All Stories

  1. Accurate through-the-thickness stress distributions in thin-walled metallic structures subjected to large displacements and large rotations
  2. Coupling 3D peridynamics and high order 1D finite elements based on local elasticity for the linear static analysis of solid beams and thin‐walled reinforced structures
  3. Efficient numerical evaluation of transmission loss in homogenized acoustic metamaterials for aeronautical application
  4. Influence of fiber misalignments on buckling performance of variable stiffness composites using layerwise models and random fields
  5. Evaluation of geometrically nonlinear terms in the large-deflection and post-buckling analysis of isotropic rectangular plates
  6. Effect of large displacements on the linearized vibration of composite beams
  7. Popular benchmarks of nonlinear shell analysis solved by 1D and 2D CUF-based finite elements
  8. Geometrically nonlinear refined shell theories by Carrera Unified Formulation
  9. Isogeometric analysis of 3D straight beam-type structures by Carrera Unified Formulation
  10. Large-deflection and post-buckling analyses of isotropic rectangular plates by Carrera Unified Formulation
  11. Global-local plug-in for high-fidelity composite stress analysis in ABAQUS
  12. Unified theory of structures based on micropolar elasticity
  13. Global-local plug-in for high-fidelity composite stress analysis in Femap/NX Nastran
  14. Higher-order structural theories for transient analysis of multi-mode Lamb waves with applications to damage detection
  15. Evaluation of Various Geometrical Nonlinearities in the Response of Beams and Shells
  16. Free-edge stress fields in generic laminated composites via higher-order kinematics
  17. Three-Dimensional Solutions for Rotor Blades Using High-Order Geometrical Nonlinear Beam Finite Elements
  18. A global/local approach based on CUF for the accurate and efficient analysis of metallic and composite structures
  19. Evaluation of shear and membrane locking in refined hierarchical shell finite elements for laminated structures
  20. Accurate stress fields of post-buckled laminated composite beams accounting for various kinematics
  21. Finite beam elements based on Legendre polynomial expansions and node-dependent kinematics for the global-local analysis of composite structures
  22. Homogenization and free-vibration analysis of elastic metamaterial plates by Carrera Unified Formulation finite elements
  23. Accurate evaluation of 3D stress fields in adhesive bonded joints via higher-order FE models
  24. An adaptable refinement approach for shell finite element models based on node-dependent kinematics
  25. Drop Test Simulations of Composite Leaf Spring Landing Gears
  26. Global/local analysis of free-edge stresses in composite laminates
  27. Simulation of Lamb waves via refined FE models with SHM applications
  28. Geometrically Nonlinear Analysis of Beam Structures via Hierarchical One-Dimensional Finite Elements
  29. Evaluation of In-Plane and Out-of-Plane Stresses in Composite Structures Subjected to Large Displacements/Rotations
  30. Nonlinear Dynamics of Rotating Structures and Helicopter Blades
  31. Virtual Vibration Correlation Technique (VCT) for Nonlinear Analysis of Metallic and Composite Structures
  32. Strong and weak form solutions of curved beams via Carrera’s unified formulation
  33. Accurate Evaluation of Interlaminar Stresses in Composite Laminates via Mixed One-Dimensional Formulation
  34. Frequency and mode change in the large deflection and post-buckling of compact and thin-walled beams
  35. Use of higher-order Legendre polynomials for multilayered plate elements with node-dependent kinematics
  36. Evaluation of geometrically nonlinear effects due to large cross-sectional deformations of compact and shell-like structures
  37. Meshless analysis of metallic and composite beam structures by advanced hierarchical models with layer-wise capabilities
  38. Effect of Localized Damages on the Free Vibration Analysis of Civil Structures by Component-Wise Approach
  39. Accurate Nonlinear Dynamics and Mode Aberration of Rotating Blades
  40. Effect of Nonstructural Masses on Civil Structures by CUF-Based Finite Element Models
  41. Accurate evaluation of failure indices of composite layered structures via various FE models
  42. A general multi-scale two-level optimisation strategy for designing composite stiffened panels
  43. Locking-free curved elements with refined kinematics for the analysis of composite structures
  44. Exact solutions for the macro-, meso- and micro-scale analysis of composite laminates and sandwich structures
  45. Component-wise analysis of laminated structures by hierarchical refined models with mapping features and enhanced accuracy at layer to fiber-matrix scales
  46. Micro-, Meso- and Macro-Scale Analysis of Composite Laminates by Unified Theory of Structures
  47. Reissner’s Mixed Variational Theorem for Layer-Wise Refined Beam Models Based on the Unified Formulation
