PORTO @ Archivio Istituzionale della Ricerca

CARRERA, Erasmo
 Distribuzione geografica
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Continente #
NA - Nord America 118.485
EU - Europa 86.649
AS - Asia 26.311
SA - Sud America 1.618
AF - Africa 489
OC - Oceania 158
Continente sconosciuto - Info sul continente non disponibili 30
Totale 233.740
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Nazione #
US - Stati Uniti d'America 117.865
IT - Italia 20.320
DE - Germania 16.576
GB - Regno Unito 14.097
FR - Francia 13.635
CN - Cina 10.138
SG - Singapore 7.217
UA - Ucraina 5.478
NL - Olanda 3.430
TR - Turchia 2.549
IE - Irlanda 2.532
RU - Federazione Russa 2.431
KR - Corea 1.821
SE - Svezia 1.559
CH - Svizzera 1.345
BR - Brasile 1.264
FI - Finlandia 1.151
IN - India 948
AT - Austria 904
BE - Belgio 673
TW - Taiwan 552
IL - Israele 506
CA - Canada 503
JP - Giappone 469
IR - Iran 451
HK - Hong Kong 422
ID - Indonesia 401
BG - Bulgaria 388
RO - Romania 290
PT - Portogallo 262
AP - ???statistics.table.value.countryCode.AP??? 239
ES - Italia 223
MY - Malesia 178
JO - Giordania 167
GR - Grecia 164
VN - Vietnam 144
DZ - Algeria 140
AU - Australia 134
PL - Polonia 134
PE - Perù 116
LU - Lussemburgo 112
EG - Egitto 102
EU - Europa 102
HR - Croazia 100
ZA - Sudafrica 93
CZ - Repubblica Ceca 90
MX - Messico 85
AR - Argentina 81
EE - Estonia 71
CL - Cile 68
UZ - Uzbekistan 68
AE - Emirati Arabi Uniti 65
DK - Danimarca 58
PK - Pakistan 45
SN - Senegal 45
PH - Filippine 44
BY - Bielorussia 42
SA - Arabia Saudita 40
HU - Ungheria 34
NG - Nigeria 31
TH - Thailandia 31
IQ - Iraq 30
BD - Bangladesh 27
EC - Ecuador 25
CO - Colombia 24
NO - Norvegia 24
NZ - Nuova Zelanda 24
KZ - Kazakistan 22
LT - Lituania 21
MA - Marocco 19
VE - Venezuela 18
SI - Slovenia 16
MD - Moldavia 15
TN - Tunisia 14
AZ - Azerbaigian 13
RS - Serbia 13
ET - Etiopia 12
SK - Slovacchia (Repubblica Slovacca) 12
CI - Costa d'Avorio 11
AL - Albania 10
DO - Repubblica Dominicana 10
KE - Kenya 10
UY - Uruguay 10
LV - Lettonia 8
LB - Libano 7
LK - Sri Lanka 7
OM - Oman 7
PY - Paraguay 7
A2 - ???statistics.table.value.countryCode.A2??? 6
KG - Kirghizistan 6
PA - Panama 6
GE - Georgia 5
JM - Giamaica 5
A1 - Anonimo 4
SC - Seychelles 4
BA - Bosnia-Erzegovina 3
BW - Botswana 3
KH - Cambogia 3
MK - Macedonia 3
NP - Nepal 3
Totale 233.690
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Città #
Council Bluffs 25.353
Ashburn 20.153
Southend 12.038
Seattle 7.545
Fairfield 6.131
Des Moines 5.564
Turin 5.387
Chandler 4.662
Ann Arbor 4.298
Beijing 4.106
Princeton 3.388
Singapore 2.872
Woodbridge 2.871
Santa Clara 2.867
Torino 2.823
Houston 2.766
Jacksonville 2.690
Dublin 2.379
Wilmington 2.209
Cambridge 2.088
Berlin 2.039
San Ramon 2.027
Izmir 1.714
Herkenbosch 1.710
Boardman 1.643
Frankfurt 1.252
Bern 1.222
San Donato Milanese 1.132
Austin 1.051
Chicago 918
Helsinki 894
Shanghai 876
Milan 870
Zhengzhou 862
New York 754
Amsterdam 657
San Francisco 637
Brussels 607
Baltimore 559
Buffalo 555
Zaporozhye 539
Pennsylvania Furnace 523
Aachen 491
Vienna 475
Overberg 462
Guangzhou 421
Bologna 414
Hangzhou 409
Fujian 397
Tel Aviv 386
Nuremberg 379
San Diego 377
Jakarta 372
Redwood City 360
Rome 351
Mountain View 348
Istanbul 345
Paris 328
Seoul 318
Saint Petersburg 310
Monopoli 301
Dearborn 284
London 258
Taipei 250
Fremont 240
Norwalk 240
Lappeenranta 232
Bari 217
Padua 213
Malatya 205
Borgosesia 189
Miami 182
Toronto 172
Frankfurt am Main 171
Shenzhen 171
San Antonio 169
Atlanta 168
Galati 163
Gilroy 161
Moscow 161
Nanjing 159
Yubileyny 157
Lauterbourg 151
Washington 143
Dallas 142
Portsmouth 134
Andover 133
San Jose 131
Melun 128
Palermo 126
Montréal 125
Hong Kong 122
Redmond 122
Falls Church 120
Naples 113
Los Angeles 112
Cupertino 109
Putian 109
Porto 107
Phoenix 106
Totale 158.870
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Nome #
A class of two-dimensional theories for anisotropic multilayered plates analysis 996
Fondamenti di Meccanica Strutturale per Allievi Ingegneri Aerospaziali 666
Appunti di costruzioni aeronautiche A 635
Analysis of laminated shells by a sinusoidalshear deformation theory and Radial Basis Functions collocation, accounting for through-the-thickness deformations. 629
Use of Lagrange multipliers to combine 1D variable kinematic finite elements 574
Some results on thermal stress of layered plates and shells by using Unified Formulation 556
Preliminary vibroacoustic analysis about the use of metamaterials in the fuselage of a regional turboprop aircraft 550
Carrera Unified Formulation for Free-Vibration Analysis of Aircraft Structures 546
Advanced models for free vibration analysis of laminated beams with compact and thin-walled open/closed sections 540
Buckling of composite thin walled beams by refined theory 538
Dynamic response of aerospace structures by means of refined beam theories 535
