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

RICCI, SERGIO
 Distribuzione geografica
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Continente #
NA - Nord America 14.565
EU - Europa 14.043
AS - Asia 7.567
SA - Sud America 1.373
AF - Africa 438
OC - Oceania 46
Continente sconosciuto - Info sul continente non disponibili 9
Totale 38.041
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Nazione #
US - Stati Uniti d'America 14.244
RU - Federazione Russa 5.362
IT - Italia 3.934
SG - Singapore 2.216
CN - Cina 2.058
VN - Vietnam 1.429
BR - Brasile 1.146
DE - Germania 708
IE - Irlanda 707
FR - Francia 472
GB - Regno Unito 458
UA - Ucraina 457
FI - Finlandia 421
SE - Svezia 388
KR - Corea 384
AT - Austria 341
NL - Olanda 286
JP - Giappone 269
CA - Canada 226
HK - Hong Kong 215
ES - Italia 192
MA - Marocco 181
CI - Costa d'Avorio 143
IN - India 140
PH - Filippine 129
ID - Indonesia 98
BE - Belgio 87
TR - Turchia 84
AR - Argentina 83
BD - Bangladesh 80
JO - Giordania 78
PL - Polonia 62
IQ - Iraq 54
MX - Messico 53
IR - Iran 50
PK - Pakistan 50
ZA - Sudafrica 41
AU - Australia 39
EC - Ecuador 37
TW - Taiwan 37
PT - Portogallo 29
CO - Colombia 28
IL - Israele 25
LT - Lituania 22
CH - Svizzera 21
SA - Arabia Saudita 21
AE - Emirati Arabi Uniti 19
UZ - Uzbekistan 19
VE - Venezuela 19
GR - Grecia 18
TH - Thailandia 18
PY - Paraguay 17
CL - Cile 16
MY - Malesia 14
AZ - Azerbaigian 13
KE - Kenya 13
NP - Nepal 11
UY - Uruguay 11
CZ - Repubblica Ceca 10
DZ - Algeria 10
PE - Perù 10
KZ - Kazakistan 9
OM - Oman 9
BJ - Benin 8
EG - Egitto 7
EU - Europa 7
HU - Ungheria 7
LB - Libano 7
NO - Norvegia 7
RO - Romania 7
SD - Sudan 7
DK - Danimarca 6
NZ - Nuova Zelanda 6
TN - Tunisia 6
TT - Trinidad e Tobago 6
BO - Bolivia 5
GT - Guatemala 5
MK - Macedonia 5
PA - Panama 5
SI - Slovenia 5
AL - Albania 4
AM - Armenia 4
AO - Angola 4
BG - Bulgaria 4
CR - Costa Rica 4
DO - Repubblica Dominicana 4
HN - Honduras 4
JM - Giamaica 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
MU - Mauritius 3
Totale 38.000
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Città #
Ashburn 1.806
Milan 1.768
Fairfield 1.279
Singapore 1.210
San Jose 1.110
Woodbridge 961
Moscow 762
Dublin 689
Ann Arbor 628
Houston 627
Chandler 609
Wilmington 601
Seattle 599
Cambridge 465
Hefei 456
Santa Clara 418
Ho Chi Minh City 345
Seoul 340
The Dalles 338
Beijing 314
Vienna 308
Council Bluffs 271
Jacksonville 260
Hanoi 248
Helsinki 241
Dearborn 230
Tokyo 229
Boardman 222
Los Angeles 216
Dallas 201
Kent 194
Lauterbourg 185
Dong Ket 183
Lawrence 170
Rome 168
North Charleston 162
Hong Kong 151
Abidjan 143
Málaga 139
Medford 135
Ottawa 133
Kenitra 125
Buffalo 118
Amsterdam 110
Davao City 110
New York 102
São Paulo 102
Shanghai 78
Amman 77
Frankfurt am Main 71
Chicago 69
Des Moines 69
Redwood City 69
San Diego 66
Jakarta 62
Orem 60
Bovisio Masciago 58
Da Nang 55
Las Vegas 54
Changsha 51
Brussels 48
Haiphong 47
Guangzhou 46
Delft 44
Munich 44
Busto Arsizio 42
Falkenstein 42
Monza 42
Casablanca 41
Princeton 40
Rio de Janeiro 39
Warsaw 39
Istanbul 38
Auburn Hills 35
Novara 34
Turin 34
Atvidaberg 31
Ciampino 30
Xi'an 30
Harbin 29
Paris 29
London 27
Brasília 26
Brooklyn 26
Giussano 26
Naples 25
Zibido San Giacomo 25
Crema 24
Lappeenranta 24
Muggiò 24
Pedrengo 24
Taipei 24
Tianjin 24
Chennai 23
Hangzhou 23
Hải Dương 23
Lecco 23
Washington 23
Boltiere 22
Luft 22
Totale 22.282
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Nome #
Gradient-Based Aerodynamic Optimization of an Airfoil with Morphing Leading and Trailing Edges 346
Active Aeroelastic Control over a Multi-Surface Wing: Modelling and Wind Tunnel Testing 341
Development of a Wind Tunnel Model for Active Flutter Suppression Studies 340
Wind Tunnel System for Active Flutter Suppression Research: Overview and Insights 335
Design and Wind Tunnel Test Validation of Gust Load Alleviation Systems 332
Compliant Structures-Based Wing and Wingtip Morphing Devices 327
Combining Density-based Approach and Optimization Refinement in the Design of Morphing Airfoil Structures 327
Aeroservoelastic Optimization of a High Aspect Transport Wing with Morphing Trailing Edge 322
