PORTO @ Archivio Istituzionale della Ricerca

ZUCCA, STEFANO
 Distribuzione geografica
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Continente #
NA - Nord America 8.547
EU - Europa 7.890
AS - Asia 2.216
AF - Africa 107
SA - Sud America 40
OC - Oceania 13
Continente sconosciuto - Info sul continente non disponibili 7
Totale 18.820
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Nazione #
US - Stati Uniti d'America 8.459
IT - Italia 2.438
GB - Regno Unito 1.308
FR - Francia 1.111
DE - Germania 1.104
CN - Cina 1.066
UA - Ucraina 447
RU - Federazione Russa 346
SG - Singapore 291
TR - Turchia 291
IE - Irlanda 230
NL - Olanda 196
SE - Svezia 185
KR - Corea 143
CH - Svizzera 115
IN - India 95
BE - Belgio 85
CA - Canada 82
FI - Finlandia 79
IR - Iran 71
AP - ???statistics.table.value.countryCode.AP??? 46
CI - Costa d'Avorio 44
MY - Malesia 43
RO - Romania 42
PK - Pakistan 37
JP - Giappone 36
SN - Senegal 35
EU - Europa 32
HK - Hong Kong 30
ID - Indonesia 30
BR - Brasile 29
AT - Austria 23
ES - Italia 23
VN - Vietnam 22
CZ - Repubblica Ceca 21
BG - Bulgaria 19
AU - Australia 12
PT - Portogallo 11
IL - Israele 10
TW - Taiwan 10
CL - Cile 8
EG - Egitto 8
HR - Croazia 7
DZ - Algeria 6
LU - Lussemburgo 6
NO - Norvegia 6
PH - Filippine 6
SA - Arabia Saudita 6
DK - Danimarca 5
GR - Grecia 5
BY - Bielorussia 4
EE - Estonia 4
NG - Nigeria 4
ZA - Sudafrica 4
JO - Giordania 3
KZ - Kazakistan 3
MX - Messico 3
PL - Polonia 3
TG - Togo 3
AE - Emirati Arabi Uniti 2
AZ - Azerbaigian 2
GE - Georgia 2
LV - Lettonia 2
SK - Slovacchia (Repubblica Slovacca) 2
TH - Thailandia 2
UZ - Uzbekistan 2
A2 - ???statistics.table.value.countryCode.A2??? 1
AG - Antigua e Barbuda 1
AR - Argentina 1
BJ - Benin 1
CO - Colombia 1
DO - Repubblica Dominicana 1
EC - Ecuador 1
ET - Etiopia 1
HN - Honduras 1
IQ - Iraq 1
MA - Marocco 1
NZ - Nuova Zelanda 1
QA - Qatar 1
SY - Repubblica araba siriana 1
YE - Yemen 1
Totale 18.820
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Città #
Ashburn 1.981
Southend 1.055
Seattle 774
Fairfield 574
Chandler 465
Turin 442
Torino 396
Des Moines 376
Beijing 324
Princeton 309
Woodbridge 284
Council Bluffs 274
Houston 268
Ann Arbor 232
Jacksonville 223
Dublin 221
Cambridge 219
Wilmington 215
Singapore 200
Berlin 185
Izmir 163
San Ramon 146
Boardman 134
Shanghai 133
Santa Clara 109
Milan 105
Chicago 103
Bern 95
Zhengzhou 93
Saint Petersburg 90
San Donato Milanese 87
Brussels 81
Istanbul 76
Hangzhou 69
Helsinki 68
Buffalo 62
Zaporozhye 56
Baltimore 49
Pennsylvania Furnace 49
Redwood City 46
Ottawa 45
Xian 45
Overberg 44
Changsha 42
London 42
Valfenera 42
Galati 38
San Jose 37
Amsterdam 36
Rome 36
Atlanta 35
Guangzhou 35
Mountain View 35
San Diego 35
Monopoli 34
Herkenbosch 33
Bologna 31
San Francisco 31
Jakarta 29
Padua 28
Abidjan 27
Fremont 27
Seoul 27
Dearborn 26
Shenzhen 25
Falls Church 24
Washington 24
New York 23
Paris 22
Moscow 21
Dayton 20
Hanover 20
Nanjing 20
Tehran 20
Los Angeles 19
Malatya 19
Toronto 19
Fazal 18
Frankfurt Am Main 18
Hanoi 18
Redmond 18
Genova 17
Norwalk 17
Perm 16
Trieste 16
Yubileyny 16
Dallas 15
Phoenix 15
Stuttgart 15
Ankara 14
Fortaleza 14
San Mauro Torinese 14
Osimo 13
Varese 13
Binasco 12
Frankfurt am Main 12
Las Vegas 12
Malo 12
Nuremberg 12
Oleggio 12
Totale 12.286
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Nome #
A reduced order model based on sector mistuning for the dynamicanalysis of mistuned bladed disks 445
Analytical Formulation of the Jacobian Matrix for Non-linear Calculation of the Forced Response of Turbine Blade Assemblies with Wedge Friction Dampers 436
Measuring the Performance of Underplatform Dampers for Turbine Blades by Rotating Laser Doppler Vibrometer 383
Modelling friction contacts in structural dynamics and its application to turbine bladed disks 380
Non-linear Dynamics of Steam Turbine Blades with Shroud: Numerical Analysis and Experiments. 373
Numerical Assessment of Friction Damping at Turbine Blade Root Joints by Simultaneous Calculation of the Static and Dynamic Contact Loads 367
Effect of crowning ofdovetail joints on turbine blade root damping 360
Modeling Underplatform Dampers for Turbine Blades: a Refined Approach in the Frequency Domain. 330
Smorzatori sotto-pala per turbomacchine: un nuovo metodo basato sul calcolo simultaneo delle forze statiche e dinamiche di contatto. 328
A new reduction technique for thermal models with fluid networks 324
Experimental and numerical investigations on the dynamic response of turbine blades with tip pin dampers 322
A METHOD FOR THE DESIGN OF RING DAMPERS FOR GEARS IN AERONAUTICAL APPLICATIONS 315
Faster on-line calculation of thermal stresses by time integration 314
