An axiomatic/asymptotic evaluation of the best theories for free vibration of laminated and sandwich shells using non-polynomial functions

J. C. Monge, J. L. Mantari, S. Charca, N. Vladimir

Research output: Contribution to journalArticlepeer-review

15 Scopus citations

Abstract

This paper presents Best Theory Diagrams (BTDs) constructed from non-polynomial terms to identify best shell theories for the free vibration analysis of laminated and sandwich shell. The shell theories have been constructed using Axiomatic/Asymptotic Method (AAM). The refined models are implemented following the compactness of a unified formulation developed. The governing equations are derived from the Hamilton's Principle. Navier-Type solution technique is used for solving the eigenvalue problem of simply supported shell. The BTDs use 3D equilibrium solutions as a reference. The BTDs built from non-polynomial functions are compared with Maclaurin expansions. The results are compared with Layerwise solutions. Cylindrical and spherical shells with different layer-configurations are investigated. The results demonstrate that the shell models obtained from the BTD using non-polynomial terms can improve the accuracy obtained from Maclaurin expansion for a given order of expansion of a displacement field.

Original languageEnglish
Pages (from-to)1011-1024
Number of pages14
JournalEngineering Structures
Volume172
DOIs
StatePublished - 1 Oct 2018

Keywords

  • Axiomatic/asymptotic
  • Best Theory Diagram
  • Carrera Unified Formulation (CUF)
  • Laminated composite
  • Shell

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