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Hierarchical High-Fidelity Analysis Methodology for Buckling Critical Structures.

Authors :
Arbocz, Johann
Starnes, James H.
Source :
Journal of Aerospace Engineering. Jul2005, Vol. 18 Issue 3, p168-178. 11p. 5 Charts, 10 Graphs.
Publication Year :
2005

Abstract

A hierarchical high-fidelity analysis methodology for predicting the critical buckling load of compression-loaded thin-walled isotropic shells is described. This hierarchical procedure includes three levels of fidelity for the analysis. Level 1 assumes that the buckling load can be predicted by the classical shell solution with simply supported boundary condition, and with a linear membrane prebuckling solution. Level 2 includes the effects of a nonlinear prebuckling solution and the effects of traditional clamped or simply supported boundary conditions. Level 3 includes the nonlinear interaction between nearly simultaneous buckling modes and the effects of boundary imperfections and general boundary conditions. Various deterministic and probabilistic approaches are used to account for the degrading effects of unavoidable shell-wall geometric imperfections. The results from the three solution levels are compared with experimental results, and the effects of the assumptions and approximations used for the three solution levels are discussed. This hierarchical analysis approach can be used in the design process to converge rapidly to an accurate prediction of the expected buckling load of a thin-shell design problem. [ABSTRACT FROM AUTHOR]

Details

Language :
English
ISSN :
08931321
Volume :
18
Issue :
3
Database :
Academic Search Index
Journal :
Journal of Aerospace Engineering
Publication Type :
Academic Journal
Accession number :
17328536
Full Text :
https://doi.org/10.1061/(ASCE)0893-1321(2005)18:3(168)