PORTO @ Archivio Istituzionale della Ricerca

DEMASI, LUCIANO
 Distribuzione geografica
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Continente #
NA - Nord America 5.790
EU - Europa 5.058
AS - Asia 823
SA - Sud America 19
AF - Africa 11
OC - Oceania 7
Continente sconosciuto - Info sul continente non disponibili 3
Totale 11.711
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Nazione #
US - Stati Uniti d'America 5.779
IT - Italia 1.092
GB - Regno Unito 1.009
DE - Germania 900
FR - Francia 693
UA - Ucraina 504
CN - Cina 425
RU - Federazione Russa 195
NL - Olanda 177
TR - Turchia 134
IE - Irlanda 122
CH - Svizzera 102
FI - Finlandia 75
JO - Giordania 64
SE - Svezia 61
KR - Corea 46
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
EE - Estonia 4
EG - Egitto 4
PT - Portogallo 4
AR - Argentina 3
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
SG - Singapore 1
TN - Tunisia 1
Totale 11.711
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Città #
Ashburn 1.472
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 122
Dublin 118
Izmir 115
Bern 95
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
Saint Petersburg 46
Baltimore 45
Rome 42
Hangzhou 38
Padua 32
San Diego 32
Monopoli 31
Vienna 30
Milan 28
Mountain View 28
Amsterdam 24
Guangzhou 23
Redwood City 23
New York 20
Moscow 18
London 16
Ningbo 14
Podenzano 13
Brussels 12
Malatya 12
Norwalk 12
Andover 11
Atlanta 11
Redmond 11
Tel Aviv 11
Boardman 10
Sedriano 10
Taipei 10
Bucharest 9
Modena 9
Kazan 8
Lappeenranta 8
Nanjing 8
Naples 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
Monza 6
Nanterre 6
Nichelino 6
Olbia 6
Salerno 6
Tapping 6
Vicenza 6
Zhitomir 6
Chengdu 5
Cotronei 5
Dearborn 5
Florence 5
Frankfurt Am Main 5
Melun 5
Miami 5
Palm Beach Gardens 5
Procida 5
San Mauro Torinese 5
Sunnyvale 5
Washington 5
Ankara 4
Astrakhan 4
Totale 8.098
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Nome #
Appunti di costruzioni aeronautiche A 588
A refined structural model for static aeroelastic response and divergence of metallic and composite wings 355
Improved response of unsymmetrically laminatedsandwich plates by using zig-zag functions 294
Improved bending analysis of sandwich plates using a zig-zag function 292
Vibration analysis of anisotropic simply supported plates by using variable kinematic and rayleigh-ritz method 288
Free vibration of sandwich plates and shells by using zig-zag function 281
Aerodinamica dei sistemi portanti chiusi: ala anulare ellittica 254
Studio aerodinamico di un'ala anulare ellittica 252
Vortex Lattice Method Coupled with Advanced One-Dimensional Structural Models 250
Classical and advanced Multilayered plate element based upon PVD and RMVT. Part II: Numerical implementations 245
2D, Quasi 3D and 3D Exact Solutions for Bending of Thick and Thin Sandwich Plates 238
Invariant formulation for the minimum induced drag conditions of nonplanar wing systems 232
On the developments of a Joined Wing Prandtlplane 222
Assess the Accuracy of the Variational Asymptotic Plate and Shell Analysis Using the Generalized Unified Formulation 207
An Invariant Finite Element Model for Composite Structures: the Generalized Unified Formulation 206
Flutter Failure Risk Assessment for Damage-Tolerant Composite Aircraft Structures 206
∞6mixed plate theories based on the Generalized Unified Formulation. Part I: Governing Equations 203
An Advanced Unified Aeroelastic Formulation based on 1D Higher-Order Finite Elements 202
Three-dimensional closed form solutions and ∞3 theories for orthotropic plates 194
∞6mixed plate theories based on the Generalized Unified Formulation. Part IV: Zig-Zag Theories 193
Two benchmarks to assess two-dimensional theories of Sandwich Composite Plates 191
∞6mixed plate theories based on the Generalized Unified Formulation. Part III: Advanced Mixed High Order Shear Deformation Theories 185
Assess the Accuracy of the Variational Asymptotic Plate and Shell Analysis (VAPAS) Using the Generalized Unified Formulation (GUF) 185
Aeroelastic coupling of Geometrically Nonlinear Structures and Linear Unsteady Aerodynamics – Two Formulations 181
Minimum Induced Drag Theorems for Nonplanar Systems and Closed Wings 178
