Free and forced vibration analysis of laminated composite plates and shells using a 9-node assumed strain shell element
DOI10.1007/s00466-005-0007-8zbMath1168.74364OpenAlexW2022369813MaRDI QIDQ835452
Publication date: 28 August 2009
Published in: Computational Mechanics (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1007/s00466-005-0007-8
lockingassumed natural strain methodnatural frequencyforced vibration analysislaminated composite plates and shellsnine-node shell element
Vibrations in dynamical problems in solid mechanics (74H45) Plates (74K20) Finite element methods applied to problems in solid mechanics (74S05) Composite and mixture properties (74E30)
Related Items (2)
Cites Work
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- A co-rotational 8-node assumed strain shell element for postbuckling analysis of laminated composite plates and shells
- A resultant 8-node solid-shell element for geometrically nonlinear analysis
- Research on thick plate vibration: a literature survey
- Buckling and vibration of laminated composite plates using various plate theories
- On the Variational Foundations of Assumed Strain Methods
- A new nine node degenerated shell element with enhanced membrane and shear interpolation
- An assumed covariant strain based 9-node shell element
- Assumed strain stabilization procedure for the 9‐node Lagrange shell element
- On the Solutions to Forced Motions of Rectangular Composite Plates
- A nine-node assumed strain finite element for large-deformation analysis of laminated shells
- Dynamic response of laminated anisotropic plates
- Geometrically nonlinear transient analysis of laminated composite plates
- An exact analysis for vibration of simply-supported homogeneous and laminated thick rectangular plates
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