| Nome |
# |
|
Advanced models for static and dynamic analysis of wing and fuselage structures, file e384c42e-20cf-d4b2-e053-9f05fe0a1d67
|
1196
|
|
Gasdynamics of rapid and explosive decompressions of pressurized aircraft including active venting, file e384c42e-7c33-d4b2-e053-9f05fe0a1d67
|
754
|
|
Unified formulation of geometrically nonlinear refined beam theories, file e384c42f-db6a-d4b2-e053-9f05fe0a1d67
|
713
|
|
Dynamic response of aerospace structures by means of refined beam theories, file e384c42e-44e7-d4b2-e053-9f05fe0a1d67
|
508
|
|
Component-wise models for static, dynamic and aeroelastic analyses of metallic and composite aerospace structures, file e384c42f-c02a-d4b2-e053-9f05fe0a1d67
|
472
|
|
Analysis of laminated composites and sandwich structures by variable-kinematic MITC9 plate elements, file e384c42f-42ea-d4b2-e053-9f05fe0a1d67
|
471
|
|
Use of Lagrange multipliers to combine 1D variable kinematic finite elements, file e384c42e-2a0b-d4b2-e053-9f05fe0a1d67
|
469
|
|
Accurate response of wing structures to free-vibration, load factors and non-structural masses, file e384c42d-aa26-d4b2-e053-9f05fe0a1d67
|
433
|
|
Advanced models for free vibration analysis of laminated beams with compact and thin-walled open/closed sections, file e384c42d-ad61-d4b2-e053-9f05fe0a1d67
|
430
|
|
Free Vibrations of Damaged Aircraft Structures by Component-Wise Analysis, file e384c42f-1e52-d4b2-e053-9f05fe0a1d67
|
399
|
|
Static and free vibration analysis of laminated beams by refined theory based on Chebyshev Polynomials, file e384c42e-4bbf-d4b2-e053-9f05fe0a1d67
|
397
|
|
Analysis of laminated beams via Unified Formulation and Legendre polynomial expansions, file e384c42f-2cfb-d4b2-e053-9f05fe0a1d67
|
384
|
|
Analysis of reinforced and thin-walled structures by multi-line refined 1D/beam models, file e384c42e-2a26-d4b2-e053-9f05fe0a1d67
|
379
|
|
Large-deflection and post-buckling analyses of laminated composite beams by Carrera Unified Formulation, file e384c42f-65d9-d4b2-e053-9f05fe0a1d67
|
371
|
|
Linearized buckling analysis of isotropic and composite beam-columns by Carrera Unified Formulation and Dynamic Stiffness Method, file e384c42e-bf1b-d4b2-e053-9f05fe0a1d67
|
368
|
|
Free vibration analysis of simply supported beams with solid and thin-walled cross-sections using higher-order theories based on displacement variables, file e384c42e-76d8-d4b2-e053-9f05fe0a1d67
|
332
|
|
Accurate static response of single- and multi-cell laminated box beams, file e384c42e-76d7-d4b2-e053-9f05fe0a1d67
|
325
|
|
Higher-order theories and radial basis functions applied to free vibration analysis of thin-walled beams, file e384c42e-b44b-d4b2-e053-9f05fe0a1d67
|
308
|
|
Extension of MITC to higher-order beam models and shear locking analysis for compact, thin-walled, and composite structures, file e384c42f-d7e6-d4b2-e053-9f05fe0a1d67
|
293
|
|
Micromechanics modeling of unit cells using CUF beam models and the Mechanics of Structure Genome, file e384c42f-dcf9-d4b2-e053-9f05fe0a1d67
|
289
|
|
Thin-walled beams subjected to load factors and non-structural masses, file e384c42e-307b-d4b2-e053-9f05fe0a1d67
|
278
|
|
Cross-sectional mapping for refined beam elements with applications to shell-like structures, file e384c42f-7ca0-d4b2-e053-9f05fe0a1d67
|
278
|
|
Influence of non-structural localized inertia on free vibration response of thin-walled structures by variable kinematic beam formulations, file e384c42e-353d-d4b2-e053-9f05fe0a1d67
|
268
|
|
Evaluation of the accuracy of classical beam FE models via locking-free hierarchically refined elements, file e384c42e-4bbe-d4b2-e053-9f05fe0a1d67
|
262
|
|
Hierarchical theories of structures based on Legendre polynomial expansions with finite element applications, file e384c42f-4447-d4b2-e053-9f05fe0a1d67
|
251
|
|
