Future directions and challenges in shell stability analysis

被引:141
作者
Arbocz, J
Starnes, JH
机构
[1] Delft Univ Technol, Fac Aerosp Engn, Koiter Inst, NL-2600 Delft, Netherlands
[2] NASA, Langley Res Ctr, Hampton, VA USA
基金
美国国家航空航天局;
关键词
D O I
10.1016/S0263-8231(02)00024-1
中图分类号
TU [建筑科学];
学科分类号
0813 ;
摘要
Recent advances in structural analysis and design technology for buckling-critical shell structures are discussed. These advances include a hierarchical analysis strategy that includes analyses that range from classical analysis methods to high-fidelity nonlinear finite element analysis methods, reliability based design methods, the development of imperfection data bases, and the identification of traditional and nontraditional initial imperfections for composite shell structures. When used judiciously, these advances provide the basis for a viable alternative to the traditional and conservative lower-bound design philosophy of the 1960s. These advances also help answer the question of why, after so many years of concentrated research effort to understand the behavior of buckling-critical thin-walled shells, one has not been able to improve on this conservative lower- bound design philosophy in the past. (C) 2002 Elsevier Science Ltd. All rights reserved.
引用
收藏
页码:729 / 754
页数:26
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