Composite_beams_HSBT_submit.pdf (193.38 kB)
Trigonometric-series solution for analysis of laminated composite beams
journal contributionposted on 2020-12-02, 06:00 authored by Trung-Kien Nguyen, Ngoc-Duong Nguyen, Thuc VoThuc Vo, Huu Tai Thai
© 2016 Elsevier Ltd
A new analytical solution based on a higher-order beam theory for static, buckling and vibration of laminated composite beams is proposed in this paper. The governing equations of motion are derived from Lagrange's equations. An analytical solution based on trigonometric series, which satisfies various boundary conditions, is developed to solve the problem. Numerical results are obtained to compare with previous studies and to investigate the effects of length-to-depth ratio, fibre angles and material anisotropy on the deflections, stresses, natural frequencies and critical buckling loads of composite beams with various configurations.
Vietnam National Foundation for Science and Technology Development | 107.02-2015.07
Pagination10p. (p. 142-151)
Rights StatementThe Author reserves all moral rights over the deposited text and must be credited if any re-use occurs. Documents deposited in OPAL are the Open Access versions of outputs published elsewhere. Changes resulting from the publishing process may therefore not be reflected in this document. The final published version may be obtained via the publisher’s DOI. Please note that additional copyright and access restrictions may apply to the published version.
CategoriesNo categories selected
Science & TechnologyTechnologyMechanicsMaterials Science, CompositesMaterials ScienceTrigonometric-series solutionLaminated composite beamsStaticBucklingVibrationFREE-VIBRATION ANALYSISHIGHER-ORDER THEORIESGENERAL BOUNDARY-CONDITIONSSHEAR DEFORMATION THEORIESGRADED SANDWICH BEAMSFINITE-ELEMENTBUCKLING ANALYSISTRANSVERSE-SHEARBENDING ANALYSISDYNAMIC-ANALYSISMaterials