Nonlinear strain--displacement equations exactly representing large rigid-body motions. I: Timoshenko--Mindlin shell theory
From MaRDI portal
Publication:1400687
DOI10.1016/S0045-7825(02)00601-1zbMath1025.74031OpenAlexW2065220572MaRDI QIDQ1400687
S. V. Plotnikova, Gennady M. Kulikov
Publication date: 13 August 2003
Published in: Computer Methods in Applied Mechanics and Engineering (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/s0045-7825(02)00601-1
Related Items
Finite deformation higher-order shell models and rigid-body motions, Nonlinear strain-displacement equations exactly representing large rigid-body motions. II: Enhanced finite element technique, The contact problem for a geometrically non-linear Timoshenko-type shell, A family of ANS four-node exact geometry shell elements in general convected curvilinear coordinates, Nonlinear strain-displacement equations exactly representing large rigid-body motions. III: Analysis of TM shells with constraints
Cites Work
- Unnamed Item
- Unnamed Item
- Unnamed Item
- On a stress resultant geometrically exact shell model. II: The linear theory; computational aspects
- Non-linear analysis of multilayered shells under initial stress
- Resultant-stress degenerated-shell element
- A three-dimensional finite-strain rod model. II. Computational aspects
- Nonlinear finite element analysis of shells. II. Two-dimensional shells
- On a stress resultant geometrically exact shell model. IV: Variable thickness shells with through-the-thickness stretching
- Nonlinear analysis of free-form shells by flat finite elements
- Refined shear-deformation models for composite laminates with finite rotations
- Simple and effective elements based upon Timoshenko-Mindlin shell theory
- Finite elements based on a first-order shear deformation moderate rotation shell theory with applications to the analysis of composite structures
- Nonlinear analysis of laminates through a Mindlin-type shear deformable shallow shell element
- Some aspects of the nonlinear finite element method
- Composite laminates: Nonlinear interlaminar stress analysis by multi-layer shell elements
- On the physical significance of higher-order kinematic and static variables in a three-dimensional shell formulation
- The finite deformation theory for beam, plate and shell. III: The three-dimensional beam theory and the FE formulation
- Nonlinear finite element shell formulation accounting for large membrane strains
- Physical stabilization of the 4-node shell element with one point quadrature
- Hybrid strain based geometrically nonlinear laminated composite triangular shell finite elements
- The finite deformation theory for beam, plate and shell. IV: The FE formulation of Mindlin plate and shell based on Green-Lagrangian strain
- The TRIC shell element: Theoretical and numerical investigation
- A theoretical and computational model for isotropic elastoplastic stress analysis in shells at large strains
- A 4-node finite shell element for the implementation of general hyperelastic 3D-elasticity at finite strains
- A consistent co-rotational formulation for nonlinear, three-dimensional, beam-elements
- An assumed strain finite element model for large deflection composite shells
- A formulation of general shell elements—the use of mixed interpolation of tensorial components
- A beam finite element non-linear theory with finite rotations
- Finite Elements Based Upon Mindlin Plate Theory With Particular Reference to the Four-Node Bilinear Isoparametric Element
- Shell theory versus degeneration—a comparison in large rotation finite element analysis
- Geometrically non-linear enhanced strain mixed methods and the method of incompatible modes
- Large displacement analysis of three-dimensional beam structures
- A finite rotation shell theory with application to composite structures
- A three‐dimensional non‐linear Timoshenko beam based on the core‐congruential formulation
- The use of ADINA for analysis of mines with explosive fills
- A continuum‐based shell theory for non‐linear applications
- An assumed strain approach avoiding artificial thickness straining for a non‐linear 4‐node shell element
- An efficient assumed strain element model with six DOF per node for geometrically non‐linear shells
- Analysis of initially stressed multilayered shells