DEMASI, LUCIANO
 Distribuzione geografica
Continente #
NA - Nord America 7.810
EU - Europa 5.654
AS - Asia 3.087
SA - Sud America 236
AF - Africa 39
Continente sconosciuto - Info sul continente non disponibili 12
OC - Oceania 7
Totale 16.845
Nazione #
US - Stati Uniti d'America 7.693
IT - Italia 1.253
GB - Regno Unito 1.039
DE - Germania 954
SG - Singapore 920
FR - Francia 814
CN - Cina 737
VN - Vietnam 606
UA - Ucraina 504
RU - Federazione Russa 350
NL - Olanda 189
BR - Brasile 181
KR - Corea 157
TR - Turchia 141
IE - Irlanda 122
HK - Hong Kong 109
CH - Svizzera 103
FI - Finlandia 92
IN - India 92
CA - Canada 67
JO - Giordania 66
SE - Svezia 62
JP - Giappone 38
AT - Austria 37
MY - Malesia 31
TW - Taiwan 30
BD - Bangladesh 27
BE - Belgio 27
IL - Israele 24
RO - Romania 23
AR - Argentina 21
IQ - Iraq 18
TH - Thailandia 17
PH - Filippine 16
AP - ???statistics.table.value.countryCode.AP??? 14
ES - Italia 13
PL - Polonia 13
MX - Messico 12
CL - Cile 10
EU - Europa 10
JM - Giamaica 10
ID - Indonesia 8
IR - Iran 8
AE - Emirati Arabi Uniti 7
AU - Australia 7
CO - Colombia 7
PK - Pakistan 7
VE - Venezuela 7
EG - Egitto 6
GT - Guatemala 6
MA - Marocco 6
UZ - Uzbekistan 6
ZA - Sudafrica 6
CR - Costa Rica 5
CZ - Repubblica Ceca 5
HR - Croazia 5
NP - Nepal 5
PT - Portogallo 5
AZ - Azerbaigian 4
DZ - Algeria 4
EE - Estonia 4
LT - Lituania 4
NG - Nigeria 4
NI - Nicaragua 4
TN - Tunisia 4
BG - Bulgaria 3
BY - Bielorussia 3
ET - Etiopia 3
HN - Honduras 3
KE - Kenya 3
KZ - Kazakistan 3
PY - Paraguay 3
SA - Arabia Saudita 3
TT - Trinidad e Tobago 3
BO - Bolivia 2
BS - Bahamas 2
DK - Danimarca 2
KG - Kirghizistan 2
KW - Kuwait 2
MN - Mongolia 2
PE - Perù 2
SI - Slovenia 2
BA - Bosnia-Erzegovina 1
CG - Congo 1
CI - Costa d'Avorio 1
CW - ???statistics.table.value.countryCode.CW??? 1
DO - Repubblica Dominicana 1
EC - Ecuador 1
GE - Georgia 1
GG - Guernsey 1
GP - Guadalupe 1
GR - Grecia 1
LU - Lussemburgo 1
LY - Libia 1
PA - Panama 1
PR - Porto Rico 1
RS - Serbia 1
SR - Suriname 1
SV - El Salvador 1
UY - Uruguay 1
Totale 16.837
Città #
Ashburn 1.889
Southend 913
Seattle 778
Singapore 500
Council Bluffs 477
Fairfield 409
San Jose 400
Santa Clara 299
Des Moines 267
Jacksonville 263
Beijing 261
Princeton 216
Chandler 205
Ho Chi Minh City 180
Woodbridge 176
Houston 153
Cambridge 152
Hanoi 151
Ann Arbor 148
Turin 136
San Ramon 132
Berlin 129
Wilmington 128
Dublin 119
Izmir 115
Bern 95
Chicago 95
Hong Kong 90
Helsinki 82
Boardman 74
Zhengzhou 74
San Donato Milanese 69
Pennsylvania Furnace 64
Overberg 61
Zaporozhye 61
Herkenbosch 57
Shanghai 57
Torino 57
Frankfurt 56
Milan 56
Lauterbourg 54
Rome 50
Los Angeles 49
Saint Petersburg 46
Baltimore 45
Frankfurt am Main 39
Seoul 39
Hangzhou 38
New York 38
Dallas 36
San Diego 35
Phoenix 33
Padua 32
Buffalo 31
Monopoli 31
Vienna 30
Guangzhou 29
Mountain View 28
Amsterdam 26
London 23
Redwood City 23
São Paulo 21
Brussels 20
Da Nang 19
Haiphong 19
Moscow 19
Atlanta 17
Toronto 17
Miano 15
Naples 15
Ningbo 14
Norwalk 13
Podenzano 13
Groningen 12
Malatya 12
Modena 12
Orem 12
Taipei 12
Andover 11
Las Vegas 11
Montreal 11
Redmond 11
Tel Aviv 11
Palermo 10
Quận Ba 10
Sedriano 10
Brasília 9
Bucharest 9
Denver 9
Kingston 9
North Bergen 9
Bangkok 8
Kazan 8
Lappeenranta 8
Miami 8
