Numerical Simulation of C-141 Lower Wing Panels with and without Simulated Exfoliation Corrosion Damage Under Compression Loading --ABSTRACT ONLY

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Conference25th Congress of International Council of the Aeronautical Sciences From 9/3/2006 To 9/8/2006
SubjectC-141; compression testing; finite element model; post-buckling; stiffened wing panel
AffiliationNRC Institute for Aerospace Research; National Research Council Canada
Access conditionavailable
Peer reviewedYes
NRC numberSMPL-2005-0120
NPARC number8930104
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Record identifier03ce1158-47bb-4e5e-b2a5-dd611b5b83f7
Record created2009-04-23
Record modified2016-05-09
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