Effects of thickness stretching in functionally graded plates and shells 529
Performance of CUF approach to analyze the structural behavior of slender bodies 521
Unified formulation of geometrically nonlinear refined beam theories 517
Thin-walled beams subjected to load factors and non-structural masses 516
Accurate static response of single- and multi-cell laminated box beams 516
Refined Beam Elements with only Displacement Variables andPlate/Shell Capabilities 510
Guidelines and Recommendations on the Use of Higher OrderFinite Elements for Bending Analysis of Plates 510
Static and free vibration analysis of laminated beams by refined theory based on Chebyshev Polynomials 499
Classical, refined and component-wise analysis of reinforced-shell structures 489
Analysis of laminated composites and sandwich structures by variable-kinematic MITC9 plate elements 487
Variable kinematic plate elements coupled via Arlequin method 483
A finite element model using a unified formulation for the analysis of viscoelastic sandwich laminates. 477
Evaluation of the accuracy of classical beam FE models via locking-free hierarchically refined elements 477
Analysis of reinforced and thin-walled structures by multi-line refined 1D/beam models 476
Analysis of thick isotropic and cross-ply laminated plates by Generalized Differential Quadrature Method and a Unified Formulation. 470
Accurate response of wing structures to free-vibration, load factors and non-structural masses 470
Heat conduction and thermal stress analysis of laminated composites by a variable kinematic MITC9 shell element 464
Free vibration analysis of simply supported beams with solid and thin-walled cross-sections using higher-order theories based on displacement variables 463
Higher-order theories and radial basis functions applied to free vibration analysis of thin-walled beams 457
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 301-329 456
Historical review of Zig-Zag theories for multilayered plates and shells, 455
Analysis of composite plates by a unified formulation-cell based smoothed finite element method and field consistent elements 452
Static aeroelastic response of wing-structures accounting for in-plane cross-section deformation 450
Analysis of composite plates through cell-based smoothed finite element and 4-noded mixed interpolation of tensorial components techniques 450
Advanced Beam Formulations for Free Vibration Analysis of Conventional and Joined Wings 449
Shell finite elements with different through-the-thickness kinematics for the linear analysis of cylindrical multilayered structures. 449
Radial Basis Functions collocation for the bending and free vibration analysis of laminated plates using the Reissner-Mixed Variational Theorem. 449
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. 448
Analysis of functionally graded material plates using triangular elements with cell-based smoothed discrete shear gap method 441
Refined shell finite elements based on RMVT and MITC for the analysis of laminated structures 439
Gasdynamics of rapid and explosive decompressions of pressurized aircraft including active venting 437
Accuracy of Refined Finite Elements for Laminated Plate Analysis 437
Reissner's Mixed Variational Theorem toward MITC finite elements for multilayered plates. 433
Multi-scale Modelling and Design of Composite Structures 433
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. 432
FINITE ELEMENT ANALYSIS OF STRUCTURES THROUGH UNIFIED FORMULATION 432
Hygrothermal analysis of multilayered composite plates by variable kinematic finite elements 430
Axiomatic/asymptotic technique applied to refined theories for piezoelectric plates 430
Finite Element Analysis of Free Vibration of the Delaminated Composite Plate with Variable Kinematic Multilayered Plate Elements 429
Variable kinematic beam elements coupled via Arlequin method 428
Best theory diagrams for cross-ply composite plates using polynomial, trigonometric and exponential thickness expansions 427
Finite element models with node-dependent kinematics for the analysis of composite beam structures 426
Variable kinematic shell elements for the analysis of electro-mechanical problems 421
Thermal Stress Analysis of laminated structures by a variable kinematic MITC9 shell element 421
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. 420
Linearized buckling analysis of isotropic and composite beam-columns by Carrera Unified Formulation and Dynamic Stiffness Method 420
Component-wise Method Applied to Vibration of Wing Structures 418
An assessment of Mixed and Classical Theories for thermal stress analysis of orthotropic Multilayered Plates 417
Non-linear dynamic analysis of a sandwich beam with pseudoelastic SMA hybrid composite faces based on higher order finite element theory 417
