VESCOVINI, RICCARDO
 Distribuzione geografica
Continente #
NA - Nord America 4.001
EU - Europa 3.213
AS - Asia 640
OC - Oceania 17
SA - Sud America 14
AF - Africa 7
Continente sconosciuto - Info sul continente non disponibili 1
Totale 7.893
Nazione #
US - Stati Uniti d'America 3.908
IT - Italia 2.113
VN - Vietnam 165
DE - Germania 155
ES - Italia 125
IE - Irlanda 120
FI - Finlandia 114
FR - Francia 104
CN - Cina 101
JO - Giordania 100
CA - Canada 93
AT - Austria 91
GB - Regno Unito 78
PH - Filippine 72
SE - Svezia 65
NL - Olanda 63
UA - Ucraina 59
TR - Turchia 51
IR - Iran 48
CH - Svizzera 33
IN - India 31
BE - Belgio 27
HK - Hong Kong 27
RU - Federazione Russa 19
KR - Corea 15
GR - Grecia 14
AU - Australia 12
BR - Brasile 8
JP - Giappone 7
PL - Polonia 6
RO - Romania 6
SG - Singapore 6
NZ - Nuova Zelanda 5
TW - Taiwan 5
DK - Danimarca 4
LU - Lussemburgo 4
SI - Slovenia 3
AE - Emirati Arabi Uniti 2
CI - Costa d'Avorio 2
CO - Colombia 2
DZ - Algeria 2
ET - Etiopia 2
KW - Kuwait 2
NO - Norvegia 2
PE - Perù 2
PT - Portogallo 2
SA - Arabia Saudita 2
AR - Argentina 1
AZ - Azerbaigian 1
BD - Bangladesh 1
CZ - Repubblica Ceca 1
EC - Ecuador 1
EU - Europa 1
HR - Croazia 1
ID - Indonesia 1
IL - Israele 1
MD - Moldavia 1
MT - Malta 1
MY - Malesia 1
NG - Nigeria 1
PK - Pakistan 1
SK - Slovacchia (Repubblica Slovacca) 1
SM - San Marino 1
Totale 7.893
Città #
Milan 781
Fairfield 581
Woodbridge 384
Chandler 316
Wilmington 263
Houston 262
Ashburn 260
Seattle 214
Ann Arbor 211
Cambridge 185
Dong Ket 115
Málaga 111
Dublin 106
Amman 100
Vienna 89
Dearborn 88
Lawrence 88
Medford 79
Davao City 72
Ottawa 68
Redmond 63
Helsinki 61
Redwood City 60
Rome 53
Beijing 43
New York 41
Bovisio Masciago 37
Crema 32
Jacksonville 30
Des Moines 29
Gavirate 29
Istanbul 28
Zurich 28
San Diego 25
Zibido San Giacomo 23
Brussels 22
Columbus 22
Amsterdam 21
Ciampino 21
Moscow 19
Torino 18
Hanover 17
Monza 17
Trento 17
Busto Arsizio 16
Montreal 16
Turin 16
Varese 16
Robbiate 15
Bergamo 13
Besana in Brianza 13
Central 12
Cameri 11
Princeton 11
Brescia 10
Delft 10
London 10
Miami 10
Palermo 10
Phoenix 10
Segrate 10
Acerra 9
Darmstadt 9
Mountain View 9
Shanghai 9
Berlin 8
Casei Gerola 8
Limerick 8
Naples 8
Norwalk 8
Venegono Superiore 8
Blacksburg 7
Boardman 7
Legnano 7
Washington 7
Atlanta 6
Bernareggio 6
Bresso 6
Bussero 6
Central District 6
Chongqing 6
Florence 6
Gambolò 6
Marnate 6
Nantes 6
Nardò 6
Pogliano Milanese 6
Singapore 6
Tehran 6
Wuhan 6
Bonn 5
Bourg-la-reine 5
Frankfurt am Main 5
Lappeenranta 5
Mumbai 5
Munich 5
State College 5
Stillwater 5
Tokyo 5
Valmadrera 5
Totale 5.590
Nome #
A Semi-Analytical Approach for the Analysis of Variable-Stiffness Panels with Curvilinear Stiffeners 192
Physics-Informed Neural Networks for the Analysis of Composite Structures 192
Buckling and Postbuckling Analysis of Composite-Stiffened Panels Using a Semi-Analytical Approach 179
Bending analysis of composite laminated and sandwich structures using sublaminate variable-kinematic Ritz models 160
Single-Stringer Compression Specimen for the Assessment of Damage Tolerance of Postbuckled Structures 157
Buckling and wrinkling of anisotropic sandwich plates 155
Sublaminate variable kinematics shell models for functionally graded sandwich panels: Bending and free vibration response 155
Thermal Buckling Response of Laminated and Sandwich Plates using Refined 2-D Models 150
Exact Refined Buckling Solutions for Laminated Plates Under Uniaxial and Biaxial Loads 145
The Ritz – Sublaminate Generalized Unified Formulation approach for piezoelectric composite plates 145
A Continuation Procedure for the Quasi-Static Analysis of Materially and Geometrically Nonlinear Structural Problems 145
Analysis of Thin-Walled Composite Structures Using Physics-Informed Neural Networks and Extreme Learning 142
Single-Mode Solution for Post-Buckling Analysis of Composite Panels with Elastic Restraints Loaded in Compression 138
Analytical Formulation for Local Buckling and Post-Buckling Analysis of Stiffened Laminated Panels 137
On the application of the Ritz method to free vibration and buckling analysis of highly anisotropic plates 136
