Transitioning the Retrogression and Re-aging Process to USAF Hardware

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TypeArticle
SubjectAluminum; Al 7075-T6; retrogression and re-aging; corrosion; stress corrosion cracking; heat treatment; RRA
AffiliationNRC Institute for Aerospace Research; National Research Council Canada
Access conditionavailable
unclassified
unlimited
Peer reviewedYes
NRC numberSMPL-2001-0238
NPARC number8926896
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Record identifier19be3046-a371-4705-920e-50b7f06cd958
Record created2009-04-23
Record modified2016-05-09
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