2015 IEEE Aerospace Conference 2015
DOI: 10.1109/aero.2015.7119048
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Aircraft corrosion monitoring and data visualization techniques for condition based maintenance

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Cited by 5 publications
(4 citation statements)
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“…Extensive corrosion may occur in aircraft structures, including general corrosion, pitting corrosion, stress corrosion cracking, environmental embrittlement, corrosion fatigue and spalling. The selection of specific metal materials to meet aircraft design requirements is mainly based on their performance attributes, such as weight, stiffness, strength, electrical characteristics, etc., rather than their ability to resist corrosion [91,92] .…”
Section: Graphene-based Ph Sensormentioning
confidence: 99%
“…Extensive corrosion may occur in aircraft structures, including general corrosion, pitting corrosion, stress corrosion cracking, environmental embrittlement, corrosion fatigue and spalling. The selection of specific metal materials to meet aircraft design requirements is mainly based on their performance attributes, such as weight, stiffness, strength, electrical characteristics, etc., rather than their ability to resist corrosion [91,92] .…”
Section: Graphene-based Ph Sensormentioning
confidence: 99%
“…For instance, GO is a functionalized form of graphene resulting from attaching oxygen atoms [57]. During the oxidation process of graphene, sp 3 bonding is heavily interrupted and makes electrical conductivity of graphene oxide decrease drastically compared to pristine graphene [62]. GO can be modified to produce functionalized GO (FGO), which has an altered electronic conductivity (lower or higher depend on the functionalization type) compared to pristine graphene and GO [63,64].…”
Section: Implementation Of Organic Thin Film Materials In Corrosion Sensingmentioning
confidence: 99%
“…A wide range of corrosion may occur in aircraft structures, such as general corrosion, pitting, stress-corrosion cracking, environmental embrittlement, and corrosion fatigue and exfoliation. Specific metallic materials are selected to fulfill aircraft design requirement based primarily on the performance attributes they exhibit, such as weight, stiffness, strength, electrical properties etc., rather than their ability to resist the onset of corrosion [ 2 , 3 ].…”
Section: Introductionmentioning
confidence: 99%
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