An Improved Beam Formulation for AeroelasticApplications 178
Ala Anulare Ellittica: Distribuzione di Circolazione di Minima Resistenza Indotta 176
Classical and advanced Multilayered plate element based upon PVD and RMVT. Part I : Derivation of finite element matrices 175
“∞3 plate theories for thick and thin plates: the generalized unified formulation 174
Refined Multilayered Plate Elements Based on Murakami Zig-Zag Functions 174
∞6mixed plate theories based on the Generalized Unified Formulation. Par V: Results 174
A Reduced Order Nonlinear Aeroelastic Analysis of Joined Wings Based on the Proper Orthogonal Decomposition 172
Minimum induced drag theorems for multiwing systems 169
Dynamic Aeroelasticity of Structurally Nonlinear Configurations Using Linear Modally Reduced Aerodynamic Generalized Forces 168
Aeroelasticity of Structurally Nonlinear Lifting Surfaces Using Linear Modally Reduced Aerodynamic Generalized Forces 168
An Invariant Model for any Composite Plate Theory and FEM Applications: the Generalized Unified Formulation 167
Induced Drag Minimization: a Variational Approach Using the Acceleration Potential 164
Dynamic Aeroelasticity of Structurally Nonlinear Configurations Using Linear Modally Reduced Aerodynamic Generalized Forces 164
Quasi-3D Analysis of Free Vibration of Anisotropic Plates 159
On Two-Dimennional FEM simulatuon of Layered Plates, 159
An Assessment of Multilayered Finite Plate Elements in View of the C0z Requirements 159
Aerodynamic analysis of non-conventional wing configurations for aeroelastic applications 154
Aeroelastic Coupling of Geometrically Nonlinear Structures and Linear Unsteady Aerodynamics: Two Formulations 153
A Theoretical Investigation on the Conditions of Minimum Induced Drag of Closed Wing Systems and C-Wings 152
∞6mixed plate theories based on the Generalized Unified Formulation. Part II: Layerwise theories 152
Partially Zig-Zag Advanced Shear Deformation Theories Based on the Generalized Unified Formulation 152
Probabilistic Modeling of the Aeroelastic Life Cycle for Risk Evaluation of Composite Structures 147
Treatment of Stress Variables in Advanced Multilayered Plate Elements Based Upon Reissner’s Mixed Variational Theorem 147
Three-Dimensional Closed Form Solutions and Exact Thin Plate Theories for Isotropic Plates 147
Contributions to Joined-Wing Aeroelasticity 131
Exploratory Studies of Joined Wing Aeroelasticity 131
Dynamic Aeroelasticity of Coupling Full Order Geometrically Nonlinear Structurs and Full Order Linear Unsteady Aerodynamic – The Joined Wing Case 124
A Plate Structural Capability for the Nonlinear Aeroelastic Analysis of Joined-Wing Configurations 118
Sandwich Plate Analysis by Finite Element Method and Reissner's Mixed Theorem 118
RADARSAT-2 Stress Summary Report, Issue 1 116
Structural Ritz-Based Simple-Polynomial Nonlinear Equivalent Approach – An Assessment 114
RADARSAT-2 Static Analysis Report, Issue 4 114
Influence of Temperature Profile on the Accuracy of Classical and Refined Multilayered Plate 113
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 110
Elementi finiti piastra C[0-z] basati sull’equazione mista di Reissner 105
Structural Ritz-Based Simple-Polynomial Nonlinear Equivalent Approach – An Assessment 105
The Structural Order Reduction Challenge in the Case of Geometrically Nonlinear Joined-Wing Configurations 103
Partially Zig-Zag Advanced Shear Deformation Theories Based on the Generalized Unified Formulation 97
Multi-Theory FEM Architecture for the Generation of Advanced Mixed Shear Deformation Theories Based on the Generalized Unified Formulation for Composite Structures 94
Totale 11.719
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Categoria #
all - tutte 31.602
article - articoli 16.910
book - libri 1.153
conference - conferenze 11.557
curatela - curatele 0
other - altro 1.636
patent - brevetti 0
selected - selezionate 0
volume - volumi 346
Totale 63.204
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2018/2019460 0 0 0 0 0 0 0 0 0 0 262 198
2019/20201.254 117 79 41 158 139 121 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
2023/2024132 14 13 6 13 31 18 8 12 4 11 2 0
Totale 11.719