PORTO @ Archivio Istituzionale della Ricerca

CARRERA, Erasmo
 Distribuzione geografica
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Continente #
NA - Nord America 116.807
EU - Europa 84.412
AS - Asia 21.435
SA - Sud America 498
AF - Africa 429
OC - Oceania 153
Continente sconosciuto - Info sul continente non disponibili 27
Totale 223.761
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Nazione #
US - Stati Uniti d'America 116.245
IT - Italia 19.677
DE - Germania 16.147
GB - Regno Unito 13.957
FR - Francia 13.311
CN - Cina 9.793
UA - Ucraina 5.454
SG - Singapore 3.597
NL - Olanda 3.384
IE - Irlanda 2.517
TR - Turchia 2.498
RU - Federazione Russa 2.389
KR - Corea 1.573
SE - Svezia 1.557
CH - Svizzera 1.343
FI - Finlandia 1.137
IN - India 881
BE - Belgio 670
TW - Taiwan 544
CA - Canada 493
IR - Iran 428
AT - Austria 423
JP - Giappone 417
ID - Indonesia 401
BG - Bulgaria 386
HK - Hong Kong 376
RO - Romania 290
PT - Portogallo 261
BR - Brasile 243
AP - ???statistics.table.value.countryCode.AP??? 239
IL - Israele 215
ES - Italia 214
MY - Malesia 177
GR - Grecia 158
JO - Giordania 158
VN - Vietnam 144
PL - Polonia 131
AU - Australia 129
DZ - Algeria 129
LU - Lussemburgo 112
PE - Perù 103
EU - Europa 102
HR - Croazia 99
EG - Egitto 95
CZ - Repubblica Ceca 88
ZA - Sudafrica 83
CL - Cile 66
AE - Emirati Arabi Uniti 62
DK - Danimarca 58
AR - Argentina 56
MX - Messico 51
UZ - Uzbekistan 51
SN - Senegal 43
BY - Bielorussia 42
PH - Filippine 41
SA - Arabia Saudita 37
HU - Ungheria 34
EE - Estonia 33
NG - Nigeria 31
TH - Thailandia 30
PK - Pakistan 29
NZ - Nuova Zelanda 24
NO - Norvegia 23
LT - Lituania 19
KZ - Kazakistan 18
SI - Slovenia 16
MD - Moldavia 15
IQ - Iraq 13
CO - Colombia 12
SK - Slovacchia (Repubblica Slovacca) 12
CI - Costa d'Avorio 11
ET - Etiopia 11
RS - Serbia 11
EC - Ecuador 10
TN - Tunisia 10
BD - Bangladesh 8
LV - Lettonia 8
AL - Albania 7
LK - Sri Lanka 7
MA - Marocco 7
A2 - ???statistics.table.value.countryCode.A2??? 6
DO - Repubblica Dominicana 6
GE - Georgia 5
A1 - Anonimo 4
AZ - Azerbaigian 4
SC - Seychelles 4
LB - Libano 3
MK - Macedonia 3
PA - Panama 3
SM - San Marino 3
SY - Repubblica araba siriana 3
VE - Venezuela 3
CY - Cipro 2
GP - Guadalupe 2
GT - Guatemala 2
KG - Kirghizistan 2
KH - Cambogia 2
ME - Montenegro 2
OM - Oman 2
QA - Qatar 2
Totale 223.737
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Città #
Council Bluffs 25.158
Ashburn 20.132
Southend 12.038
Seattle 7.541
Fairfield 6.131
Des Moines 5.564
Turin 5.031
Chandler 4.662
Ann Arbor 4.298
Beijing 4.082
Princeton 3.388
Woodbridge 2.871
Santa Clara 2.862
Torino 2.823
Houston 2.766
Jacksonville 2.690
Singapore 2.659
Dublin 2.365
Wilmington 2.209
Cambridge 2.088
Berlin 2.038
San Ramon 2.027
Izmir 1.714
Herkenbosch 1.710
Boardman 1.638
Frankfurt 1.252
Bern 1.222
San Donato Milanese 1.132
Chicago 915
Helsinki 893
Shanghai 862
Zhengzhou 857
Milan 797
New York 738
Amsterdam 653
San Francisco 636
Brussels 607
Baltimore 559
Buffalo 555
Zaporozhye 539
Pennsylvania Furnace 523
Aachen 491
Overberg 462
Guangzhou 418
Hangzhou 409
Bologna 403
Fujian 397
San Diego 377
Jakarta 372
Redwood City 360
Vienna 349
Mountain View 348
Rome 346
Istanbul 332
Seoul 318
Saint Petersburg 310
Monopoli 301
Dearborn 284
London 257
Taipei 249
Fremont 240
Norwalk 240
Paris 237
Lappeenranta 223
Padua 213
Bari 211
Malatya 205
Miami 182
Borgosesia 178
Shenzhen 170
Toronto 170
Atlanta 168
Frankfurt am Main 168
San Antonio 167
Galati 163
Gilroy 161
Yubileyny 157
Moscow 156
Nanjing 156
Washington 143
Dallas 141
Andover 133
San Jose 130
Melun 128
Montréal 125
Redmond 122
Falls Church 120
Palermo 120
Cupertino 109
Putian 109
Naples 107
Porto 107
Phoenix 105
Austin 101
Las Vegas 97
Jinan 96
Sofia 96
Tel Aviv 96
Los Angeles 95
Hong Kong 92
Totale 155.945
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Nome #
A class of two-dimensional theories for anisotropic multilayered plates analysis 894
Fondamenti di Meccanica Strutturale per Allievi Ingegneri Aerospaziali 654
Appunti di costruzioni aeronautiche A 628
Analysis of laminated shells by a sinusoidalshear deformation theory and Radial Basis Functions collocation, accounting for through-the-thickness deformations. 621
Use of Lagrange multipliers to combine 1D variable kinematic finite elements 560
Some results on thermal stress of layered plates and shells by using Unified Formulation 544
Preliminary vibroacoustic analysis about the use of metamaterials in the fuselage of a regional turboprop aircraft 533
Carrera Unified Formulation for Free-Vibration Analysis of Aircraft Structures 533
Advanced models for free vibration analysis of laminated beams with compact and thin-walled open/closed sections 530