Identification of a low-order model for thermal stress monitoring 308
A reduced order model based on sector mistuning for the dynamic analysis of mistuned bladed disks 306
A Method for the Calculation of Friction Damping in Blade Root Joints 293
The effect of underplatform dampers on the forced response of bladed disks by a coupled static/dynamic harmonic balance method 291
Forced response of shrouded blades with a coupled static/dynamic approach 291
Numerical Computation of Stress Intensity Factors in Ultrasonic Very-High-Cycle Fatigue Tests 276
Effect of crowning of dovetail joints on turbine blade root damping 271
Effects of contact mistuning on shrouded blisk dynamics 268
Coupled static/dynamic modeling of wedge dampers for turbine blades 261
Reduced-Order Models for the Calculation of Thermal Transients of Heat Conduction/Convection FE Models. 260
Reduction of a turbine disk thermal finite element model including the fluid network, Part I: Theoretical Development. 259
A method for the design of ring dampers for gears in aeronautical applications 259
Experimental and numerical investigations on the dynamic response of turbine blades with tip pin dampers 259
A methodology for on-line calculation of temperature and thermal stress under non-linear boundary conditions 258
Range of variability in the dynamics of semi-cylindrical friction dampers for turbine blades. 252
Passive control of vibration of thin-walled gears: advanced modelling of ring dampers 251
Bi-linear modal reduction for the dynamic analysis of structures with intermittent contacts and friction 251
Adaptive microslip projection (AMP) for reduction of frictional and contact non-linearities in shrouded blisks 244
Nonlinear dynamics of mechanical systems with friction contacts: Coupled static and dynamic Multi-Harmonic Balance Method and multiple solutions 243
Underplatform dampers for turbine blades: the effect of damper static balance on the blade dynamics 234
Underplatform damper performance with turbine blades. 232
Reduced order models for nonlinear dynamic analysis of structures with intermittent contacts 231
Riduzione modale applicata a modelli termici non lineari di dischi di turbina 226
Influence of actual static transmission error and contact ratio on gear engagement dynamics 223
The calculation of thermal transients in mechanical components with reduced order models based on component mode synthesis 223
On the dual Craig–Bampton method for the forced response of structures with contact interfaces 220
Adaptive Microslip Projection for Reduction of Frictional and Contact Nonlinearities in Shrouded Blisks 219
A method for on-line temperature calculation of aircraft engine turbine discs, GT-2002-30006 219
Jacobian projection reduced-order models for dynamic systems with contact nonlinearities 218
Forced Response of Bladed Disks in Cyclic Symmetry with Underplatform Dampers 217
Calcolo approssimato dello stato di tensione in dischi di turbine aeronautiche 216
Static/dynamic coupling of gears with a ring damper for the nonlinear forced response calculation 213
Detection of a Blade Crack in Bladed Disks: Methodology and Validation 212
Nonlinear dynamics of mechanical systems with friction contacts: Harmonic Balance Method and multiple solutions 207
Bi-linear reduced-order models of structures with friction intermittent contacts 205
Parametric study of the kinematic behaviour of the underplatform damper and correlation with experimental data 203
Nonlinear Vibration Analysis of Turbine Bladed Disks with Midspan Dampers 199
Identificazione di un modello di ordine ridotto per il calcolo in tempo reale delle tensioni termiche 194
Experimental investigation on the damping effectiveness of blade root joints 194
Numerical Computation of Stress Intensity Factors in Ultrasonic Very-High-Cycle Fatigue Tests 194
Sviluppo di un codice di calcoloper la progettazione di smorzatori sotto-pala per pale di turbina 189
Forced response of interlocked vane segments: numerical predictions and experimental results 183
Methods for Reducing a Thermal Finite Element Model Including the Advection Network Contribution 182
Un metodo per la progettazione di smorzatori ad anello per ingranagggi di applicazione aeronautica. 181
Riduzione di sistemi in simmetria ciclica attraverso la 'sintesi dei modi componenti utilizzando i modi di intefaccia' 180
Metodi di progetto per la ricostruzione approssimata delle temperature nei dischi di turbina aeronautica 179
On-line calculation of thermal stresses by time integration 171
Jacobian projection for the reduction of friction induced nonlinearities 170
