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...

Full description

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

Similar Items