PORTO @ Archivio Istituzionale della Ricerca

PAGANI, ALFONSO
 Distribuzione geografica
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Continente #
NA - Nord America 18374
EU - Europa 16585
AS - Asia 2859
SA - Sud America 91
AF - Africa 61
OC - Oceania 42
Continente sconosciuto - Info sul continente non disponibili 5
Totale 38017
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Nazione #
US - Stati Uniti d'America 18213
IT - Italia 4476
DE - Germania 3786
GB - Regno Unito 3005
FR - Francia 2034
CN - Cina 1547
UA - Ucraina 766
IE - Irlanda 691
TR - Turchia 439
NL - Olanda 356
SE - Svezia 344
BE - Belgio 263
KR - Corea 223
CA - Canada 156
RU - Federazione Russa 127
AT - Austria 120
IN - India 117
HK - Hong Kong 113
FI - Finlandia 98
PT - Portogallo 95
IR - Iran 89
JP - Giappone 87
TW - Taiwan 74
VN - Vietnam 66
ES - Italia 58
RO - Romania 58
BG - Bulgaria 54
MY - Malesia 43
JO - Giordania 41
AU - Australia 38
CH - Svizzera 35
PE - Perù 32
ZA - Sudafrica 30
IL - Israele 28
BR - Brasile 27
GR - Grecia 24
HR - Croazia 23
PL - Polonia 20
CZ - Repubblica Ceca 18
CL - Cile 16
LU - Lussemburgo 14
AR - Argentina 13
DK - Danimarca 12
EU - Europa 12
ID - Indonesia 10
EE - Estonia 9
PK - Pakistan 9
SG - Singapore 9
AE - Emirati Arabi Uniti 8
DZ - Algeria 8
HU - Ungheria 8
UZ - Uzbekistan 8
EG - Egitto 7
SN - Senegal 7
NO - Norvegia 6
BY - Bielorussia 5
ET - Etiopia 4
NZ - Nuova Zelanda 4
RS - Serbia 4
MX - Messico 3
A2 - ???statistics.table.value.countryCode.A2??? 2
AL - Albania 2
KZ - Kazakistan 2
MA - Marocco 2
SA - Arabia Saudita 2
SK - Slovacchia (Repubblica Slovacca) 2
BD - Bangladesh 1
BZ - Belize 1
CO - Colombia 1
CY - Cipro 1
EC - Ecuador 1
GE - Georgia 1
GT - Guatemala 1
IQ - Iraq 1
IS - Islanda 1
KH - Cambogia 1
NG - Nigeria 1
SC - Seychelles 1
TH - Thailandia 1
TN - Tunisia 1
UY - Uruguay 1
Totale 38017
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Città #
Ashburn 3785
Southend 2521
Chandler 1572
Ann Arbor 1553
Fairfield 1543
Torino 1130
Turin 1129
Seattle 1071
Princeton 924
Houston 882
Woodbridge 720
Dublin 648
Wilmington 581
Berlin 577
Cambridge 499
Beijing 475
Des Moines 414
Jacksonville 380
Izmir 353
San Ramon 273
San Francisco 272
Brussels 248
San Donato Milanese 243
Aachen 241
Fujian 176
Herkenbosch 176
Milan 174
Buffalo 164
Guangzhou 130
Frankfurt 127
Chicago 120
Hangzhou 111
Vienna 109
Boardman 108
Fremont 105
Norwalk 98
Bari 93
Helsinki 92
Dearborn 90
Shanghai 85
Zhengzhou 83
San Diego 81
Redwood City 77
Cupertino 73
New York 66
Montréal 63
Zaporozhye 61
Mountain View 60
Baltimore 58
Redmond 58
Seoul 57
Falls Church 53
Shenzhen 53
Sofia 53
Rome 51
Amsterdam 48
Dong Ket 48
Jinan 47
Phoenix 46
San Antonio 45
Nanjing 44
Nürnberg 43
Taipei 41
Lake Forest 40
Menlo Park 40
Putian 40
Pennsylvania Furnace 39
Saint Petersburg 39
Biancavilla 37
Dallas 36
Galati 36
San Jose 35
Malatya 34
Monopoli 34
Porto 33
Toronto 33
Columbus 32
Lima 32
Lansing 31
London 30
Paris 30
Hefei 28
Osaka 28
Andover 27
Austin 27
Muizenberg 27
Mcallen 26
Frankfurt am Main 24
Las Vegas 24
Kayseri 23
Sacramento 23
Seongnam 23
Victoria 23
Zagreb 23
Changsha 22
San Giuliano Milanese 22
San Mateo 22
Brooklyn 21
Fronteira 21
Basking Ridge 20
Totale 26386
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Nome #
Use of Lagrange multipliers to combine 1D variable kinematic finite elements 471
Dynamic response of aerospace structures by means of refined beam theories 445
Advanced models for free vibration analysis of laminated beams with compact and thin-walled open/closed sections 442
Thin-walled beams subjected to load factors and non-structural masses 422
Accurate static response of single- and multi-cell laminated box beams 412
Static and free vibration analysis of laminated beams by refined theory based on Chebyshev Polynomials 398
Analysis of laminated composites and sandwich structures by variable-kinematic MITC9 plate elements 390
Unified formulation of geometrically nonlinear refined beam theories 385
Component-wise models for static, dynamic and aeroelastic analyses of metallic and composite aerospace structures 381
Accurate response of wing structures to free-vibration, load factors and non-structural masses 376
Analysis of reinforced and thin-walled structures by multi-line refined 1D/beam models 370
Free vibration analysis of simply supported beams with solid and thin-walled cross-sections using higher-order theories based on displacement variables 370
Evaluation of the accuracy of classical beam FE models via locking-free hierarchically refined elements 367
Higher-order theories and radial basis functions applied to free vibration analysis of thin-walled beams 360
