ZUCCA, STEFANO
 Distribuzione geografica
Continente #
NA - Nord America 8.097
EU - Europa 7.639
AS - Asia 1.684
AF - Africa 104
SA - Sud America 38
OC - Oceania 8
Continente sconosciuto - Info sul continente non disponibili 7
Totale 17.577
Nazione #
US - Stati Uniti d'America 8.010
IT - Italia 2.311
GB - Regno Unito 1.302
FR - Francia 1.110
DE - Germania 1.071
CN - Cina 919
UA - Ucraina 447
TR - Turchia 265
IE - Irlanda 254
RU - Federazione Russa 253
NL - Olanda 192
SE - Svezia 185
CH - Svizzera 115
KR - Corea 99
IN - India 95
BE - Belgio 91
CA - Canada 81
FI - Finlandia 73
IR - Iran 69
AP - ???statistics.table.value.countryCode.AP??? 46
CI - Costa d'Avorio 44
RO - Romania 42
MY - Malesia 41
PK - Pakistan 35
SN - Senegal 35
JP - Giappone 33
EU - Europa 32
BR - Brasile 27
HK - Hong Kong 25
AT - Austria 23
ES - Italia 23
CZ - Repubblica Ceca 21
VN - Vietnam 21
SG - Singapore 20
PT - Portogallo 11
BG - Bulgaria 10
IL - Israele 10
TW - Taiwan 10
AU - Australia 8
CL - Cile 8
EG - Egitto 8
HR - Croazia 7
LU - Lussemburgo 6
PH - Filippine 6
SA - Arabia Saudita 6
GR - Grecia 5
NO - Norvegia 5
BY - Bielorussia 4
DK - Danimarca 4
EE - Estonia 4
NG - Nigeria 4
ZA - Sudafrica 4
DZ - Algeria 3
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
ID - Indonesia 1
IQ - Iraq 1
MA - Marocco 1
QA - Qatar 1
SY - Repubblica araba siriana 1
YE - Yemen 1
Totale 17.577
Città #
Ashburn 1.953
Southend 1.055
Seattle 774
Fairfield 574
Chandler 465
Turin 402
Torino 396
Des Moines 376
Beijing 322
Princeton 309
Woodbridge 284
Houston 268
Dublin 245
Ann Arbor 232
Jacksonville 223
Cambridge 219
Council Bluffs 218
Wilmington 215
Berlin 185
Izmir 163
San Ramon 146
Shanghai 130
Chicago 106
Milan 101
Bern 95
Zhengzhou 93
Saint Petersburg 90
Brussels 87
San Donato Milanese 87
Hangzhou 69
Helsinki 65
Buffalo 62
Zaporozhye 56
Istanbul 51
Baltimore 49
Pennsylvania Furnace 49
Redwood City 46
Xian 45
Ottawa 44
Overberg 44
Changsha 42
London 42
Valfenera 42
Galati 38
San Jose 36
Amsterdam 35
Atlanta 35
Mountain View 35
San Diego 35
Monopoli 34
Guangzhou 33
Herkenbosch 33
Boardman 31
San Francisco 31
Rome 30
Bologna 29
Padua 28
Abidjan 27
Fremont 27
Dearborn 26
Falls Church 24
Shenzhen 24
Paris 22
Dayton 20
Nanjing 20
Seoul 20
Malatya 19
Tehran 19
Toronto 19
Fazal 18
Frankfurt Am Main 18
Hanoi 18
Hanover 18
Redmond 18
Genova 17
Moscow 17
Norwalk 17
Perm 16
Washington 16
Dallas 15
Phoenix 15
Stuttgart 15
Fortaleza 14
San Mauro Torinese 14
Ankara 13
Los Angeles 13
New York 13
Osimo 13
Varese 13
Binasco 12
Malo 12
Oleggio 12
San Antonio 12
Vienna 12
Brooklyn 11
Frankfurt 11
Kiev 11
Las Vegas 11
Mumbai 11
Zurich 11
Totale 11.686
Nome #
Analytical Formulation of the Jacobian Matrix for Non-linear Calculation of the Forced Response of Turbine Blade Assemblies with Wedge Friction Dampers 426
A reduced order model based on sector mistuning for the dynamicanalysis of mistuned bladed disks 418
Modelling friction contacts in structural dynamics and its application to turbine bladed disks 374
Measuring the Performance of Underplatform Dampers for Turbine Blades by Rotating Laser Doppler Vibrometer 367
Non-linear Dynamics of Steam Turbine Blades with Shroud: Numerical Analysis and Experiments. 364
Numerical Assessment of Friction Damping at Turbine Blade Root Joints by Simultaneous Calculation of the Static and Dynamic Contact Loads 358
Effect of crowning ofdovetail joints on turbine blade root damping 351
Smorzatori sotto-pala per turbomacchine: un nuovo metodo basato sul calcolo simultaneo delle forze statiche e dinamiche di contatto. 320
Experimental and numerical investigations on the dynamic response of turbine blades with tip pin dampers 316
Modeling Underplatform Dampers for Turbine Blades: a Refined Approach in the Frequency Domain. 315
A new reduction technique for thermal models with fluid networks 309
A METHOD FOR THE DESIGN OF RING DAMPERS FOR GEARS IN AERONAUTICAL APPLICATIONS 305
Faster on-line calculation of thermal stresses by time integration 302
Identification of a low-order model for thermal stress monitoring 298
A reduced order model based on sector mistuning for the dynamic analysis of mistuned bladed disks 298
A Method for the Calculation of Friction Damping in Blade Root Joints 287
Forced response of shrouded blades with a coupled static/dynamic approach 278
The effect of underplatform dampers on the forced response of bladed disks by a coupled static/dynamic harmonic balance method 275
