PORTO @ Archivio Istituzionale della Ricerca

CARRERA, Erasmo
 Distribuzione geografica
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Continente #
NA - Nord America 138.543
EU - Europa 103.600
AS - Asia 71.568
SA - Sud America 5.572
AF - Africa 1.134
OC - Oceania 196
Continente sconosciuto - Info sul continente non disponibili 34
Totale 320.647
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Nazione #
US - Stati Uniti d'America 137.231
IT - Italia 22.998
SG - Singapore 19.806
DE - Germania 17.245
CN - Cina 16.716
FR - Francia 15.337
VN - Vietnam 14.986
GB - Regno Unito 14.608
NL - Olanda 9.938
RU - Federazione Russa 5.791
UA - Ucraina 5.542
BR - Brasile 4.342
KR - Corea 3.832
HK - Hong Kong 3.471
IN - India 2.676
TR - Turchia 2.675
IE - Irlanda 2.575
SE - Svezia 1.619
FI - Finlandia 1.556
CH - Svizzera 1.388
JP - Giappone 1.301
AT - Austria 1.096
BD - Bangladesh 954
TW - Taiwan 841
CA - Canada 810
BE - Belgio 709
ID - Indonesia 547
IR - Iran 538
IL - Israele 527
PH - Filippine 494
ES - Italia 464
IQ - Iraq 447
TH - Thailandia 419
BG - Bulgaria 402
AR - Argentina 395
PT - Portogallo 323
RO - Romania 305
MX - Messico 276
PL - Polonia 274
ZA - Sudafrica 261
MY - Malesia 255
AP - ???statistics.table.value.countryCode.AP??? 237
JO - Giordania 235
PE - Perù 191
PK - Pakistan 191
DZ - Algeria 181
GR - Grecia 181
AU - Australia 164
EG - Egitto 149
CL - Cile 144
EC - Ecuador 141
AE - Emirati Arabi Uniti 124
UZ - Uzbekistan 121
LU - Lussemburgo 119
VE - Venezuela 116
SA - Arabia Saudita 115
MA - Marocco 112
CO - Colombia 110
HR - Croazia 109
CZ - Repubblica Ceca 104
EU - Europa 102
EE - Estonia 77
KE - Kenya 76
TN - Tunisia 75
DK - Danimarca 65
SN - Senegal 64
NP - Nepal 63
PY - Paraguay 59
ET - Etiopia 52
AZ - Azerbaigian 50
BY - Bielorussia 50
LT - Lituania 50
JM - Giamaica 48
KZ - Kazakistan 46
HU - Ungheria 45
NG - Nigeria 44
OM - Oman 43
UY - Uruguay 39
AL - Albania 32
LB - Libano 32
TT - Trinidad e Tobago 29
NZ - Nuova Zelanda 28
MD - Moldavia 27
NO - Norvegia 26
AO - Angola 25
DO - Repubblica Dominicana 25
BH - Bahrain 24
RS - Serbia 23
BO - Bolivia 22
CI - Costa d'Avorio 20
PS - Palestinian Territory 19
SI - Slovenia 19
LV - Lettonia 18
SK - Slovacchia (Repubblica Slovacca) 18
CR - Costa Rica 17
HN - Honduras 17
PA - Panama 16
SY - Repubblica araba siriana 16
IS - Islanda 14
GE - Georgia 13
Totale 320.342
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Città #
Council Bluffs 25.837
Ashburn 23.412
Southend 12.022
Singapore 10.883
Seattle 7.560
Amsterdam 6.573
Turin 6.387
San Jose 6.265
Fairfield 6.132
Des Moines 5.559
Beijing 5.293
Chandler 4.663
Ann Arbor 4.296
Ho Chi Minh City 3.970
Hanoi 3.494
Princeton 3.385
Santa Clara 3.185
Woodbridge 2.870
Torino 2.822
Houston 2.812
Hong Kong 2.805
Jacksonville 2.707
Dublin 2.419
Wilmington 2.213
Cambridge 2.094
Berlin 2.044
San Ramon 2.025
Dallas 1.964
Izmir 1.720
Herkenbosch 1.707
Boardman 1.691
Seoul 1.657
Lauterbourg 1.363
Los Angeles 1.286
Frankfurt 1.250
Bern 1.219
Milan 1.215
San Donato Milanese 1.130
New York 1.123
Helsinki 1.099
Austin 1.084
Chicago 1.004
Shanghai 992
Buffalo 971
Zhengzhou 922
Hefei 901
Tokyo 746
San Francisco 704
North Bergen 629
Brussels 625
Da Nang 619
Haiphong 599
Baltimore 569
Groningen 554
Zaporozhye 539
Pennsylvania Furnace 523
Guangzhou 518
Vienna 516
Nuremberg 501
Aachen 492
Rome 483
Overberg 461
Hangzhou 456
Frankfurt am Main 454
Bologna 440
Jakarta 406
Fujian 397
Istanbul 394
São Paulo 392
Tel Aviv 391
Moscow 383
San Diego 381
Paris 367
Redwood City 360
Tongling 355
London 347
Mountain View 347
Lappeenranta 315
Saint Petersburg 310
Bari 304
Monopoli 301
Dearborn 284
Taipei 284
Atlanta 257
Fremont 243
Norwalk 241
Orem 232
Toronto 229
Padua 226
The Dalles 223
Miami 209
Malatya 205
Shenzhen 199
Columbus 197
Borgosesia 189
Munich 184
Baghdad 182
San Antonio 178
Chennai 176
Nanjing 176
Totale 208.317
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Nome #
Synergistic Use of CUF and Machine Learning for Structural Mechanics Problems 1.267
A class of two-dimensional theories for anisotropic multilayered plates analysis 1.234
CUF Multifield Models for Virtual Manufacturing of Composites 1.147
Numerical Analysis of Reinforced Concrete Beam using Carrera Unified Formulation based on a Concrete Damage Model 1.130
Parametric stability analyses of composite reinforced structures 1.116
Variable kinematics models for the analysis of thermal stresses in metallic and composite laminates 1.087
Global/local and coupled FEM-peridynamics models for localized progressive failure analysis 935
Fondamenti di Meccanica Strutturale per Allievi Ingegneri Aerospaziali 725
Appunti di costruzioni aeronautiche A 708
