RE.PUBLIC@POLIMI pubblicazioni di ricerca del Politecnico di Milano

RICCI, SERGIO
 Distribuzione geografica
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Continente #
NA - Nord America 15.757
EU - Europa 14.998
AS - Asia 7.790
SA - Sud America 1.397
AF - Africa 439
Continente sconosciuto - Info sul continente non disponibili 214
OC - Oceania 46
Totale 40.641
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Nazione #
US - Stati Uniti d'America 15.332
RU - Federazione Russa 5.362
IT - Italia 4.846
SG - Singapore 2.244
CN - Cina 2.072
VN - Vietnam 1.465
BR - Brasile 1.157
DE - Germania 715
IE - Irlanda 707
FR - Francia 476
GB - Regno Unito 465
UA - Ucraina 457
FI - Finlandia 422
KR - Corea 389
SE - Svezia 388
AT - Austria 341
NL - Olanda 291
JP - Giappone 277
CA - Canada 275
HK - Hong Kong 218
ES - Italia 195
MA - Marocco 181
IN - India 146
CI - Costa d'Avorio 143
BD - Bangladesh 141
PH - Filippine 130
ID - Indonesia 99
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 38
CO - Colombia 32
PT - Portogallo 30
CH - Svizzera 28
IL - Israele 25
LT - Lituania 25
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
CR - Costa Rica 14
JM - Giamaica 14
AZ - Azerbaigian 13
KE - Kenya 13
HN - Honduras 12
NP - Nepal 11
PE - Perù 11
UY - Uruguay 11
CZ - Repubblica Ceca 10
DZ - Algeria 10
GT - Guatemala 10
TT - Trinidad e Tobago 10
KZ - Kazakistan 9
OM - Oman 9
BJ - Benin 8
HU - Ungheria 8
EG - Egitto 7
EU - Europa 7
LB - Libano 7
NI - Nicaragua 7
NO - Norvegia 7
RO - Romania 7
SD - Sudan 7
DK - Danimarca 6
NZ - Nuova Zelanda 6
SV - El Salvador 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
BB - Barbados 3
ET - Etiopia 3
HR - Croazia 3
LK - Sri Lanka 3
Totale 40.385
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Città #
Milan 2.199
Ashburn 1.926
Fairfield 1.279
Singapore 1.224
San Jose 1.186
Woodbridge 962
Moscow 762
Dublin 690
Houston 639
Ann Arbor 628
Chandler 611
Wilmington 603
Seattle 602
Cambridge 465
Hefei 456
Santa Clara 447
Council Bluffs 405
Ho Chi Minh City 360
Seoul 345
The Dalles 338
Beijing 318
Vienna 308
Rome 273
Jacksonville 262
Hanoi 260
Helsinki 242
Los Angeles 239
Boardman 238
Dearborn 232
Tokyo 232
Dallas 216
Kent 194
Lauterbourg 185
Dong Ket 183
Lawrence 170
North Charleston 164
Hong Kong 154
Abidjan 143
Málaga 140
Medford 135
Ottawa 133
Buffalo 125
Kenitra 125
New York 119
Amsterdam 110
Davao City 110
São Paulo 102
Chicago 82
Shanghai 78
Amman 77
Frankfurt am Main 71
Des Moines 70
Redwood City 69
San Diego 66
Kuala Lumpur 63
Orem 63
Jakarta 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
Washington 30
Xi'an 30
Harbin 29
Montreal 28
Brasília 27
Giussano 26
Chennai 25
Tianjin 25
Zibido San Giacomo 25
Crema 24
Lappeenranta 24
Muggiò 24
Pedrengo 24
Taipei 24
Atlanta 23
Hangzhou 23
Hải Dương 23
Totale 23.486
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Nome #
Gradient-Based Aerodynamic Optimization of an Airfoil with Morphing Leading and Trailing Edges 438
Combining Density-based Approach and Optimization Refinement in the Design of Morphing Airfoil Structures 417
Aeroservoelastic Optimization of a High Aspect Transport Wing with Morphing Trailing Edge 407
Active Aeroelastic Control over a Multi-Surface Wing: Modelling and Wind Tunnel Testing 348
Wind Tunnel System for Active Flutter Suppression Research: Overview and Insights 344
Development of a Wind Tunnel Model for Active Flutter Suppression Studies 344
Numerical and experimental investigations on active flutter suppression technologies 341
Compliant Structures-Based Wing and Wingtip Morphing Devices 340
Design and Wind Tunnel Test Validation of Gust Load Alleviation Systems 338
Active Flutter Suppression Analysis and Wind Tunnel Studies of an Uncertain Commercial Transport Configuration 328
U-HARWARD: a CS2 EU Funded Project Aiming at the Design of Ultra High Aspect Ratio Wings Aircraft 300
Aeroelastic analysis of a slender wing 292