Effect of crowning of dovetail joints on turbine blade root damping 265
Coupled static/dynamic modeling of wedge dampers for turbine blades 256
Effects of contact mistuning on shrouded blisk dynamics 254
A methodology for on-line calculation of temperature and thermal stress under non-linear boundary conditions 251
A method for the design of ring dampers for gears in aeronautical applications 250
Reduction of a turbine disk thermal finite element model including the fluid network, Part I: Theoretical Development. 249
Experimental and numerical investigations on the dynamic response of turbine blades with tip pin dampers 249
Reduced-Order Models for the Calculation of Thermal Transients of Heat Conduction/Convection FE Models. 249
Numerical Computation of Stress Intensity Factors in Ultrasonic Very-High-Cycle Fatigue Tests 248
Bi-linear modal reduction for the dynamic analysis of structures with intermittent contacts and friction 243
Range of variability in the dynamics of semi-cylindrical friction dampers for turbine blades. 242
Passive control of vibration of thin-walled gears: advanced modelling of ring dampers 241
Nonlinear dynamics of mechanical systems with friction contacts: Coupled static and dynamic Multi-Harmonic Balance Method and multiple solutions 235
Adaptive microslip projection (AMP) for reduction of frictional and contact non-linearities in shrouded blisks 234
Underplatform damper performance with turbine blades. 225
Underplatform dampers for turbine blades: the effect of damper static balance on the blade dynamics 225
Riduzione modale applicata a modelli termici non lineari di dischi di turbina 218
The calculation of thermal transients in mechanical components with reduced order models based on component mode synthesis 216
On the dual Craig–Bampton method for the forced response of structures with contact interfaces 215
Reduced order models for nonlinear dynamic analysis of structures with intermittent contacts 215
Forced Response of Bladed Disks in Cyclic Symmetry with Underplatform Dampers 212
Adaptive Microslip Projection for Reduction of Frictional and Contact Nonlinearities in Shrouded Blisks 212
Calcolo approssimato dello stato di tensione in dischi di turbine aeronautiche 210
A method for on-line temperature calculation of aircraft engine turbine discs, GT-2002-30006 209
Static/dynamic coupling of gears with a ring damper for the nonlinear forced response calculation 208
Jacobian projection reduced-order models for dynamic systems with contact nonlinearities 206
Influence of actual static transmission error and contact ratio on gear engagement dynamics 202
Detection of a Blade Crack in Bladed Disks: Methodology and Validation 201
Nonlinear dynamics of mechanical systems with friction contacts: Harmonic Balance Method and multiple solutions 200
Bi-linear reduced-order models of structures with friction intermittent contacts 197
Identificazione di un modello di ordine ridotto per il calcolo in tempo reale delle tensioni termiche 187
Parametric study of the kinematic behaviour of the underplatform damper and correlation with experimental data 187
Experimental investigation on the damping effectiveness of blade root joints 185
Sviluppo di un codice di calcoloper la progettazione di smorzatori sotto-pala per pale di turbina 182
Methods for Reducing a Thermal Finite Element Model Including the Advection Network Contribution 177
Forced response of interlocked vane segments: numerical predictions and experimental results 175
Riduzione di sistemi in simmetria ciclica attraverso la 'sintesi dei modi componenti utilizzando i modi di intefaccia' 174
Un metodo per la progettazione di smorzatori ad anello per ingranagggi di applicazione aeronautica. 171
Metodi di progetto per la ricostruzione approssimata delle temperature nei dischi di turbina aeronautica 170
Numerical Computation of Stress Intensity Factors in Ultrasonic Very-High-Cycle Fatigue Tests 168
Nonlinear Vibration Analysis of Turbine Bladed Disks with Midspan Dampers 166
Effect of static/dynamic coupling on the forced reponse of turbine bladed disks with underplatform dampers 162
On-line calculation of thermal stresses by time integration 161
Jacobian projection for the reduction of friction induced nonlinearities 160
Component modes synthesis applied to a thermal transient analysis of a turbine disc 160