Analysis of laminated shells by a sinusoidalshear deformation theory and Radial Basis Functions collocation, accounting for through-the-thickness deformations. 706
Carrera Unified Formulation for Free-Vibration Analysis of Aircraft Structures 664
Some results on thermal stress of layered plates and shells by using Unified Formulation 661
Use of Lagrange multipliers to combine 1D variable kinematic finite elements 644
Advanced models for free vibration analysis of laminated beams with compact and thin-walled open/closed sections 641
Dynamic response of aerospace structures by means of refined beam theories 629
Preliminary vibroacoustic analysis about the use of metamaterials in the fuselage of a regional turboprop aircraft 620
Buckling of composite thin walled beams by refined theory 618
Effects of thickness stretching in functionally graded plates and shells 601
Performance of CUF approach to analyze the structural behavior of slender bodies 600
Guidelines and Recommendations on the Use of Higher OrderFinite Elements for Bending Analysis of Plates 599
Unified formulation of geometrically nonlinear refined beam theories 593
Thin-walled beams subjected to load factors and non-structural masses 591
Classical, refined and component-wise analysis of reinforced-shell structures 589
FINITE ELEMENT ANALYSIS OF STRUCTURES THROUGH UNIFIED FORMULATION 587
Analysis of laminated composites and sandwich structures by variable-kinematic MITC9 plate elements 586
Accurate static response of single- and multi-cell laminated box beams 586
Static and free vibration analysis of laminated beams by refined theory based on Chebyshev Polynomials 580
Refined Beam Elements with only Displacement Variables andPlate/Shell Capabilities 578
Variable kinematic plate elements coupled via Arlequin method 573
Multi-scale Modelling and Design of Composite Structures 562
Variable kinematic beam elements coupled via Arlequin method 562
Analysis of reinforced and thin-walled structures by multi-line refined 1D/beam models 551
Accurate response of wing structures to free-vibration, load factors and non-structural masses 549
Evaluation of the accuracy of classical beam FE models via locking-free hierarchically refined elements 546
Analysis of thick isotropic and cross-ply laminated plates by Generalized Differential Quadrature Method and a Unified Formulation. 544
Static aeroelastic response of wing-structures accounting for in-plane cross-section deformation 543
A finite element model using a unified formulation for the analysis of viscoelastic sandwich laminates. 542
Free vibration analysis of simply supported beams with solid and thin-walled cross-sections using higher-order theories based on displacement variables 541
Shell finite elements with different through-the-thickness kinematics for the linear analysis of cylindrical multilayered structures. 526
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. 524
Heat conduction and thermal stress analysis of laminated composites by a variable kinematic MITC9 shell element 522
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 301-329 520
Analysis of functionally graded material plates using triangular elements with cell-based smoothed discrete shear gap method 520
Higher-order theories and radial basis functions applied to free vibration analysis of thin-walled beams 519
Radial Basis Functions collocation for the bending and free vibration analysis of laminated plates using the Reissner-Mixed Variational Theorem. 516
Gasdynamics of rapid and explosive decompressions of pressurized aircraft including active venting 516
Thermal Stress Analysis of laminated structures by a variable kinematic MITC9 shell element 516
Advanced Beam Formulations for Free Vibration Analysis of Conventional and Joined Wings 513
Axiomatic/asymptotic technique applied to refined theories for piezoelectric plates 513
A static analysis of three-dimensional sandwich beam structures by hierarchical finite elements modelling 505
Analysis of composite plates by a unified formulation-cell based smoothed finite element method and field consistent elements 504
Finite element models with node-dependent kinematics for the analysis of composite beam structures 501
Analysis of composite plates through cell-based smoothed finite element and 4-noded mixed interpolation of tensorial components techniques 499
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. 498
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. 498
Finite Element Analysis of Free Vibration of the Delaminated Composite Plate with Variable Kinematic Multilayered Plate Elements 498
Evaluation of shear and membrane locking in refined hierarchical shell finite elements for laminated structures 496
Variable kinematic shell elements for the analysis of electro-mechanical problems 495