An Active Flutter Suppression (AFS) Project: Overview, Results and Lessons Learned 285
Design, Manufacturing and Wind Tunnel Validation of a Morphing Compliant Wing 284
Morphing Wing Technologies within the Airgreen 2 Project 284
Design and Experimental Validation of Gust Load Alleviation Systems Based on Static Output Feedback 283
Coupling Equivalent Plate and Beam Models at Conceptual Design Level 282
Aeroelastic Analysis of the CAWAPI F-16XL Configuration at Transonic Speeds 282
Gust and Manouvre Loads Alleviation Technologies: Overview, Results and Lesson Learned in the Framework of the CS2 AIRGREEN2 Project 280
Optimization of compliant adaptive structures in the design of a morphing droop nose 280
Extended computational capabilities for high-fidelity fluid–structure simulations 275
Active Camber Morphing Wings Based on Compliant Structures: an Aeroelastic Assessment 273
A Meta-Model for composite wingbox sizing in aircraft conceptual design 272
Aeroelastic Optimization of High Aspect Ratio Wings for Environmentally Friendly Aircraft 272
Introduction and application of PyPAD, a framework for multidisciplinary airframe design 270
Preliminary Aero-Elastic Optimization of a Twin-Aisle Long-Haul Aircraft with Increased Aspect Ratio 264
Design of a Leading Edge Morphing Based on Compliant Structures for a Twin-Prop Regional Aircraft 264
Computation of aeroelastic effects on F-16XL at flight conditions FC70 and FC25 263
Structural Sizing, Aeroelastic Analysis, and Optimization in Aircraft Conceptual Design 263
Design of a wing tip device for active maneuver and gust load alleviation 263
Gust Load Alleviation for a Regional Aircraft Through a Static Output Feedback 260
PyPAD: a Multidisciplinary Framework for Preliminary Airframe Design 259
Design, Manufacturing and Wind Tunnel Test of a Morphing Wing Based on Compliant Structures 258
Multilevel Structural Optimization for Preliminary Wing-Box Weight Estimation 257
Advanced Design of a Full-Scale Active Morphing Droop Nose 256
Adaptive Trailing Edge: Specifications, Aerodynamics, and Exploitation 255
Active Aeroelastic Control over a Multisurface Wing: Modeling and Wind-Tunnel Testing 254
AFS-Active Flutter Suppression Project: Activities Overview and Final Results 253
Active Aeroelastic Control over a Four Control Surface Wing Model 250
Buckling optimization of variable stiffness cylindrical shells through artificial intelligence techniques 248
Analytical and Experimental Evaluation of Multivariable Stability Margins in Active Flutter Suppression Wind Tunnel Tests 244
Application of Active Camber Morphing Concept to a Regional Aircraft 242
Use of MDO Techniques for the Design of Morphing Aircraft 238
Gust Load Alleviation Wind Tunnel Tests of a Folding Wing Tip Configuration 234
Application of MDO Techniques to the Preliminary Design of Morphed Aircraft 233
NeoCASS: An integrated tool for structural sizing, aeroelastic analysis and MDO at Conceptual Design Level 231
Design, manufacturing and validation of a gust generator for wind tunnel test of a large scale aeroelastic model 231
Aeroelastic Analysis of a Regional Aircraft with Active Camber Morphing Device 230
Aeroelastic Control of Morphing Wings 228
CS2-THT U-HARWARD Project: Final Assessment and Project Outcomes Evaluation 227
Design, Manufacturing and Preliminary Test Results of an Adaptive Wing Camber Model 226
Active Control of Three-Surface Aeroelastic Model 226
Wind Tunnel Testing of Gust Load Alleviation Performance of Flexible wing with Semi-Aeroelastic Hinge 225
A Two-Level Approach for the Optimal Design of Morphing Wings Based on Compliant Structures 225
Active Flutter Suppression Techniques in Aircraft Wings 225
An Optimization Procedure for the Optimal Design of Morphing Devices 225
Design and Testing of a Droop Nose Morphing for Advanced Regional Aircraft: Numerical and Experimental Validation 224
