PORTO @ Archivio Istituzionale della Ricerca

DEMASI, LUCIANO
 Distribuzione geografica
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Continente #
NA - Nord America 6.494
EU - Europa 5.272
AS - Asia 2.075
SA - Sud America 200
AF - Africa 23
OC - Oceania 7
Continente sconosciuto - Info sul continente non disponibili 3
Totale 14.074
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Nazione #
US - Stati Uniti d'America 6.464
IT - Italia 1.139
GB - Regno Unito 1.025
DE - Germania 931
SG - Singapore 755
CN - Cina 718
FR - Francia 718
UA - Ucraina 504
RU - Federazione Russa 250
NL - Olanda 179
BR - Brasile 161
TR - Turchia 141
IE - Irlanda 122
CH - Svizzera 102
KR - Corea 99
FI - Finlandia 80
HK - Hong Kong 69
JO - Giordania 65
SE - Svezia 62
VN - Vietnam 49
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 16
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
AZ - Azerbaigian 4
CZ - Repubblica Ceca 4
DZ - Algeria 4
EE - Estonia 4
LT - Lituania 4
PT - Portogallo 4
UZ - Uzbekistan 4
BY - Bielorussia 3
CO - Colombia 3
SA - Arabia Saudita 3
TN - Tunisia 3
ZA - Sudafrica 3
DK - Danimarca 2
KE - Kenya 2
KG - Kirghizistan 2
KZ - Kazakistan 2
MA - Marocco 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
DO - Repubblica Dominicana 1
EC - Ecuador 1
GG - Guernsey 1
GR - Grecia 1
JM - Giamaica 1
KW - Kuwait 1
LU - Lussemburgo 1
LY - Libia 1
NP - Nepal 1
PH - Filippine 1
RS - Serbia 1
Totale 14.074
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Città #
Ashburn 1.590
Southend 913
Seattle 776
Singapore 423
Fairfield 409
Council Bluffs 393
Santa Clara 274
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 123
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
Redwood City 23
Brussels 20
Frankfurt am Main 19
Ho Chi Minh City 18
London 18
Moscow 18
São Paulo 18
Atlanta 14
Hanoi 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
Toronto 9
Brasília 8
Kazan 8
Lappeenranta 8
Las Vegas 8
Nanjing 8
North Bergen 8
Palermo 8
Paris 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
Nichelino 6
Totale 9.309
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Nome #
Appunti di costruzioni aeronautiche A 666
A refined structural model for static aeroelastic response and divergence of metallic and composite wings 414
Vibration analysis of anisotropic simply supported plates by using variable kinematic and rayleigh-ritz method 353
Improved response of unsymmetrically laminatedsandwich plates by using zig-zag functions 339
Improved bending analysis of sandwich plates using a zig-zag function 328
Free vibration of sandwich plates and shells by using zig-zag function 312
Vortex Lattice Method Coupled with Advanced One-Dimensional Structural Models 311
Invariant formulation for the minimum induced drag conditions of nonplanar wing systems 289
Aerodinamica dei sistemi portanti chiusi: ala anulare ellittica 285
Classical and advanced Multilayered plate element based upon PVD and RMVT. Part II: Numerical implementations 280
Studio aerodinamico di un'ala anulare ellittica 278
On the developments of a Joined Wing Prandtlplane 274
2D, Quasi 3D and 3D Exact Solutions for Bending of Thick and Thin Sandwich Plates 266
An Advanced Unified Aeroelastic Formulation based on 1D Higher-Order Finite Elements 255
An Invariant Finite Element Model for Composite Structures: the Generalized Unified Formulation 253
Flutter Failure Risk Assessment for Damage-Tolerant Composite Aircraft Structures 250
Assess the Accuracy of the Variational Asymptotic Plate and Shell Analysis Using the Generalized Unified Formulation 242
Minimum Induced Drag Theorems for Nonplanar Systems and Closed Wings 241
Three-dimensional closed form solutions and ∞3 theories for orthotropic plates 239
∞6mixed plate theories based on the Generalized Unified Formulation. Part I: Governing Equations 237
Assess the Accuracy of the Variational Asymptotic Plate and Shell Analysis (VAPAS) Using the Generalized Unified Formulation (GUF) 229
Aeroelastic coupling of Geometrically Nonlinear Structures and Linear Unsteady Aerodynamics – Two Formulations 225
Minimum induced drag theorems for multiwing systems 223
An Improved Beam Formulation for AeroelasticApplications 222
∞6mixed plate theories based on the Generalized Unified Formulation. Part IV: Zig-Zag Theories 221
