Effect of prepreg gaps and overlaps on mechanical properties of fibre metal laminates
, 2018 M. Abouhamzeh +3 more
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CRASH SIMULATION OF FIBRE METAL LAMINATE FUSELAGE
, 2014 A finite element model of fibre metal laminate (FML) fuselage was developed in order to evaluate its impact response under survivable crash event. To create a reliable crash finite element (FE) model of FML fuselage, a ‘building block approach’ is adapted. It involves a series of validation and verification tasks in order to establish reliable material
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Validated Cohesive Zone Models for Epoxy-Based Adhesive Joints Between Steel and CFRP Composites for Multimaterial Structural Design in Transportation Applications. [PDF]
Polymers (Basel)Špirk S, Kalina T.
europepmc +1 more source
Investigation on fatigue life behaviour of sustainable bio-based fibre metal laminate / D. Sivakumar...[et al.] [PDF]
, 2017 Sivakumar Dhar Malingam +2 more
openalex
Mapping Life Cycle Assessment Methods for Components of Carbon Fibre Metal Laminates: A Systematic and AI-Based Review of Aluminium, Carbon Fibre, and Epoxy Resin [PDF]
Isla Hodgkinson +2 more
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Off‐axis fatigue cracking behaviour in notched fibre metal laminates [PDF]
, 2007 P.Y. Chang +3 more
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Electrospun Ni-doped ZnO nanofiber coatings on carbon fabric for enhanced electromagnetic interference shielding. [PDF]
Sci RepSuresha R +6 more
europepmc +1 more source