Abstract
The in-plane mechanical properties of FMLs have been described with methods ranging from simple engineering methods to scientific laminated plate theories. This chapter describes the current understanding of stress and strain in FMLs, explaining the laminated plate theories adapted for the different thermal expansion properties of both metal and composites, and the plasticity induced by the metallic constituent. The application and limitations of the various methods are addressed.
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Notes
- 1.
Note that the definition of S and C here is opposite to the definition of Jones [1].
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Alderliesten, R. (2017). Stress and Strain. In: Fatigue and Fracture of Fibre Metal Laminates. Solid Mechanics and Its Applications, vol 236. Springer, Cham. https://doi.org/10.1007/978-3-319-56227-8_4
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DOI: https://doi.org/10.1007/978-3-319-56227-8_4
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