Pages that link to "Item:Q2952158"
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The following pages link to Shell finite elements with different through-the-thickness kinematics for the linear analysis of cylindrical multilayered structures (Q2952158):
Displaying 11 items.
- Refined shell model for the linear analysis of isotropic and composite elastic structures (Q338141) (← links)
- A finite element-difference computational model for stress analysis of layered composite cylindrical shells (Q1309566) (← links)
- Classical, higher-order, zig-zag and variable kinematic shell elements for the analysis of composite multilayered structures (Q1797635) (← links)
- A new efficient higher-order shear deformation theory for a doubly curved laminated composite shell (Q2014456) (← links)
- Methods and guidelines for the choice of shell theories (Q2191397) (← links)
- Shell element formulation of multi-step inverse analysis for axisymmetric deep drawing process (Q2709582) (← links)
- Finite element analysis of multilayered shells of revolution (Q4202897) (← links)
- (Q4493863) (← links)
- Finite elements based on Jacobi shape functions for the analysis of beams, plates and shells (Q6082607) (← links)
- Finite strip method based on Carrera unified formulation for the free vibration analysis of variable stiffness composite laminates (Q6090787) (← links)
- Multiresolution strategies for the modeling of composite shell structures based on the variable separation method (Q6555404) (← links)