Hygrothermal analysis of multilayered composite plates by variable kinematic finite elements 494
Linearized buckling analysis of isotropic and composite beam-columns by Carrera Unified Formulation and Dynamic Stiffness Method 494
Refined shell finite elements based on RMVT and MITC for the analysis of laminated structures 493
Historical review of Zig-Zag theories for multilayered plates and shells, 491
Free Vibration Analysis of Laminated Beam by Polynomial, Trigonometric, Exponential and Zig-Zag Theories 490
Reissner's Mixed Variational Theorem toward MITC finite elements for multilayered plates. 489
Refined theories based on non-polynomial kinematics for the thermoelastic analysis of functionally graded plates 488
Accuracy of Refined Finite Elements for Laminated Plate Analysis 486
Extension of MITC to higher-order beam models and shear locking analysis for compact, thin-walled, and composite structures 484
Best theory diagrams for cross-ply composite plates using polynomial, trigonometric and exponential thickness expansions 482
Effect of different geometrically nonlinear strain measures on the static nonlinear response of isotropic and composite shells with constant curvature 482
Best Theory Diagrams for multilayered plates considering multifield analysis 480
Guest Editorial of MAMS Special Issue on Modeling and Analysis of Smart Structures 480
Simulation of shock wave impactdue to explosion on a flying, flexible aircraft 479
Component-wise Method Applied to Vibration of Wing Structures 476
Refined beam finite elements for static and dynamic analysis of hull structures 475
Influence of non-structural localized inertia on free vibration response of thin-walled structures by variable kinematic beam formulations 474
"Assessments of refined theoriesfor buckling analysis of laminated plates" 471
Micromechanics modeling of unit cells using CUF beam models and the Mechanics of Structure Genome 470
Velivolo con ali biplano e sistema propulsivo rotanti, tilt-prandtlplane 465
An assessment of Mixed and Classical Theories for thermal stress analysis of orthotropic Multilayered Plates 462
Analysis of laminated doubly-curved shells by alayerwise theory and radial basis functions collocation, accounting for through-the-thickness deformations 461
Recent developments on refined theories for beams with applications 461
A refined structural model for static aeroelastic response and divergence of metallic and composite wings 458
Multiobjective Best Theory Diagrams for cross-ply composite plates employing polynomial, zig-zag, trigonometric and exponential thickness expansions 457
A thermal stress finite element analysis of beam structures by hierarchical modelling 456
Non-linear dynamic analysis of a sandwich beam with pseudoelastic SMA hybrid composite faces based on higher order finite element theory 455
Acoustic analysis of passive metamaterial panels using the finite element method and homogenized properties 454
Large-deflection and post-buckling analyses of laminated composite beams by Carrera Unified Formulation 453
Structural Design of ELOTAC Full Composite, Inflatable UAV 452
Analysis of laminated beams via Unified Formulation and Legendre polynomial expansions 449
Shell elements with through-the-thickness variable kinematics for the analysis of laminated composite and sandwich structures 447
Guidelines and Recommendations to Construct Theories for Metallic and composite plates 446
Theories and Finite Elements for Multilayered Anisotropic, Composite Plates and Shells, 445
Coupling of hierarchical piezoelectric plate finite elements via Arlequin method 443
Cross-sectional mapping for refined beam elements with applications to shell-like structures 442
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 438
Component-Wise Analysis of Laminated Anisotropic Composites 434
Advanced models for static and dynamic analysis of wing and fuselage structures 433
Refined beam elements with arbitrary cross-section geometries 433
Static buckling of moderately thick, anisotropic, laminated and sandwich cylindrical shell panels 432
Free Vibrations of Damaged Aircraft Structures by Component-Wise Analysis 432
Totale 56.220
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Categoria #
all - tutte 890.403
article - articoli 507.608
book - libri 10.384
conference - conferenze 317.960
curatela - curatele 792
other - altro 35.154
patent - brevetti 1.019
selected - selezionate 0
volume - volumi 15.696
Totale 1.779.016
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021863 0 0 0 0 0 0 0 0 0 0 0 863
2021/202214.287 537 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
2025/202681.098 4.006 3.433 5.418 6.482 4.900 4.589 11.204 4.908 22.726 8.942 1.939 2.551
Totale 323.023