Defect Detection in Aerospace Sandwich Composite Panels Using Conductive Thermography and Contact Sensors

Sandwich panels consisting of two Carbon Fibre Reinforced Polymer (CFRP) outer skins and an aluminium honeycomb core are a common structure of surfaces on commercial aircraft due to the beneficial strength–weight ratio. Mechanical defects such as a crushed honeycomb core, dis-bonds and delaminations...

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Detalles Bibliográficos
Autores principales: Gillespie, David I., Hamilton, Andrew W., Atkinson, Robert C., Bellekens, Xavier, Michie, Craig, Andonovic, Ivan, Tachtatzis, Christos
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2020
Materias:
Letter
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC7700599/
https://www.ncbi.nlm.nih.gov/pubmed/33238398
http://dx.doi.org/10.3390/s20226689

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC7700599/
https://www.ncbi.nlm.nih.gov/pubmed/33238398
http://dx.doi.org/10.3390/s20226689

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