Nanjing 8
Nuremberg 8
Paris 8
Roubaix 8
Verona 8
Totale 10.863
Nome #
Appunti di costruzioni aeronautiche A 725
A refined structural model for static aeroelastic response and divergence of metallic and composite wings 480
Vibration analysis of anisotropic simply supported plates by using variable kinematic and rayleigh-ritz method 403
Improved response of unsymmetrically laminatedsandwich plates by using zig-zag functions 376
Improved bending analysis of sandwich plates using a zig-zag function 376
Vortex Lattice Method Coupled with Advanced One-Dimensional Structural Models 372
Free vibration of sandwich plates and shells by using zig-zag function 357
Invariant formulation for the minimum induced drag conditions of nonplanar wing systems 337
Aerodinamica dei sistemi portanti chiusi: ala anulare ellittica 317
An Advanced Unified Aeroelastic Formulation based on 1D Higher-Order Finite Elements 313
On the developments of a Joined Wing Prandtlplane 312
Classical and advanced Multilayered plate element based upon PVD and RMVT. Part II: Numerical implementations 311
Studio aerodinamico di un'ala anulare ellittica 311
Three-dimensional closed form solutions and ∞3 theories for orthotropic plates 302
An Invariant Finite Element Model for Composite Structures: the Generalized Unified Formulation 300
2D, Quasi 3D and 3D Exact Solutions for Bending of Thick and Thin Sandwich Plates 296
Minimum Induced Drag Theorems for Nonplanar Systems and Closed Wings 289
Assess the Accuracy of the Variational Asymptotic Plate and Shell Analysis Using the Generalized Unified Formulation 288
Flutter Failure Risk Assessment for Damage-Tolerant Composite Aircraft Structures 282
Minimum induced drag theorems for multiwing systems 278
∞6mixed plate theories based on the Generalized Unified Formulation. Part I: Governing Equations 277
Assess the Accuracy of the Variational Asymptotic Plate and Shell Analysis (VAPAS) Using the Generalized Unified Formulation (GUF) 277
∞6mixed plate theories based on the Generalized Unified Formulation. Par V: Results 274
Aeroelastic coupling of Geometrically Nonlinear Structures and Linear Unsteady Aerodynamics – Two Formulations 273
A Reduced Order Nonlinear Aeroelastic Analysis of Joined Wings Based on the Proper Orthogonal Decomposition 267
An Improved Beam Formulation for AeroelasticApplications 266
“∞3 plate theories for thick and thin plates: the generalized unified formulation 261
∞6mixed plate theories based on the Generalized Unified Formulation. Part IV: Zig-Zag Theories 261
Two benchmarks to assess two-dimensional theories of Sandwich Composite Plates 254
An Invariant Model for any Composite Plate Theory and FEM Applications: the Generalized Unified Formulation 254
An Assessment of Multilayered Finite Plate Elements in View of the C0z Requirements 252
Refined Multilayered Plate Elements Based on Murakami Zig-Zag Functions 251
Ala Anulare Ellittica: Distribuzione di Circolazione di Minima Resistenza Indotta 247
∞6mixed plate theories based on the Generalized Unified Formulation. Part III: Advanced Mixed High Order Shear Deformation Theories 245
∞6mixed plate theories based on the Generalized Unified Formulation. Part II: Layerwise theories 242