Preliminary vibroacoustic analysis about the use of metamaterials in the fuselage of a regional turboprop aircraft 346
Gasdynamics of rapid and explosive decompressions of pressurized aircraft including active venting 335
Velivolo con ali biplano e sistema propulsivo rotanti, tilt-prandtlplane 330
Linearized buckling analysis of isotropic and composite beam-columns by Carrera Unified Formulation and Dynamic Stiffness Method 320
Influence of non-structural localized inertia on free vibration response of thin-walled structures by variable kinematic beam formulations 319
Advanced models for static and dynamic analysis of wing and fuselage structures 315
Component-wise Method Applied to Vibration of Wing Structures 314
Refined beam finite elements for static and dynamic analysis of hull structures 311
Refined theories based on non-polynomial kinematics for the thermoelastic analysis of functionally graded plates 311
Buckling of Beams by Refined Theories and Dynamic Stiffness Method 309
Recent developments on refined theories for beams with applications 308
Shell elements with through-the-thickness variable kinematics for the analysis of laminated composite and sandwich structures 297
A Component-Wise Approach in Structural Analysis 290
Analysis of laminated beams via Unified Formulation and Legendre polynomial expansions 289
Hierarchical theories of structures based on Legendre polynomial expansions with finite element applications 287
Cross-sectional mapping for refined beam elements with applications to shell-like structures 286
Analysis of piezoelectric actuators under mechanical and electrical loads 282
Comparison of various 1D, 2D and 3D FE models for the analysis of thin-walled box with transverse ribs subjected to load factors 276
Classical, refined and component-wise analysis of reinforced-shell structures 275
Free-vibration tailoring of single- and multi-bay laminated box structures by refined beam theories 274
Large-deflection and post-buckling analyses of laminated composite beams by Carrera Unified Formulation 272
Free Vibrations of Damaged Aircraft Structures by Component-Wise Analysis 271
Static and dynamic analysis of aircraft structures by component-wise approach 269
Multi-line Enhanced Beam Model for the Analysis of Laminated Composite Structures 265
Extension of MITC to higher-order beam models and shear locking analysis for compact, thin-walled, and composite structures 264
Micromechanics modeling of unit cells using CUF beam models and the Mechanics of Structure Genome 262
Refined dynamic stiffness elements applied to free vibration analysis of generally laminated composite beams with arbitrary boundary conditions 257
Global-local analysis of laminated plates by node-dependent kinematic finite elements with variable ESL/LW capabilities 257
Free vibration analysis of civil engineering structures by component-wise models 256
1D multi-line refined models for the analysis of aerospace and civil engineering structures 255
Free vibration analysis of composite plates by higher-order 1D dynamic stiffness elements and experiments 255
Multilayered plate elements accounting for refined theories and node-dependent kinematics 247
Exact solutions for free vibration analysis of laminated, box and sandwich beams by refined layer-wise theory 246
Exact solutions for static analysis of laminated, box and sandwich beams by refined layer-wise theory 242
Refined 1D models for the analysis of reinforced-shell aeronautical structures including load factors effect 240
Exact dynamic stiffness elements based on one-dimensional higher-order theories for free vibration analysis of solid and thin-walled structures 240
Acoustic analysis of passive metamaterial panels using the finite element method and homogenized properties 238
Enhanced free vibration analysis of composite wing-box structures by one-dimensional Component-wise and dynamic stiffness formulations 236
Buckling analysis and vibrations of pre-stressed reinforced-shell structures by Component-Wise models 232
Flutter analysis by refined 1D dynamic stiffness elements and doublet lattice method 228
Analysis of laminated box beams using 1D Carrera Unified Formulation 225
Effect of different geometrically nonlinear strain measures on the static nonlinear response of isotropic and composite shells with constant curvature 221
Dynamic Response Analysis of Pressurized Cabins Subjected to Decompression Loadings 220
Micromechanics of periodically heterogeneous materials using higher-order beam theories and the mechanics of structure genome 215
Analysis of Laminated Structures by combined ESL-LW Variable Kinematics Plate Elements 213
