RICCI, SERGIO
 Distribuzione geografica
Continente #
NA - Nord America 15.406
EU - Europa 14.937
AS - Asia 7.756
SA - Sud America 1.397
AF - Africa 438
OC - Oceania 46
Continente sconosciuto - Info sul continente non disponibili 11
Totale 39.991
Nazione #
US - Stati Uniti d'America 15.024
RU - Federazione Russa 5.362
IT - Italia 4.797
SG - Singapore 2.224
CN - Cina 2.069
VN - Vietnam 1.465
BR - Brasile 1.157
DE - Germania 712
IE - Irlanda 707
FR - Francia 475
GB - Regno Unito 464
UA - Ucraina 457
FI - Finlandia 422
KR - Corea 389
SE - Svezia 388
AT - Austria 341
NL - Olanda 291
JP - Giappone 271
CA - Canada 260
HK - Hong Kong 218
ES - Italia 194
MA - Marocco 181
CI - Costa d'Avorio 143
IN - India 143
BD - Bangladesh 141
PH - Filippine 130
ID - Indonesia 98
AR - Argentina 87
BE - Belgio 87
TR - Turchia 84
JO - Giordania 78
MY - Malesia 72
PL - Polonia 63
MX - Messico 56
IQ - Iraq 54
PK - Pakistan 51
IR - Iran 50
ZA - Sudafrica 41
EC - Ecuador 40
AU - Australia 39
TW - Taiwan 37
CO - Colombia 32
PT - Portogallo 30
IL - Israele 25
LT - Lituania 25
CH - Svizzera 22
SA - Arabia Saudita 21
GR - Grecia 20
VE - Venezuela 20
AE - Emirati Arabi Uniti 19
UZ - Uzbekistan 19
TH - Thailandia 18
PY - Paraguay 17
CL - Cile 16
JM - Giamaica 14
AZ - Azerbaigian 13
KE - Kenya 13
NP - Nepal 11
PE - Perù 11
UY - Uruguay 11
CZ - Repubblica Ceca 10
DZ - Algeria 10
KZ - Kazakistan 9
OM - Oman 9
BJ - Benin 8
CR - Costa Rica 8
HU - Ungheria 8
EG - Egitto 7
EU - Europa 7
HN - Honduras 7
LB - Libano 7
NO - Norvegia 7
RO - Romania 7
SD - Sudan 7
TT - Trinidad e Tobago 7
DK - Danimarca 6
GT - Guatemala 6
NI - Nicaragua 6
NZ - Nuova Zelanda 6
TN - Tunisia 6
BO - Bolivia 5
MK - Macedonia 5
PA - Panama 5
SI - Slovenia 5
AL - Albania 4
AM - Armenia 4
AO - Angola 4
BG - Bulgaria 4
DO - Repubblica Dominicana 4
KG - Kirghizistan 4
KH - Cambogia 4
KW - Kuwait 4
LV - Lettonia 4
PS - Palestinian Territory 4
BA - Bosnia-Erzegovina 3
ET - Etiopia 3
HR - Croazia 3
LK - Sri Lanka 3
LU - Lussemburgo 3
MD - Moldavia 3
Totale 39.945
Città #
Milan 2.175
Ashburn 1.884
Fairfield 1.279
Singapore 1.215
San Jose 1.172
Woodbridge 962
Moscow 762
Dublin 690
Houston 636
Ann Arbor 628
Chandler 611
Wilmington 602
Seattle 600
Cambridge 465
Hefei 456
Santa Clara 434
Ho Chi Minh City 360
Seoul 345
The Dalles 338
Beijing 316
Vienna 308
Council Bluffs 305
Rome 271
Jacksonville 261
Hanoi 260
Helsinki 242
Boardman 236
Dearborn 232
Los Angeles 232
Tokyo 231
Dallas 213
Kent 194
Lauterbourg 185
Dong Ket 183
Lawrence 170
North Charleston 162
Hong Kong 154
Abidjan 143
Málaga 139
Medford 135
Ottawa 133
Buffalo 125
Kenitra 125
New York 118
Amsterdam 110
Davao City 110
São Paulo 102
Shanghai 78
Amman 77
Chicago 76
Frankfurt am Main 71
Des Moines 70
Redwood City 69
San Diego 66
Kuala Lumpur 63
Jakarta 62
Orem 62
Bovisio Masciago 58
Da Nang 57
Naples 56
Las Vegas 55
Changsha 51
Haiphong 49
Turin 49
Brussels 48
Guangzhou 47
Munich 47
Delft 45
Monza 45
Busto Arsizio 42
Falkenstein 42
Casablanca 41
Princeton 40
Rio de Janeiro 40
Warsaw 39
Istanbul 38
Auburn Hills 36
Novara 34
Brooklyn 32
Atvidaberg 31
Ciampino 30
London 30
Paris 30
Xi'an 30
Harbin 29
Washington 29
Brasília 27
Montreal 27
Giussano 26
Tianjin 25
Zibido San Giacomo 25
Crema 24
Lappeenranta 24
Muggiò 24
Pedrengo 24
Taipei 24
Chennai 23
Hangzhou 23
Hải Dương 23
Lecco 23
Totale 23.245
Nome #
Gradient-Based Aerodynamic Optimization of an Airfoil with Morphing Leading and Trailing Edges 429
Combining Density-based Approach and Optimization Refinement in the Design of Morphing Airfoil Structures 404
Aeroservoelastic Optimization of a High Aspect Transport Wing with Morphing Trailing Edge 397
Active Aeroelastic Control over a Multi-Surface Wing: Modelling and Wind Tunnel Testing 347
Development of a Wind Tunnel Model for Active Flutter Suppression Studies 344
Wind Tunnel System for Active Flutter Suppression Research: Overview and Insights 342
Numerical and experimental investigations on active flutter suppression technologies 338
Design and Wind Tunnel Test Validation of Gust Load Alleviation Systems 337
Compliant Structures-Based Wing and Wingtip Morphing Devices 336
