PORTO @ Archivio Istituzionale della Ricerca

CARRERA, Erasmo
 Distribuzione geografica
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Continente #
NA - Nord America 140.604
EU - Europa 104.396
AS - Asia 72.403
SA - Sud America 5.774
Continente sconosciuto - Info sul continente non disponibili 2.488
AF - Africa 1.143
OC - Oceania 199
Totale 327.007
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Nazione #
US - Stati Uniti d'America 139.095
IT - Italia 23.606
SG - Singapore 20.107
DE - Germania 17.266
CN - Cina 16.752
FR - Francia 15.374
VN - Vietnam 15.006
GB - Regno Unito 14.623
NL - Olanda 9.951
RU - Federazione Russa 5.792
UA - Ucraina 5.549
BR - Brasile 4.432
KR - Corea 3.836
HK - Hong Kong 3.485
IN - India 2.695
TR - Turchia 2.683
IE - Irlanda 2.577
SE - Svezia 1.629
FI - Finlandia 1.559
CH - Svizzera 1.389
BD - Bangladesh 1.333
JP - Giappone 1.306
AT - Austria 1.097
CA - Canada 880
TW - Taiwan 843
BE - Belgio 712
ID - Indonesia 553
IR - Iran 553
IL - Israele 527
PH - Filippine 495
ES - Italia 493
IQ - Iraq 447
TH - Thailandia 428
AR - Argentina 415
BG - Bulgaria 403
PT - Portogallo 336
RO - Romania 311
MX - Messico 289
PL - Polonia 279
ZA - Sudafrica 261
MY - Malesia 258
AP - ???statistics.table.value.countryCode.AP??? 237
JO - Giordania 235
PE - Perù 195
PK - Pakistan 192
DZ - Algeria 182
GR - Grecia 181
AU - Australia 167
EC - Ecuador 165
CO - Colombia 152
EG - Egitto 150
CL - Cile 149
VE - Venezuela 125
AE - Emirati Arabi Uniti 124
UZ - Uzbekistan 122
LU - Lussemburgo 119
SA - Arabia Saudita 119
MA - Marocco 115
HR - Croazia 109
CZ - Repubblica Ceca 106
EU - Europa 102
EE - Estonia 77
KE - Kenya 76
TN - Tunisia 75
JM - Giamaica 70
DK - Danimarca 67
NP - Nepal 65
SN - Senegal 64
PY - Paraguay 62
ET - Etiopia 53
LT - Lituania 51
AZ - Azerbaigian 50
BY - Bielorussia 50
HU - Ungheria 50
KZ - Kazakistan 46
NG - Nigeria 45
OM - Oman 44
UY - Uruguay 42
CR - Costa Rica 40
TT - Trinidad e Tobago 37
AL - Albania 33
HN - Honduras 32
LB - Libano 32
NO - Norvegia 29
NZ - Nuova Zelanda 28
MD - Moldavia 27
DO - Repubblica Dominicana 26
AO - Angola 25
BH - Bahrain 24
BO - Bolivia 23
GT - Guatemala 23
RS - Serbia 23
NI - Nicaragua 22
CI - Costa d'Avorio 20
SI - Slovenia 20
LV - Lettonia 19
PS - Palestinian Territory 19
SK - Slovacchia (Repubblica Slovacca) 18
PA - Panama 16
PR - Porto Rico 16
Totale 324.210
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Città #
Council Bluffs 25.858
Ashburn 23.836
Southend 12.022
Singapore 10.894
Seattle 7.566
Amsterdam 6.573
Turin 6.541
San Jose 6.355
Fairfield 6.132
Des Moines 5.559
Beijing 5.298
Chandler 4.663
Ann Arbor 4.296
Ho Chi Minh City 3.974
Hanoi 3.503
Princeton 3.385
Santa Clara 3.317
Woodbridge 2.870
Torino 2.822
Hong Kong 2.818
Houston 2.815
Jacksonville 2.712
Dublin 2.420
Wilmington 2.218
Cambridge 2.094
Berlin 2.047
San Ramon 2.025
Dallas 1.986
Izmir 1.722
Herkenbosch 1.707
Boardman 1.694
Seoul 1.658
Lauterbourg 1.363
Los Angeles 1.350
Milan 1.318
Frankfurt 1.250
Bern 1.219
New York 1.151
San Donato Milanese 1.130
Helsinki 1.099
Austin 1.085
Chicago 1.024
Shanghai 995
Buffalo 981
Zhengzhou 922
Hefei 901
Tokyo 749
San Francisco 706
North Bergen 629
Brussels 627
Da Nang 621
Haiphong 599
Baltimore 577
Rome 558
Groningen 554
Zaporozhye 539
Pennsylvania Furnace 523
Guangzhou 518
Vienna 516
Nuremberg 501
Aachen 492
Overberg 461
Frankfurt am Main 458
Hangzhou 458
Bologna 442
Jakarta 406
São Paulo 401
Fujian 397
Istanbul 395
Tel Aviv 391
San Diego 384
Moscow 383
Paris 368
Redwood City 360
Tongling 355
London 351
Mountain View 347
Bari 316
Lappeenranta 315
Saint Petersburg 310
Monopoli 301
Taipei 285
Dearborn 284
The Dalles 280
Atlanta 270
Fremont 243
Norwalk 242
Toronto 233
Orem 232
Padua 228
Miami 215
Malatya 205
Shenzhen 200
Columbus 199
Borgosesia 189
Munich 189
Naples 189
Baghdad 182
Phoenix 182
San Antonio 180
Totale 209.703
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Nome #
Synergistic Use of CUF and Machine Learning for Structural Mechanics Problems 1.277
A class of two-dimensional theories for anisotropic multilayered plates analysis 1.255
Numerical Analysis of Reinforced Concrete Beam using Carrera Unified Formulation based on a Concrete Damage Model 1.160
CUF Multifield Models for Virtual Manufacturing of Composites 1.152
Parametric stability analyses of composite reinforced structures 1.118
Variable kinematics models for the analysis of thermal stresses in metallic and composite laminates 1.089
Global/local and coupled FEM-peridynamics models for localized progressive failure analysis 938
Fondamenti di Meccanica Strutturale per Allievi Ingegneri Aerospaziali 728
Appunti di costruzioni aeronautiche A 712
Analysis of laminated shells by a sinusoidalshear deformation theory and Radial Basis Functions collocation, accounting for through-the-thickness deformations. 711
Carrera Unified Formulation for Free-Vibration Analysis of Aircraft Structures 680
