Experimental and numerical investigation of ply size effects of steel foil reinforced composites

Journal Article (2021)
Author(s)

A. Keller (University of Applied Sciences and Arts Northwestern Switzerland)

R. Geissberger (University of Applied Sciences and Arts Northwestern Switzerland)

Julia Studer (University of Applied Sciences and Arts Northwestern Switzerland)

F. Leone (University of Applied Sciences and Arts Northwestern Switzerland)

D. Stefaniak (Deutsches Zentrum für Luft- und Raumfahrt (DLR))

John-Alan Pascoe (TU Delft - Structural Integrity & Composites)

C. A. Dransfeld (TU Delft - Aerospace Manufacturing Technologies, University of Applied Sciences and Arts Northwestern Switzerland)

K. Masania (University of Applied Sciences and Arts Northwestern Switzerland, TU Delft - Aerospace Manufacturing Technologies)

Research Group
Codesigning Social Change
Copyright
© 2021 A. Keller, R. Geissberger, J. Studer, F. Leone, D. Stefaniak, J.A. Pascoe, C.A. Dransfeld, K. Masania
DOI related publication
https://doi.org/10.1016/j.matdes.2020.109302
More Info
expand_more
Publication Year
2021
Language
English
Copyright
© 2021 A. Keller, R. Geissberger, J. Studer, F. Leone, D. Stefaniak, J.A. Pascoe, C.A. Dransfeld, K. Masania
Research Group
Codesigning Social Change
Volume number
198
Reuse Rights

Other than for strictly personal use, it is not permitted to download, forward or distribute the text or part of it, without the consent of the author(s) and/or copyright holder(s), unless the work is under an open content license such as Creative Commons.

Abstract

The effect of ply thickness on the notch sensitivity and bearing properties on carbon fibre reinforced polymer composites and their hybrid laminates with steel foils were studied. Laminates with ply thicknesses of 0.3 mm and 0.03 mm comprising of CFRP and hybrid laminates were manufactured and characterized using tension, open hole tension and double lap bearing tests. A 25% ply substitution was found to double the bearing load with extensive plastic deformation in the joint while maintaining high stress and maintaining constant cross-sectional thickness in the laminate. With a good agreement between the finite element predicted values and failure behaviour, the damage initiation and progression behaviour could be observed experimentally. We numerically captured (i) rapid failure of 0° plies in the thin ply CFRP hybrid and (ii) continuous delamination with significant plastic deformation for the thick ply CFRP hybrid. The numerical results significantly reduce future experimental work when designing hybrid laminates and could allow the laminate lay-up to be tailored for load cases. Both the experiments and numerical models underline the distinct size effects occurring with respect to the ply thicknesses when hybridising a very ductile metal with a brittle yet strong composite material.