PORTO @ Archivio Istituzionale della Ricerca

DEMASI, LUCIANO
 Distribuzione geografica
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Continente #
NA - Nord America 6.661
EU - Europa 5.290
AS - Asia 2.252
SA - Sud America 216
AF - Africa 26
OC - Oceania 7
Continente sconosciuto - Info sul continente non disponibili 3
Totale 14.455
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Nazione #
US - Stati Uniti d'America 6.629
IT - Italia 1.142
GB - Regno Unito 1.025
DE - Germania 935
SG - Singapore 844
CN - Cina 729
FR - Francia 727
UA - Ucraina 504
RU - Federazione Russa 252
NL - Olanda 179
BR - Brasile 170
TR - Turchia 141
IE - Irlanda 122
CH - Svizzera 102
KR - Corea 101
HK - Hong Kong 97
VN - Vietnam 87
FI - Finlandia 80
JO - Giordania 66
SE - Svezia 62
AT - Austria 37
JP - Giappone 30
IN - India 28
BE - Belgio 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
IQ - Iraq 9
PL - Polonia 9
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
MA - Marocco 4
PT - Portogallo 4
BY - Bielorussia 3
CO - Colombia 3
NG - Nigeria 3
PY - Paraguay 3
SA - Arabia Saudita 3
TN - Tunisia 3
ZA - Sudafrica 3
BD - Bangladesh 2
BO - Bolivia 2
DK - Danimarca 2
JM - Giamaica 2
KE - Kenya 2
KG - Kirghizistan 2
KZ - Kazakistan 2
MN - Mongolia 2
NP - Nepal 2
PE - Perù 2
PH - Filippine 2
PK - Pakistan 2
SI - Slovenia 2
TH - Thailandia 2
BG - Bulgaria 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
PA - Panama 1
RS - Serbia 1
UY - Uruguay 1
Totale 14.455
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Città #
Ashburn 1.602
Southend 913
Seattle 776
Singapore 442
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 Jose 136
San Ramon 132
Berlin 128
Wilmington 128
Turin 125
Dublin 118
Izmir 115
Bern 95
Hong Kong 89
Chicago 75
Boardman 74
Zhengzhou 74
Helsinki 70
San Donato Milanese 69
Pennsylvania Furnace 64
Overberg 61
Zaporozhye 61
Herkenbosch 57
Shanghai 57
Torino 57
Frankfurt 56
Rome 47
Saint Petersburg 46
Baltimore 45
Hangzhou 38
Los Angeles 38
Ho Chi Minh City 34
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
Hanoi 24
Frankfurt am Main 23
Redwood City 23
Brussels 20
Moscow 19
São Paulo 19
London 18
Atlanta 14
Naples 14
Ningbo 14
Podenzano 13
Malatya 12
Norwalk 12
Andover 11
Modena 11
Redmond 11
Tel Aviv 11
Lauterbourg 10
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
Totale 9.552
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Nome #
Appunti di costruzioni aeronautiche A 672
A refined structural model for static aeroelastic response and divergence of metallic and composite wings 420
Vibration analysis of anisotropic simply supported plates by using variable kinematic and rayleigh-ritz method 358
Improved response of unsymmetrically laminatedsandwich plates by using zig-zag functions 343
Improved bending analysis of sandwich plates using a zig-zag function 332
Vortex Lattice Method Coupled with Advanced One-Dimensional Structural Models 328
Free vibration of sandwich plates and shells by using zig-zag function 318
Invariant formulation for the minimum induced drag conditions of nonplanar wing systems 297
Aerodinamica dei sistemi portanti chiusi: ala anulare ellittica 290
Classical and advanced Multilayered plate element based upon PVD and RMVT. Part II: Numerical implementations 283
Studio aerodinamico di un'ala anulare ellittica 282
On the developments of a Joined Wing Prandtlplane 280
2D, Quasi 3D and 3D Exact Solutions for Bending of Thick and Thin Sandwich Plates 268
An Advanced Unified Aeroelastic Formulation based on 1D Higher-Order Finite Elements 263
An Invariant Finite Element Model for Composite Structures: the Generalized Unified Formulation 260
Flutter Failure Risk Assessment for Damage-Tolerant Composite Aircraft Structures 255
Three-dimensional closed form solutions and ∞3 theories for orthotropic plates 252
Assess the Accuracy of the Variational Asymptotic Plate and Shell Analysis Using the Generalized Unified Formulation 247
Minimum Induced Drag Theorems for Nonplanar Systems and Closed Wings 246
∞6mixed plate theories based on the Generalized Unified Formulation. Part I: Governing Equations 240
Assess the Accuracy of the Variational Asymptotic Plate and Shell Analysis (VAPAS) Using the Generalized Unified Formulation (GUF) 236
Aeroelastic coupling of Geometrically Nonlinear Structures and Linear Unsteady Aerodynamics – Two Formulations 232
Minimum induced drag theorems for multiwing systems 231
