CINEFRA, MARIA
 Distribuzione geografica
Continente #
NA - Nord America 20.363
EU - Europa 15.296
AS - Asia 6.693
SA - Sud America 699
AF - Africa 169
OC - Oceania 33
Continente sconosciuto - Info sul continente non disponibili 6
Totale 43.259
Nazione #
US - Stati Uniti d'America 20.260
IT - Italia 3.501
DE - Germania 3.410
CN - Cina 2.681
FR - Francia 2.595
SG - Singapore 2.199
GB - Regno Unito 2.195
UA - Ucraina 952
NL - Olanda 574
BR - Brasile 569
RU - Federazione Russa 422
TR - Turchia 361
KR - Corea 343
IE - Irlanda 336
CH - Svizzera 225
AT - Austria 202
VN - Vietnam 188
HK - Hong Kong 180
FI - Finlandia 168
SE - Svezia 161
IN - India 151
JP - Giappone 115
ID - Indonesia 90
PT - Portogallo 82
TW - Taiwan 75
IL - Israele 69
IR - Iran 69
GR - Grecia 59
RO - Romania 57
BE - Belgio 56
CA - Canada 56
ES - Italia 56
ZA - Sudafrica 42
PL - Polonia 41
AR - Argentina 39
DZ - Algeria 37
MX - Messico 31
AP - ???statistics.table.value.countryCode.AP??? 29
JO - Giordania 27
BD - Bangladesh 26
BG - Bulgaria 26
EG - Egitto 26
AU - Australia 23
CL - Cile 23
EU - Europa 22
MY - Malesia 22
CZ - Repubblica Ceca 21
UZ - Uzbekistan 21
IQ - Iraq 19
PE - Perù 18
HR - Croazia 17
EC - Ecuador 15
LU - Lussemburgo 15
CO - Colombia 14
SA - Arabia Saudita 14
AE - Emirati Arabi Uniti 13
HU - Ungheria 13
SN - Senegal 12
KE - Kenya 11
ET - Etiopia 10
NZ - Nuova Zelanda 10
VE - Venezuela 9
BY - Bielorussia 8
PK - Pakistan 8
AL - Albania 7
MA - Marocco 7
PH - Filippine 7
TN - Tunisia 7
NO - Norvegia 6
SK - Slovacchia (Repubblica Slovacca) 6
UY - Uruguay 6
CI - Costa d'Avorio 5
KZ - Kazakistan 5
MD - Moldavia 5
NG - Nigeria 5
OM - Oman 5
DK - Danimarca 4
LT - Lituania 4
AZ - Azerbaigian 3
DO - Repubblica Dominicana 3
EE - Estonia 3
JM - Giamaica 3
NP - Nepal 3
PY - Paraguay 3
TH - Thailandia 3
A1 - Anonimo 2
BB - Barbados 2
GA - Gabon 2
GY - Guiana 2
LV - Lettonia 2
ME - Montenegro 2
ML - Mali 2
PA - Panama 2
QA - Qatar 2
A2 - ???statistics.table.value.countryCode.A2??? 1
AO - Angola 1
BA - Bosnia-Erzegovina 1
BN - Brunei Darussalam 1
BO - Bolivia 1
BS - Bahamas 1
Totale 43.243
Città #
Ashburn 3.663
Council Bluffs 3.320
Southend 1.810
Fairfield 1.243
Seattle 1.207
Singapore 1.107
Turin 879
Beijing 826
Des Moines 774
Chandler 615
Woodbridge 611
Ann Arbor 567
Cambridge 495
Torino 473
Jacksonville 459
Princeton 459
Houston 454
Santa Clara 430
Wilmington 404
San Ramon 363
Fujian 344
Dublin 308
Buffalo 305
Herkenbosch 297
Berlin 282
San Francisco 278
Dallas 262
Izmir 252
Boardman 250
Bern 209
Frankfurt 203
Chicago 171
San Donato Milanese 164
Zhengzhou 159
New York 153
Hong Kong 149
Helsinki 146
Milan 144
Paris 143
Shanghai 143
North Bergen 142
Austin 119
Lauterbourg 114
Amsterdam 111
Nuremberg 104
Baltimore 96
Pennsylvania Furnace 85
Gilroy 81
Hangzhou 81
Mountain View 79
Guangzhou 76
Jakarta 73
Saint Petersburg 71
Zaporozhye 71
Seoul 69
San Jose 68
Ho Chi Minh City 66
Los Angeles 66
London 65
San Diego 64
Overberg 61
Vienna 61
Bari 59
Hefei 58
Dearborn 55
Norwalk 52
São Paulo 49
Tel Aviv 49
Phoenix 48
Porto 48
Redwood City 48
Rome 47
Athens 46
Brussels 44
Monopoli 43
Frankfurt am Main 42
Shenzhen 41
Aachen 40
Hanoi 39
Las Vegas 38
Tokyo 37
Columbus 35
Melun 35
Osaka 35
Clearwater 31
Moscow 29
San Antonio 29
Wuhan 29
Fremont 28
Malatya 28
Madrid 27
Muizenberg 27
Putian 27
Andover 26
Munich 26
Istanbul 25
San Mauro Torinese 25
Taipei 25
Atlanta 24
Bologna 24
Totale 27.762
Nome #
Fondamenti di Meccanica Strutturale per Allievi Ingegneri Aerospaziali 684
Analysis of laminated shells by a sinusoidalshear deformation theory and Radial Basis Functions collocation, accounting for through-the-thickness deformations. 677