  48. Micromechanics of periodically heterogeneous materials using higher-order beam theories and the mechanics of structure genome
  49. Static and free-vibration analyses of dental prosthesis and atherosclerotic human artery by refined finite element models
  50. Exact solutions for static analysis of laminated, box and sandwich beams by refined layer-wise theory
  51. Dynamic response of laminated and sandwich composite structures via 1D models based on Chebyshev polynomials
  52. Global-local analysis of laminated plates by node-dependent kinematic finite elements with variable ESL/LW capabilities
  53. Extension of MITC to higher-order beam models and shear locking analysis for compact, thin-walled, and composite structures
  54. Large-deflection and post-buckling analyses of laminated composite beams by Carrera Unified Formulation
  55. Application of aerospace structural models to marine engineering
  56. Exact solutions for free vibration analysis of laminated, box and sandwich beams by refined layer-wise theory
  57. Cross-sectional mapping for refined beam elements with applications to shell-like structures
  58. Multilayered plate elements accounting for refined theories and node-dependent kinematics
  59. Shell elements with through-the-thickness variable kinematics for the analysis of laminated composite and sandwich structures
  60. Node-dependent kinematics, refined zig-zag and multi-line beam theories for the analysis of composite structures
  61. Hierarchical theories of structures based on Legendre polynomial expansions with finite element applications
  62. Free-vibration tailoring of single- and multi-bay laminated box structures by refined beam theories
  63. Analysis of laminated beams via Unified Formulation and Legendre polynomial expansions
  64. Free Vibrations of Damaged Aircraft Structures by Component-Wise Analysis
  65. Unified formulation of geometrically nonlinear refined beam theories
  66. Refined theories based on non-polynomial kinematics for the thermoelastic analysis of functionally graded plates
  67. Analysis of laminated composites and sandwich structures by variable-kinematic MITC9 plate elements
  68. Refined beam finite elements for static and dynamic analysis of hull structures
  69. Guest editorial ofMAMSspecial issue on: Applications of Unified Formulation and advanced theories using several numerical approaches
  70. Higher-order theories and radial basis functions applied to free vibration analysis of thin-walled beams
  71. Linearized buckling analysis of isotropic and composite beam-columns by Carrera Unified Formulation and dynamic stiffness method
  72. Accurate static response of single- and multi-cell laminated box beams
  73. Gasdynamics of rapid and explosive decompressions of pressurized aircraft including active venting
  74. Accurate Response of Wing Structures to Free-Vibration, Load Factors, and Nonstructural Masses
  75. Free vibration analysis of simply supported beams with solid and thin-walled cross-sections using higher-order theories based on displacement variables
  76. Static and free vibration analysis of laminated beams by refined theory based on Chebyshev polynomials
  77. Dynamic response of aerospace structures by means of refined beam theories
  78. Evaluation of the accuracy of classical beam FE models via locking-free hierarchically refined elements
  79. Refined 1D Finite Elements for the Analysis of Secondary, Primary, and Complete Civil Engineering Structures
  80. Comparison of various 1D, 2D and 3D FE models for the analysis of thin-walled box with transverse ribs subjected to load factors
  81. Recent developments on refined theories for beams with applications
  82. Free vibration analysis of composite plates by higher-order 1D dynamic stiffness elements and experiments
  83. Free vibration analysis of civil engineering structures by component-wise models
  84. Flutter analysis by refined 1D dynamic stiffness elements and doublet lattice method
  85. Advanced models for free vibration analysis of laminated beams with compact and thin-walled open/closed sections
  86. Refined dynamic stiffness elements applied to free vibration analysis of generally laminated composite beams with arbitrary boundary conditions
  87. Thin-walled beams subjected to load factors and non-structural masses
  88. Multi-line enhanced beam model for the analysis of laminated composite structures
  89. Influence of Non-Structural Localized Inertia on Free Vibration Response of Thin-Walled Structures by Variable Kinematic Beam Formulations
  90. Use of Lagrange multipliers to combine 1D variable kinematic finite elements
  91. Static and Dynamic Analysis of Aircraft Structures by Component-Wise Approach
  92. Exact dynamic stiffness elements based on one-dimensional higher-order theories for free vibration analysis of solid and thin-walled structures
  93. Analysis of reinforced and thin-walled structures by multi-line refined 1D/beam models
  94. Component-Wise Method Applied to Vibration of Wing Structures
  95. Classical, Refined, and Component-Wise Analysis of Reinforced-Shell Wing Structures