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Methodologies for the Damage Detection Based on Fiber-Optic Sensors. Applications to the Fuselage Panel and Lower Wing Panel

  • Güemes A
  • Sierra J
  • Grooteman F
  • et al.
Springer International Publishing, (2016), 407-431
DOI: 10.1007/978-3-319-22413-8_19
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Abstract

Damages in aircrafts start as local cracks or delaminations, which, even though they do not change strongly the overall strain field, form initiation points for an eventual failure. Fiber-optic sensors act primarily as strain sensors, so unless damage happens to be...

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APA

Güemes, A., Sierra, J., Grooteman, F., Kanakis, T., Michaelides, P., Habas, D., … Kontis, N. (2016). Methodologies for the Damage Detection Based on Fiber-Optic Sensors. Applications to the Fuselage Panel and Lower Wing Panel. In Smart Intelligent Aircraft Structures (SARISTU) (pp. 407–431). Springer International Publishing. https://doi.org/10.1007/978-3-319-22413-8_19

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