A simplified geometric stiffness in stability analysis of thin-walled structures by the finite element method
Author(s) -
Ivo Senjanović,
Nikola Vladimir,
DaeSeung Cho
Publication year - 2012
Publication title -
international journal of naval architecture and ocean engineering
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 1.047
H-Index - 26
eISSN - 2092-6790
pISSN - 2092-6782
DOI - 10.2478/ijnaoe-2013-0099
Subject(s) - direct stiffness method , stiffness , stiffness matrix , tangent stiffness matrix , mass matrix , deflection (physics) , finite element method , matrix (chemical analysis) , vibration , structural engineering , mathematical analysis , buckling , geometry , mathematics , engineering , materials science , physics , classical mechanics , composite material , quantum mechanics , nuclear physics , neutrino
Vibration analysis of a thin-walled structure can be performed with a consistent mass matrix determined by the shape functions of all degrees of freedom (d.o.f.) used for construction of conventional stiffness matrix, or with a lumped mass matrix. In similar way stability of a structure can be analysed with consistent geometric stiffness matrix or geometric stiffness matrix with lumped buckling load, related only to the rotational d.o.f. Recently, the simplified mass matrix is constructed employing shape functions of in-plane displacements for plate deflection. In this paper the same approach is used for construction of simplified geometric stiffness matrix. Beam element, and triangular and rectangular plate element are considered. Application of the new geometric stiffness is illustrated in the case of simply supported beam and square plate. The same problems are solved with consistent and lumped geometric stiffness matrix, and the obtained results are compared with the analytical solution. Also, a combination of simplified and lumped geometric stiffness matrix is analysed in order to increase accuracy of stability analysis
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