Analysis of multiple-core sandwich cylindrical shells using a sublaminate formulation 133
Fast analysis of non-symmetric panels using semi-analytical techniques 132
Buckling Analysis and Optimization of Stiffened Composite Flat and Curved Panels 129
A Fast Procedure for the Design of Composite Stiffened Panels 120
Semi-Analytical Buckling Analysis of Omega Stiffened Panels Under Multi-Axial Loads 113
Thermal Buckling Behaviour of Thin and Thick Variable-Stiffness Panels 113
Strong- and Weak-Form Physics Informed Neural Networks for the Analysis of Composite Plates and Shells 113
Assessment of dynamic effects on aircraft design loads: the landing impact case 112
A framework based on physics-informed neural networks and extreme learning for the analysis of composite structures 110
Fast Tool for Buckling Analysis and Optimization of Stiffened Panels 109
Dynamic finite element simulations of composite stiffened panels with a transverse-isotropic viscoelastic energy dissipation model 108
Analysis of Monolithic and Sandwich Panels Subjected To Non-Uniform Thickness-Wise Boundary Conditions 108
Non-linear vibrations of variable-sti ness plates: Fast analysis using semi-analytical methods 108
A procedure for the evaluation of damping effects in composite laminated structures 105
Static and Dynamic Buckling of a Daedalos Composite Panel Including Material Damping 101
A Variable-Kinematic Model for Variable Stiffness Plates: Vibration and Buckling Analysis 101
Pre-buckling and Buckling Analysis of Variable-Stiffness, Curvilinearly Stiffened Panels 100
Efficient post-buckling analysis of variable-stiffness plates using a perturbation approach 97
Buckling Optimization of Stiffened Composite Flat and Curved Panels 96
Assessment of the Damage Tolerance of Postbuckled Hat-Stiffened Panels Using Single Stringer Specimens 95
A Fast Procedure for the Design of Composite Stiffened Panels 89
Analysis of Lightweight Structures Using Physics Informed Neural Networks 89
Radial Point Interpolation Method for isotropic nanoplates in bending using strain gradient theory 88
A Fast Tool for Analysis and Optimization of Isotropic and Composite Stiffened Panels 87
An Analysis Tool for Composite Plates Based on the Ritz Method and a Sublaminate Generalized Unified Formulation 85
A Study of the Dynamic Effects on the Design Loads of Civil Aircraft 83
The vk-Ritz Method for Bending, Vibration and Buckling Analysis of Heterogeneous Multilayered Plates 82
Two-Step Procedure for Fast Post-Buckling Analysis of Composite Stiffened Panels 81
Analysis of post-buckled variable stiness panels using Ritz and Koiter's method 81
Dynamic response of viscoelastic multiple-core sandwich structures 81
Analysis of Variable Stiffness Structures Using Physics Informed Neural Networks 77
Hybrid geometric-dissipative arc-length methods for the quasi-static analysis of delamination problems 75
A Sublaminate Generalized Unified Formulation for buckling and wrinkling of sandwich plates 73
A Semi-Analytical Framework for Nonlinear Vibration Analysis of Variable Stiffness Plates 72
Dynamic Analysis of Multilayered Plates with Viscoelastic Layers Using a Sublaminate Generalized Unified Formulation 70
Fast analysis of panels with curvilinear stringers 70
Mechanical Response of Composite Plates by Means of a Sublaminate Generalized Unied Formulation and Ritz Solution 68
Pre-Buckling and Buckling Response of Composite Curvilinearly Stiffened Panels 68
Nonlinear Vibrations of Variable-Stiffness Plates using Different Semi-Analytical Models 66
Extension to Piezoelectric Plates of the Ritz Sublaminate Generalized Unified Formulation Approach 65
Analysis of Functionally Graded Carbon Nanotubes Reinforced Composite Panels Using Sublaminate Variable-Kinematics Models 65
Dynamic Analysis of Composite Stiffened Panels Subjected to Compressive Load 64
Analysis and Optimization of Composite Panels for Aerospace Applications 64
Structural and acoustic response of finite sandwich plates by using sublaminate models with variable kinematics 63