Free-vibration tailoring of single- and multi-bay laminated box structures by refined beam theories, file e384c42f-16bf-d4b2-e053-9f05fe0a1d67
|
249
|
|
Unified theory of one-dimensional structures and flows with applications to biomedical engineering and coupled problems, file e384c42e-f47f-d4b2-e053-9f05fe0a1d67
|
248
|
|
Refined beam finite elements for static and dynamic analysis of hull structures, file e384c42e-b26a-d4b2-e053-9f05fe0a1d67
|
246
|
|
Shell elements with through-the-thickness variable kinematics for the analysis of laminated composite and sandwich structures, file e384c42f-4976-d4b2-e053-9f05fe0a1d67
|
237
|
|
Micromechanics of periodically heterogeneous materials using higher-order beam theories and the mechanics of structure genome, file e384c42f-9d55-d4b2-e053-9f05fe0a1d67
|
235
|
|
Dynamic Response Analysis of Pressurized Cabins Subjected to Decompression Loadings, file e384c42e-4bc0-d4b2-e053-9f05fe0a1d67
|
226
|
|
Multilayered plate elements accounting for refined theories and node-dependent kinematics, file e384c42f-620a-d4b2-e053-9f05fe0a1d67
|
219
|
|
Enhanced free vibration analysis of composite wing-box structures by one-dimensional Component-wise and dynamic stiffness formulations, file e384c42d-aa25-d4b2-e053-9f05fe0a1d67
|
211
|
|
Refined theories based on non-polynomial kinematics for the thermoelastic analysis of functionally graded plates, file e384c42e-f1b3-d4b2-e053-9f05fe0a1d67
|
204
|
|
Finite beam elements based on Legendre polynomial expansions and node-dependent kinematics for the global-local analysis of composite structures, file e384c42f-d74c-d4b2-e053-9f05fe0a1d67
|
191
|
|
Exact solutions for free vibration analysis of laminated, box and sandwich beams by refined layer-wise theory, file e384c42f-83d4-d4b2-e053-9f05fe0a1d67
|
188
|
|
Exact solutions for static analysis of laminated, box and sandwich beams by refined layer-wise theory, file e384c42f-9628-d4b2-e053-9f05fe0a1d67
|
184
|
|
A Variable Kinematic One-Dimensional Model for the Hygro-Mechanical Analysis of Composite Materials, file e384c42f-b68e-d4b2-e053-9f05fe0a1d67
|
174
|
|
Global-local analysis of laminated plates by node-dependent kinematic finite elements with variable ESL/LW capabilities, file e384c431-2de2-d4b2-e053-9f05fe0a1d67
|
164
|
|
Classical, refined and component-wise analysis of reinforced-shell structures, file e384c42e-22cc-d4b2-e053-9f05fe0a1d67
|
162
|
|
Hierarchical and component-wise 1D models for fluid-structure interaction problems, file e384c42e-4601-d4b2-e053-9f05fe0a1d67
|
147
|
|
Analysis of Laminated Structures by combined ESL-LW Variable Kinematics Plate Elements, file e384c42e-4bc1-d4b2-e053-9f05fe0a1d67
|
135
|
|
Australasian research on Applied Mechanics and Aerospace - Preface, file e384c42e-7673-d4b2-e053-9f05fe0a1d67
|
135
|
|
Global-Local Structural Analysis Of Composite Wings, file e384c430-80f6-d4b2-e053-9f05fe0a1d67
|
131
|
|
Component-Wise Method Applied to Static and Dynamic Analysis of Reinforced Structures with Applications to Aerospace, Civil Engineering and Marine Constructions, file e384c42e-6e60-d4b2-e053-9f05fe0a1d67
|
124
|
|
Unified beam theory with higher-order mapping capabilities, file e384c42e-f765-d4b2-e053-9f05fe0a1d67
|
120
|
|
Variable Kinematics and Component-Wise Models for Failure Analysis of Composite Structures, file e384c42e-5a47-d4b2-e053-9f05fe0a1d67
|
118
|
|
Exact solutions for the macro-, meso- and micro-scale analysis of composite laminates and sandwich structures, file e384c430-38d9-d4b2-e053-9f05fe0a1d67
|
118
|
|
ADVANCED NUMERICAL METHODS FOR FAILURE ANALYSIS OF METALLIC AND COMPOSITE AEROSPACE STRUCTURES, file e384c42f-dc17-d4b2-e053-9f05fe0a1d67
|
111
|
|
Vibration analysis of metallic and composite damaged structures by Component-Wise models, file e384c42d-b217-d4b2-e053-9f05fe0a1d67
|
106
|
|