Micromechanics modeling of unit cells using CUF beam models and the Mechanics of Structure Genome 416
Extension of MITC to higher-order beam models and shear locking analysis for compact, thin-walled, and composite structures 415
Simulation of shock wave impactdue to explosion on a flying, flexible aircraft 412
Influence of non-structural localized inertia on free vibration response of thin-walled structures by variable kinematic beam formulations 411
Free Vibration Analysis of Laminated Beam by Polynomial, Trigonometric, Exponential and Zig-Zag Theories 408
Refined beam finite elements for static and dynamic analysis of hull structures 406
Refined theories based on non-polynomial kinematics for the thermoelastic analysis of functionally graded plates 406
Recent developments on refined theories for beams with applications 405
A static analysis of three-dimensional sandwich beam structures by hierarchical finite elements modelling 400
Analysis of laminated doubly-curved shells by alayerwise theory and radial basis functions collocation, accounting for through-the-thickness deformations 398
Guidelines and Recommendations to Construct Theories for Metallic and composite plates 396
Acoustic analysis of passive metamaterial panels using the finite element method and homogenized properties 393
Guest Editorial of MAMS Special Issue on Modeling and Analysis of Smart Structures 390
Esercizi di Costruzioni Aeronautiche A 389
Multiobjective Best Theory Diagrams for cross-ply composite plates employing polynomial, zig-zag, trigonometric and exponential thickness expansions 388
Refined One-Dimensional Formulations for LaminatedStructure Analysis 388
Shell elements with through-the-thickness variable kinematics for the analysis of laminated composite and sandwich structures 387
Best Theory Diagrams for multilayered plates considering multifield analysis 386
Structural Design of ELOTAC Full Composite, Inflatable UAV 386
Analysis of laminated beams via Unified Formulation and Legendre polynomial expansions 386
Velivolo con ali biplano e sistema propulsivo rotanti, tilt-prandtlplane 385
A refined structural model for static aeroelastic response and divergence of metallic and composite wings 383
Effect of different geometrically nonlinear strain measures on the static nonlinear response of isotropic and composite shells with constant curvature 381
Computationally efficient, high-fidelity micromechanics framework using refined 1D models 379
Component-Wise Analysis of Laminated Anisotropic Composites 377
Cross-sectional mapping for refined beam elements with applications to shell-like structures 376
Variable kinematic shell elements for composite laminates accounting for hygrothermal effects 376
Hierarchical theories of structures based on Legendre polynomial expansions with finite element applications 375
The effects of boundary conditions on postbuckling of compressed, Symmetrically, laminated, thick plates 374
Analysis of laminated composites and sandwich structures by trigonometric, exponential and miscellaneous polynomials and a MITC9 plate element 374
Evaluation of shear and membrane locking in refined hierarchical shell finite elements for laminated structures 374
Analysis of thin-walled structures with longitudinal and transversal stiffeners 373
ANALYSIS OF THIN-WALLED BEAMS VIA A ONE-DIMENSIONAL UNIFIED FORMULATION THROUGH A NAVIER-TYPE SOLUTION 367
Comparison of various 1D, 2D and 3D FE models for the analysis of thin-walled box with transverse ribs subjected to load factors 365
Analysis of thickness locking in classical, refined and mixed multilayered plate theories 364
Theories and Finite Elements for Multilayered Anisotropic, Composite Plates and Shells, 364
Transverse Normal Stress Effects in Multilayered Plates 363
Aeroelastic Analysis of Composite Pinched Panels using Higher-Order Shell Elements 361
A thermal stress finite element analysis of beam structures by hierarchical modelling 361
Free Vibrations of Damaged Aircraft Structures by Component-Wise Analysis 361
Totale 44.541
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Categoria #
all - tutte 685.757
article - articoli 403.394
book - libri 8.560
conference - conferenze 231.033
curatela - curatele 630
other - altro 27.822
patent - brevetti 811
selected - selezionate 0
volume - volumi 12.146
Totale 1.370.153
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/20203.482 0 0 0 0 0 0 0 0 0 1.216 1.780 486
2020/202115.772 2.032 1.809 597 1.817 638 1.379 817 1.444 1.181 1.925 1.270 863
2021/202214.296 537 1.052 594 662 890 923 1.024 590 715 1.149 1.946 4.214
2022/202351.331 1.829 3.098 508 1.546 1.804 2.574 6.677 1.086 1.782 806 2.129 27.492
2023/20247.771 495 520 557 698 885 819 403 546 248 493 887 1.220
2024/202523.303 662 3.391 1.524 3.095 2.706 2.263 1.329 2.821 4.358 1.154 0 0
Totale 235.907