PORTO @ Archivio Istituzionale della Ricerca

DEMASI, LUCIANO
 Distribuzione geografica
Salva come PNG Salva come JPEG
Continente #
NA - Nord America 6.506
EU - Europa 5.279
AS - Asia 2.170
SA - Sud America 209
AF - Africa 25
OC - Oceania 7
Continente sconosciuto - Info sul continente non disponibili 3
Totale 14.199
Salva come PNG Salva come JPEG
Nazione #
US - Stati Uniti d'America 6.474
IT - Italia 1.141
GB - Regno Unito 1.025
DE - Germania 935
SG - Singapore 828
CN - Cina 725
FR - Francia 718
UA - Ucraina 504
RU - Federazione Russa 251
NL - Olanda 179
BR - Brasile 165
TR - Turchia 141
IE - Irlanda 122
CH - Svizzera 102
KR - Corea 101
FI - Finlandia 80
HK - Hong Kong 69
JO - Giordania 66
SE - Svezia 62
VN - Vietnam 60
AT - Austria 37
JP - Giappone 30
BE - Belgio 27
IN - India 27
MY - Malesia 26
IL - Israele 24
RO - Romania 21
TW - Taiwan 21
AR - Argentina 19
CA - Canada 16
AP - ???statistics.table.value.countryCode.AP??? 14
ES - Italia 12
MX - Messico 12
EU - Europa 10
CL - Cile 9
PL - Polonia 9
IQ - Iraq 8
IR - Iran 8
AE - Emirati Arabi Uniti 7
AU - Australia 7
VE - Venezuela 6
EG - Egitto 5
HR - Croazia 5
ID - Indonesia 5
UZ - Uzbekistan 5
AZ - Azerbaigian 4
CZ - Repubblica Ceca 4
DZ - Algeria 4
EE - Estonia 4
LT - Lituania 4
PT - Portogallo 4
BY - Bielorussia 3
CO - Colombia 3
MA - Marocco 3
NG - Nigeria 3
PY - Paraguay 3
SA - Arabia Saudita 3
TN - Tunisia 3
ZA - Sudafrica 3
DK - Danimarca 2
JM - Giamaica 2
KE - Kenya 2
KG - Kirghizistan 2
KZ - Kazakistan 2
MN - Mongolia 2
PE - Perù 2
SI - Slovenia 2
TH - Thailandia 2
BD - Bangladesh 1
BG - Bulgaria 1
BO - Bolivia 1
CG - Congo 1
DO - Repubblica Dominicana 1
EC - Ecuador 1
GG - Guernsey 1
GR - Grecia 1
KW - Kuwait 1
LU - Lussemburgo 1
LY - Libia 1
NP - Nepal 1
PA - Panama 1
PH - Filippine 1
RS - Serbia 1
Totale 14.199
Salva come PNG Salva come JPEG
Città #
Ashburn 1.594
Southend 913
Seattle 776
Singapore 430
Fairfield 409
Council Bluffs 393
Santa Clara 278
Des Moines 267
Jacksonville 260
Beijing 259
Princeton 215
Chandler 205
Woodbridge 176
Cambridge 152
Houston 149
Ann Arbor 148
San Ramon 132
Berlin 128
Wilmington 128
Turin 125
Dublin 118
Izmir 115
Bern 95
Chicago 75
Boardman 74
Zhengzhou 74
Helsinki 70
San Donato Milanese 69
Hong Kong 65
Pennsylvania Furnace 64
Overberg 61
Zaporozhye 61
Herkenbosch 57
Shanghai 57
Torino 57
Frankfurt 56
Rome 47
Saint Petersburg 46
Baltimore 45
Hangzhou 38
San Diego 34
Padua 32
Monopoli 31
New York 31
Buffalo 30
Milan 30
Vienna 30
Guangzhou 29
Mountain View 28
Amsterdam 26
Dallas 26
Los Angeles 25
Frankfurt am Main 23
Ho Chi Minh City 23
Redwood City 23
Brussels 20
Moscow 19
São Paulo 19
London 18
Hanoi 16
Atlanta 14
Naples 14
Ningbo 14
Podenzano 13
Malatya 12
Norwalk 12
Andover 11
Modena 11
Redmond 11
Tel Aviv 11
Sedriano 10
Taipei 10
Bucharest 9
North Bergen 9
Toronto 9
Brasília 8
Kazan 8
Lappeenranta 8
Las Vegas 8
Nanjing 8
Palermo 8
Paris 8
Seoul 8
Verona 8
West Jordan 8
Yubileyny 8
Belo Horizonte 7
Edinburgh 7
Florence 7
Kiev 7
Puglianello 7
Xian 7
Belluno 6
Bologna 6
Changsha 6
Hefei 6
Istanbul 6
Jinan 6
Monza 6
Nanterre 6
Totale 9.342
Salva come PNG Salva come JPEG
Nome #
Appunti di costruzioni aeronautiche A 668
A refined structural model for static aeroelastic response and divergence of metallic and composite wings 418