Two-Step Post-Buckling Analysis of Composite Stiffened Panels 61
Optimization of Stiffened Composite Panels with Buckling and Failure Requirements 61
Analytical Approach for the Buckling of Composite Panels with Different Stringer Shapes 60
Variable Kinematics Models for Advanced Composite Plates 59
Analysis of Plates and Sandwich Structures Subjected to Non-Classical Boundary Conditions 58
Progressive Failure Analysis of Postbuckled Plates via Mixed Formulation 54
Fast Methods for Nonlinear Vibration Analysis of Variable Stiffness Panels 53
Refined Buckling Analysis of Composite Plates Under Various Boundary Conditions 51
Nonlinear Analyses for the Study of Damage in Composite Stiffened Panels 51
Failure Analysis of Composite Multi-Stringer Panels Using Simplified Models 51
Fast Analysis Methods for the Design of Composite Panels 49
A ps-FEM Approach for the Analysis of Laminated Shells 47
Fast analysis of curvilinearly stiffened panels operating in the postbuckling field 47
An investigation over the effects of anisotropy on the convergence of the Ritz method for thin and thick composite plates 47
A neural network-based approach for bending analysis of strain gradient nanoplates 45
Bending and free vibration of FG-CNTRC panels using a variable-kinematic approach 45
Simplified Models for the Study of Postbuckled Hat-Stiffened Composite Panels 42
Numerical/Experimental Procedure for the Transient Dynamic Analysis of Composite Laminated Structures 40
Benchmark for modelization of acoustic transmission loss applied to helicopter trim panels 40
Meshless Computational Strategy for Higher Order Strain Gradient Plate Models 40
Multibody Analysis of a Micro-Aerial Vehicle Flapping Wing 39
Analysis of Variable Stiffness Panels with Complex Geometries using R-Functions 38
Nonlinear Vibration and Instability of a Randomly Distributed CNT-Reinforced Composite Plate Subjected to Localized In-plane Parametric Excitation 38
Sublaminate Variable-Kinematic Models for Vibroacoustic Analysis of Composite Trim Panels 37
Laminated Composite Strain Gradient Nanoplates Analyzed with Meshless Methods 35
Higher-Order Solutions for Buckling and Vibration Analysis of Variable Stiffness Plates 34
Optimization of Non-Symmetric Composite Panels Using Fast Analysis Techniques 33
Buckling Optimization of Composite Omega-Stiffened Panels 32
Free vibrations of conical shells via Ritz method 31
A Meshless Approach for the Analysis of Variable Stiffness Panels with Arbitrary Shapes 31
Meshless Computational Strategy for Higher Order Strain Gradient Plate Models 30
Fast Analysis of Postbuckled Curvilinearly Stiffened Panels 30
Development and Applications of a Virtual Hybrid Platform for Multiscale Analysis of Advanced Structures of Aircraft (DEVISU) 29
Free vibrations and buckling analysis of cross-ply composite nanoplates by means of a Mesh Free Radial Point Interpolation Method 29
Postbuckling of Curvilinearly-Stiffened Panels via Asymptotic-Numerical Approach 29
Application of the ps-Version of the Finite Element Method to the Analysis of Laminated Shells 28
Ritz R-Function Method for the Analysis of Variable-Stiffness Plates 28
Stiffness Tailoring of Aerospace Panels Using Curvilinear Fibers and Stringers 28
A Neural Network-based Approach for Strain Gradient Nanoplates 26
Vibrations and Buckling of Composite Plates Based on Strain Gradient Theory and Meshless Methods 26
Radial Point Interpolation Method for Higher Order Composite Strain Gradient Plate Models 22
Totale 7.991
Categoria #
all - tutte 21.280
article - articoli 11.848
book - libri 0
conference - conferenze 8.545
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 408
Totale 42.081


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2018/2019558 0 0 0 0 0 0 0 0 0 144 206 208
2019/20201.835 157 109 63 113 313 278 200 156 160 94 126 66
2020/20211.001 80 49 70 110 71 58 35 87 70 79 68 224
2021/20221.291 46 177 148 96 105 66 123 116 71 73 117 153
2022/20231.366 145 109 51 151 145 142 38 107 207 141 72 58
2023/2024723 57 115 100 80 67 107 122 16 8 51 0 0
Totale 8.072