PORTO @ Archivio Istituzionale della Ricerca

CARRERA, Erasmo
 Distribuzione geografica
Salva come PNG Salva come JPEG
Continente #
NA - Nord America 111.963
EU - Europa 82.260
AS - Asia 17.919
AF - Africa 399
SA - Sud America 393
OC - Oceania 149
Continente sconosciuto - Info sul continente non disponibili 27
Totale 213.110
Salva come PNG Salva come JPEG
Nazione #
US - Stati Uniti d'America 111.434
IT - Italia 18.912
DE - Germania 16.035
GB - Regno Unito 13.910
FR - Francia 13.212
CN - Cina 9.445
UA - Ucraina 5.457
NL - Olanda 3.350
IE - Irlanda 2.511
TR - Turchia 2.195
SG - Singapore 1.790
SE - Svezia 1.555
RU - Federazione Russa 1.484
CH - Svizzera 1.339
KR - Corea 1.119
FI - Finlandia 1.097
IN - India 813
BE - Belgio 590
TW - Taiwan 541
CA - Canada 472
IR - Iran 412
AT - Austria 409
JP - Giappone 404
BG - Bulgaria 386
RO - Romania 289
HK - Hong Kong 278
PT - Portogallo 256
AP - ???statistics.table.value.countryCode.AP??? 239
IL - Israele 214
ES - Italia 209
MY - Malesia 176
JO - Giordania 156
GR - Grecia 154
BR - Brasile 147
VN - Vietnam 136
AU - Australia 127
PL - Polonia 126
DZ - Algeria 118
LU - Lussemburgo 108
PE - Perù 103
EU - Europa 102
HR - Croazia 97
EG - Egitto 92
CZ - Repubblica Ceca 85
ZA - Sudafrica 78
CL - Cile 65
AE - Emirati Arabi Uniti 59
DK - Danimarca 57
AR - Argentina 55
UZ - Uzbekistan 48
ID - Indonesia 44
MX - Messico 43
BY - Bielorussia 42
SN - Senegal 42
SA - Arabia Saudita 37
EE - Estonia 33
HU - Ungheria 33
PH - Filippine 32
NG - Nigeria 31
TH - Thailandia 27
PK - Pakistan 25
NO - Norvegia 22
NZ - Nuova Zelanda 22
KZ - Kazakistan 17
SI - Slovenia 16
MD - Moldavia 14
CO - Colombia 12
SK - Slovacchia (Repubblica Slovacca) 12
CI - Costa d'Avorio 11
ET - Etiopia 11
RS - Serbia 11
IQ - Iraq 9
AL - Albania 7
BD - Bangladesh 7
EC - Ecuador 7
LT - Lituania 7
A2 - ???statistics.table.value.countryCode.A2??? 6
LV - Lettonia 6
TN - Tunisia 6
GE - Georgia 5
LK - Sri Lanka 5
MA - Marocco 5
A1 - Anonimo 4
DO - Repubblica Dominicana 4
AZ - Azerbaigian 3
LB - Libano 3
MK - Macedonia 3
SC - Seychelles 3
SM - San Marino 3
SY - Repubblica araba siriana 3
GP - Guadalupe 2
GT - Guatemala 2
ME - Montenegro 2
QA - Qatar 2
VE - Venezuela 2
VG - Isole Vergini Britanniche 2
BA - Bosnia-Erzegovina 1
BS - Bahamas 1
BZ - Belize 1
CY - Cipro 1
Totale 213.095
Salva come PNG Salva come JPEG
Città #
Council Bluffs 25.206
Ashburn 19.884
Southend 12.052
Seattle 7.542
Fairfield 6.132
Des Moines 5.567
Turin 4.714
Chandler 4.665
Ann Arbor 4.300
Beijing 4.077
Princeton 3.391
Woodbridge 2.871
Torino 2.826
Houston 2.766
Jacksonville 2.695
Dublin 2.359
Wilmington 2.209
Cambridge 2.089
Berlin 2.040
San Ramon 2.029
Izmir 1.719
Herkenbosch 1.713
Frankfurt 1.254
Bern 1.220
Singapore 1.204
San Donato Milanese 1.133
Chicago 914
Helsinki 868
Zhengzhou 857
Shanghai 848
New York 723
Milan 703
Amsterdam 646
San Francisco 636
Baltimore 560
Buffalo 555
Zaporozhye 540
Boardman 533
Brussels 527
Pennsylvania Furnace 524
Aachen 491
Overberg 463
Guangzhou 410
Hangzhou 407
Bologna 403
Fujian 397
San Diego 378
Redwood City 360
Mountain View 350
Vienna 339
Seoul 318
Rome 314
Saint Petersburg 310
Monopoli 301
Dearborn 285
Taipei 248
Fremont 240
Norwalk 240
London 235
Paris 215
Padua 213
Lappeenranta 208
Malatya 205
Bari 202
Miami 183
Santa Clara 172
Atlanta 169
Shenzhen 169
San Antonio 167
Galati 163
Gilroy 161
Toronto 157
Moscow 154
Nanjing 153
Washington 142
Dallas 141
Andover 133
San Jose 130
Melun 129
Montréal 125
Falls Church 120
Redmond 120
Palermo 118
Cupertino 109
Putian 108
Porto 107
Phoenix 105
Austin 101
Naples 101
Frankfurt am Main 99
Las Vegas 97
Tel Aviv 96
Jinan 95
Sofia 95
Osaka 92
Genoa 84
Nürnberg 84
Lima 81
Lake Forest 80
Zagreb 79
Totale 149.042
Salva come PNG Salva come JPEG
Nome #
A class of two-dimensional theories for anisotropic multilayered plates analysis 779
Fondamenti di Meccanica Strutturale per Allievi Ingegneri Aerospaziali 632
Analysis of laminated shells by a sinusoidalshear deformation theory and Radial Basis Functions collocation, accounting for through-the-thickness deformations. 614
Appunti di costruzioni aeronautiche A 607
Use of Lagrange multipliers to combine 1D variable kinematic finite elements 548
Some results on thermal stress of layered plates and shells by using Unified Formulation 531
Carrera Unified Formulation for Free-Vibration Analysis of Aircraft Structures 523
Dynamic response of aerospace structures by means of refined beam theories 517
Advanced models for free vibration analysis of laminated beams with compact and thin-walled open/closed sections 516
Buckling of composite thin walled beams by refined theory 516
Performance of CUF approach to analyze the structural behavior of slender bodies 499
Effects of thickness stretching in functionally graded plates and shells 498
