Lesson plan

Glare

Glare (derived from GLAss REinforced laminate ) is a fiber metal laminate (FML) composed of several very thin layers of metal (usually aluminum) interspersed with layers of S-2 glass-fiber pre-preg, bonded together with a matrix such as epoxy. The uni-directional pre-preg layers may be aligned in different directions to suit predicted stress conditions. Though Glare is a composite material, its material properties and fabrication are very similar to bulk aluminum sheets. It has far less in common with composite structures when it comes to design, manufacture, inspection, or maintenance. Glare parts are constructed and repaired using mostly conventional metal working techniques. Its major advantages over conventional aluminum are: * Better "damage tolerance" behavior, especially in impact and metal fatigue. Since the elastic strain is larger than other metal materials , it can consume more impact energy. It is dented more easily but has a higher penetration resistance. * Better corrosion resistance. * Better fire resistance. * Lower specific weight. Furthermore, the material can be tailored during design and manufacture so that the number, type and alignment of layers can suit the local stresses and shapes throughout the aircraft. This allows the production of double-curved sections, complex integrated panels, or very large sheets.…

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Article summary

Glare (derived from GLAss REinforced laminate ) is a fiber metal laminate (FML) composed of several very thin layers of metal (usually aluminum) interspersed with layers of S-2 glass-fiber pre-preg, bonded together with a matrix such as epoxy. The uni-directional pre-preg layers may be aligned in different directions to suit predicted stress conditions. Though Glare is a composite material, its material properties and fabrication are very similar to bulk aluminum sheets. It has far less in common with composite structures when it comes to design, manufacture, inspection, or maintenance. Glare parts are constructed and repaired using mostly conventional metal working techniques. Its major advantages over conventional aluminum are: * Better "damage tolerance" behavior, especially in impact and metal fatigue. Since the elastic strain is larger than other metal materials , it can consume more impact energy. It is dented more easily but has a higher penetration resistance. * Better corrosion resistance. * Better fire resistance. * Lower specific weight. Furthermore, the material can be tailored during design and manufacture so that the number, type and alignment of layers can suit the local stresses and shapes throughout the aircraft. This allows the production of double-curved sections, complex integrated panels, or very large sheets.…

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Discussion questions

  1. Summarise the article in your own words. Which single claim would you verify first, and why?
  2. Which claim in this article is most likely to be revised as the sources update? How would you check its current status?
  3. If two sources disagreed about one of these facts, what would you need in order to trust one over the other?

Bibliography

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Key claims and bibliography are generated from the same tracked claims and sources as the article page.