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Fast analysis of non-symmetric panels using semi-analytical techniques, file e0c31c0a-bfb8-4599-e053-1705fe0aef77
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255
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Analysis of Lightweight Structures Using Physics Informed Neural Networks, file e0c31c12-0d62-4599-e053-1705fe0aef77
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252
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Physics-Informed Neural Networks for the Analysis of Composite Structures, file e0c31c10-06f7-4599-e053-1705fe0aef77
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195
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Hybrid geometric-dissipative arc-length methods for the quasi-static analysis of delamination problems, file e0c31c0a-c705-4599-e053-1705fe0aef77
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167
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Bending analysis of composite laminated and sandwich structures using sublaminate variable-kinematic Ritz models, file e0c31c0a-ca31-4599-e053-1705fe0aef77
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166
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Assessment of dynamic effects on aircraft design loads: the landing impact case, file e0c31c0d-9382-4599-e053-1705fe0aef77
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162
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A Continuation Procedure for the Quasi-Static Analysis of Materially and Geometrically Nonlinear Structural Problems, file e0c31c0e-bb77-4599-e053-1705fe0aef77
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138
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Thermal Buckling Behaviour of Thin and Thick Variable-Stiffness Panels, file e0c31c0c-4fb3-4599-e053-1705fe0aef77
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131
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On the application of the Ritz method to free vibration and buckling analysis of highly anisotropic plates, file e0c31c0b-daed-4599-e053-1705fe0aef77
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128
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A Fast Procedure for the Design of Composite Stiffened Panels, file e0c31c08-5dc2-4599-e053-1705fe0aef77
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126
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Semi-Analytical Buckling Analysis of Omega Stiffened Panels Under Multi-Axial Loads, file e0c31c0d-eb8f-4599-e053-1705fe0aef77
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120
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Nonlinear Vibrations of Variable-Stiffness Plates using Different Semi-Analytical Models, file e0c31c0f-81dd-4599-e053-1705fe0aef77
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118
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Simplified Approach to Nonlinear Vibration Analysis of Variable Stiffness Plates, file c31dc2a7-1729-4c6a-9714-cab2742216f7
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114
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Buckling and wrinkling of anisotropic sandwich plates, file e0c31c0c-830c-4599-e053-1705fe0aef77
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99
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Analysis of Monolithic and Sandwich Panels Subjected To Non-Uniform Thickness-Wise Boundary Conditions, file e0c31c0c-af99-4599-e053-1705fe0aef77
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96
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Fast analysis of panels with curvilinear stringers, file e0c31c0d-9b22-4599-e053-1705fe0aef77
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91
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A Variable-Kinematic Model for Variable Stiffness Plates: Vibration and Buckling Analysis, file e0c31c09-b6df-4599-e053-1705fe0aef77
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90
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A Semi-Analytical Approach for the Analysis of Variable-Stiffness Panels with Curvilinear Stiffeners, file e0c31c0f-32b2-4599-e053-1705fe0aef77
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80
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Dynamic finite element simulations of composite stiffened panels with a transverse-isotropic viscoelastic energy dissipation model, file e0c31c0d-a038-4599-e053-1705fe0aef77
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76
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Strong- and Weak-Form Physics Informed Neural Networks for the Analysis of Composite Plates and Shells, file e0c31c11-c17b-4599-e053-1705fe0aef77
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70
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Efficient post-buckling analysis of variable-stiffness plates using a perturbation approach, file e0c31c0d-7990-4599-e053-1705fe0aef77
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66
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A procedure for the evaluation of damping effects in composite laminated structures, file e0c31c0d-a041-4599-e053-1705fe0aef77
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65
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Ritz R-Function Method for the Analysis of Variable-Stiffness Plates, file 6d505ec0-ffb8-44de-a2c9-70e414ab1a27
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63
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Laminated Composite Strain Gradient Nanoplates Analyzed with Meshless Methods, file e0c31c11-9e27-4599-e053-1705fe0aef77
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60
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Exact Refined Buckling Solutions for Laminated Plates Under Uniaxial and Biaxial Loads, file e0c31c08-6083-4599-e053-1705fe0aef77
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53
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Meshless Computational Strategy for Higher Order Strain Gradient Plate Models, file e0c31c12-55e2-4599-e053-1705fe0aef77
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52
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Non-linear vibrations of variable-sti ness plates: Fast analysis using semi-analytical methods, file e0c31c0f-e152-4599-e053-1705fe0aef77
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46
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The Ritz – Sublaminate Generalized Unified Formulation approach for piezoelectric composite plates, file e0c31c0c-07f6-4599-e053-1705fe0aef77
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42
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Pre-buckling and Buckling Analysis of Variable-Stiffness, Curvilinearly Stiffened Panels, file e0c31c0f-6846-4599-e053-1705fe0aef77
