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Embry Riddle Aeronautical University

Experimental Investigation of Enhanced Damage Resistant Fiber Metal Laminates

Abstract

dc:description.abstract

<p>Fiber metal laminates (FMLs) are hybrid composite structures made from fiber reinforced polymeric materials sandwiched between layers of thin metal alloy sheets. FMLs combine the advantages of metallic materials and fiber reinforced matrix systems. Some of these advantages include: lighter weight, enhanced impact tolerance, improved corrosion resistance, better fire resistance, longer fatigue life, greater tensile strength, easier repair ability and maintainability, etc. The most well-known commercially available FML is GLARE (Glass Laminate Aluminum Reinforced Epoxy), however there are ongoing issues, which include a very high fabrication cost compared to many competing material systems and substantial delamination upon impact and failure. The main purpose of this study is to fabricate and test similar types of FMLs, but ones made using simpler, less expensive approaches. Two different adhesive systems were used; high strain epoxy as the matrix for all S-2 glass fiber reinforced composite layers and either the same epoxy or a high strain methacrylate to bond the composite layers to the metal layers. For effective comparison, the new FMLs laminate arrangement(s) closely mimic a few common grades of GLARE. The experimental investigation comprised of shear lap testing, tensile testing, and microscopy (e.g., optical and SEM). These experimental methods were used to assess potential improvements. The fabricated FMLs showed similar behaviors to GLARE but with some substantially improved damage tolerance characteristics.</p>

Degree

thesis:*
Name thesis:degree_name
Master of Science in Aerospace Engineering
Level thesis:degree_level
Thesis - Open Access
Discipline thesis:degree_discipline
Aerospace Engineering
Year
2018

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Tefoung, Cannelle Metang

Subjects

dc:subject × 5

Identifiers

dc:identifier.*
Repository record dc:identifier
https://commons.erau.edu/edt/400
OAI identifier oai:identifier
oai:commons.erau.edu:edt-1399

Chain of custody

source
Harvested from
Embry Riddle Aeronautical University
Base URL
commons.erau.edu/do/oai/
Last updated
2026-07-27
Source record
OAI-PMH GetRecord
citation

Tefoung, Cannelle Metang. Experimental Investigation of Enhanced Damage Resistant Fiber Metal Laminates. Thesis - Open Access thesis, 2018. https://commons.erau.edu/edt/400