Active Flutter Suppression Analysis and Wind Tunnel Studies of an Uncertain Commercial Transport Configuration 319
Numerical and experimental investigations on active flutter suppression technologies 316
Aeroelastic analysis of a slender wing 286
Design, Manufacturing and Wind Tunnel Validation of a Morphing Compliant Wing 281
Coupling Equivalent Plate and Beam Models at Conceptual Design Level 278
U-HARWARD: a CS2 EU Funded Project Aiming at the Design of Ultra High Aspect Ratio Wings Aircraft 278
Aeroelastic Analysis of the CAWAPI F-16XL Configuration at Transonic Speeds 276
Optimization of compliant adaptive structures in the design of a morphing droop nose 275
An Active Flutter Suppression (AFS) Project: Overview, Results and Lessons Learned 272
Extended computational capabilities for high-fidelity fluid–structure simulations 265
Gust and Manouvre Loads Alleviation Technologies: Overview, Results and Lesson Learned in the Framework of the CS2 AIRGREEN2 Project 262
Design and Experimental Validation of Gust Load Alleviation Systems Based on Static Output Feedback 262
Introduction and application of PyPAD, a framework for multidisciplinary airframe design 261
Aeroelastic Optimization of High Aspect Ratio Wings for Environmentally Friendly Aircraft 260
Active Camber Morphing Wings Based on Compliant Structures: an Aeroelastic Assessment 259
Design of a Leading Edge Morphing Based on Compliant Structures for a Twin-Prop Regional Aircraft 257
A Meta-Model for composite wingbox sizing in aircraft conceptual design 256
Computation of aeroelastic effects on F-16XL at flight conditions FC70 and FC25 256
Structural Sizing, Aeroelastic Analysis, and Optimization in Aircraft Conceptual Design 254
Design, Manufacturing and Wind Tunnel Test of a Morphing Wing Based on Compliant Structures 249
Design of a wing tip device for active maneuver and gust load alleviation 248
PyPAD: a Multidisciplinary Framework for Preliminary Airframe Design 248
Active Aeroelastic Control over a Multisurface Wing: Modeling and Wind-Tunnel Testing 247
Active Aeroelastic Control over a Four Control Surface Wing Model 245
Gust Load Alleviation for a Regional Aircraft Through a Static Output Feedback 245
Preliminary Aero-Elastic Optimization of a Twin-Aisle Long-Haul Aircraft with Increased Aspect Ratio 244
Adaptive Trailing Edge: Specifications, Aerodynamics, and Exploitation 240
Advanced Design of a Full-Scale Active Morphing Droop Nose 240
AFS-Active Flutter Suppression Project: Activities Overview and Final Results 238
Application of Active Camber Morphing Concept to a Regional Aircraft 235
Multilevel Structural Optimization for Preliminary Wing-Box Weight Estimation 235
Buckling optimization of variable stiffness cylindrical shells through artificial intelligence techniques 233
Analytical and Experimental Evaluation of Multivariable Stability Margins in Active Flutter Suppression Wind Tunnel Tests 231
Application of MDO Techniques to the Preliminary Design of Morphed Aircraft 229
Use of MDO Techniques for the Design of Morphing Aircraft 229
Aeroelastic Control of Morphing Wings 223
NeoCASS: An integrated tool for structural sizing, aeroelastic analysis and MDO at Conceptual Design Level 220
Aeroelastic Analysis of a Regional Aircraft with Active Camber Morphing Device 219
A Two-Level Approach for the Optimal Design of Morphing Wings Based on Compliant Structures 218
Design and Testing of a Droop Nose Morphing for Advanced Regional Aircraft: Numerical and Experimental Validation 217
Design, manufacturing and validation of a gust generator for wind tunnel test of a large scale aeroelastic model 217
Active Control of Three-Surface Aeroelastic Model 216
An Optimization Procedure for the Optimal Design of Morphing Devices 215
Experimental Identification and Control of Flutter Beyond the First Flutter Mechanism 213
PyPAD: a Multidisciplinary Framework for Preliminary Airframe Design 213
Active Flutter Suppression Techniques in Aircraft Wings 212
Preliminary Sizing of the Wing-Box Structure by Multi-Level Approach 211
Flow Field Around the Flapping Flag 211
Active Load Control of a Regional Aircraft Wing Equipped with Morphing Winglets 211
