Static analysis of delaminated composite shell panels using layerwise theory
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Publication:478329
DOI10.1007/s00707-014-1200-7zbMath1302.74103OpenAlexW2012392112MaRDI QIDQ478329
Publication date: 3 December 2014
Published in: Acta Mechanica (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1007/s00707-014-1200-7
Related Items (3)
Linear and nonlinear flexural analysis of higher-order shear deformation laminated plates with circular delamination ⋮ Delamination Effect on Flexural Responses of Layered Curved Shallow Shell Panel-Experimental and Numerical Analysis ⋮ Nonlinear finite element solutions of thermoelastic deflection and stress responses of internally damaged curved panel structure
Cites Work
- Modelling of delamination in composite laminates using a layer-wise plate theory
- Static deformations and vibration analysis of composite and sandwich plates using a layerwise theory and multiquadrics discretizations
- Dynamic analysis of composite plate with multiple delaminations based on higher-order zigzag theory
- A Simple Higher-Order Theory for Laminated Composite Plates
- Higher-Order Zig-Zag Theory for Laminated Composites With Multiple Delaminations
- General two-dimensional theory of laminated cylindrical shells
- A generalization of two-dimensional theories of laminated composite plates
- Layerwise mechanics and finite element model for laminated piezoelectric shells
- Thermally induced buckling of laminated composites by a layerwise theory
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