Vibration analysis of anisotropic simply supported plates by using variable kinematic and rayleigh-ritz method 355
Improved response of unsymmetrically laminatedsandwich plates by using zig-zag functions 340
Improved bending analysis of sandwich plates using a zig-zag function 329
Free vibration of sandwich plates and shells by using zig-zag function 315
Vortex Lattice Method Coupled with Advanced One-Dimensional Structural Models 315
Invariant formulation for the minimum induced drag conditions of nonplanar wing systems 294
Aerodinamica dei sistemi portanti chiusi: ala anulare ellittica 287
Classical and advanced Multilayered plate element based upon PVD and RMVT. Part II: Numerical implementations 281
Studio aerodinamico di un'ala anulare ellittica 279
On the developments of a Joined Wing Prandtlplane 276
2D, Quasi 3D and 3D Exact Solutions for Bending of Thick and Thin Sandwich Plates 267
An Advanced Unified Aeroelastic Formulation based on 1D Higher-Order Finite Elements 257
An Invariant Finite Element Model for Composite Structures: the Generalized Unified Formulation 255
Flutter Failure Risk Assessment for Damage-Tolerant Composite Aircraft Structures 253
Assess the Accuracy of the Variational Asymptotic Plate and Shell Analysis Using the Generalized Unified Formulation 244
Minimum Induced Drag Theorems for Nonplanar Systems and Closed Wings 243
Three-dimensional closed form solutions and ∞3 theories for orthotropic plates 241
∞6mixed plate theories based on the Generalized Unified Formulation. Part I: Governing Equations 238
Assess the Accuracy of the Variational Asymptotic Plate and Shell Analysis (VAPAS) Using the Generalized Unified Formulation (GUF) 232
Aeroelastic coupling of Geometrically Nonlinear Structures and Linear Unsteady Aerodynamics – Two Formulations 228
Minimum induced drag theorems for multiwing systems 227
An Improved Beam Formulation for AeroelasticApplications 225
∞6mixed plate theories based on the Generalized Unified Formulation. Part IV: Zig-Zag Theories 222
A Reduced Order Nonlinear Aeroelastic Analysis of Joined Wings Based on the Proper Orthogonal Decomposition 222
Two benchmarks to assess two-dimensional theories of Sandwich Composite Plates 219
∞6mixed plate theories based on the Generalized Unified Formulation. Part III: Advanced Mixed High Order Shear Deformation Theories 217
An Invariant Model for any Composite Plate Theory and FEM Applications: the Generalized Unified Formulation 215
∞6mixed plate theories based on the Generalized Unified Formulation. Par V: Results 210
“∞3 plate theories for thick and thin plates: the generalized unified formulation 207
Classical and advanced Multilayered plate element based upon PVD and RMVT. Part I : Derivation of finite element matrices 207
Ala Anulare Ellittica: Distribuzione di Circolazione di Minima Resistenza Indotta 203
Refined Multilayered Plate Elements Based on Murakami Zig-Zag Functions 203
Aeroelasticity of Structurally Nonlinear Lifting Surfaces Using Linear Modally Reduced Aerodynamic Generalized Forces 198
Partially Zig-Zag Advanced Shear Deformation Theories Based on the Generalized Unified Formulation 198
Dynamic Aeroelasticity of Structurally Nonlinear Configurations Using Linear Modally Reduced Aerodynamic Generalized Forces 195