Preliminary vibroacoustic analysis about the use of metamaterials in the fuselage of a regional turboprop aircraft 496
Thin-walled beams subjected to load factors and non-structural masses 495
Unified formulation of geometrically nonlinear refined beam theories 488
Refined Beam Elements with only Displacement Variables andPlate/Shell Capabilities 486
Accurate static response of single- and multi-cell laminated box beams 482
Static and free vibration analysis of laminated beams by refined theory based on Chebyshev Polynomials 480
Guidelines and Recommendations on the Use of Higher OrderFinite Elements for Bending Analysis of Plates 475
Classical, refined and component-wise analysis of reinforced-shell structures 468
Analysis of laminated composites and sandwich structures by variable-kinematic MITC9 plate elements 468
A finite element model using a unified formulation for the analysis of viscoelastic sandwich laminates. 460
Variable kinematic plate elements coupled via Arlequin method 459
Analysis of reinforced and thin-walled structures by multi-line refined 1D/beam models 458
Accurate response of wing structures to free-vibration, load factors and non-structural masses 454
Evaluation of the accuracy of classical beam FE models via locking-free hierarchically refined elements 450
Analysis of thick isotropic and cross-ply laminated plates by Generalized Differential Quadrature Method and a Unified Formulation. 448
Free vibration analysis of simply supported beams with solid and thin-walled cross-sections using higher-order theories based on displacement variables 446
Historical review of Zig-Zag theories for multilayered plates and shells, 443
Heat conduction and thermal stress analysis of laminated composites by a variable kinematic MITC9 shell element 442
Higher-order theories and radial basis functions applied to free vibration analysis of thin-walled beams 441
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 301-329 439
Analysis of composite plates by a unified formulation-cell based smoothed finite element method and field consistent elements 436
Analysis of composite plates through cell-based smoothed finite element and 4-noded mixed interpolation of tensorial components techniques 432
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. 429
Advanced Beam Formulations for Free Vibration Analysis of Conventional and Joined Wings 428
Shell finite elements with different through-the-thickness kinematics for the linear analysis of cylindrical multilayered structures. 426
Radial Basis Functions collocation for the bending and free vibration analysis of laminated plates using the Reissner-Mixed Variational Theorem. 426
Refined shell finite elements based on RMVT and MITC for the analysis of laminated structures 420
Analysis of functionally graded material plates using triangular elements with cell-based smoothed discrete shear gap method 417
Static aeroelastic response of wing-structures accounting for in-plane cross-section deformation 416
Gasdynamics of rapid and explosive decompressions of pressurized aircraft including active venting 414
Best theory diagrams for cross-ply composite plates using polynomial, trigonometric and exponential thickness expansions 414
Axiomatic/asymptotic technique applied to refined theories for piezoelectric plates 414
Accuracy of Refined Finite Elements for Laminated Plate Analysis 412
Finite Element Analysis of Free Vibration of the Delaminated Composite Plate with Variable Kinematic Multilayered Plate Elements 409
Reissner's Mixed Variational Theorem toward MITC finite elements for multilayered plates. 408
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. 406
Variable kinematic shell elements for the analysis of electro-mechanical problems 403
FINITE ELEMENT ANALYSIS OF STRUCTURES THROUGH UNIFIED FORMULATION 403
Hygrothermal analysis of multilayered composite plates by variable kinematic finite elements 403
An assessment of Mixed and Classical Theories for thermal stress analysis of orthotropic Multilayered Plates 402
Component-wise Method Applied to Vibration of Wing Structures 401
Variable kinematic beam elements coupled via Arlequin method 401
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. 398
Finite element models with node-dependent kinematics for the analysis of composite beam structures 394
Micromechanics modeling of unit cells using CUF beam models and the Mechanics of Structure Genome 393
Free Vibration Analysis of Laminated Beam by Polynomial, Trigonometric, Exponential and Zig-Zag Theories 392
Non-linear dynamic analysis of a sandwich beam with pseudoelastic SMA hybrid composite faces based on higher order finite element theory 392
