Effect of Process-Induced Residual Stresses on Fatigue Crack Initiation and Growth in Fibre Metal Laminates - ABSTRACT ONLY

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TypeArticle
ConferenceInternational Committee on Aeronautical Fatigue Symposium 2007 From 05/14/2007 To 05/18/2007, Napoli, Italy
SubjectFML; cure cycle; residual stress; fatigue; process optimisation
AffiliationNRC Institute for Aerospace Research; National Research Council Canada
Access conditionavailable
unclassified
unlimited
Peer reviewedYes
NRC numberSMPL-2006-0135
NPARC number8929283
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Record identifier36fa48bc-63d3-4376-a76a-94b71f358681
Record created2009-04-23
Record modified2016-05-09
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