Pages that link to "Item:Q396109"
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The following pages link to A \(\mathrm C^0\)-type zig-zag theory and finite element for laminated composite and sandwich plates with general configurations (Q396109):
Displaying 15 items.
- A new zig-zag theory and \(C^0\) plate bending element for composite and sandwich plates (Q363389) (← 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)
- Improved thermo-mechanical stress prediction of laminated composite and sandwich plates using enhanced LCW theory (Q1658843) (← links)
- An efficient zigzag theory based finite element modeling of composite and sandwich plates with multiple delaminations using a hybrid continuity method (Q1986774) (← links)
- \(\mathrm{C}_{\mathrm{0}}\) FE model based on HOZT for the analysis of laminated soft core skew sandwich plates: bending and vibration (Q1994436) (← links)
- Free vibration analysis of laminated composite hybrid and GFRP shells based on higher order zigzag theory with experimental validation (Q2035240) (← links)
- A global-local higher order theory including interlaminar stress continuity and \(\text C^{0}\) plate bending element for cross-ply laminated composite plates (Q2268480) (← links)
- Explicit matrices for a composite beam-column with refined zigzag kinematics (Q2398657) (← links)
- A mixed finite element model with enhanced zigzag kinematics for the non-linear analysis of multilayer plates (Q2665014) (← links)
- A four-noded quadrilateral element for composite laminated plates/shells using the refined zigzag theory (Q2952327) (← links)
- Layerwise mixed element with sublaminates approximation and 3D zig-zag field, for analysis of local effects in laminated and sandwich composites (Q3587858) (← links)
- Modal validation of sandwich shell finite elements based on a <i>p</i>‐order shear deformation theory including zigzag terms (Q3619737) (← links)
- C0 REISSNER-MINDLIN MULTILAYERED PLATE ELEMENTS INCLUDING ZIG-ZAG AND INTERLAMINAR STRESS CONTINUITY (Q4349469) (← links)
- Zigzag theory for composite laminates (Q4876567) (← links)
- An efficient eight-node quadrilateral element for free vibration analysis of multilayer sandwich plates (Q6553944) (← links)
