Canadian Forces In-Flight Acoustic Emission Monitoring Program

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1979
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McBride, S.
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Abstract

A crack growing in the forward wing trunnion of a CF100 aircraft was monitored for over 60 flying hours. Acoustic emission data was detected which indicated that during climb, following take-off,the 3mm crack made unstable advances on a few occasions. The detected crack advances produced about 1mm2 of new fracture surface.

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Mon Jan 01 00:00:00 UTC 1979
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