Development of Invariant-Based Triangular Element for Nonlinear Thermoelastic Analysis of Laminated Shells

DOI10.1007/978-3-030-17747-8_22zbMath1461.74084OpenAlexW2976024868MaRDI QIDQ5131288

S. V. Levyakov

Publication date: 5 November 2020

Published in: Advanced Structured Materials (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/978-3-030-17747-8_22

zbMATH Keywords

stabilitybucklingthermal loadingnonlinear deformationtemperature-dependent material

Mathematics Subject Classification ID

Finite element methods applied to problems in solid mechanics (74S05) Composite and mixture properties (74E30) Thermal effects in solid mechanics (74F05) Shells (74K25)

Uses Software

• TRIC

Cites Work

• Unnamed Item
• Thermal buckling of laminated plates using a shear flexible finite element
• TRIC: A simple but sophisticated 3-node triangular element based on 6 rigid-body and 12 straining modes for fast computational simulations of arbitrary isotropic and laminated composite shells
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• Thermal buckling of shear-deformable composite laminated plates by the spline finite strip method
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• Linear and geometrically nonlinear bending of isotropic and multilayered composite plates by the natural mode method
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• Complete system of two-dimensional invariants for formulation of triangular finite element of composite shells
• Phenomenological invariants and their application to geometrically nonlinear formulation of triangular finite elements of shear deformable shells
• Thermal stress analysis of laminated doubly curved shells using a shear flexible finite element
• Thermal buckling of laminated composite plates
• Thermal buckling of composite laminated plates
• Large deflections of laminated cylindrical and doubly-curved panels under thermal loading
• A simple triangular facet shell element with applications to linear and non-linear equilibrium and elastic stability problems
• Thermal postbuckling behavior of imperfect shear deformable laminated plates with temperature-dependent properties

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