Buckling of composite thin walled beams by refined theory 527
Dynamic response of aerospace structures by means of refined beam theories 525
Effects of thickness stretching in functionally graded plates and shells 515
Performance of CUF approach to analyze the structural behavior of slender bodies 510
Thin-walled beams subjected to load factors and non-structural masses 507
Accurate static response of single- and multi-cell laminated box beams 507
Unified formulation of geometrically nonlinear refined beam theories 504
Refined Beam Elements with only Displacement Variables andPlate/Shell Capabilities 495
Guidelines and Recommendations on the Use of Higher OrderFinite Elements for Bending Analysis of Plates 490
Static and free vibration analysis of laminated beams by refined theory based on Chebyshev Polynomials 487
Analysis of laminated composites and sandwich structures by variable-kinematic MITC9 plate elements 478
Classical, refined and component-wise analysis of reinforced-shell structures 476
Variable kinematic plate elements coupled via Arlequin method 471
A finite element model using a unified formulation for the analysis of viscoelastic sandwich laminates. 467
Analysis of reinforced and thin-walled structures by multi-line refined 1D/beam models 466
Evaluation of the accuracy of classical beam FE models via locking-free hierarchically refined elements 464
Analysis of thick isotropic and cross-ply laminated plates by Generalized Differential Quadrature Method and a Unified Formulation. 462
Accurate response of wing structures to free-vibration, load factors and non-structural masses 461
Free vibration analysis of simply supported beams with solid and thin-walled cross-sections using higher-order theories based on displacement variables 455
Heat conduction and thermal stress analysis of laminated composites by a variable kinematic MITC9 shell element 453
Historical review of Zig-Zag theories for multilayered plates and shells, 449
Higher-order theories and radial basis functions applied to free vibration analysis of thin-walled beams 448
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 301-329 447
Analysis of composite plates by a unified formulation-cell based smoothed finite element method and field consistent elements 444
Analysis of composite plates through cell-based smoothed finite element and 4-noded mixed interpolation of tensorial components techniques 441
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. 439
Radial Basis Functions collocation for the bending and free vibration analysis of laminated plates using the Reissner-Mixed Variational Theorem. 438
Advanced Beam Formulations for Free Vibration Analysis of Conventional and Joined Wings 437
Shell finite elements with different through-the-thickness kinematics for the linear analysis of cylindrical multilayered structures. 433
Refined shell finite elements based on RMVT and MITC for the analysis of laminated structures 430
Static aeroelastic response of wing-structures accounting for in-plane cross-section deformation 429
Analysis of functionally graded material plates using triangular elements with cell-based smoothed discrete shear gap method 428
Reissner's Mixed Variational Theorem toward MITC finite elements for multilayered plates. 424
Gasdynamics of rapid and explosive decompressions of pressurized aircraft including active venting 423
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. 421
Best theory diagrams for cross-ply composite plates using polynomial, trigonometric and exponential thickness expansions 421
Axiomatic/asymptotic technique applied to refined theories for piezoelectric plates 421
Hygrothermal analysis of multilayered composite plates by variable kinematic finite elements 420
Accuracy of Refined Finite Elements for Laminated Plate Analysis 420
Finite Element Analysis of Free Vibration of the Delaminated Composite Plate with Variable Kinematic Multilayered Plate Elements 419
FINITE ELEMENT ANALYSIS OF STRUCTURES THROUGH UNIFIED FORMULATION 416
Variable kinematic shell elements for the analysis of electro-mechanical problems 412
Variable kinematic beam elements coupled via Arlequin method 411
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. 409
An assessment of Mixed and Classical Theories for thermal stress analysis of orthotropic Multilayered Plates 408
Finite element models with node-dependent kinematics for the analysis of composite beam structures 408
Component-wise Method Applied to Vibration of Wing Structures 408
Non-linear dynamic analysis of a sandwich beam with pseudoelastic SMA hybrid composite faces based on higher order finite element theory 408
