Buckling analysis of stringer-stiffened laminated cylindrical shells with nonuniform eccentricity
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Publication:363623
DOI10.1007/S00419-010-0457-0zbMath1271.74100OpenAlexW2147260148MaRDI QIDQ363623
Publication date: 3 September 2013
Published in: Archive of Applied Mechanics (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1007/s00419-010-0457-0
Related Items (2)
Nonlinear stability of functionally graded material (FGM) sandwich cylindrical shells reinforced by FGM stiffeners in thermal environment ⋮ Mechanical and thermal postbuckling of FGM thick circular cylindrical shells reinforced by FGM stiffener system using higher-order shear deformation theory
Cites Work
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- Mechanical stability of functionally graded stiffened cylindrical shells
- Repeated buckling and its influence on the geometrical imperfections of stiffened cylindrical shells under combined loading
- Vibrations and buckling of axially loaded stiffened cylindrical shells with elastic restraints
- Vibrations of rotating cross-ply laminated circular cylindrical shells with stringer and ring stiffeners.
- Free vibration and buckling response of hat-stiffened composite panels under general loading
- General solution for nonlinear buckling of nonhomogeneous axial symmetric ring- and stringer-stiffened cylindrical shells
- Vibration analysis of rotating composite cylindrical shells with orthogonal stiffeners
- General buckling of stiffened circular cylindrical shells according to a layerwise theory
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