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A Nonlinear Viscoelastic Modeling of Fiber Metal Laminates
Volume 12: New Developments in Simulation Methods and Software for Engineering Applications, 2007A new class of advanced composite materials namely the fibermetal laminates (FMLs) such as ARALL (Aramid Reinforced Aluminum laminate) and GLARE (Glass Reinforced Aluminum laminate) has been developed for primary load bearing components of aircraft fuselage and wings.
Sourabh Sawant, Anastasia Muliana
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Investigation on Formability of Fiber Metal Laminates
2020In this study, the formability of fiber metal laminates (FML) used in aerospace industry were experimentally examined. Al5754-H22 sheets in two different thicknesses (0.6 and 1.2 mm) were used in top and bottom layers of FML specimens. Carbon fiber plates made of prepreg carbon fiber fabrics were placed in the middle layer of FML specimens. In order to
IŞIKTAŞ, Ali, TAŞKIN, Vedat
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Method for fabrication of a fiber metal laminate
2012Aerospace Materials ...
Alderliesten, R.C. (author) +1 more
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Investigation of Scaling Effects in Fiber—Metal Laminates
Journal of Composite Materials, 2008The results of a series of quasi-static and impact tests on four scale-model sizes of fiber—metal laminate (FML) are compared to a scaling law that predicts response parameters based on a simple geometrical relationship of the input parameters. The FMLs consist of an aluminum alloy and a self-reinforced thermoplastic composite based on polypropylene ...
S. Mckown, W.J. Cantwell, N. Jones
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Fracture of Fiber-Metal Laminate GLARE 2
2000Low temperature regimes impose various constraints with regard to structural material performance. In this context, advanced composite materials and fiber-reinforced metal laminates (FML) have been considered to be appropriate candidates, and in some cases even a favored choice.
A. Bussiba, M. Kupiec, S. Ifergane
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Nondestructive Evaluation of Fiber-Metal Laminates
2009International Conference on Composites Engineering, ICCE7, Denver ...
Fahr, A. +3 more
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Fatigue crack growth in fiber-metal laminates
International Journal of Solids and Structures, 1995Abstract The fatigue behavior of cracked fiber-metal laminates containing residual stresses is studied. A finite element model employing special interface elements is developed for this study. The use of the interface element allows the simulation to be completed in a single finite element analysis conducted within the limitations of elasticity ...
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