PORTO @ Archivio Istituzionale della Ricerca

DEMASI, LUCIANO
 Distribuzione geografica
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Continente #
NA - Nord America 6.942
EU - Europa 5.541
AS - Asia 3.036
SA - Sud America 224
AF - Africa 39
OC - Oceania 7
Continente sconosciuto - Info sul continente non disponibili 3
Totale 15.792
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Nazione #
US - Stati Uniti d'America 6.907
IT - Italia 1.154
GB - Regno Unito 1.035
DE - Germania 952
SG - Singapore 905
FR - Francia 813
CN - Cina 737
VN - Vietnam 604
UA - Ucraina 504
RU - Federazione Russa 350
NL - Olanda 189
BR - Brasile 175
KR - Corea 147
TR - Turchia 141
IE - Irlanda 122
HK - Hong Kong 109
CH - Svizzera 102
FI - Finlandia 92
IN - India 90
JO - Giordania 66
SE - Svezia 62
JP - Giappone 38
AT - Austria 37
MY - Malesia 30
TW - Taiwan 30
BE - Belgio 27
IL - Israele 24
RO - Romania 21
AR - Argentina 20
CA - Canada 18
IQ - Iraq 18
TH - Thailandia 17
PH - Filippine 16
AP - ???statistics.table.value.countryCode.AP??? 14
ES - Italia 12
MX - Messico 12
PL - Polonia 12
EU - Europa 10
CL - Cile 9
IR - Iran 8
AE - Emirati Arabi Uniti 7
AU - Australia 7
BD - Bangladesh 7
ID - Indonesia 7
PK - Pakistan 7
VE - Venezuela 7
EG - Egitto 6
MA - Marocco 6
UZ - Uzbekistan 6
ZA - Sudafrica 6
CZ - Repubblica Ceca 5
HR - Croazia 5
NP - Nepal 5
AZ - Azerbaigian 4
DZ - Algeria 4
EE - Estonia 4
LT - Lituania 4
NG - Nigeria 4
PT - Portogallo 4
TN - Tunisia 4
BG - Bulgaria 3
BY - Bielorussia 3
CO - Colombia 3
ET - Etiopia 3
KE - Kenya 3
KZ - Kazakistan 3
PY - Paraguay 3
SA - Arabia Saudita 3
BO - Bolivia 2
DK - Danimarca 2
JM - Giamaica 2
KG - Kirghizistan 2
KW - Kuwait 2
MN - Mongolia 2
PE - Perù 2
SI - Slovenia 2
CG - Congo 1
CI - Costa d'Avorio 1
CR - Costa Rica 1
DO - Repubblica Dominicana 1
EC - Ecuador 1
GE - Georgia 1
GG - Guernsey 1
GR - Grecia 1
LU - Lussemburgo 1
LY - Libia 1
PA - Panama 1
RS - Serbia 1
SR - Suriname 1
UY - Uruguay 1
Totale 15.792
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Città #
Ashburn 1.628
Southend 913
Seattle 776
Singapore 498
Fairfield 409
Council Bluffs 393
San Jose 301
Santa Clara 282
Des Moines 267
Beijing 261
Jacksonville 260
Princeton 215
Chandler 205
Ho Chi Minh City 179
Woodbridge 176
Cambridge 152
Hanoi 151
Houston 150
Ann Arbor 148
San Ramon 132
Berlin 128
Turin 128
Wilmington 128
Dublin 118
Izmir 115
Bern 95
Hong Kong 90
Helsinki 82
Chicago 75
Boardman 74
Zhengzhou 74
San Donato Milanese 69
Pennsylvania Furnace 64
Overberg 61
Zaporozhye 61
Herkenbosch 57
Shanghai 57
Torino 57
Frankfurt 56
Lauterbourg 54
Rome 47
Saint Petersburg 46
Baltimore 45
Los Angeles 40
Seoul 39
Frankfurt am Main 38
Hangzhou 38
New York 35
San Diego 35
Milan 34
Padua 32
Monopoli 31
Buffalo 30
Vienna 30
Guangzhou 29
Dallas 28
Mountain View 28
Amsterdam 26
Redwood City 23
London 21
Brussels 20
São Paulo 20
Da Nang 19
Haiphong 19
Moscow 19
Atlanta 15
Naples 14
Ningbo 14
Podenzano 13
Groningen 12
Malatya 12
Norwalk 12
Orem 12
Taipei 12
Andover 11
Modena 11
Redmond 11
Tel Aviv 11
Quận Ba 10
Sedriano 10
Bucharest 9
North Bergen 9
Palermo 9
Toronto 9
Bangkok 8
Brasília 8
Kazan 8
Lappeenranta 8
Las Vegas 8
Nanjing 8
Nuremberg 8
Paris 8
Roubaix 8
Verona 8
West Jordan 8
Yubileyny 8
Baghdad 7
Belo Horizonte 7
Bexley 7
Bến Tre 7
Totale 10.251
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Nome #
Appunti di costruzioni aeronautiche A 705
A refined structural model for static aeroelastic response and divergence of metallic and composite wings 455
Vibration analysis of anisotropic simply supported plates by using variable kinematic and rayleigh-ritz method 385
Improved response of unsymmetrically laminatedsandwich plates by using zig-zag functions 358
Vortex Lattice Method Coupled with Advanced One-Dimensional Structural Models 357
Improved bending analysis of sandwich plates using a zig-zag function 354
Free vibration of sandwich plates and shells by using zig-zag function 339
Invariant formulation for the minimum induced drag conditions of nonplanar wing systems 319
Aerodinamica dei sistemi portanti chiusi: ala anulare ellittica 307
On the developments of a Joined Wing Prandtlplane 301
Classical and advanced Multilayered plate element based upon PVD and RMVT. Part II: Numerical implementations 298
An Advanced Unified Aeroelastic Formulation based on 1D Higher-Order Finite Elements 298
Studio aerodinamico di un'ala anulare ellittica 297
Three-dimensional closed form solutions and ∞3 theories for orthotropic plates 282
2D, Quasi 3D and 3D Exact Solutions for Bending of Thick and Thin Sandwich Plates 280
An Invariant Finite Element Model for Composite Structures: the Generalized Unified Formulation 276
Minimum Induced Drag Theorems for Nonplanar Systems and Closed Wings 272
Assess the Accuracy of the Variational Asymptotic Plate and Shell Analysis Using the Generalized Unified Formulation 271
