PORTO @ Archivio Istituzionale della Ricerca

DEMASI, LUCIANO
 Distribuzione geografica
Salva come PNG Salva come JPEG
Continente #
NA - Nord America 5.931
EU - Europa 5.081
AS - Asia 1.067
SA - Sud America 20
AF - Africa 11
OC - Oceania 7
Continente sconosciuto - Info sul continente non disponibili 3
Totale 12.120
Salva come PNG Salva come JPEG
Nazione #
US - Stati Uniti d'America 5.920
IT - Italia 1.110
GB - Regno Unito 1.009
DE - Germania 903
FR - Francia 693
UA - Ucraina 504
CN - Cina 500
RU - Federazione Russa 197
NL - Olanda 177
SG - Singapore 154
TR - Turchia 134
IE - Irlanda 122
CH - Svizzera 102
FI - Finlandia 75
JO - Giordania 64
KR - Corea 62
SE - Svezia 61
AT - Austria 33
JP - Giappone 29
MY - Malesia 25
IL - Israele 24
IN - India 22
RO - Romania 21
TW - Taiwan 21
BE - Belgio 17
AP - ???statistics.table.value.countryCode.AP??? 14
EU - Europa 10
BR - Brasile 9
CA - Canada 9
IR - Iran 8
VN - Vietnam 8
AU - Australia 7
CL - Cile 7
ES - Italia 7
HR - Croazia 5
AE - Emirati Arabi Uniti 4
AR - Argentina 4
EE - Estonia 4
EG - Egitto 4
PT - Portogallo 4
BY - Bielorussia 3
CZ - Repubblica Ceca 3
DZ - Algeria 3
HK - Hong Kong 3
UZ - Uzbekistan 3
DK - Danimarca 2
ID - Indonesia 2
MX - Messico 2
NG - Nigeria 2
PL - Polonia 2
SI - Slovenia 2
TH - Thailandia 2
BG - Bulgaria 1
GR - Grecia 1
KZ - Kazakistan 1
LU - Lussemburgo 1
LY - Libia 1
PH - Filippine 1
RS - Serbia 1
TN - Tunisia 1
Totale 12.120
Salva come PNG Salva come JPEG
Città #
Ashburn 1.484
Southend 913
Seattle 772
Fairfield 409
Council Bluffs 392
Des Moines 267
Jacksonville 260
Princeton 215
Chandler 205
Beijing 180
Woodbridge 176
Cambridge 152
Ann Arbor 148
Houston 148
San Ramon 132
Berlin 128
Wilmington 128
Turin 123
Dublin 118
Izmir 115
Singapore 106
Bern 95
Boardman 74
Chicago 72
Zhengzhou 72
San Donato Milanese 69
Helsinki 66
Pennsylvania Furnace 64
Overberg 61
Zaporozhye 61
Herkenbosch 57
Torino 57
Frankfurt 56
Shanghai 53
Rome 47
Saint Petersburg 46
Baltimore 45
Hangzhou 38
Padua 32
San Diego 32
Monopoli 31
Milan 30
Vienna 30
Mountain View 28
New York 27
Amsterdam 24
Guangzhou 24
Redwood City 23
Santa Clara 20
Moscow 18
London 16
Ningbo 14
Podenzano 13
Brussels 12
Malatya 12
Norwalk 12
Andover 11
Atlanta 11
Redmond 11
Tel Aviv 11
Sedriano 10
Taipei 10
Bucharest 9
Modena 9
Naples 9
Kazan 8
Lappeenranta 8
Nanjing 8
Palermo 8
Verona 8
Edinburgh 7
Hanoi 7
Kiev 7
Las Vegas 7
Paris 7
Puglianello 7
Toronto 7
Xian 7
Belluno 6
Bologna 6
Florence 6
Monza 6
Nanterre 6
Nichelino 6
Olbia 6
Salerno 6
Tapping 6
Vicenza 6
Zhitomir 6
Chengdu 5
Cotronei 5
Dearborn 5
Frankfurt Am Main 5
Melun 5
Miami 5
Palm Beach Gardens 5
Procida 5
San Mauro Torinese 5
Sunnyvale 5
Washington 5
Totale 8.310
Salva come PNG Salva come JPEG
Nome #
Appunti di costruzioni aeronautiche A 612
A refined structural model for static aeroelastic response and divergence of metallic and composite wings 362
Improved response of unsymmetrically laminatedsandwich plates by using zig-zag functions 306
Improved bending analysis of sandwich plates using a zig-zag function 302
Vibration analysis of anisotropic simply supported plates by using variable kinematic and rayleigh-ritz method 300
Free vibration of sandwich plates and shells by using zig-zag function 289
Aerodinamica dei sistemi portanti chiusi: ala anulare ellittica 260
Studio aerodinamico di un'ala anulare ellittica 258
Vortex Lattice Method Coupled with Advanced One-Dimensional Structural Models 258
Classical and advanced Multilayered plate element based upon PVD and RMVT. Part II: Numerical implementations 249
2D, Quasi 3D and 3D Exact Solutions for Bending of Thick and Thin Sandwich Plates 243
Invariant formulation for the minimum induced drag conditions of nonplanar wing systems 240
On the developments of a Joined Wing Prandtlplane 234
Flutter Failure Risk Assessment for Damage-Tolerant Composite Aircraft Structures 217
An Invariant Finite Element Model for Composite Structures: the Generalized Unified Formulation 214
∞6mixed plate theories based on the Generalized Unified Formulation. Part I: Governing Equations 213
Assess the Accuracy of the Variational Asymptotic Plate and Shell Analysis Using the Generalized Unified Formulation 211
An Advanced Unified Aeroelastic Formulation based on 1D Higher-Order Finite Elements 210
Three-dimensional closed form solutions and ∞3 theories for orthotropic plates 202
∞6mixed plate theories based on the Generalized Unified Formulation. Part IV: Zig-Zag Theories 198
Two benchmarks to assess two-dimensional theories of Sandwich Composite Plates 194