Coupling three-dimensional peridynamics and high-order one-dimensional finite elements based on local elasticity for the linear static analysis of solid beams and thin-walled reinforced structures, file e384c432-3250-d4b2-e053-9f05fe0a1d67
|
90
|
|
Guest editorial of MAMS special issue on: Applications of Unified Formulation and advanced theories using several numerical approaches, file e384c42d-e4fc-d4b2-e053-9f05fe0a1d67
|
86
|
|
Refined 1D finite elements for thin-walled curved structures, file e384c42e-f169-d4b2-e053-9f05fe0a1d67
|
68
|
|
Veering and modes aberration of structures subjected to in-plane loadings according to linearized and full nonlinear formulations, file e384c42f-db5e-d4b2-e053-9f05fe0a1d67
|
68
|
|
A novel refined 1D model for the accurate stress analysis of composite structures with arbitrary curved sections, file e384c42f-26d1-d4b2-e053-9f05fe0a1d67
|
67
|
|
Evaluation of geometrically nonlinear terms in the large-deflection and post-buckling analysis of isotropic rectangular plates, file e384c432-1aec-d4b2-e053-9f05fe0a1d67
|
59
|
|
Evaluation of Various Geometrical Nonlinearities in the Response of Beams and Shells, file e384c431-2aa4-d4b2-e053-9f05fe0a1d67
|
57
|
|
Efficient analysis of geometrically nonlinear deployable thin shell structures using Carrera unified formulation, file e384c431-388e-d4b2-e053-9f05fe0a1d67
|
54
|
|
Mechanics of structure genome based on the Carrera Unified Formulation, file e384c42f-dae9-d4b2-e053-9f05fe0a1d67
|
53
|
|
Accurate Evaluation of Interlaminar Stresses in Composite Laminates via Mixed One-Dimensional Formulation, file e384c430-59bf-d4b2-e053-9f05fe0a1d67
|
50
|
|
Static and free-vibration analyses of dental prosthesis and atherosclerotic human artery by refined finite element models, file e384c430-09aa-d4b2-e053-9f05fe0a1d67
|
49
|
|
Exact solutions for free vibration analysis of laminated beams by refined layer-wise theory, file e384c42f-d795-d4b2-e053-9f05fe0a1d67
|
48
|
|
Higher-order modelling of one-dimensional flows, file e384c42f-da8f-d4b2-e053-9f05fe0a1d67
|
47
|
|
Dynamic response of laminated and sandwich composite structures via 1D models based on Chebyshev polynomials, file e384c430-cdc2-d4b2-e053-9f05fe0a1d67
|
47
|
|
Validation of FEM models based on Carrera Unified Formulation for the parametric characterization of composite metamaterials, file e384c432-b7ed-d4b2-e053-9f05fe0a1d67
|
47
|
|
Use of higher-order Legendre polynomials for multilayered plate elements with node-dependent kinematics, file e384c430-01b2-d4b2-e053-9f05fe0a1d67
|
46
|
|
EFFECT OF FIBER ORIENTATION PATH ON THE BUCKLING, FREE VIBRATION, AND STATIC ANALYSES OF VARIABLE ANGLE TOW PANELS, file e384c432-5eac-d4b2-e053-9f05fe0a1d67
|
43
|
|
Vibration of metallic and composite shells in geometrical nonlinear equilibrium states, file e384c432-46a5-d4b2-e053-9f05fe0a1d67
|
41
|
|
Accurate through-the-thickness stress distributions in thin-walled metallic structures subjected to large displacements and large rotations, file e384c432-469f-d4b2-e053-9f05fe0a1d67
|
40
|
|
Accurate evaluation of failure indices of composite layered structures via various FE models, file e384c430-3a43-d4b2-e053-9f05fe0a1d67
|
39
|
|
Geometrical nonlinear analysis of shells by Carrera Unified Formulation, file e384c431-4d9e-d4b2-e053-9f05fe0a1d67
|
39
|
|
Use of Lagrange polynomials to build refined theories for laminated beams, plates and shells, file e384c434-494f-d4b2-e053-9f05fe0a1d67
|
37
|
|
Effect of Localized Damages on the Free Vibration Analysis of Civil Structures by Component-Wise Approach, file e384c430-2428-d4b2-e053-9f05fe0a1d67
|
36
|
|
Global/local sensitivity analysis and design optimization of aerospace composite laminates, file e384c431-4d9f-d4b2-e053-9f05fe0a1d67
|
33
|
|
Microscale thermo-elastic analysis of composite materials by high-order geometrically accurate finite elements, file ca9ae89b-6556-4098-a400-f60bba36a6bd