A novel test rig to study the effect of fretting wear on the forced response dynamics with a friction contact 130
Design and Calibration of a Tri-Directional Contact Force Measurement System 127
On the non-uniqueness of friction forces and the systematic computation of dynamic response boundaries for turbine bladed disks with contacts 115
Experimental and Numerical Assessment of Mistuning Effects on Vibratory Response of a Bladed Disk with Underplatform Dampers 108
An experimental and computational comparison of the dynamic response variability in a turbine blade with under-platform dampers 104
Nonlinear dynamic analysis of gas turbine combustor leaf seal 98
Determination of periodic response limits among multiple solutions for mechanical systems with wedge dampers 97
Application of Multiple-Scales Method for the Dynamic Modelling of a Gear Coupling 93
An Experimental Investigation on the Dynamic Response Variability of a Turbine Blade With Midspan Dampers 90
Effect of wear on the dynamics of structures with contact interfaces by a coupled static/dynamic multi-harmonic balance method 87
Experimental and Numerical Assessment of Mistuning Effects on Vibratory Response of a Bladed Disk With Underplatform Dampers 79
A Comparison of Two Reduction Techniques for Forced Response of Shrouded Blades with Contact Interfaces 78
A coupled approach to model wear effect on shrouded bladed disk dynamics 75
A reduced order model for nonlinear dynamics of mistuned bladed disks with shroud friction contacts 75
Comparison of contact parameters measured with two different friction rigs for nonlinear dynamic analysis 71
A coupled approach to model the effect of wear on the dynamics of bladed disks 69
Relative cyclic component mode synthesis and its application to nonlinear vibration analysis of mistuned bladed disks with friction joints 68
Effect of variation in contact friction on the performance of the under-platform dampers 68
A Reduced Order Model for Nonlinear Dynamics of Mistuned Bladed Disks with Shroud Friction Contacts 65
Mixed-Boundary Component Mode Substitution for Nonlinear Dynamics of Mistuned Shrouded Bladed Disks 64
Design of wave-like dry friction and piezoelectric hybrid dampers for thin-walled structures 64
A Comparison between Two Reduction Strategies for Shrouded Bladed Disks 63
Nonlinear Vibration Analysis of Turbine Bladed Disks With Mid-Span Dampers 63
Nonlinear forced response analysis of bladed disks using a relative cyclic component mode synthesis approach 61
Design of dry friction and piezoelectric hybrid ring dampers for integrally bladed disks based on complex nonlinear modes 48
Relative cyclic component mode synthesis: A reduced order modeling approach for mistuned bladed disks with friction interfaces 44
Hybrid reduction of mistuned bladed disks for nonlinear forced response analysis with dry friction 43
Evaluation of free interface-based reduction techniques for nonlinear forced response analysis of shrouded blades 41
Multiple response levels of structures with wedge friction dampers 40
A method for on-line temperature calculation of aircraft engine turbine discs 39
A test rig for the full characterization of the dynamics of shrouded turbine blades 38
Experimental Investigation of Three-Dimensional Shroud Contact Forces in Forced-Vibration Testing of a Shrouded Blade 37
Dynamic model order reduction of blisks with nonlinear damping coatings using amplitude dependent mistuning 37
A sensitivity based heuristic for optimal blade arrangement in a linear mistuned rotor 31
AN EXPERIMENTAL INVESTIGATION ON THE DYNAMIC RESPONSE VARIABILITY OF A TURBINE BLADE WITH MID-SPAN DAMPERS 30
Upgraded reduction technique for dynamic analysis of structures with friction contact 20
Guidelines to use input contact parameters for nonlinear dynamic analysis of jointed structures: Results of a round robin test 15
Totale 17.858
Categoria #
all - tutte 44.822
article - articoli 19.406
book - libri 0
conference - conferenze 24.551
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 865
Totale 89.644


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2018/20191.078 0 0 0 0 0 0 0 0 167 228 385 298
2019/20201.973 178 122 73 238 279 210 138 261 212 129 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
2022/20232.090 162 319 52 131 145 259 497 89 180 22 90 144
2023/2024670 40 198 71 103 77 90 26 33 32 0 0 0
Totale 17.858