Thermal buckling and free vibration of viscoelastic functionally graded sandwich shells with tunable auxetic honeycomb core
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Publication:2109646
DOI10.1016/J.APM.2022.04.019zbMath1503.74036OpenAlexW4225146246MaRDI QIDQ2109646
Publication date: 21 December 2022
Published in: Applied Mathematical Modelling (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/j.apm.2022.04.019
viscoelastic materialsthermal bucklingsandwich shellnegative Poisson's ratiohybrid auxetic honeycomb
Vibrations in dynamical problems in solid mechanics (74H45) Thermal effects in solid mechanics (74F05) Bifurcation and buckling (74G60) Shells (74K25)
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Cites Work
- Semi-analytical buckling analysis of heterogeneous variable thickness viscoelastic circular plates on elastic foundations
- Static and free vibration analysis of sandwich cylindrical shell based on theory of elasticity and using DQM
- Assessment of the effect of negative Poisson's ratio on the thermal postbuckling of temperature dependent FG-GRMMC laminated cylindrical shells
- Equivalent-single-layer discontinuous Galerkin methods for static analysis of multilayered shells
- Nonlinear buckling and postbuckling of sandwich FGM cylindrical shells reinforced by spiral stiffeners under torsion loads in thermal environment
- An Edge-Based Smoothed MITC3 (ES-MITC3) Shell Finite Element in Laminated Composite Shell Structures Analysis
- Transverse vibrations analysis of a beam with degrading hysteretic behavior by using Euler-Bernoulli beam model
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