Thermal control of corrosion in aluminum panels of airplanes

V. P. Vavilov, Guo Sin'yan', V. V. Shiryaev, D. A. Nesteruk

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Аннотация

The sensitivity threshold of thermal testing was found experimentally during corrosion detection in aircraft aluminum panels no thicker than 2 mm. The possibilities of computer simulation and developed processing of infrared thermograms, including a simple algorithm of quantitative estimation of a material loss, are shown.

Язык оригинала	Английский
Страницы (с-по)	266-273
Число страниц	8
Журнал	Russian Journal of Nondestructive Testing
Том	44
Номер выпуска	4
DOI	https://doi.org/10.1134/S1061830908040062
Состояние	Опубликовано - апр 2008

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ASJC Scopus subject areas

Materials Science (miscellaneous)

Цитировать

Vavilov, V. P., Sin'yan', G., Shiryaev, V. V., & Nesteruk, D. A. (2008). Thermal control of corrosion in aluminum panels of airplanes. Russian Journal of Nondestructive Testing, 44(4), 266-273. https://doi.org/10.1134/S1061830908040062

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Доступ к документу

10.1134/S1061830908040062