|
32
|
|
Effect of large displacements on the linearized vibration of composite beams, file e384c431-ea75-d4b2-e053-9f05fe0a1d67
|
32
|
|
Component-wise analysis of laminated structures by hierarchical refined models with mapping features and enhanced accuracy at layer to fiber-matrix scales, file e384c430-0676-d4b2-e053-9f05fe0a1d67
|
31
|
|
Locking-free curved elements with refined kinematics for the analysis of composite structures, file e384c430-1c0c-d4b2-e053-9f05fe0a1d67
|
31
|
|
An adaptable refinement approach for shell finite element models based on node-dependent kinematics, file e384c430-8642-d4b2-e053-9f05fe0a1d67
|
30
|
|
Effect of Nonstructural Masses on Civil Structures by CUF-Based Finite Element Models, file e384c430-7559-d4b2-e053-9f05fe0a1d67
|
29
|
|
Experimental and numerical analysis of 3D printed open-hole plates reinforced with carbon fibers, file e384c432-d83f-d4b2-e053-9f05fe0a1d67
|
29
|
|
Influence of fiber misalignments on buckling performance of variable stiffness composites using layerwise models and random fields, file e384c433-c1d5-d4b2-e053-9f05fe0a1d67
|
29
|
|
A component-wise formulation for virtual testing of composites, file e384c430-3436-d4b2-e053-9f05fe0a1d67
|
27
|
|
Static and dynamic experimental analysis of a full composite VLA aircraft, file e384c431-29d1-d4b2-e053-9f05fe0a1d67
|
27
|
|
Large-deformation analysis of isotropic elastomeric structures by Carrera Unified Formulation, file e384c431-4d9c-d4b2-e053-9f05fe0a1d67
|
26
|
|
Unified theory of structures based on micropolar elasticity, file e384c430-296f-d4b2-e053-9f05fe0a1d67
|
25
|
|
Accurate evaluation of 3D stress fields in adhesive bonded joints via higher-order FE models, file e384c432-144f-d4b2-e053-9f05fe0a1d67
|
25
|
|
Evaluation of geometrically nonlinear effects due to large cross-sectional deformations of compact and shell-like structures, file e384c432-3399-d4b2-e053-9f05fe0a1d67
|
25
|
|
Advanced FEs for the analysis of composite structure with global/local and node-dependent kinematics approaches, file e384c433-c1d8-d4b2-e053-9f05fe0a1d67
|
24
|
|
Large deflection and post-buckling of thin-walled structures by finite elements with node-dependent kinematics, file e384c432-f02d-d4b2-e053-9f05fe0a1d67
|
23
|
|
Post-buckling and Large-deflection analysis of a sandwich FG plate with FG porous core using Carrera’s Unified Formulation, file e384c433-de95-d4b2-e053-9f05fe0a1d67
|
23
|
|
Effect of in-plane loadings on the free vibration of plates in nonlinear regime, file e384c430-736a-d4b2-e053-9f05fe0a1d67
|
22
|
|
Accurate stress analysis of variable angle tow shells by high-order equivalent-single-layer and layer-wise finite element models, file e384c434-24db-d4b2-e053-9f05fe0a1d67
|
22
|
|
High-order finite beam elements for propagation analyses of arbitrary-shaped one-dimensional waveguides, file e384c434-4b0b-d4b2-e053-9f05fe0a1d67
|
22
|
|
Effect of Nonstructural Masses on Civil Structures by CUF-Based Finite Element Models, file e384c430-7d6d-d4b2-e053-9f05fe0a1d67
|
21
|
|
Mixing layer-wise and refined equivalent-single layer FEs based on Lagrange expansions, file e384c433-3d4c-d4b2-e053-9f05fe0a1d67
|
21
|
|
Geometrically Nonlinear Analysis of Beam Structures via Hierarchical One-Dimensional Finite Elements, file e384c430-5c01-d4b2-e053-9f05fe0a1d67
|
19
|
|
Design optimization of a VLA composite wing, file e384c431-29d2-d4b2-e053-9f05fe0a1d67
|
19
|
|
Vibration around non-trivial equilibrium of highly flexible composite thin-walled structures and plates, file e384c431-3891-d4b2-e053-9f05fe0a1d67
|
19
|
|
Mechanical performance of variable stiffness composite plates subjected to multiscale defects, file e384c434-3678-d4b2-e053-9f05fe0a1d67
|
19
|
| Totale |
16907 |
Archivio Istituzionale della Ricerca