Analytical prediction model for fatigue crack growth in Fibre Metal Laminates with MSD scenario

Journal Article (2017)
Author(s)

W Wang (TU Delft - Structural Integrity & Composites)

C.D. Rans (TU Delft - Structural Integrity & Composites)

R. Benedictus (TU Delft - Aerospace Structures & Materials)

Research Group
Structural Integrity & Composites
DOI related publication
https://doi.org/10.1016/j.ijfatigue.2017.07.024
More Info
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Publication Year
2017
Language
English
Research Group
Structural Integrity & Composites
Volume number
104
Pages (from-to)
263-272

Abstract

This paper presents a theoretical and experimental study on Multiple-site Damage (MSD) crack growth behaviour in Fibre Metal Laminates (FMLs). The prediction model is developed based on a simplified analysis of the effects of load redistribution on a single crack in FMLs containing multiple cracks. Test results show that the crack growth accelerates as cracks grow towards each other. The tests also show non-symmetric crack growth behaviour and non-symmetric interfacial delamination propagation in case of multiple cracks. The prediction model successfully captures the crack growth acceleration and non-symmetric growth behaviour.

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