Experimental Identification and Control of Flutter Beyond the First Flutter Mechanism 223
Experimental Studies on Dynamic Freeplay Nonlinearity 223
Active Load Control of a Regional Aircraft Wing Equipped with Morphing Winglets 222
Preliminary Sizing of the Wing-Box Structure by Multi-Level Approach 221
Freeplay-Induced Limit-Cycle Oscillations in a T-Tail: Numerical vs Experimental Validation 220
PyPAD: a Multidisciplinary Framework for Preliminary Airframe Design 220
Aero-Servo-Elastic Optimization in Early Design Phases 220
Aeroservoelastic Response of Nonlinear Wind Tunnel Model to Non-Uniform Gust Field 219
Design of a Leading Edge Morphing Based on Compliant Structures in the Framework of the CS2-Airgreen2 Project 216
Experimental and performance validation of a full-scale morphing droop nose design based on composite compliant structures 215
Flow Field Around the Flapping Flag 215
Multi-Fidelity Design of Aeroelastic Wing Tip Devices 214
Aeroelastic Investigation and Design Improvements on a Three Surface Transport Airplane 213
Design of an Innovative Wing Tip Device 213
Aero-Structural Design Optimization of a Morphing Aileron Considering Actuation Aspects 212
A Two Levels Approach for the Optimal Design of Morphing Airfoils 212
Validation of Numerical Prediction of Dynamic Derivatives: the DLR-F12 and the Transcruiser Test Cases 212
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 209
Comparison Between Density-Based And Load-Pathbased Method In Various Camber Aerofoil Design 208
Integrated Servostructural Optimization in the Design of Aerospace Systems 206
Minimum-weight design for three dimensional woven composite stiffened panels using neural networks and genetic algorithms 206
Expected Performances 206
Multi-scale analysis and optimisation of three-dimensional woven composite structures combining response surface method and genetic algorithms 205
NeoCASS+, a Conceptual Design and Simulation Framework for Morphing Aircraft 202
Wind Tunnel Evaluation of a Static Output Feedback Controller for Gust Load Alleviation on a Regional Aircraft 202
Recent developments of NeoCass the open source suite for structural sizing and aeroelastic analysis 201
A Fast Tool for Structural Sizing, Aeroelastic Analysis and Optimization in Aircraft Conceptual Design 201
NeOPT: an Optimization Suite for the Aeroelastic Preliminary Design 199
Development of an Active Wingtip for Aeroelastic Control 198
Application of the Active Camber Morphing Concept Based on Compliant Structures to a Regional Aircraft 198
Wingbox Meta-Model and Aero-Servo-Elastic Optimization With NEOPT 197
Bringing Aeroelasticit Analysis in the Conceptual Design of Future Aircraft 196
Aeroelastic Testing on a Three Surface Airplane 196
Coupled CSD/CFD Non-Linear Aeroelastic Trim of Free-Flying Flexible Aircraft 193
SMorph - Smart Aircraft Morphing Technologies Project 193
Definition, Design Assessment and Parameterization of a Metasensor for LC&A and Load Monitoring Purposes 193
Model Updating and Aeroelastic Correlation of a Scaled Wind Tunnel Model for Active Flutter Suppression Test 193
A Multi-Level Procedure for the Preliminary Sizing of Aircraft Wing-Box Structures 191
An Italian Experience On Morphing Aircraft Systems 191
Knowledge-Based Shape Optimization of Morphing Wing for More Efficient Aircraft 191
Active Aeroelastic Control over a Four Control Surface Wind Tunnel Wing Model 190
Development of a Buffet Load Mitigation System Based on Multi-Surface Control 190
Totale 24.494
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Categoria #
all - tutte 102.168
article - articoli 28.040
book - libri 0
conference - conferenze 72.420
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 1.708
Totale 204.336
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2021/20221.853 0 223 112 156 223 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
2026/2027714 459 255 0 0 0 0 0 0 0 0 0 0
Totale 40.641