Some results on thermal stress of layered plates and shells by using Unified Formulation 665
Advanced models for free vibration analysis of laminated beams with compact and thin-walled open/closed sections 651
Use of Lagrange multipliers to combine 1D variable kinematic finite elements 646
Dynamic response of aerospace structures by means of refined beam theories 632
Preliminary vibroacoustic analysis about the use of metamaterials in the fuselage of a regional turboprop aircraft 623
Buckling of composite thin walled beams by refined theory 623
Effects of thickness stretching in functionally graded plates and shells 609
Guidelines and Recommendations on the Use of Higher OrderFinite Elements for Bending Analysis of Plates 605
Classical, refined and component-wise analysis of reinforced-shell structures 604
Performance of CUF approach to analyze the structural behavior of slender bodies 603
Thin-walled beams subjected to load factors and non-structural masses 600
FINITE ELEMENT ANALYSIS OF STRUCTURES THROUGH UNIFIED FORMULATION 597
Unified formulation of geometrically nonlinear refined beam theories 595
Accurate static response of single- and multi-cell laminated box beams 589
Analysis of laminated composites and sandwich structures by variable-kinematic MITC9 plate elements 588
Refined Beam Elements with only Displacement Variables andPlate/Shell Capabilities 581
Static and free vibration analysis of laminated beams by refined theory based on Chebyshev Polynomials 581
Hygrothermal analysis of multilayered composite plates by variable kinematic finite elements 578
Variable kinematic plate elements coupled via Arlequin method 577
Multi-scale Modelling and Design of Composite Structures 577
Variable kinematic beam elements coupled via Arlequin method 565
Accurate response of wing structures to free-vibration, load factors and non-structural masses 554
Analysis of reinforced and thin-walled structures by multi-line refined 1D/beam models 553
Evaluation of the accuracy of classical beam FE models via locking-free hierarchically refined elements 551
Analysis of thick isotropic and cross-ply laminated plates by Generalized Differential Quadrature Method and a Unified Formulation. 548
A finite element model using a unified formulation for the analysis of viscoelastic sandwich laminates. 547
Static aeroelastic response of wing-structures accounting for in-plane cross-section deformation 545
Free vibration analysis of simply supported beams with solid and thin-walled cross-sections using higher-order theories based on displacement variables 545
Shell finite elements with different through-the-thickness kinematics for the linear analysis of cylindrical multilayered structures. 533
Heat conduction and thermal stress analysis of laminated composites by a variable kinematic MITC9 shell element 533
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. 529
Developments, Ideas and Evaluations based upon the Reissner's Mixed Variational Theorem in the Modeling of Multilayered Plates and Shells, Applied Mechanics Review, vol 54, pp 301-329 525
Thermal Stress Analysis of laminated structures by a variable kinematic MITC9 shell element 524
Radial Basis Functions collocation for the bending and free vibration analysis of laminated plates using the Reissner-Mixed Variational Theorem. 523
Analysis of functionally graded material plates using triangular elements with cell-based smoothed discrete shear gap method 522
Higher-order theories and radial basis functions applied to free vibration analysis of thin-walled beams 521
Gasdynamics of rapid and explosive decompressions of pressurized aircraft including active venting 521
Axiomatic/asymptotic technique applied to refined theories for piezoelectric plates 518
Advanced Beam Formulations for Free Vibration Analysis of Conventional and Joined Wings 516
Analysis of composite plates by a unified formulation-cell based smoothed finite element method and field consistent elements 508
Finite element models with node-dependent kinematics for the analysis of composite beam structures 507
A static analysis of three-dimensional sandwich beam structures by hierarchical finite elements modelling 506
Finite Element Analysis of Free Vibration of the Delaminated Composite Plate with Variable Kinematic Multilayered Plate Elements 506
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. 504
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. 502
Variable kinematic shell elements for the analysis of electro-mechanical problems 502
Analysis of composite plates through cell-based smoothed finite element and 4-noded mixed interpolation of tensorial components techniques 502
Refined shell finite elements based on RMVT and MITC for the analysis of laminated structures 500
Linearized buckling analysis of isotropic and composite beam-columns by Carrera Unified Formulation and Dynamic Stiffness Method 499