An Improved Beam Formulation for AeroelasticApplications 226
∞6mixed plate theories based on the Generalized Unified Formulation. Par V: Results 226
∞6mixed plate theories based on the Generalized Unified Formulation. Part IV: Zig-Zag Theories 225
A Reduced Order Nonlinear Aeroelastic Analysis of Joined Wings Based on the Proper Orthogonal Decomposition 224
Two benchmarks to assess two-dimensional theories of Sandwich Composite Plates 221
An Invariant Model for any Composite Plate Theory and FEM Applications: the Generalized Unified Formulation 220
∞6mixed plate theories based on the Generalized Unified Formulation. Part III: Advanced Mixed High Order Shear Deformation Theories 219
Refined Multilayered Plate Elements Based on Murakami Zig-Zag Functions 215
Aerodynamic analysis of non-conventional wing configurations for aeroelastic applications 211
Dynamic Aeroelasticity of Structurally Nonlinear Configurations Using Linear Modally Reduced Aerodynamic Generalized Forces 210
“∞3 plate theories for thick and thin plates: the generalized unified formulation 209
Classical and advanced Multilayered plate element based upon PVD and RMVT. Part I : Derivation of finite element matrices 209
Ala Anulare Ellittica: Distribuzione di Circolazione di Minima Resistenza Indotta 205
Partially Zig-Zag Advanced Shear Deformation Theories Based on the Generalized Unified Formulation 202
Aeroelasticity of Structurally Nonlinear Lifting Surfaces Using Linear Modally Reduced Aerodynamic Generalized Forces 200
Induced Drag Minimization: a Variational Approach Using the Acceleration Potential 199
Dynamic Aeroelasticity of Structurally Nonlinear Configurations Using Linear Modally Reduced Aerodynamic Generalized Forces 199
A Theoretical Investigation on the Conditions of Minimum Induced Drag of Closed Wing Systems and C-Wings 190
An Assessment of Multilayered Finite Plate Elements in View of the C0z Requirements 189
∞6mixed plate theories based on the Generalized Unified Formulation. Part II: Layerwise theories 187
On Two-Dimennional FEM simulatuon of Layered Plates, 186
Aeroelastic Coupling of Geometrically Nonlinear Structures and Linear Unsteady Aerodynamics: Two Formulations 184
Quasi-3D Analysis of Free Vibration of Anisotropic Plates 182
Contributions to Joined-Wing Aeroelasticity 179
Treatment of Stress Variables in Advanced Multilayered Plate Elements Based Upon Reissner’s Mixed Variational Theorem 179
Probabilistic Modeling of the Aeroelastic Life Cycle for Risk Evaluation of Composite Structures 176
Sandwich Plate Analysis by Finite Element Method and Reissner's Mixed Theorem 173
Three-Dimensional Closed Form Solutions and Exact Thin Plate Theories for Isotropic Plates 170
Exploratory Studies of Joined Wing Aeroelasticity 164
Influence of Temperature Profile on the Accuracy of Classical and Refined Multilayered Plate 163
A Plate Structural Capability for the Nonlinear Aeroelastic Analysis of Joined-Wing Configurations 153
Dynamic Aeroelasticity of Coupling Full Order Geometrically Nonlinear Structurs and Full Order Linear Unsteady Aerodynamic – The Joined Wing Case 150
Multi-Theory FEM Architecture for the Generation of Advanced Mixed Shear Deformation Theories Based on the Generalized Unified Formulation for Composite Structures 150
Partially Zig-Zag Advanced Shear Deformation Theories Based on the Generalized Unified Formulation 148
RADARSAT-2 Stress Summary Report, Issue 1 147
The Structural Order Reduction Challenge in the Case of Geometrically Nonlinear Joined-Wing Configurations 147
RADARSAT-2 Static Analysis Report, Issue 4 145
Structural Ritz-Based Simple-Polynomial Nonlinear Equivalent Approach – An Assessment 138
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 137
Structural Ritz-Based Simple-Polynomial Nonlinear Equivalent Approach – An Assessment 137
Elementi finiti piastra C[0-z] basati sull’equazione mista di Reissner 136
Totale 14.463
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Categoria #
all - tutte 42.242
article - articoli 22.525
book - libri 1.391
conference - conferenze 15.533
curatela - curatele 0
other - altro 2.247
patent - brevetti 0
selected - selezionate 0
volume - volumi 546
Totale 84.484
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021306 0 0 0 0 0 0 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
2025/20261.457 190 151 223 265 241 155 232 0 0 0 0 0
Totale 14.463