Quantitative thermoelastic measurement on a helicopter glass fibre component underneath a surface anti-fretting coating.

Quantitative thermoelastic measurement on a helicopter glass fibre component underneath a surface anti-fretting coating.

Thermoelastic stress analysis (TSA) has been applied to measure the first stress invariant on a composite helicopter component under load. The component comprised inner mono-directional glass fiber layers with an outer central plate in glass fiber cloth, covered by an anti-fretting surface coatin...

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Bibliographic Details
Main Authors: Costa A., Salerno A.
Format: Article
Language:English
Published: EDP Sciences 2010-06-01
Series:EPJ Web of Conferences
Online Access:http://dx.doi.org/10.1051/epjconf/20100638006
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spelling doaj-381fea98976945b78a549feec4431fb92021-08-02T09:18:44ZengEDP SciencesEPJ Web of Conferences2100-014X2010-06-0163800610.1051/epjconf/20100638006Quantitative thermoelastic measurement on a helicopter glass fibre component underneath a surface anti-fretting coating.Costa A.Salerno A.Thermoelastic stress analysis (TSA) has been applied to measure the first stress invariant on a composite helicopter component under load. The component comprised inner mono-directional glass fiber layers with an outer central plate in glass fiber cloth, covered by an anti-fretting surface coating. In order to obtain quantitative results, a previous calibration of the thermoelastic constant obtained on a composite sample with a similar anti-fretting coating has been necessary. http://dx.doi.org/10.1051/epjconf/20100638006
collection DOAJ
language English
format Article
sources DOAJ
author Costa A.
Salerno A.
spellingShingle Costa A.
Salerno A.
Quantitative thermoelastic measurement on a helicopter glass fibre component underneath a surface anti-fretting coating.
EPJ Web of Conferences
author_facet Costa A.
Salerno A.
author_sort Costa A.
title Quantitative thermoelastic measurement on a helicopter glass fibre component underneath a surface anti-fretting coating.
title_short Quantitative thermoelastic measurement on a helicopter glass fibre component underneath a surface anti-fretting coating.
title_full Quantitative thermoelastic measurement on a helicopter glass fibre component underneath a surface anti-fretting coating.
title_fullStr Quantitative thermoelastic measurement on a helicopter glass fibre component underneath a surface anti-fretting coating.
title_full_unstemmed Quantitative thermoelastic measurement on a helicopter glass fibre component underneath a surface anti-fretting coating.
title_sort quantitative thermoelastic measurement on a helicopter glass fibre component underneath a surface anti-fretting coating.
publisher EDP Sciences
series EPJ Web of Conferences
issn 2100-014X
publishDate 2010-06-01
description Thermoelastic stress analysis (TSA) has been applied to measure the first stress invariant on a composite helicopter component under load. The component comprised inner mono-directional glass fiber layers with an outer central plate in glass fiber cloth, covered by an anti-fretting surface coating. In order to obtain quantitative results, a previous calibration of the thermoelastic constant obtained on a composite sample with a similar anti-fretting coating has been necessary.
url http://dx.doi.org/10.1051/epjconf/20100638006
work_keys_str_mv AT costaa quantitativethermoelasticmeasurementonahelicopterglassfibrecomponentunderneathasurfaceantifrettingcoating
AT salernoa quantitativethermoelasticmeasurementonahelicopterglassfibrecomponentunderneathasurfaceantifrettingcoating
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