Nonlinear displacement-based and hybrid-mixed quadrilaterals for three-dimensional stress analysis through sampling surfaces formulation
Authors:
- G.M. KulikovGKG.M. Kulikov
- Mehdi BohloolyMehdi Bohlooly
- S.V. PlotnikovaSPS.V. Plotnikova
- M.A. KouchakzadehMKM.A. Kouchakzadeh
- A.O. GlebovA.O. Glebov
- 1 October 2020
- journal article
- research article
- Published by Elsevier in Thin-Walled Structures
- Vol. 155
Abstract
No abstract availableKeywords
Funding Information
- Russian Science Foundation (18-19-00092)
This publication has 48 references indexed in Scilit:
- Geometrically exact assumed stress–strain multilayered solid-shell elements based on the 3D analytical integrationComputers & Structures, 2006
- A robust non-linear solid shell element based on a mixed variational formulationComputer Methods in Applied Mechanics and Engineering, 2006
- Non-linear strain–displacement equations exactly representing large rigid-body motions. Part I Timoshenko–Mindlin shell theoryComputer Methods in Applied Mechanics and Engineering, 2003
- Optimal solid shells for non-linear analyses of multilayer composites. I. StaticsComputer Methods in Applied Mechanics and Engineering, 2003
- An eight‐node hybrid‐stress solid‐shell element for geometric non‐linear analysis of elastic shellsInternational Journal for Numerical Methods in Engineering, 2002
- A stabilized hybrid-stress solid element for geometrically nonlinear homogeneous and laminated shell analysesComputer Methods in Applied Mechanics and Engineering, 2002
- An efficient assumed strain element model with six DOF per node for geometrically non‐linear shellsInternational Journal for Numerical Methods in Engineering, 1995
- Nonlinear shell formulations for complete three-dimensional constitutive laws including composites and laminatesComputational Mechanics, 1994
- Three‐dimensional extension of non‐linear shell formulation based on the enhanced assumed strain conceptInternational Journal for Numerical Methods in Engineering, 1994
- A solid element formulation for large deflection analysis of composite shell structuresComputers & Structures, 1988