Dynamic Aeroelasticity of Structurally Nonlinear Configurations Using Linear Modally Reduced Aerodynamic Generalized Forces 194
Aerodynamic analysis of non-conventional wing configurations for aeroelastic applications 194
Induced Drag Minimization: a Variational Approach Using the Acceleration Potential 193
A Theoretical Investigation on the Conditions of Minimum Induced Drag of Closed Wing Systems and C-Wings 188
An Assessment of Multilayered Finite Plate Elements in View of the C0z Requirements 186
∞6mixed plate theories based on the Generalized Unified Formulation. Part II: Layerwise theories 185
On Two-Dimennional FEM simulatuon of Layered Plates, 182
Aeroelastic Coupling of Geometrically Nonlinear Structures and Linear Unsteady Aerodynamics: Two Formulations 181
Quasi-3D Analysis of Free Vibration of Anisotropic Plates 180
Contributions to Joined-Wing Aeroelasticity 177
Treatment of Stress Variables in Advanced Multilayered Plate Elements Based Upon Reissner’s Mixed Variational Theorem 175
Probabilistic Modeling of the Aeroelastic Life Cycle for Risk Evaluation of Composite Structures 174
Sandwich Plate Analysis by Finite Element Method and Reissner's Mixed Theorem 172
Three-Dimensional Closed Form Solutions and Exact Thin Plate Theories for Isotropic Plates 167
Exploratory Studies of Joined Wing Aeroelasticity 161
A Plate Structural Capability for the Nonlinear Aeroelastic Analysis of Joined-Wing Configurations 151
Influence of Temperature Profile on the Accuracy of Classical and Refined Multilayered Plate 150
Dynamic Aeroelasticity of Coupling Full Order Geometrically Nonlinear Structurs and Full Order Linear Unsteady Aerodynamic – The Joined Wing Case 149
Multi-Theory FEM Architecture for the Generation of Advanced Mixed Shear Deformation Theories Based on the Generalized Unified Formulation for Composite Structures 148
The Structural Order Reduction Challenge in the Case of Geometrically Nonlinear Joined-Wing Configurations 147
Partially Zig-Zag Advanced Shear Deformation Theories Based on the Generalized Unified Formulation 145
RADARSAT-2 Stress Summary Report, Issue 1 144
RADARSAT-2 Static Analysis Report, Issue 4 141
Structural Ritz-Based Simple-Polynomial Nonlinear Equivalent Approach – An Assessment 136
Structural Ritz-Based Simple-Polynomial Nonlinear Equivalent Approach – An Assessment 136
Effetto delle condizioni al contorno sulla modellizzazione di piastre multistrato” (English translation of the title: “Effects of the Boundary Conditions for 2D Models of Multilayered Plates 135
Elementi finiti piastra C[0-z] basati sull’equazione mista di Reissner 133
Totale 14.207
Salva come PNG Salva come JPEG
Categoria #
all - tutte 41.767
article - articoli 22.259
book - libri 1.380
conference - conferenze 15.378
curatela - curatele 0
other - altro 2.211
patent - brevetti 0
selected - selezionate 0
volume - volumi 539
Totale 83.534
Salva come PNG Salva come JPEG


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021418 0 0 0 0 0 112 38 77 23 77 70 21
2021/2022532 34 37 6 14 5 25 27 20 27 36 116 185
2022/20231.641 100 188 26 50 52 149 333 42 148 15 36 502
2023/2024213 14 13 6 13 31 18 8 12 4 11 28 55
2024/20251.206 19 246 58 104 182 117 22 45 192 39 104 78
2025/20261.201 190 151 223 265 241 131 0 0 0 0 0 0
Totale 14.207