Effect of static/dynamic coupling on the forced reponse of turbine bladed disks with underplatform dampers 168
Component modes synthesis applied to a thermal transient analysis of a turbine disc 167
A novel test rig to study the effect of fretting wear on the forced response dynamics with a friction contact 163
Design and Calibration of a Tri-Directional Contact Force Measurement System 147
On the non-uniqueness of friction forces and the systematic computation of dynamic response boundaries for turbine bladed disks with contacts 129
An experimental and computational comparison of the dynamic response variability in a turbine blade with under-platform dampers 127
An Experimental Investigation on the Dynamic Response Variability of a Turbine Blade With Midspan Dampers 117
Experimental and Numerical Assessment of Mistuning Effects on Vibratory Response of a Bladed Disk with Underplatform Dampers 116
Nonlinear dynamic analysis of gas turbine combustor leaf seal 113
Effect of wear on the dynamics of structures with contact interfaces by a coupled static/dynamic multi-harmonic balance method 110
Determination of periodic response limits among multiple solutions for mechanical systems with wedge dampers 108
A coupled approach to model wear effect on shrouded bladed disk dynamics 105
Application of Multiple-Scales Method for the Dynamic Modelling of a Gear Coupling 103
A Comparison of Two Reduction Techniques for Forced Response of Shrouded Blades with Contact Interfaces 88
Comparison of contact parameters measured with two different friction rigs for nonlinear dynamic analysis 88
Experimental and Numerical Assessment of Mistuning Effects on Vibratory Response of a Bladed Disk With Underplatform Dampers 84
Design of wave-like dry friction and piezoelectric hybrid dampers for thin-walled structures 81
A coupled approach to model the effect of wear on the dynamics of bladed disks 79
Effect of variation in contact friction on the performance of the under-platform dampers 79
A reduced order model for nonlinear dynamics of mistuned bladed disks with shroud friction contacts 78
Relative cyclic component mode synthesis and its application to nonlinear vibration analysis of mistuned bladed disks with friction joints 76
Nonlinear Vibration Analysis of Turbine Bladed Disks With Mid-Span Dampers 73
A Comparison between Two Reduction Strategies for Shrouded Bladed Disks 72
A Reduced Order Model for Nonlinear Dynamics of Mistuned Bladed Disks with Shroud Friction Contacts 71
Mixed-Boundary Component Mode Substitution for Nonlinear Dynamics of Mistuned Shrouded Bladed Disks 69
Nonlinear forced response analysis of bladed disks using a relative cyclic component mode synthesis approach 65
Multiple response levels of structures with wedge friction dampers 64
A test rig for the full characterization of the dynamics of shrouded turbine blades 58
Design of dry friction and piezoelectric hybrid ring dampers for integrally bladed disks based on complex nonlinear modes 58
Relative cyclic component mode synthesis: A reduced order modeling approach for mistuned bladed disks with friction interfaces 54
Evaluation of free interface-based reduction techniques for nonlinear forced response analysis of shrouded blades 52
Experimental Investigation of Three-Dimensional Shroud Contact Forces in Forced-Vibration Testing of a Shrouded Blade 50
Hybrid reduction of mistuned bladed disks for nonlinear forced response analysis with dry friction 49
A method for on-line temperature calculation of aircraft engine turbine discs 48
Dynamic model order reduction of blisks with nonlinear damping coatings using amplitude dependent mistuning 42
A sensitivity based heuristic for optimal blade arrangement in a linear mistuned rotor 42
Upgraded reduction technique for dynamic analysis of structures with friction contact 41
AN EXPERIMENTAL INVESTIGATION ON THE DYNAMIC RESPONSE VARIABILITY OF A TURBINE BLADE WITH MID-SPAN DAMPERS 41
Experimental dataset from a round robin test of contact parameters and hysteresis loops for nonlinear dynamic analysis 33
Totale 19.020
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Categoria #
all - tutte 52.713
article - articoli 23.635
book - libri 0
conference - conferenze 28.135
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 943
Totale 105.426
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/20201.362 0 0 0 0 279 210 138 261 212 129 90 43
2020/20211.461 175 186 73 141 101 159 122 119 84 143 82 76
2021/20221.541 148 90 9 103 35 140 140 90 139 103 225 319
2022/20232.040 162 319 52 131 145 259 473 82 173 18 85 141
2023/2024912 36 195 67 91 70 90 26 33 43 40 109 112
2024/20251.069 80 434 140 252 163 0 0 0 0 0 0 0
Totale 19.119