Some results on thermal stress of layered plates and shells by using Unified Formulation 614
Preliminary vibroacoustic analysis about the use of metamaterials in the fuselage of a regional turboprop aircraft 578
Effects of thickness stretching in functionally graded plates and shells 573
A finite element model using a unified formulation for the analysis of viscoelastic sandwich laminates. 518
FINITE ELEMENT ANALYSIS OF STRUCTURES THROUGH UNIFIED FORMULATION 516
Analysis of thick isotropic and cross-ply laminated plates by Generalized Differential Quadrature Method and a Unified Formulation. 511
A variable kinematic doubly-curved MITC9 shell element for the analysis of laminated composites 511
Shell finite elements with different through-the-thickness kinematics for the linear analysis of cylindrical multilayered structures. 500
Heat conduction and thermal stress analysis of laminated composites by a variable kinematic MITC9 shell element 493
Radial Basis Functions collocation for the bending and free vibration analysis of laminated plates using the Reissner-Mixed Variational Theorem. 488
Static, free vibration and buckling analysis of isotropic and sandwich functionally graded plates using a quasi-3D higher-order shear deformation theory and a meshless technique. 486
Analysis of composite plates by a unified formulation-cell based smoothed finite element method and field consistent elements 483
Analysis of functionally graded material plates using triangular elements with cell-based smoothed discrete shear gap method 483
Analysis of composite plates through cell-based smoothed finite element and 4-noded mixed interpolation of tensorial components techniques 476
Finite Element Analysis of Free Vibration of the Delaminated Composite Plate with Variable Kinematic Multilayered Plate Elements 474
Free vibration analysis of functionally graded shells by a higher-order shear deformation theory and radial basis functions collocation, accounting for through-the-thickness deformations. 471
Thermal Stress Analysis of laminated structures by a variable kinematic MITC9 shell element 471
Refined shell finite elements based on RMVT and MITC for the analysis of laminated structures 465
Axiomatic/asymptotic technique applied to refined theories for piezoelectric plates 463
Reissner's Mixed Variational Theorem toward MITC finite elements for multilayered plates. 462
Radial Basis Functions collocation and a Unified Formulation for bending, vibration and buckling analysis of laminated plates, according to a variation of Murakami’s zig-zag theory. 458
Variable kinematic shell elements for the analysis of electro-mechanical problems 456
Hygrothermal analysis of multilayered composite plates by variable kinematic finite elements 455
Best Theory Diagrams for multilayered plates considering multifield analysis 432
MITC9 shell elements based on refined theories for the analysis of isotropic cylindrical structures. 431
Guest Editorial of MAMS Special Issue on Modeling and Analysis of Smart Structures 430
Analysis of laminated doubly-curved shells by alayerwise theory and radial basis functions collocation, accounting for through-the-thickness deformations 428
Evaluation of shear and membrane locking in refined hierarchical shell finite elements for laminated structures 421
Acoustic analysis of passive metamaterial panels using the finite element method and homogenized properties 418
Velivolo con ali biplano e sistema propulsivo rotanti, tilt-prandtlplane 417
Radial basis functions-finite differences collocation and a Unified Formulation for bending, vibration and buckling analysis of laminated plates, according to Murakami’s zig-zag theory 407
