In-situ Retrogression and Re-aging of a C-130 Al 7075-T6511 Sloping Longeron

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TypeArticle
Conference2000 USAF Aircraft Structural Integrity Program Conference, Texas, 5-7 December 2000
Subject7075 aluminum; heat treating; retrogression; re-aging; stress corrosion cracking
AffiliationNRC Institute for Aerospace Research; National Research Council Canada
Access conditionavailable
unclassified
unlimited
Peer reviewedYes
NRC numberSMPL-2000-0298
NPARC number8929790
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Record identifier3a6f656c-11f4-4408-ad7b-dd45885b8cef
Record created2009-04-23
Record modified2016-05-09
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