∞6mixed plate theories based on the Generalized Unified Formulation. Part III: Advanced Mixed High Order Shear Deformation Theories 193
Aeroelastic coupling of Geometrically Nonlinear Structures and Linear Unsteady Aerodynamics – Two Formulations 189
Assess the Accuracy of the Variational Asymptotic Plate and Shell Analysis (VAPAS) Using the Generalized Unified Formulation (GUF) 189
Minimum Induced Drag Theorems for Nonplanar Systems and Closed Wings 187
An Improved Beam Formulation for AeroelasticApplications 184
∞6mixed plate theories based on the Generalized Unified Formulation. Par V: Results 183
A Reduced Order Nonlinear Aeroelastic Analysis of Joined Wings Based on the Proper Orthogonal Decomposition 183
Ala Anulare Ellittica: Distribuzione di Circolazione di Minima Resistenza Indotta 180
Refined Multilayered Plate Elements Based on Murakami Zig-Zag Functions 180
“∞3 plate theories for thick and thin plates: the generalized unified formulation 178
Classical and advanced Multilayered plate element based upon PVD and RMVT. Part I : Derivation of finite element matrices 178
Minimum induced drag theorems for multiwing systems 176
An Invariant Model for any Composite Plate Theory and FEM Applications: the Generalized Unified Formulation 174
Aeroelasticity of Structurally Nonlinear Lifting Surfaces Using Linear Modally Reduced Aerodynamic Generalized Forces 172
Dynamic Aeroelasticity of Structurally Nonlinear Configurations Using Linear Modally Reduced Aerodynamic Generalized Forces 171
Dynamic Aeroelasticity of Structurally Nonlinear Configurations Using Linear Modally Reduced Aerodynamic Generalized Forces 169
Induced Drag Minimization: a Variational Approach Using the Acceleration Potential 166
An Assessment of Multilayered Finite Plate Elements in View of the C0z Requirements 166
On Two-Dimennional FEM simulatuon of Layered Plates, 164
Quasi-3D Analysis of Free Vibration of Anisotropic Plates 162
∞6mixed plate theories based on the Generalized Unified Formulation. Part II: Layerwise theories 160
Aerodynamic analysis of non-conventional wing configurations for aeroelastic applications 160
Partially Zig-Zag Advanced Shear Deformation Theories Based on the Generalized Unified Formulation 158
Aeroelastic Coupling of Geometrically Nonlinear Structures and Linear Unsteady Aerodynamics: Two Formulations 157
A Theoretical Investigation on the Conditions of Minimum Induced Drag of Closed Wing Systems and C-Wings 155
Three-Dimensional Closed Form Solutions and Exact Thin Plate Theories for Isotropic Plates 153
Probabilistic Modeling of the Aeroelastic Life Cycle for Risk Evaluation of Composite Structures 151
Treatment of Stress Variables in Advanced Multilayered Plate Elements Based Upon Reissner’s Mixed Variational Theorem 149
Contributions to Joined-Wing Aeroelasticity 139
Exploratory Studies of Joined Wing Aeroelasticity 134
Dynamic Aeroelasticity of Coupling Full Order Geometrically Nonlinear Structurs and Full Order Linear Unsteady Aerodynamic – The Joined Wing Case 128
Sandwich Plate Analysis by Finite Element Method and Reissner's Mixed Theorem 122
A Plate Structural Capability for the Nonlinear Aeroelastic Analysis of Joined-Wing Configurations 121
RADARSAT-2 Stress Summary Report, Issue 1 120
Influence of Temperature Profile on the Accuracy of Classical and Refined Multilayered Plate 120
RADARSAT-2 Static Analysis Report, Issue 4 119
Structural Ritz-Based Simple-Polynomial Nonlinear Equivalent Approach – An Assessment 117
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 113
Elementi finiti piastra C[0-z] basati sull’equazione mista di Reissner 111
Structural Ritz-Based Simple-Polynomial Nonlinear Equivalent Approach – An Assessment 110
Multi-Theory FEM Architecture for the Generation of Advanced Mixed Shear Deformation Theories Based on the Generalized Unified Formulation for Composite Structures 107
The Structural Order Reduction Challenge in the Case of Geometrically Nonlinear Joined-Wing Configurations 106
Partially Zig-Zag Advanced Shear Deformation Theories Based on the Generalized Unified Formulation 102
Totale 12.128
Salva come PNG Salva come JPEG
Categoria #
all - tutte 34.077
article - articoli 18.192
book - libri 1.222
conference - conferenze 12.485
curatela - curatele 0
other - altro 1.786
patent - brevetti 0
selected - selezionate 0
volume - volumi 392
Totale 68.154
Salva come PNG Salva come JPEG


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/20201.017 0 0 0 158 139 121 84 187 137 121 52 18
2020/2021824 134 134 22 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
2024/2025328 19 246 58 5 0 0 0 0 0 0 0 0
Totale 12.128