Thermal Stress Analysis of laminated structures by a variable kinematic MITC9 shell element 406
Linearized buckling analysis of isotropic and composite beam-columns by Carrera Unified Formulation and Dynamic Stiffness Method 406
Micromechanics modeling of unit cells using CUF beam models and the Mechanics of Structure Genome 404
Influence of non-structural localized inertia on free vibration response of thin-walled structures by variable kinematic beam formulations 401
Free Vibration Analysis of Laminated Beam by Polynomial, Trigonometric, Exponential and Zig-Zag Theories 398
Refined beam finite elements for static and dynamic analysis of hull structures 397
Simulation of shock wave impactdue to explosion on a flying, flexible aircraft 396
Multi-scale Modelling and Design of Composite Structures 396
Recent developments on refined theories for beams with applications 395
Refined theories based on non-polynomial kinematics for the thermoelastic analysis of functionally graded plates 395
Analysis of laminated doubly-curved shells by alayerwise theory and radial basis functions collocation, accounting for through-the-thickness deformations 391
Guidelines and Recommendations to Construct Theories for Metallic and composite plates 389
Esercizi di Costruzioni Aeronautiche A 386
Guest Editorial of MAMS Special Issue on Modeling and Analysis of Smart Structures 384
Refined One-Dimensional Formulations for LaminatedStructure Analysis 382
Multiobjective Best Theory Diagrams for cross-ply composite plates employing polynomial, zig-zag, trigonometric and exponential thickness expansions 380
Structural Design of ELOTAC Full Composite, Inflatable UAV 378
Analysis of laminated beams via Unified Formulation and Legendre polynomial expansions 378
Best Theory Diagrams for multilayered plates considering multifield analysis 377
Shell elements with through-the-thickness variable kinematics for the analysis of laminated composite and sandwich structures 377
Computationally efficient, high-fidelity micromechanics framework using refined 1D models 371
A refined structural model for static aeroelastic response and divergence of metallic and composite wings 370
Hierarchical theories of structures based on Legendre polynomial expansions with finite element applications 369
Variable kinematic shell elements for composite laminates accounting for hygrothermal effects 368
Analysis of thin-walled structures with longitudinal and transversal stiffeners 368
The effects of boundary conditions on postbuckling of compressed, Symmetrically, laminated, thick plates 367
Cross-sectional mapping for refined beam elements with applications to shell-like structures 365
Analysis of laminated composites and sandwich structures by trigonometric, exponential and miscellaneous polynomials and a MITC9 plate element 365
Component-Wise Analysis of Laminated Anisotropic Composites 364
Velivolo con ali biplano e sistema propulsivo rotanti, tilt-prandtlplane 363
A static analysis of three-dimensional sandwich beam structures by hierarchical finite elements modelling 360
Comparison of various 1D, 2D and 3D FE models for the analysis of thin-walled box with transverse ribs subjected to load factors 359
ANALYSIS OF THIN-WALLED BEAMS VIA A ONE-DIMENSIONAL UNIFIED FORMULATION THROUGH A NAVIER-TYPE SOLUTION 358
Transverse Normal Stress Effects in Multilayered Plates 356
Aeroelastic Analysis of Composite Pinched Panels using Higher-Order Shell Elements 356
Analysis of thickness locking in classical, refined and mixed multilayered plate theories 354
Free Vibrations of Damaged Aircraft Structures by Component-Wise Analysis 353
Large-deflection and post-buckling analyses of laminated composite beams by Carrera Unified Formulation 352
Coupling of hierarchical piezoelectric plate finite elements via Arlequin method 352
Theories and Finite Elements for Multilayered Anisotropic, Composite Plates and Shells, 351
Free-vibration tailoring of single- and multi-bay laminated box structures by refined beam theories 349
Multi-scale Modelling of Sandwich Structures Using HierarchicalKinematics 348
A thermal stress finite element analysis of beam structures by hierarchical modelling 348
Totale 43.211
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Categoria #
all - tutte 622.682
article - articoli 364.256
book - libri 8.189
conference - conferenze 209.721
curatela - curatele 582
other - altro 26.549
patent - brevetti 759
selected - selezionate 0
volume - volumi 11.412
Totale 1.244.150
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/202012.057 0 0 0 0 0 1.895 1.482 2.737 2.461 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
2024/202513.229 662 3.391 1.524 3.095 2.706 1.851 0 0 0 0 0 0
Totale 225.833