Flutter Failure Risk Assessment for Damage-Tolerant Composite Aircraft Structures 269
Assess the Accuracy of the Variational Asymptotic Plate and Shell Analysis (VAPAS) Using the Generalized Unified Formulation (GUF) 264
∞6mixed plate theories based on the Generalized Unified Formulation. Part I: Governing Equations 260
Minimum induced drag theorems for multiwing systems 259
Aeroelastic coupling of Geometrically Nonlinear Structures and Linear Unsteady Aerodynamics – Two Formulations 255
A Reduced Order Nonlinear Aeroelastic Analysis of Joined Wings Based on the Proper Orthogonal Decomposition 250
An Improved Beam Formulation for AeroelasticApplications 248
∞6mixed plate theories based on the Generalized Unified Formulation. Par V: Results 247
∞6mixed plate theories based on the Generalized Unified Formulation. Part IV: Zig-Zag Theories 246
Two benchmarks to assess two-dimensional theories of Sandwich Composite Plates 241
An Invariant Model for any Composite Plate Theory and FEM Applications: the Generalized Unified Formulation 240
“∞3 plate theories for thick and thin plates: the generalized unified formulation 232
Refined Multilayered Plate Elements Based on Murakami Zig-Zag Functions 232
∞6mixed plate theories based on the Generalized Unified Formulation. Part III: Advanced Mixed High Order Shear Deformation Theories 229
Dynamic Aeroelasticity of Structurally Nonlinear Configurations Using Linear Modally Reduced Aerodynamic Generalized Forces 228
Aeroelasticity of Structurally Nonlinear Lifting Surfaces Using Linear Modally Reduced Aerodynamic Generalized Forces 227
Ala Anulare Ellittica: Distribuzione di Circolazione di Minima Resistenza Indotta 226
Aerodynamic analysis of non-conventional wing configurations for aeroelastic applications 226
Classical and advanced Multilayered plate element based upon PVD and RMVT. Part I : Derivation of finite element matrices 226
Partially Zig-Zag Advanced Shear Deformation Theories Based on the Generalized Unified Formulation 223
Dynamic Aeroelasticity of Structurally Nonlinear Configurations Using Linear Modally Reduced Aerodynamic Generalized Forces 222
Induced Drag Minimization: a Variational Approach Using the Acceleration Potential 217
Aeroelastic Coupling of Geometrically Nonlinear Structures and Linear Unsteady Aerodynamics: Two Formulations 209
∞6mixed plate theories based on the Generalized Unified Formulation. Part II: Layerwise theories 207
A Theoretical Investigation on the Conditions of Minimum Induced Drag of Closed Wing Systems and C-Wings 206
Contributions to Joined-Wing Aeroelasticity 205
An Assessment of Multilayered Finite Plate Elements in View of the C0z Requirements 204
Quasi-3D Analysis of Free Vibration of Anisotropic Plates 203
Probabilistic Modeling of the Aeroelastic Life Cycle for Risk Evaluation of Composite Structures 197
On Two-Dimennional FEM simulatuon of Layered Plates, 194
Sandwich Plate Analysis by Finite Element Method and Reissner's Mixed Theorem 193
Treatment of Stress Variables in Advanced Multilayered Plate Elements Based Upon Reissner’s Mixed Variational Theorem 192
Three-Dimensional Closed Form Solutions and Exact Thin Plate Theories for Isotropic Plates 186
Influence of Temperature Profile on the Accuracy of Classical and Refined Multilayered Plate 184
Exploratory Studies of Joined Wing Aeroelasticity 178
RADARSAT-2 Stress Summary Report, Issue 1 176
A Plate Structural Capability for the Nonlinear Aeroelastic Analysis of Joined-Wing Configurations 175
Multi-Theory FEM Architecture for the Generation of Advanced Mixed Shear Deformation Theories Based on the Generalized Unified Formulation for Composite Structures 175
Partially Zig-Zag Advanced Shear Deformation Theories Based on the Generalized Unified Formulation 172
Dynamic Aeroelasticity of Coupling Full Order Geometrically Nonlinear Structurs and Full Order Linear Unsteady Aerodynamic – The Joined Wing Case 172
The Structural Order Reduction Challenge in the Case of Geometrically Nonlinear Joined-Wing Configurations 170
RADARSAT-2 Static Analysis Report, Issue 4 167
Elementi finiti piastra C[0-z] basati sull’equazione mista di Reissner 156
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 153
Structural Ritz-Based Simple-Polynomial Nonlinear Equivalent Approach – An Assessment 153
Structural Ritz-Based Simple-Polynomial Nonlinear Equivalent Approach – An Assessment 152
Totale 15.800
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Categoria #
all - tutte 44.468
article - articoli 23.649
book - libri 1.436
conference - conferenze 16.409
curatela - curatele 0
other - altro 2.382
patent - brevetti 0
selected - selezionate 0
volume - volumi 592
Totale 88.936
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/202191 0 0 0 0 0 0 0 0 0 0 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
2025/20262.794 190 151 223 265 241 155 365 143 655 377 29 0
Totale 15.800