Unified theory of one-dimensional structures and flows with applications to biomedical engineering and coupled problems 212
Application of aerospace structural models to marine engineering 211
Hierarchical and component-wise 1D models for fluid-structure interaction problems 210
On the effectiveness of Component-Wise models in analysing civil engineering framed structures 209
Effect of loading factors on the Analysis of Aeronautical Structures by Component-Wise Models 208
Exact Dynamic Stiffness Elements Using 1D Higher-Order Theories: Application to Laminated Composites 204
Component-Wise Method Applied to Static and Dynamic Analysis of Reinforced Structures with Applications to Aerospace, Civil Engineering and Marine Constructions 204
Finite beam elements based on Legendre polynomial expansions and node-dependent kinematics for the global-local analysis of composite structures 201
Vibration analysis of metallic and composite damaged structures by Component-Wise models 200
Variable Kinematics and Component-Wise Models for Failure Analysis of Composite Structures 199
A Variable Kinematic One-Dimensional Model for the Hygro-Mechanical Analysis of Composite Materials 198
One-dimensional CUF models for the analysis of laminated structures 198
Vibration of laminated composite beams via Carrera Unified Formulation and radial basis functions 198
Node-dependent kinematics, refined zig-zag and multi-line beam theories for the analysis of composite structures 196
Refined 1D finite elements for thin-walled curved structures 194
Multi-line-beam with variable kinematic models for the analysis of composite structures 192
Reissner's mixed variational theorem for layer-wise refined beam models based on the unified formulation 192
Comparison of dynamic stiffness and finite element methods in dynamics and aeroelastic response 191
Australasian research on Applied Mechanics and Aerospace - Preface 191
Advanced 1D models for fluid-structure interaction of viscous flows in thin-walled cylinders 188
Free vibrations of beams accounting for refined theories and radial basis functions 187
Component-Wise Method for Macro-Meso-Micro Modeling and Failure Analysis of Composite Structures 181
Analysis of curved composite structures through refined 1D finite elements with aerospace applications 180
Exact Dynamic Stiffness Elements Using 1D Higher-Order Theories: Application to Sandwich Beams 174
Dynamic Stiffness Analysis of Advanced Beams (DySAAB), EMBRAER technical report 171
Micro-, meso- and macro-scale analysis of composite laminates by unified theory of structures 167
Refined 1D finite elements for the analysis of secondary, primary and complete civil engineering structure 167
Accurate evaluation of failure indices of composite layered structures via various FE models 167
Free vibration analysis of complex wing structures by refined one-dimensional formulations 163
REFINED BEAM FINITE ELEMENT TO ANALYSE HULL STRUCTURES 163
Dynamic response of laminated and sandwich composite structures via 1D models based on Chebyshev polynomials 163
Low-Fidelity versus High-Fidelity Finite Element Models for Static, Dynamic and Aeroelastic Analyses of Composite Wings (LoHCW), EMBRAER technical report 158
Guest editorial of MAMS special issue on: Applications of Unified Formulation and advanced theories using several numerical approaches 157
ADVANCED NUMERICAL METHODS FOR FAILURE ANALYSIS OF METALLIC AND COMPOSITE AEROSPACE STRUCTURES 155
Unified beam theory with higher-order mapping capabilities 154
Component-wise models for the accurate dynamic and buckling analysis of composite wing structures 151
A component-wise approach to analyse a composite launcher structure subjected to loading factor 147
Vibrations of rotors by geometric nonlinear and higher-order beam models 145
A novel refined 1D model for the accurate stress analysis of composite structures with arbitrary curved sections 144
On the use of refined 1D structural models for reinforced cylinders with ends sealed 143
Nonlinear analysis of thin-walled beams with highly deformable sections 143
Totale 25165
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Categoria #
all - tutte 68909
article - articoli 36688
book - libri 0
conference - conferenze 27824
curatela - curatele 0
other - altro 2761
patent - brevetti 544
selected - selezionate 0
volume - volumi 520
Totale 137246
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2017/20181529 0000 00 00 607273428221
2018/20194187 219104436392 96314 24686 328501837628
2019/20204671 381281131580 610404 342587 537284371163
2020/20214587 481321173492 235320 307450 469591370378
2021/20225486 240500356287 515316 308271 3774476221247
2022/20236187 5731013347691 747838 840489 649000
Totale 38891