Active Flutter Suppression Analysis and Wind Tunnel Studies of an Uncertain Commercial Transport Configuration 327
U-HARWARD: a CS2 EU Funded Project Aiming at the Design of Ultra High Aspect Ratio Wings Aircraft 298
Aeroelastic analysis of a slender wing 291
Design, Manufacturing and Wind Tunnel Validation of a Morphing Compliant Wing 283
Coupling Equivalent Plate and Beam Models at Conceptual Design Level 282
Morphing Wing Technologies within the Airgreen 2 Project 282
Aeroelastic Analysis of the CAWAPI F-16XL Configuration at Transonic Speeds 282
An Active Flutter Suppression (AFS) Project: Overview, Results and Lessons Learned 280
Optimization of compliant adaptive structures in the design of a morphing droop nose 279
Gust and Manouvre Loads Alleviation Technologies: Overview, Results and Lesson Learned in the Framework of the CS2 AIRGREEN2 Project 276
Design and Experimental Validation of Gust Load Alleviation Systems Based on Static Output Feedback 276
Active Camber Morphing Wings Based on Compliant Structures: an Aeroelastic Assessment 273
Extended computational capabilities for high-fidelity fluid–structure simulations 271
Introduction and application of PyPAD, a framework for multidisciplinary airframe design 270
A Meta-Model for composite wingbox sizing in aircraft conceptual design 269
Aeroelastic Optimization of High Aspect Ratio Wings for Environmentally Friendly Aircraft 269
Design of a Leading Edge Morphing Based on Compliant Structures for a Twin-Prop Regional Aircraft 263
Structural Sizing, Aeroelastic Analysis, and Optimization in Aircraft Conceptual Design 262
Computation of aeroelastic effects on F-16XL at flight conditions FC70 and FC25 261
Preliminary Aero-Elastic Optimization of a Twin-Aisle Long-Haul Aircraft with Increased Aspect Ratio 260
Design of a wing tip device for active maneuver and gust load alleviation 260
PyPAD: a Multidisciplinary Framework for Preliminary Airframe Design 259
Gust Load Alleviation for a Regional Aircraft Through a Static Output Feedback 257
Adaptive Trailing Edge: Specifications, Aerodynamics, and Exploitation 254
Design, Manufacturing and Wind Tunnel Test of a Morphing Wing Based on Compliant Structures 253
Advanced Design of a Full-Scale Active Morphing Droop Nose 252
Active Aeroelastic Control over a Multisurface Wing: Modeling and Wind-Tunnel Testing 251
AFS-Active Flutter Suppression Project: Activities Overview and Final Results 251
Active Aeroelastic Control over a Four Control Surface Wing Model 249
Multilevel Structural Optimization for Preliminary Wing-Box Weight Estimation 248
Buckling optimization of variable stiffness cylindrical shells through artificial intelligence techniques 244
Application of Active Camber Morphing Concept to a Regional Aircraft 241
Analytical and Experimental Evaluation of Multivariable Stability Margins in Active Flutter Suppression Wind Tunnel Tests 239
Use of MDO Techniques for the Design of Morphing Aircraft 234
Application of MDO Techniques to the Preliminary Design of Morphed Aircraft 232
NeoCASS: An integrated tool for structural sizing, aeroelastic analysis and MDO at Conceptual Design Level 228
Aeroelastic Analysis of a Regional Aircraft with Active Camber Morphing Device 228
Aeroelastic Control of Morphing Wings 227
Design, manufacturing and validation of a gust generator for wind tunnel test of a large scale aeroelastic model 227
Gust Load Alleviation Wind Tunnel Tests of a Folding Wing Tip Configuration 226
Design, Manufacturing and Preliminary Test Results of an Adaptive Wing Camber Model 225
Active Control of Three-Surface Aeroelastic Model 225
Active Flutter Suppression Techniques in Aircraft Wings 224
A Two-Level Approach for the Optimal Design of Morphing Wings Based on Compliant Structures 223
Design and Testing of a Droop Nose Morphing for Advanced Regional Aircraft: Numerical and Experimental Validation 221
An Optimization Procedure for the Optimal Design of Morphing Devices 221
Active Load Control of a Regional Aircraft Wing Equipped with Morphing Winglets 220
Experimental Identification and Control of Flutter Beyond the First Flutter Mechanism 219
Aeroservoelastic Response of Nonlinear Wind Tunnel Model to Non-Uniform Gust Field 218