Design, Manufacturing and Preliminary Test Results of an Adaptive Wing Camber Model 210
Aeroservoelastic Response of Nonlinear Wind Tunnel Model to Non-Uniform Gust Field 210
Design of a Leading Edge Morphing Based on Compliant Structures in the Framework of the CS2-Airgreen2 Project 209
Aeroelastic Investigation and Design Improvements on a Three Surface Transport Airplane 208
Aero-Servo-Elastic Optimization in Early Design Phases 208
Experimental Studies on Dynamic Freeplay Nonlinearity 207
Multi-Fidelity Design of Aeroelastic Wing Tip Devices 206
A Multi-Level Approach to Preliminary Optimization of a Wing Structure 205
A Two Levels Approach for the Optimal Design of Morphing Airfoils 205
Active Control for Buffet Load Alleviation on the Fin of a High Performance Training Aircraft 205
Aero-Structural Design Optimization of a Morphing Aileron Considering Actuation Aspects 204
Experimental and performance validation of a full-scale morphing droop nose design based on composite compliant structures 204
Comparison Between Density-Based And Load-Pathbased Method In Various Camber Aerofoil Design 204
Validation of Numerical Prediction of Dynamic Derivatives: the DLR-F12 and the Transcruiser Test Cases 203
Design of an Innovative Wing Tip Device 201
Integrated Servostructural Optimization in the Design of Aerospace Systems 199
Expected Performances 198
A Fast Tool for Structural Sizing, Aeroelastic Analysis and Optimization in Aircraft Conceptual Design 198
Wind Tunnel Testing of Gust Load Alleviation Performance of Flexible wing with Semi-Aeroelastic Hinge 195
Minimum-weight design for three dimensional woven composite stiffened panels using neural networks and genetic algorithms 195
Wind Tunnel Evaluation of a Static Output Feedback Controller for Gust Load Alleviation on a Regional Aircraft 195
Multi-scale analysis and optimisation of three-dimensional woven composite structures combining response surface method and genetic algorithms 194
Morphing Wing Technologies within the Airgreen 2 Project 194
Aeroelastic Testing on a Three Surface Airplane 193
Freeplay-Induced Limit-Cycle Oscillations in a T-Tail: Numerical vs Experimental Validation 191
NeoCASS+, a Conceptual Design and Simulation Framework for Morphing Aircraft 191
Application of the Active Camber Morphing Concept Based on Compliant Structures to a Regional Aircraft 190
CS2-THT U-HARWARD Project: Final Assessment and Project Outcomes Evaluation 189
Bringing Aeroelasticit Analysis in the Conceptual Design of Future Aircraft 188
Knowledge-Based Shape Optimization of Morphing Wing for More Efficient Aircraft 188
Wingbox Meta-Model and Aero-Servo-Elastic Optimization With NEOPT 188
SMorph - Smart Aircraft Morphing Technologies Project 186
Coupled CSD/CFD Non-Linear Aeroelastic Trim of Free-Flying Flexible Aircraft 184
Estimated Performances of an Adaptive Trailing-Edge Device Aimed at Reducing Fuel Consumption on a Medium-Size Aircraft 183
An Italian Experience On Morphing Aircraft Systems 183
Model Updating and Aeroelastic Correlation of a Scaled Wind Tunnel Model for Active Flutter Suppression Test 183
Active Aeroelastic Control over a Four Control Surface Wind Tunnel Wing Model 182
Gust Loads Assessment: a Multi-Fidelity Approach 182
A Multi-Level Procedure for the Preliminary Sizing of Aircraft Wing-Box Structures 181
NeOPT: an Optimization Suite for the Aeroelastic Preliminary Design 181
Recent developments of NeoCass the open source suite for structural sizing and aeroelastic analysis 180
A Multi-Level Procedure for the Preliminary Sizing of Aircraft Wing-Box Structures 179
Design of an Innovative Wing Tip for Aeroelastic Control: from Scratch to Flight Test 177
Totale 23.051
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Categoria #
all - tutte 92.841
article - articoli 25.701
book - libri 0
conference - conferenze 65.563
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 1.577
Totale 185.682
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/2021783 0 0 0 0 0 0 0 0 0 200 154 429
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
2025/202615.415 3.531 2.437 922 1.084 802 868 2.549 889 968 1.365 0 0
Totale 38.243