Ruixue Ji
Beihang University
Composite numberDeformation (engineering)Composite laminatesMaterials scienceUltimate failureMultiple failureUniaxial compressionCohesive zone modelStructural engineeringBuckling
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#1Ruixue Ji (Beihang University)
#2Libin Zhao (Beihang University)H-Index: 21
Last. Jianyu Zhang (Chongqing University)H-Index: 25
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Abstract Effects of stiffener debonding defects on postbuckling responses and failure behaviors of composite stiffened panels which have extensive applications in aerospace structures attract significantly increasing attention recently. Aiming to this problem, a series of nonlinear analyses comprehensively accounting for multiple failure modes including intra- and inter-laminar damage in composite laminates, adhesive layer damage between stiffeners and skin, as well as buckling and postbuckling ...
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