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39
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Vibrations and Buckling of Composite Plates Based on Strain Gradient Theory and Meshless Methods, file e0c31c11-7b32-4599-e053-1705fe0aef77
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37
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Fast Analysis of Postbuckled Curvilinearly Stiffened Panels, file e0c31c12-d9ad-4599-e053-1705fe0aef77
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36
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Development and Applications of a Virtual Hybrid Platform for Multiscale Analysis of Advanced Structures of Aircraft (DEVISU), file 6ad0d497-5e1f-4f0e-ab11-07a8eac09085
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35
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Application of the ps-Version of the Finite Element Method to the Analysis of Laminated Shells, file 79da2e21-da17-4084-8cd2-c55b19de1be7
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31
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A ps-FEM Approach for the Analysis of Laminated Shells, file b693c0e4-0e17-4857-a8a8-6bcb0c389fef
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30
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Sublaminate variable kinematics shell models for functionally graded sandwich panels: Bending and free vibration response, file e0c31c0f-4ce7-4599-e053-1705fe0aef77
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30
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A Neural Network-based Approach for Strain Gradient Nanoplates, file 0c9610fd-e2fe-4df5-917f-4ad51469dc15
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27
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Thermal Buckling Response of Laminated and Sandwich Plates using Refined 2-D Models, file e0c31c0a-ef6e-4599-e053-1705fe0aef77
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25
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Analysis of multiple-core sandwich cylindrical shells using a sublaminate formulation, file e0c31c0d-6137-4599-e053-1705fe0aef77
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25
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Dynamic response of viscoelastic multiple-core sandwich structures, file e0c31c11-03b9-4599-e053-1705fe0aef77
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15
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A Numerical-Asymptotic Framework Based on the ps-FEM for the Analysis of Laminated Shells, file 15531918-eb86-4128-8177-b321d845e624
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13
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Progressive Failure Analysis of Postbuckled Plates via Mixed Formulation, file 0d52fcfc-252e-45a4-9689-22cd94ee6a43
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12
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Stiffness Tailoring of Aerospace Panels Using Curvilinear Fibers and Stringers, file e0c31c10-2254-4599-e053-1705fe0aef77
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11
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Meshless Computational Strategy for Higher Order Strain Gradient Plate Models, file e0c31c12-1e14-4599-e053-1705fe0aef77
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11
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Radial Point Interpolation Method for Higher Order Composite Strain Gradient Plate Models, file ae2678cf-efda-4438-a4dd-1bbeabdc19df
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10
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Fast analysis of curvilinearly stiffened panels operating in the postbuckling field, file e967c5cc-ba9c-422f-8e37-9f29c2636318
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10
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Radial Point Interpolation Method for isotropic nanoplates in bending using strain gradient theory, file 7389431b-0e20-470c-bc6c-1a1bd644aa3f
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9
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A Semi-Analytical Framework for Nonlinear Vibration Analysis of Variable Stiffness Plates, file e0c31c11-2fed-4599-e053-1705fe0aef77
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6
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A framework based on physics-informed neural networks and extreme learning for the analysis of composite structures, file e0c31c12-7d5d-4599-e053-1705fe0aef77
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6
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Refined Buckling Analysis of Composite Plates Under Various Boundary Conditions, file e0c31c09-39a3-4599-e053-1705fe0aef77
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5
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An Analysis Tool for Composite Plates Based on the Ritz Method and a Sublaminate Generalized Unified Formulation, file e0c31c09-cf6d-4599-e053-1705fe0aef77
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5
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Nonlinear Vibration and Instability of a Randomly Distributed CNT-Reinforced Composite Plate Subjected to Localized In-plane Parametric Excitation, file e0c31c11-6208-4599-e053-1705fe0aef77
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5
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Radial Point Interpolation Method for isotropic nanoplates in bending using strain gradient theory, file b0f954dd-2752-487a-bc5f-3c58d0fc1975
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3
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Dynamic Analysis of Multilayered Plates with Viscoelastic Layers Using a Sublaminate Generalized Unified Formulation, file e0c31c09-d050-4599-e053-1705fe0aef77
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3
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Mechanical Response of Composite Plates by Means of a Sublaminate Generalized Unied Formulation and Ritz Solution, file e0c31c09-d052-4599-e053-1705fe0aef77
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3
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Optimization of Stiffened Composite Panels with Buckling and Failure Requirements, file e0c31c09-d263-4599-e053-1705fe0aef77
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3
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A Sublaminate Generalized Unified Formulation for buckling and wrinkling of sandwich plates, file e0c31c09-dd92-4599-e053-1705fe0aef77
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3