Evaluation of shear and membrane locking in refined hierarchical shell finite elements for laminated structures 498
Refined theories based on non-polynomial kinematics for the thermoelastic analysis of functionally graded plates 497
Historical review of Zig-Zag theories for multilayered plates and shells, 496
Free Vibration Analysis of Laminated Beam by Polynomial, Trigonometric, Exponential and Zig-Zag Theories 494
Reissner's Mixed Variational Theorem toward MITC finite elements for multilayered plates. 491
Best theory diagrams for cross-ply composite plates using polynomial, trigonometric and exponential thickness expansions 488
Guest Editorial of MAMS Special Issue on Modeling and Analysis of Smart Structures 486
Extension of MITC to higher-order beam models and shear locking analysis for compact, thin-walled, and composite structures 486
Accuracy of Refined Finite Elements for Laminated Plate Analysis 486
Best Theory Diagrams for multilayered plates considering multifield analysis 484
Effect of different geometrically nonlinear strain measures on the static nonlinear response of isotropic and composite shells with constant curvature 484
Simulation of shock wave impactdue to explosion on a flying, flexible aircraft 482
"Assessments of refined theoriesfor buckling analysis of laminated plates" 481
Refined beam finite elements for static and dynamic analysis of hull structures 479
Influence of non-structural localized inertia on free vibration response of thin-walled structures by variable kinematic beam formulations 478
Analysis of laminated doubly-curved shells by alayerwise theory and radial basis functions collocation, accounting for through-the-thickness deformations 477
Component-wise Method Applied to Vibration of Wing Structures 477
A thermal stress finite element analysis of beam structures by hierarchical modelling 474
Micromechanics modeling of unit cells using CUF beam models and the Mechanics of Structure Genome 473
Velivolo con ali biplano e sistema propulsivo rotanti, tilt-prandtlplane 467
Recent developments on refined theories for beams with applications 466
An assessment of Mixed and Classical Theories for thermal stress analysis of orthotropic Multilayered Plates 465
Guidelines and Recommendations to Construct Theories for Metallic and composite plates 463
Multiobjective Best Theory Diagrams for cross-ply composite plates employing polynomial, zig-zag, trigonometric and exponential thickness expansions 461
A refined structural model for static aeroelastic response and divergence of metallic and composite wings 461
Large-deflection and post-buckling analyses of laminated composite beams by Carrera Unified Formulation 459
Structural Design of ELOTAC Full Composite, Inflatable UAV 457
Analysis of laminated beams via Unified Formulation and Legendre polynomial expansions 457
Acoustic analysis of passive metamaterial panels using the finite element method and homogenized properties 456
Non-linear dynamic analysis of a sandwich beam with pseudoelastic SMA hybrid composite faces based on higher order finite element theory 456
Theories and Finite Elements for Multilayered Anisotropic, Composite Plates and Shells, 451
Shell elements with through-the-thickness variable kinematics for the analysis of laminated composite and sandwich structures 449
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 446
Coupling of hierarchical piezoelectric plate finite elements via Arlequin method 446
Cross-sectional mapping for refined beam elements with applications to shell-like structures 445
Variable kinematic shell elements for composite laminates accounting for hygrothermal effects 442
Static buckling of moderately thick, anisotropic, laminated and sandwich cylindrical shell panels 441
Advanced models for static and dynamic analysis of wing and fuselage structures 439
Bending and vibration of laminated plates by a layerwise meshless formulation. 437
Free Vibrations of Damaged Aircraft Structures by Component-Wise Analysis 437
Totale 56.865
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Categoria #
all - tutte 912.698
article - articoli 518.657
book - libri 10.556
conference - conferenze 327.856
curatela - curatele 820
other - altro 35.883
patent - brevetti 1.036
selected - selezionate 0
volume - volumi 16.045
Totale 1.823.551
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2021/202213.750 0 1.051 594 660 890 923 1.024 590 715 1.147 1.944 4.212
2022/202351.295 1.827 3.096 508 1.546 1.802 2.571 6.668 1.085 1.781 798 2.126 27.487
2023/20247.764 495 518 557 698 884 818 403 546 248 493 885 1.219
2024/202529.533 660 3.388 1.524 3.090 2.705 2.261 1.322 2.814 4.323 1.889 2.188 3.369
2025/202682.091 4.006 3.433 5.418 6.482 4.900 4.589 11.204 4.908 22.726 8.942 1.939 3.544
2026/20272.991 2.635 356 0 0 0 0 0 0 0 0 0 0
Totale 327.007