Proceedings of the 2015 4th International Conference on Sustainable Energy and Environmental Engineering 2016
DOI: 10.2991/icseee-15.2016.146
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Ultimate Strength of Steel Panels and Stiffened Plates with Longitudinal Through-thickness Cracks under Compression

Abstract: A series of nonlinear finite element analysis for unstiffened and stiffened plates with initial defect is carried out by ANSYS software. The ultimate strength of steel panels and stiffened plates with longitudinal through-thickness cracks under longitudinal compression is studied in this paper. The influence of mesh size, initial deflections of plate and stiffeners to ultimate strength is considered in the numerical analyses. Comparisons between the results by the paper and those from the experiment are made. … Show more

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Cited by 2 publications
(2 citation statements)
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“…Quantification of the structural results in this work provides a set of reference data that build on pioneering works on plated structures, which predominantly applied shell elements. ese works have varied, e.g., nonlinear buckling [47], compressive strength [48,49], and plate-beam combination [50]. Salomon [51] studied similar subjects to those presented in this work and introduced an analytical theory describing different deflection phenomena on the shell model and 3D model (solid).…”
Section: Overall Discussionmentioning
confidence: 99%
“…Quantification of the structural results in this work provides a set of reference data that build on pioneering works on plated structures, which predominantly applied shell elements. ese works have varied, e.g., nonlinear buckling [47], compressive strength [48,49], and plate-beam combination [50]. Salomon [51] studied similar subjects to those presented in this work and introduced an analytical theory describing different deflection phenomena on the shell model and 3D model (solid).…”
Section: Overall Discussionmentioning
confidence: 99%
“…In the present study, the first mode of linear eigenvalue buckling analysis is chosen to simulate the initial deformation of plates and stiffened plates. However, the ultimate strength and the mode of collapse of the stiffened panels are affected only slightly [43,44].…”
Section: Initial Imperfectionsmentioning
confidence: 98%