorrentino, L. (2019). Experimental analysis of aluminium/carbon epoxy hybrid laminates under flexural load. Fracture and Structural Integrity, 13(49), 739–747. https://doi.org/10.3221/IGF-ESIS.49.66

IEEE

C. Bellini, V. Di Cocco, F. Iacoviello, and L. Sorrentino, “Experimental analysis of aluminium/carbon epoxy hybrid laminates under flexural load,” Fracture and Structural Integrity, vol. 13, no. 49, pp. 739–747, 2019, doi: 10.3221/IGF-ESIS.49.66.

MLA

Bellini, Costanzo, et al. “Experimental analysis of aluminium/carbon epoxy hybrid laminates under flexural load.” Fracture and Structural Integrity, vol. 13, no. 49, 2019, pp. 739–747. https://doi.org/10.3221/IGF-ESIS.49.66.

Chicago

Bellini, Costanzo, Vittorio Di Cocco, Francesco Iacoviello, and Luca Sorrentino. 2019. “Experimental analysis of aluminium/carbon epoxy hybrid laminates under flexural load.” Fracture and Structural Integrity 13 (49): 739–747. https://doi.org/10.3221/IGF-ESIS.49.66.

Harvard

Bellini, C., Di Cocco, V., Iacoviello, F. and Sorrentino, L. (2019) ‘Experimental analysis of aluminium/carbon epoxy hybrid laminates under flexural load’, Fracture and Structural Integrity, 13(49), pp. 739–747. doi: 10.3221/IGF-ESIS.49.66.

Vancouver

Bellini C, Di Cocco V, Iacoviello F, Sorrentino L. Experimental analysis of aluminium/carbon epoxy hybrid laminates under flexural load. Fracture and Structural Integrity. 2019;13(49):739-747. doi:10.3221/IGF-ESIS.49.66

BibTeX

@article{bellini2019, author = {Bellini, Costanzo and Di Cocco, Vittorio and Iacoviello, Francesco and Sorrentino, Luca}, title = {Experimental analysis of aluminium/carbon epoxy hybrid laminates under flexural load}, journal = {Fracture and Structural Integrity}, year = {2019}, volume = {13}, number = {49}, pages = {739--747}, doi = {10.3221/IGF-ESIS.49.66}, url = {https://doi.org/10.3221/IGF-ESIS.49.66}, issn = {1971-8993} }

RIS

TY - JOUR AU - Bellini, Costanzo AU - Di Cocco, Vittorio AU - Iacoviello, Francesco AU - Sorrentino, Luca TI - Experimental analysis of aluminium/carbon epoxy hybrid laminates under flexural load JO - Fracture and Structural Integrity T2 - Fracture and Structural Integrity PY - 2019 DA - 2019/06/22 VL - 13 IS - 49 SP - 739 EP - 747 DO - 10.3221/IGF-ESIS.49.66 UR - https://doi.org/10.3221/IGF-ESIS.49.66 SN - 1971-8993 ER -

Licence

Copyright © 2019 Costanzo Bellini.

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