Dynamic Aeroelasticity of Structurally Nonlinear Configurations Using Linear Modally Reduced Aerodynamic Generalized Forces 242
Aeroelasticity of Structurally Nonlinear Lifting Surfaces Using Linear Modally Reduced Aerodynamic Generalized Forces 237
Partially Zig-Zag Advanced Shear Deformation Theories Based on the Generalized Unified Formulation 237
Aerodynamic analysis of non-conventional wing configurations for aeroelastic applications 236
Classical and advanced Multilayered plate element based upon PVD and RMVT. Part I : Derivation of finite element matrices 236
Dynamic Aeroelasticity of Structurally Nonlinear Configurations Using Linear Modally Reduced Aerodynamic Generalized Forces 235
Induced Drag Minimization: a Variational Approach Using the Acceleration Potential 229
A Theoretical Investigation on the Conditions of Minimum Induced Drag of Closed Wing Systems and C-Wings 228
Sandwich Plate Analysis by Finite Element Method and Reissner's Mixed Theorem 223
Aeroelastic Coupling of Geometrically Nonlinear Structures and Linear Unsteady Aerodynamics: Two Formulations 222
Contributions to Joined-Wing Aeroelasticity 221
Quasi-3D Analysis of Free Vibration of Anisotropic Plates 214
Probabilistic Modeling of the Aeroelastic Life Cycle for Risk Evaluation of Composite Structures 209
On Two-Dimennional FEM simulatuon of Layered Plates, 205
Treatment of Stress Variables in Advanced Multilayered Plate Elements Based Upon Reissner’s Mixed Variational Theorem 202
Three-Dimensional Closed Form Solutions and Exact Thin Plate Theories for Isotropic Plates 200
Influence of Temperature Profile on the Accuracy of Classical and Refined Multilayered Plate 197
RADARSAT-2 Stress Summary Report, Issue 1 194
Exploratory Studies of Joined Wing Aeroelasticity 192
Multi-Theory FEM Architecture for the Generation of Advanced Mixed Shear Deformation Theories Based on the Generalized Unified Formulation for Composite Structures 189
A Plate Structural Capability for the Nonlinear Aeroelastic Analysis of Joined-Wing Configurations 188
Partially Zig-Zag Advanced Shear Deformation Theories Based on the Generalized Unified Formulation 186
Dynamic Aeroelasticity of Coupling Full Order Geometrically Nonlinear Structurs and Full Order Linear Unsteady Aerodynamic – The Joined Wing Case 183
RADARSAT-2 Static Analysis Report, Issue 4 182
The Structural Order Reduction Challenge in the Case of Geometrically Nonlinear Joined-Wing Configurations 179
Elementi finiti piastra C[0-z] basati sull’equazione mista di Reissner 173
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 161
Structural Ritz-Based Simple-Polynomial Nonlinear Equivalent Approach – An Assessment 160
Structural Ritz-Based Simple-Polynomial Nonlinear Equivalent Approach – An Assessment 159
Totale 16.845
Categoria #
all - tutte 48.648
article - articoli 25.797
book - libri 1.508
conference - conferenze 18.057
curatela - curatele 0
other - altro 2.635
patent - brevetti 0
selected - selezionate 0
volume - volumi 651
Totale 97.296


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2021/2022441 0 0 0 0 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
2025/20262.939 190 151 223 265 241 155 365 143 655 377 37 137
2026/2027900 92 75 252 417 64 0 0 0 0 0 0 0
Totale 16.845