PyPAD: a Multidisciplinary Framework for Preliminary Airframe Design 218
Aero-Servo-Elastic Optimization in Early Design Phases 218
Wind Tunnel Testing of Gust Load Alleviation Performance of Flexible wing with Semi-Aeroelastic Hinge 216
Freeplay-Induced Limit-Cycle Oscillations in a T-Tail: Numerical vs Experimental Validation 216
Experimental Studies on Dynamic Freeplay Nonlinearity 216
Preliminary Sizing of the Wing-Box Structure by Multi-Level Approach 215
Flow Field Around the Flapping Flag 215
Design of a Leading Edge Morphing Based on Compliant Structures in the Framework of the CS2-Airgreen2 Project 214
Aeroelastic Investigation and Design Improvements on a Three Surface Transport Airplane 213
Multi-Fidelity Design of Aeroelastic Wing Tip Devices 213
Validation of Numerical Prediction of Dynamic Derivatives: the DLR-F12 and the Transcruiser Test Cases 212
Experimental and performance validation of a full-scale morphing droop nose design based on composite compliant structures 211
Aero-Structural Design Optimization of a Morphing Aileron Considering Actuation Aspects 210
A Two Levels Approach for the Optimal Design of Morphing Airfoils 210
Design of an Innovative Wing Tip Device 210
A Multi-Level Approach to Preliminary Optimization of a Wing Structure 209
Active Control for Buffet Load Alleviation on the Fin of a High Performance Training Aircraft 207
Comparison Between Density-Based And Load-Pathbased Method In Various Camber Aerofoil Design 207
Integrated Servostructural Optimization in the Design of Aerospace Systems 206
Expected Performances 205
Multi-scale analysis and optimisation of three-dimensional woven composite structures combining response surface method and genetic algorithms 205
Minimum-weight design for three dimensional woven composite stiffened panels using neural networks and genetic algorithms 203
Wind Tunnel Evaluation of a Static Output Feedback Controller for Gust Load Alleviation on a Regional Aircraft 200
A Fast Tool for Structural Sizing, Aeroelastic Analysis and Optimization in Aircraft Conceptual Design 200
NeoCASS+, a Conceptual Design and Simulation Framework for Morphing Aircraft 199
Recent developments of NeoCass the open source suite for structural sizing and aeroelastic analysis 199
CS2-THT U-HARWARD Project: Final Assessment and Project Outcomes Evaluation 198
NeOPT: an Optimization Suite for the Aeroelastic Preliminary Design 197
Aeroelastic Testing on a Three Surface Airplane 196
Bringing Aeroelasticit Analysis in the Conceptual Design of Future Aircraft 195
Application of the Active Camber Morphing Concept Based on Compliant Structures to a Regional Aircraft 195
Wingbox Meta-Model and Aero-Servo-Elastic Optimization With NEOPT 194
SMorph - Smart Aircraft Morphing Technologies Project 193
Model Updating and Aeroelastic Correlation of a Scaled Wind Tunnel Model for Active Flutter Suppression Test 193
Development of an Active Wingtip for Aeroelastic Control 192
Coupled CSD/CFD Non-Linear Aeroelastic Trim of Free-Flying Flexible Aircraft 191
Definition, Design Assessment and Parameterization of a Metasensor for LC&A and Load Monitoring Purposes 191
Knowledge-Based Shape Optimization of Morphing Wing for More Efficient Aircraft 191
A Multi-Level Procedure for the Preliminary Sizing of Aircraft Wing-Box Structures 190
An Italian Experience On Morphing Aircraft Systems 190
Active Aeroelastic Control over a Four Control Surface Wind Tunnel Wing Model 189
Development of a Buffet Load Mitigation System Based on Multi-Surface Control 189
Totale 24.215
Categoria #
all - tutte 99.280
article - articoli 27.365
book - libri 0
conference - conferenze 70.248
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 1.667
Totale 198.560


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2021/20221.918 65 223 112 156 223 88 132 232 102 93 203 289
2022/20232.551 209 63 121 138 259 324 71 226 674 234 155 77
2023/20241.658 97 206 67 154 133 145 216 64 80 217 79 200
2024/20256.174 238 102 162 125 1.065 394 297 463 650 295 711 1.672
2025/202617.099 3.531 2.437 922 1.084 802 868 2.549 889 968 1.420 527 1.102
2026/2027266 266 0 0 0 0 0 0 0 0 0 0 0
Totale 40.193