Linearized buckling analysis of isotropic and composite beam-columns by Carrera Unified Formulation and Dynamic Stiffness Method 391
Simulation of shock wave impactdue to explosion on a flying, flexible aircraft 390
Thermal Stress Analysis of laminated structures by a variable kinematic MITC9 shell element 390
Influence of non-structural localized inertia on free vibration response of thin-walled structures by variable kinematic beam formulations 389
Refined theories based on non-polynomial kinematics for the thermoelastic analysis of functionally graded plates 389
Recent developments on refined theories for beams with applications 388
Analysis of laminated doubly-curved shells by alayerwise theory and radial basis functions collocation, accounting for through-the-thickness deformations 381
Guidelines and Recommendations to Construct Theories for Metallic and composite plates 380
Refined beam finite elements for static and dynamic analysis of hull structures 379
Esercizi di Costruzioni Aeronautiche A 378
Refined One-Dimensional Formulations for LaminatedStructure Analysis 376
Guest Editorial of MAMS Special Issue on Modeling and Analysis of Smart Structures 375
Multiobjective Best Theory Diagrams for cross-ply composite plates employing polynomial, zig-zag, trigonometric and exponential thickness expansions 373
Structural Design of ELOTAC Full Composite, Inflatable UAV 373
Shell elements with through-the-thickness variable kinematics for the analysis of laminated composite and sandwich structures 363
The effects of boundary conditions on postbuckling of compressed, Symmetrically, laminated, thick plates 362
Analysis of thin-walled structures with longitudinal and transversal stiffeners 362
Analysis of laminated beams via Unified Formulation and Legendre polynomial expansions 362
Computationally efficient, high-fidelity micromechanics framework using refined 1D models 361
A refined structural model for static aeroelastic response and divergence of metallic and composite wings 361
Best Theory Diagrams for multilayered plates considering multifield analysis 358
Hierarchical theories of structures based on Legendre polynomial expansions with finite element applications 358
Cross-sectional mapping for refined beam elements with applications to shell-like structures 356
Multi-scale Modelling and Design of Composite Structures 356
Analysis of laminated composites and sandwich structures by trigonometric, exponential and miscellaneous polynomials and a MITC9 plate element 354
Variable kinematic shell elements for composite laminates accounting for hygrothermal effects 354
Component-Wise Analysis of Laminated Anisotropic Composites 354
Velivolo con ali biplano e sistema propulsivo rotanti, tilt-prandtlplane 353
Transverse Normal Stress Effects in Multilayered Plates 349
ANALYSIS OF THIN-WALLED BEAMS VIA A ONE-DIMENSIONAL UNIFIED FORMULATION THROUGH A NAVIER-TYPE SOLUTION 348
Aeroelastic Analysis of Composite Pinched Panels using Higher-Order Shell Elements 348
Analysis of thickness locking in classical, refined and mixed multilayered plate theories 347
Comparison of various 1D, 2D and 3D FE models for the analysis of thin-walled box with transverse ribs subjected to load factors 347
Free Vibrations of Damaged Aircraft Structures by Component-Wise Analysis 346
A static analysis of three-dimensional sandwich beam structures by hierarchical finite elements modelling 346
Large-deflection and post-buckling analyses of laminated composite beams by Carrera Unified Formulation 345
Coupling of hierarchical piezoelectric plate finite elements via Arlequin method 342
Free-vibration tailoring of single- and multi-bay laminated box structures by refined beam theories 341
Refined shell elements for the analysis of functionally graded structures 339
Theories and Finite Elements for Multilayered Plates and Shells: A Unified Compact Formulation with Numerical Assessment and Benchmarking 339
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 339
Totale 41.989
Salva come PNG Salva come JPEG
Categoria #
all - tutte 568.955
article - articoli 332.229
book - libri 7.731
conference - conferenze 191.175
curatela - curatele 537
other - altro 24.925
patent - brevetti 712
selected - selezionate 0
volume - volumi 10.537
Totale 1.136.801
Salva come PNG Salva come JPEG


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/202018.904 0 1.244 759 2.367 2.470 1.897 1.482 2.740 2.462 1.217 1.780 486
2020/202115.785 2.034 1.811 597 1.818 638 1.380 821 1.445 1.181 1.926 1.271 863
2021/202214.306 537 1.053 594 663 891 923 1.026 590 715 1.149 1.947 4.218
2022/202351.404 1.830 3.101 508 1.547 1.805 2.576 6.681 1.086 1.782 807 2.131 27.550
2023/20247.797 495 520 557 701 898 821 403 547 248 494 893 1.220
2024/20252.228 663 1.565 0 0 0 0 0 0 0 0 0 0
Totale 215.107