Hierarchical Evaluation of Failure Parameters in Composite Plates

被引:31
作者
Carrera, E. [1 ]
Giunta, G. [1 ,2 ]
机构
[1] Politecn Torino, Dept Aeronaut & Space Engn, I-10129 Turin, Italy
[2] Ctr Rech Publ Henri Tudor, L-1855 Luxembourg, Luxembourg
关键词
INITIAL FLEXURAL FAILURE; MULTILAYERED PLATES; SANDWICH; FORMULATION; MODELS; BENT;
D O I
10.2514/1.38585
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper presents a failure analysis of simply supported, orthotropic plates subjected to global/local bending loadings via the Navier-type solution. Carrera's unified formulation is adopted in order to implement a large variety of two-dimensional theories. The minimum first-ply failure loading and the failure locations are obtained via classical, refined, zig-zag, layerwise, and mixed theories. The maximum stress, Tsai-Wu, Tsai-Hill, Hoffman, and Hashin failure criteria are assumed. The accuracy of two-dimensional theories is assessed via comparison with the three-dimensional Pagano's solution, which has here been extended to the considered cases. The influence of the side-to-thickness ratio, the aspect ratio, the material properties, the lamination layup, and the loading localization is investigated. A hierarchy among the Carrera's unified formulation two-dimensional models has been established.
引用
收藏
页码:692 / 702
页数:11
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