A Reduced Order Nonlinear Aeroelastic Analysis of Joined Wings Based on the Proper Orthogonal Decomposition 219
Two benchmarks to assess two-dimensional theories of Sandwich Composite Plates 218
∞6mixed plate theories based on the Generalized Unified Formulation. Part III: Advanced Mixed High Order Shear Deformation Theories 214
An Invariant Model for any Composite Plate Theory and FEM Applications: the Generalized Unified Formulation 213
∞6mixed plate theories based on the Generalized Unified Formulation. Par V: Results 208
“∞3 plate theories for thick and thin plates: the generalized unified formulation 206
Classical and advanced Multilayered plate element based upon PVD and RMVT. Part I : Derivation of finite element matrices 206
Ala Anulare Ellittica: Distribuzione di Circolazione di Minima Resistenza Indotta 202
Refined Multilayered Plate Elements Based on Murakami Zig-Zag Functions 200
Aeroelasticity of Structurally Nonlinear Lifting Surfaces Using Linear Modally Reduced Aerodynamic Generalized Forces 196
Partially Zig-Zag Advanced Shear Deformation Theories Based on the Generalized Unified Formulation 195
Dynamic Aeroelasticity of Structurally Nonlinear Configurations Using Linear Modally Reduced Aerodynamic Generalized Forces 194
Dynamic Aeroelasticity of Structurally Nonlinear Configurations Using Linear Modally Reduced Aerodynamic Generalized Forces 193
Induced Drag Minimization: a Variational Approach Using the Acceleration Potential 192
Aerodynamic analysis of non-conventional wing configurations for aeroelastic applications 191
A Theoretical Investigation on the Conditions of Minimum Induced Drag of Closed Wing Systems and C-Wings 187
An Assessment of Multilayered Finite Plate Elements in View of the C0z Requirements 184
∞6mixed plate theories based on the Generalized Unified Formulation. Part II: Layerwise theories 183
On Two-Dimennional FEM simulatuon of Layered Plates, 180
Quasi-3D Analysis of Free Vibration of Anisotropic Plates 179
Aeroelastic Coupling of Geometrically Nonlinear Structures and Linear Unsteady Aerodynamics: Two Formulations 179
Contributions to Joined-Wing Aeroelasticity 175
Treatment of Stress Variables in Advanced Multilayered Plate Elements Based Upon Reissner’s Mixed Variational Theorem 174
Probabilistic Modeling of the Aeroelastic Life Cycle for Risk Evaluation of Composite Structures 173
Sandwich Plate Analysis by Finite Element Method and Reissner's Mixed Theorem 168
Three-Dimensional Closed Form Solutions and Exact Thin Plate Theories for Isotropic Plates 166
Exploratory Studies of Joined Wing Aeroelasticity 159
A Plate Structural Capability for the Nonlinear Aeroelastic Analysis of Joined-Wing Configurations 150
Influence of Temperature Profile on the Accuracy of Classical and Refined Multilayered Plate 149
Dynamic Aeroelasticity of Coupling Full Order Geometrically Nonlinear Structurs and Full Order Linear Unsteady Aerodynamic – The Joined Wing Case 148
Multi-Theory FEM Architecture for the Generation of Advanced Mixed Shear Deformation Theories Based on the Generalized Unified Formulation for Composite Structures 146
The Structural Order Reduction Challenge in the Case of Geometrically Nonlinear Joined-Wing Configurations 146
RADARSAT-2 Stress Summary Report, Issue 1 142
Partially Zig-Zag Advanced Shear Deformation Theories Based on the Generalized Unified Formulation 142
RADARSAT-2 Static Analysis Report, Issue 4 138
Structural Ritz-Based Simple-Polynomial Nonlinear Equivalent Approach – An Assessment 135
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 134
Structural Ritz-Based Simple-Polynomial Nonlinear Equivalent Approach – An Assessment 134
Elementi finiti piastra C[0-z] basati sull’equazione mista di Reissner 132
Totale 14.082
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Categoria #
all - tutte 41.333
article - articoli 22.065
book - libri 1.373
conference - conferenze 15.179
curatela - curatele 0
other - altro 2.181
patent - brevetti 0
selected - selezionate 0
volume - volumi 535
Totale 82.666
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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
2025/20261.076 190 151 223 265 241 6 0 0 0 0 0 0
Totale 14.082