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A Sublaminate Generalized Unified Formulation for buckling and wrinkling of sandwich plates, file e0c31c0a-a671-4599-e053-1705fe0aef77
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3
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Extension to Piezoelectric Plates of the Ritz Sublaminate Generalized Unified Formulation Approach, file e0c31c0b-01d8-4599-e053-1705fe0aef77
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3
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Postbuckling of Curvilinearly-Stiffened Panels via Asymptotic-Numerical Approach, file 91de2765-a2f9-4355-8e91-e56600d50340
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2
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Optimal design of composite sandwich panel with auxetic reentrant honeycomb using asymptotic equivalent model and PSO algorithm, file a9c2b903-bab1-492e-9bf9-db757c0f69fb
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2
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Single-Stringer Compression Specimen for the Assessment of Damage Tolerance of Postbuckled Structures, file e0c31c08-6746-4599-e053-1705fe0aef77
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2
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The vk-Ritz Method for Bending, Vibration and Buckling Analysis of Heterogeneous Multilayered Plates, file e0c31c08-a97a-4599-e053-1705fe0aef77
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2
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Analysis and Optimization of Composite Panels for Aerospace Applications, file e0c31c09-d265-4599-e053-1705fe0aef77
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2
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Nonlinear Analyses for the Study of Damage in Composite Stiffened Panels, file e0c31c09-d266-4599-e053-1705fe0aef77
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2
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Fast analysis of non-symmetric panels using semi-analytical techniques, file e0c31c0a-c5c7-4599-e053-1705fe0aef77
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2
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Thermal Buckling Response of Laminated and Sandwich Plates using Refined 2-D Models, file e0c31c0a-f075-4599-e053-1705fe0aef77
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2
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Sublaminate variable kinematics shell models for functionally graded sandwich panels: Bending and free vibration response, file e0c31c0f-64ef-4599-e053-1705fe0aef77
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2
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Free vibrations and buckling analysis of cross-ply composite nanoplates by means of a Mesh Free Radial Point Interpolation Method, file 1b41599e-6fcb-4386-a518-bda5f6fe52e8
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1
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A neural network-based approach for bending analysis of strain gradient nanoplates, file 9413b735-d538-4629-b645-c569efca7702
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1
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Optimal design of composite sandwich panel with auxetic reentrant honeycomb using asymptotic equivalent model and PSO algorithm, file ca4c80e6-ebe2-4aba-8424-371a69db6b44
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1
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Single-Mode Solution for Post-Buckling Analysis of Composite Panels with Elastic Restraints Loaded in Compression, file e0c31c07-f420-4599-e053-1705fe0aef77
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1
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Buckling Analysis and Optimization of Stiffened Composite Flat and Curved Panels, file e0c31c07-f5b0-4599-e053-1705fe0aef77
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1
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A Study of the Dynamic Effects on the Design Loads of Civil Aircraft, file e0c31c09-9a00-4599-e053-1705fe0aef77
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1
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Numerical/Experimental Procedure for the Transient Dynamic Analysis of Composite Laminated Structures, file e0c31c09-d261-4599-e053-1705fe0aef77
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1
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Fast Analysis Methods for the Design of Composite Panels, file e0c31c09-d747-4599-e053-1705fe0aef77
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1
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Dynamic Analysis of Multilayered Plates with Viscoelastic Layers Using a Sublaminate Generalized Unified Formulation, file e0c31c0a-aa09-4599-e053-1705fe0aef77
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1
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Hybrid geometric-dissipative arc-length methods for the quasi-static analysis of delamination problems, file e0c31c0a-cca6-4599-e053-1705fe0aef77
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1
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Analysis of Plates and Sandwich Structures Subjected to Non-Classical Boundary Conditions, file e0c31c0b-1bd7-4599-e053-1705fe0aef77
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1
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Buckling and wrinkling of anisotropic sandwich plates, file e0c31c0c-830d-4599-e053-1705fe0aef77
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1
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Structural and acoustic response of finite sandwich plates by using sublaminate models with variable kinematics, file e0c31c0e-46d8-4599-e053-1705fe0aef77
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1
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A Semi-Analytical Approach for the Analysis of Variable-Stiffness Panels with Curvilinear Stiffeners, file e0c31c0e-ccb7-4599-e053-1705fe0aef77
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1
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Dynamic response of viscoelastic multiple-core sandwich structures, file e0c31c10-2f2a-4599-e053-1705fe0aef77
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1
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Analysis of Variable Stiffness Structures Using Physics Informed Neural Networks, file e0c31c11-6a7f-4599-e053-1705fe0aef77
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1
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Fast Methods for Nonlinear Vibration Analysis of Variable Stiffness Panels, file e0c31c12-302b-4599-e053-1705fe0aef77
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1
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| Totale |
3.610 |