Variable kinematic shell elements for composite laminates accounting for hygrothermal effects 402
Aeroelastic Analysis of Composite Pinched Panels using Higher-Order Shell Elements 398
Free-vibration analysis of laminated shells via refined MITC9 elements 389
Evaluation of various trough the thickness andcurvature approximations for free vibrationalanalysis of cylindrical and spherical shells. 381
Refined shell elements for the analysis of functionally graded structures 375
Variable kinematic models applied to free vibration analysis of functionally graded materials shells. 375
Bending and vibration of laminated plates by a layerwise meshless formulation. 369
Results on best theories for metallic and laminated shells including Layer-Wise models 356
Comparisons between 1D (Beam) and 2D (Plate/Shell) Finite Elements to Analyze ThinWalled Structures 356
A Finite Elements with Continue Transverse Electric Displacement for the Electro-Mechanical Analysis of Shell Structures 354
Evaluation of mixed theories for laminated plates through the axiomatic/asymptotic method 351
Refined Shell Elements for the Analysis of Multifield Problems in Multilayered Structures 350
MITC Technique Extended to Variable Kinematic Multilayered Plate Elements 346
FEM-Aided Structural Design of a Natural Fiber Composite Made Skiff 346
Accurate vibration analysis of multilayered plates made of functionally graded materials. 345
Thermo-mechanical analysis of functionally graded shells 344
Analysis of sandwich plates by Radial Basis Functions collocation, according to Murakami’s Zig-Zag theory 342
A radial basis functions solution for the analysis of laminated doubly-curved shells by a Reissner-Mixed Variational Theorem 340
A Finite Element with Continous Transverse Electric Displacement for Static and Free-Vibration Analysis of Piezoelectric Shells 339
Classical, refined, zig-zag and layer-wise models for laminated structures. 337
A quasi-3D hyperbolic shear deformation theory for the static and free vibration analysis of functionally graded plates 334
A quasi-3D sinusoidal shear deformation theory for the static and free vibration analysis of functionally graded plates 333
A Finite Elements Model embedding Piezoelectric Patches 333
Approximation of anisotropic multilayered plates through RMVT and MITC elements. 332
Refined shell elements for the analysis of functionally graded structures. 330
Buckling behaviour of cross-ply laminated plates by a higher-order shear deformation theory. 325
Analysis of Thick Isotropic and Cross-PlyLaminated Plates by Radial Basis Functionsand Unified Formulation 325
Refined shell elements for the thermo-mechanical analysis of multilayered structures 324
Bending of FGM plates by a sinusoidal plate formulation and collocation with radial basis functions 323
A layer-wise MITC9 finite element for the free-vibration analysis of plates with piezo-patches 320
MITC9 shell elements based on RMVT and CUF for the analysis of composite plates and shells 308
Free-Vibration Analysis of Delaminated Shells via Unified Formulation 307
Mixed LW/ESL models for the analysis of sandwich plates with composite faces 307
Refined shell models for the vibration analysis of multiwalled carbon nanotubes 302
SMART’13: Smart Materials and Structures 301
Buckling of Laminated and Functionally Graded Plates using Radial Basis Functions, 298
Static analysis of functionally graded sandwich plates according to a hyperbolic theory considering Zig-Zag and warping effects. 295
Radial Basis Functions-Differential Quadrature collocation and a Unified Formulation for bending, vibration and buckling analysis of laminated plates, according to Murakami’s zig-zag theory. 290
