2015
DOI: 10.1016/j.compstruct.2014.10.021
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Effect of the stiffener stiffness on the buckling and post-buckling behavior of stiffened composite panels – Experimental investigation

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Cited by 61 publications
(17 citation statements)
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References 28 publications
(38 reference statements)
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“…1 In aircraft structures, stiffened composite plates are often subject to tension, compression, bending, shear, and several of combination loadings. The main failure modes are buckling, post-buckling, matrix cracking, fiber damage, and debending.…”
Section: Introductionmentioning
confidence: 99%
“…1 In aircraft structures, stiffened composite plates are often subject to tension, compression, bending, shear, and several of combination loadings. The main failure modes are buckling, post-buckling, matrix cracking, fiber damage, and debending.…”
Section: Introductionmentioning
confidence: 99%
“…Zhu et al [3] investigated the performance of stiffness due to stiffener on the buckling and post-buckling behaviors of composite panels with stiffeners. Equivalent compression stiffness increases as buckling load reduce and it has a minor effect on final failure strength of composites that is made up of stiffened panels.…”
Section: Introductionmentioning
confidence: 99%
“…The delamination buckling and post-buckling behaviors of repaired stiffened composite panels have been studied by many researchers over the years. Many of the published works focus on the influences of geometric parameters such as panel thickness 3 and the dimension of stiffeners 4 on the buckling and post-buckling behaviors of stiffened composite panels in axial compression experiments. Riccio et al 5 performed a series of experiments to study the delamination buckling and growth phenomena of composite stiffened panels with initial delamination subjected to compressive loading.…”
Section: Introductionmentioning
confidence: 99%