Thermo-piezoelectric effects on the postbuckling of axially-loaded hybrid laminated cylindrical panels

DOI10.1007/BF02437291zbMath1062.74534OpenAlexW363317757MaRDI QIDQ1890315

Hui Shen Shen

Publication date: 3 January 2005

Published in: Applied Mathematics and Mechanics. (English Edition) (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/bf02437291

Mathematics Subject Classification ID

Composite and mixture properties (74E30) Thermal effects in solid mechanics (74F05) Stability of dynamical problems in solid mechanics (74H55) Bifurcation and buckling (74G60) Shells (74K25) Electromagnetic effects in solid mechanics (74F15)

Related Items (1)

An analytical approach for postbuckling of eccentrically or concentrically stiffened composite double curved panel on nonlinear elastic foundation

Cites Work

• Three-dimensional buckling analysis of laminated composite hollow cylinders and cylindrical panels
• A boundary layer theory for the buckling of thin cylindrical shells under external pressure
• Postbuckling analysis of axially-loaded laminated cylindrical shells with piezoelectric actuators
• Postbuckling of laminated cylindrical shells with piezoelectric actuators under combined external pressure and heating.
• Postbuckling of pressure-loaded shear deformable laminated cylindrical panels
• POSTBUCKLING AND VIBRATION CHARACTERISTICS OF PIEZOLAMINATED COMPOSITE PLATE SUBJECT TO THERMO-PIEZOELECTRIC LOADS
• Large Deflection Behavior of Simply Supported Laminated Panels Under In-Plane Loading
• Mixed Laminate Theory and Finite Element for Smart Piezoelectric Composite Shell Structures
• Nonaxisymmetric Exact Piezothermoelastic Solution for Laminated Cylindrical Shell
• Accurate determination of transverse normal stresses in hybrid laminated panels subjected to electro-thermo-mechanical loadings

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