Pages that link to "Item:Q2268480"
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The following pages link to A global-local higher order theory including interlaminar stress continuity and \(\text C^{0}\) plate bending element for cross-ply laminated composite plates (Q2268480):
Displaying 12 items.
- An advanced higher-order theory for laminated composite plates with general lamination angles (Q362954) (← links)
- \(\mathrm{C}^0\)-type global-local theory with non-zero normal strain for the analysis of thick multilayer composite plates (Q539436) (← links)
- Shear correction factors for layered plates and shells (Q683678) (← links)
- \(C^0\) plate element for global/local analysis of multilayered composites, based on a 3D zig-zag model and strain energy updating (Q986266) (← links)
- A refined laminated plate theory accounting for the third-order shear deformation and interlaminar transverse stress continuity (Q2282663) (← links)
- Theory and numerics of layered shells with variationally embedded interlaminar stresses (Q2310088) (← links)
- Hybrid-mixed ANS finite elements for stress analysis of laminated composite structures: sampling surfaces plate formulation (Q2417633) (← links)
- A quadrilateral element based on refined global-local higher-order theory for coupling bending and extension thermo-elastic multilayered plates (Q2459816) (← links)
- Axisymmetric vibrations of composite annular sandwich plates of quadratically varying thickness by harmonic differential quadrature method (Q2516704) (← links)
- On the radially symmetric vibrations of circular sandwich plates with polar orthotropic facings and isotropic core of quadratically varying thickness by harmonic differential quadrature method (Q2629382) (← links)
- A new triangular element to model inter-laminar shear stress continuous plate theory (Q3157045) (← links)
- Refined global–local higher-order theory and finite element for laminated plates (Q3587794) (← links)
