Composites airframe panel design for post-buckling – An experimental investigation

Published 2020 View Full Article

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Title
Composites airframe panel design for post-buckling – An experimental investigation
Authors
Keywords
Composite stiffened panel, Compression load, Delamination, Disbond, Impact damage
Journal
COMPOSITE STRUCTURES
Volume 241, Issue -, Pages 112104
Publisher
Elsevier BV
Online
2020-02-23
DOI
10.1016/j.compstruct.2020.112104

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