Classical, Refined, Zig-Zag, Layer-Wise Models and Best Theory Diagrams for Laminated Structures 287
An adaptable refinement approach for shell finite element models based on node-dependent kinematics 282
Two higher-order Zig-Zag theories for accurate bending, vibration and buckling response of laminated plates by Radial Basis Functions collocation and a Unified Formulation. 281
Effects of Thermo-Mechanical Loads on the Aeroelastic Instabilities of Metallic and Composite Panels 281
Buckling analysis of functionally graded sandwich plates using a new quasi-3D hyperbolic shear deformation theory and collocation with radial basis functions. 279
Refined and advanced shell models for the analysis of advanced structures. 279
Refined and advanced models for multilayered plates andshells embedding functionally graded material layers 279
Thermal Stress Analysis of Composite Beams, Plates and Shells 271
Thermomechanical Bending in Functionally Graded Material Shells 268
Hygro-thermal analysis of multilayered structures by means of MITC9 shell finite elements based on the CUF 260
Aeroelastic behavior of launcher thermal insulation panel, accounting for various aerodynamic and structural models 256
A Best Theory Diagram for Metallic and Laminated Shells 254
Influence of Zig-Zag and warping effects on buckling of functionally graded sandwich plates according to sinusoidal shear deformation theories 253
A Best Theory Diagram for Metallic andLaminated Shells 244
Influence of zig-zag and warping effects on the free vibration of functionally graded sandwich plates according to hyperbolic shear deformation theories. 244
Doubly-curved shell finite elements based on MITC-type technique and Unified Formulation for the analysis of multilayered structures 242
Hierarchic plate and shell theories with direct evaluation of transverse electric displacement 241
Variable Kinematics and Component-Wise Models for Failure Analysis of Composite Structures 238
Axiomatic/asymptotic evaluation of refined plate models for thermomechanical analysis 238
Aeroelastic Instabilities of FGM Panels under Thermo-Mechanical Loads 236
Analysis of viscoelastic sandwich laminates by a unified formulation 235
Benchmarking of commercial codes by refined shell finite element models in the analysis of composite structures 234
MITC9 Shell Finite Elements with Miscellaneous Through-the-thickness Approximating Functions for the Analysis of Laminated Structures 232
ADVANCED NUMERICAL METHODS FOR FAILURE ANALYSIS OF METALLIC AND COMPOSITE AEROSPACE STRUCTURES 231
Efficient numerical evaluation of transmission loss in homogenized acoustic metamaterials for aeronautical application 231
Isoparametric shell finite elements based on Unified Formulation 229
Analysis of functionally grades structures by radial basis functions using several theories under Carrera’s Unified Formulation 227
Use of molecular dynamic analysis to build appropriate structural models for CNTs 224
Effects of Thermo-Mechanical Loads on the Aeroelastic Instabilities of Metallic and Composite Panels 221
Totale 36.309
Categoria #
all - tutte 107.750
article - articoli 65.108
book - libri 2.964
conference - conferenze 33.484
curatela - curatele 717
other - altro 0
patent - brevetti 929
selected - selezionate 0
volume - volumi 3.761
Totale 214.713


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/20211.444 0 0 0 0 0 252 125 251 168 334 173 141
2021/20221.916 73 121 36 70 111 156 229 79 53 148 278 562
2022/20236.835 248 424 57 202 266 329 902 116 234 108 315 3.634
2023/20241.019 77 53 55 95 121 96 39 97 30 40 141 175
2024/20253.934 73 574 183 380 442 262 244 357 477 276 280 386
2025/20263.788 449 399 667 859 730 684 0 0 0 0 0 0
Totale 43.622