PORTO @ Archivio Istituzionale della Ricerca

DEMASI, LUCIANO
 Distribuzione geografica
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Continente #
NA - Nord America 6.428
EU - Europa 5.262
AS - Asia 1.709
SA - Sud America 177
AF - Africa 21
OC - Oceania 7
Continente sconosciuto - Info sul continente non disponibili 3
Totale 13.607
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Nazione #
US - Stati Uniti d'America 6.403
IT - Italia 1.138
GB - Regno Unito 1.024
DE - Germania 926
FR - Francia 718
CN - Cina 649
UA - Ucraina 504
SG - Singapore 493
RU - Federazione Russa 249
NL - Olanda 179
BR - Brasile 144
TR - Turchia 141
IE - Irlanda 122
CH - Svizzera 102
KR - Corea 99
FI - Finlandia 80
JO - Giordania 65
SE - Svezia 62
HK - Hong Kong 56
AT - Austria 37
VN - Vietnam 33
JP - Giappone 29
BE - Belgio 27
IN - India 26
MY - Malesia 25
IL - Israele 24
RO - Romania 21
TW - Taiwan 21
CA - Canada 15
AP - ???statistics.table.value.countryCode.AP??? 14
AR - Argentina 12
ES - Italia 12
EU - Europa 10
MX - Messico 9
CL - Cile 8
IQ - Iraq 8
IR - Iran 8
PL - Polonia 8
AE - Emirati Arabi Uniti 7
AU - Australia 7
VE - Venezuela 6
EG - Egitto 5
HR - Croazia 5
ID - Indonesia 5
AZ - Azerbaigian 4
DZ - Algeria 4
EE - Estonia 4
LT - Lituania 4
PT - Portogallo 4
UZ - Uzbekistan 4
BY - Bielorussia 3
CZ - Repubblica Ceca 3
TN - Tunisia 3
ZA - Sudafrica 3
CO - Colombia 2
DK - Danimarca 2
KG - Kirghizistan 2
KZ - Kazakistan 2
MN - Mongolia 2
NG - Nigeria 2
PE - Perù 2
PY - Paraguay 2
SI - Slovenia 2
TH - Thailandia 2
BD - Bangladesh 1
BG - Bulgaria 1
CG - Congo 1
EC - Ecuador 1
GG - Guernsey 1
GR - Grecia 1
JM - Giamaica 1
KE - Kenya 1
KW - Kuwait 1
LU - Lussemburgo 1
LY - Libia 1
MA - Marocco 1
PH - Filippine 1
RS - Serbia 1
SA - Arabia Saudita 1
Totale 13.607
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Città #
Ashburn 1.576
Southend 913
Seattle 776
Fairfield 409
Council Bluffs 393
Santa Clara 272
Des Moines 267
Singapore 262
Jacksonville 260
Beijing 233
Princeton 215
Chandler 205
Woodbridge 176
Cambridge 152
Ann Arbor 148
Houston 148
San Ramon 132
Berlin 128
Wilmington 128
Turin 123
Dublin 118
Izmir 115
Bern 95
Boardman 74
Chicago 74
Zhengzhou 73
Helsinki 70
San Donato Milanese 69
Pennsylvania Furnace 64
Overberg 61
Zaporozhye 61
Herkenbosch 57
Torino 57
Frankfurt 56
Shanghai 54
Hong Kong 52
Rome 47
Saint Petersburg 46
Baltimore 45
Hangzhou 38
San Diego 33
Padua 32
Monopoli 31
Milan 30
New York 30
Vienna 30
Guangzhou 29
Mountain View 28
Amsterdam 26
Dallas 26
Redwood City 23
Brussels 20
Buffalo 18
London 18
Los Angeles 18
Moscow 18
São Paulo 17
Frankfurt am Main 15
Ningbo 14
Atlanta 13
Naples 13
Podenzano 13
Hanoi 12
Malatya 12
Norwalk 12
Andover 11
Modena 11
Redmond 11
Tel Aviv 11
Sedriano 10
Taipei 10
Bucharest 9
Ho Chi Minh City 9
Toronto 9
Brasília 8
Kazan 8
Lappeenranta 8
Las Vegas 8
Nanjing 8
Palermo 8
Paris 8
Verona 8
West Jordan 8
Yubileyny 8
Edinburgh 7
Florence 7
Kiev 7
Puglianello 7
Xian 7
Belluno 6
Bologna 6
Hefei 6
Istanbul 6
Jinan 6
Monza 6
Nanterre 6
Nichelino 6
Nuremberg 6
Olbia 6
Salerno 6
Totale 9.045
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Nome #
Appunti di costruzioni aeronautiche A 658
A refined structural model for static aeroelastic response and divergence of metallic and composite wings 403
Vibration analysis of anisotropic simply supported plates by using variable kinematic and rayleigh-ritz method 344
Improved response of unsymmetrically laminatedsandwich plates by using zig-zag functions 332
Improved bending analysis of sandwich plates using a zig-zag function 322
Free vibration of sandwich plates and shells by using zig-zag function 304
Vortex Lattice Method Coupled with Advanced One-Dimensional Structural Models 298
Invariant formulation for the minimum induced drag conditions of nonplanar wing systems 279
Aerodinamica dei sistemi portanti chiusi: ala anulare ellittica 278
Classical and advanced Multilayered plate element based upon PVD and RMVT. Part II: Numerical implementations 275
Studio aerodinamico di un'ala anulare ellittica 273
On the developments of a Joined Wing Prandtlplane 268
2D, Quasi 3D and 3D Exact Solutions for Bending of Thick and Thin Sandwich Plates 261
An Invariant Finite Element Model for Composite Structures: the Generalized Unified Formulation 244
Flutter Failure Risk Assessment for Damage-Tolerant Composite Aircraft Structures 242
An Advanced Unified Aeroelastic Formulation based on 1D Higher-Order Finite Elements 242
Assess the Accuracy of the Variational Asymptotic Plate and Shell Analysis Using the Generalized Unified Formulation 236
Three-dimensional closed form solutions and ∞3 theories for orthotropic plates 232
∞6mixed plate theories based on the Generalized Unified Formulation. Part I: Governing Equations 231
Minimum Induced Drag Theorems for Nonplanar Systems and Closed Wings 229
Assess the Accuracy of the Variational Asymptotic Plate and Shell Analysis (VAPAS) Using the Generalized Unified Formulation (GUF) 221
Aeroelastic coupling of Geometrically Nonlinear Structures and Linear Unsteady Aerodynamics – Two Formulations 218
∞6mixed plate theories based on the Generalized Unified Formulation. Part IV: Zig-Zag Theories 216
Two benchmarks to assess two-dimensional theories of Sandwich Composite Plates 214
An Improved Beam Formulation for AeroelasticApplications 213
Minimum induced drag theorems for multiwing systems 212
∞6mixed plate theories based on the Generalized Unified Formulation. Part III: Advanced Mixed High Order Shear Deformation Theories 208
A Reduced Order Nonlinear Aeroelastic Analysis of Joined Wings Based on the Proper Orthogonal Decomposition 208
An Invariant Model for any Composite Plate Theory and FEM Applications: the Generalized Unified Formulation 206
∞6mixed plate theories based on the Generalized Unified Formulation. Par V: Results 202
Classical and advanced Multilayered plate element based upon PVD and RMVT. Part I : Derivation of finite element matrices 202
“∞3 plate theories for thick and thin plates: the generalized unified formulation 198
Ala Anulare Ellittica: Distribuzione di Circolazione di Minima Resistenza Indotta 196
Refined Multilayered Plate Elements Based on Murakami Zig-Zag Functions 195
Dynamic Aeroelasticity of Structurally Nonlinear Configurations Using Linear Modally Reduced Aerodynamic Generalized Forces 191
Induced Drag Minimization: a Variational Approach Using the Acceleration Potential 187
Aeroelasticity of Structurally Nonlinear Lifting Surfaces Using Linear Modally Reduced Aerodynamic Generalized Forces 187
Dynamic Aeroelasticity of Structurally Nonlinear Configurations Using Linear Modally Reduced Aerodynamic Generalized Forces 185
Partially Zig-Zag Advanced Shear Deformation Theories Based on the Generalized Unified Formulation 183
A Theoretical Investigation on the Conditions of Minimum Induced Drag of Closed Wing Systems and C-Wings 180
An Assessment of Multilayered Finite Plate Elements in View of the C0z Requirements 179
Aerodynamic analysis of non-conventional wing configurations for aeroelastic applications 179
On Two-Dimennional FEM simulatuon of Layered Plates, 178
∞6mixed plate theories based on the Generalized Unified Formulation. Part II: Layerwise theories 175
Quasi-3D Analysis of Free Vibration of Anisotropic Plates 174
Aeroelastic Coupling of Geometrically Nonlinear Structures and Linear Unsteady Aerodynamics: Two Formulations 174
Contributions to Joined-Wing Aeroelasticity 170
Treatment of Stress Variables in Advanced Multilayered Plate Elements Based Upon Reissner’s Mixed Variational Theorem 169
Probabilistic Modeling of the Aeroelastic Life Cycle for Risk Evaluation of Composite Structures 166
Three-Dimensional Closed Form Solutions and Exact Thin Plate Theories for Isotropic Plates 164
Exploratory Studies of Joined Wing Aeroelasticity 154
Sandwich Plate Analysis by Finite Element Method and Reissner's Mixed Theorem 152
Influence of Temperature Profile on the Accuracy of Classical and Refined Multilayered Plate 143
Dynamic Aeroelasticity of Coupling Full Order Geometrically Nonlinear Structurs and Full Order Linear Unsteady Aerodynamic – The Joined Wing Case 142
A Plate Structural Capability for the Nonlinear Aeroelastic Analysis of Joined-Wing Configurations 139
RADARSAT-2 Stress Summary Report, Issue 1 136
Multi-Theory FEM Architecture for the Generation of Advanced Mixed Shear Deformation Theories Based on the Generalized Unified Formulation for Composite Structures 135
Partially Zig-Zag Advanced Shear Deformation Theories Based on the Generalized Unified Formulation 134
The Structural Order Reduction Challenge in the Case of Geometrically Nonlinear Joined-Wing Configurations 134
RADARSAT-2 Static Analysis Report, Issue 4 133
Structural Ritz-Based Simple-Polynomial Nonlinear Equivalent Approach – An Assessment 131
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 130
Structural Ritz-Based Simple-Polynomial Nonlinear Equivalent Approach – An Assessment 126
Elementi finiti piastra C[0-z] basati sull’equazione mista di Reissner 125
Totale 13.615
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Categoria #
all - tutte 39.853
article - articoli 21.274
book - libri 1.351
conference - conferenze 14.624
curatela - curatele 0
other - altro 2.103
patent - brevetti 0
selected - selezionate 0
volume - volumi 501
Totale 79.706
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021534 0 0 0 93 23 112 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
2025/2026609 190 151 223 45 0 0 0 0 0 0 0 0
Totale 13.615