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

RICCI, SERGIO
 Distribuzione geografica
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Continente #
NA - Nord America 8.977
EU - Europa 6.191
AS - Asia 1.348
AF - Africa 149
SA - Sud America 37
OC - Oceania 20
Continente sconosciuto - Info sul continente non disponibili 7
Totale 16.729
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Nazione #
US - Stati Uniti d'America 8.802
IT - Italia 2.899
IE - Irlanda 661
UA - Ucraina 443
DE - Germania 418
SE - Svezia 368
VN - Vietnam 368
CN - Cina 341
GB - Regno Unito 329
AT - Austria 257
FI - Finlandia 249
SG - Singapore 179
CA - Canada 164
ES - Italia 156
CI - Costa d'Avorio 135
NL - Olanda 118
PH - Filippine 112
FR - Francia 101
BE - Belgio 85
JO - Giordania 66
IN - India 44
IR - Iran 39
KR - Corea 31
HK - Hong Kong 29
TR - Turchia 27
PK - Pakistan 20
PL - Polonia 20
AU - Australia 18
BR - Brasile 18
JP - Giappone 18
PT - Portogallo 18
CH - Svizzera 17
IL - Israele 17
ID - Indonesia 13
CO - Colombia 11
GR - Grecia 11
MX - Messico 11
RU - Federazione Russa 9
TW - Taiwan 9
MY - Malesia 8
AE - Emirati Arabi Uniti 7
EU - Europa 7
SD - Sudan 7
TH - Thailandia 7
MK - Macedonia 5
LT - Lituania 4
NO - Norvegia 4
RO - Romania 4
AR - Argentina 3
AZ - Azerbaigian 3
CL - Cile 3
CZ - Repubblica Ceca 3
MU - Mauritius 3
DK - Danimarca 2
DZ - Algeria 2
EC - Ecuador 2
IQ - Iraq 2
KH - Cambogia 2
NZ - Nuova Zelanda 2
RS - Serbia 2
SA - Arabia Saudita 2
SI - Slovenia 2
AM - Armenia 1
BD - Bangladesh 1
BG - Bulgaria 1
BY - Bielorussia 1
EG - Egitto 1
HR - Croazia 1
KZ - Kazakistan 1
LA - Repubblica Popolare Democratica del Laos 1
LU - Lussemburgo 1
LV - Lettonia 1
MA - Marocco 1
SK - Slovacchia (Repubblica Slovacca) 1
Totale 16.729
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Città #
Fairfield 1.279
Milan 1.106
Woodbridge 961
Dublin 643
Ashburn 630
Ann Arbor 626
Houston 619
Chandler 609
Wilmington 598
Seattle 593
Cambridge 465
Jacksonville 254
Vienna 250
Dearborn 230
Dong Ket 183
Lawrence 170
Málaga 139
Abidjan 135
Medford 135
Ottawa 132
Rome 123
Davao City 108
Beijing 99
Helsinki 99
Singapore 96
Redwood City 69
Amman 66
Des Moines 66
San Diego 64
Bovisio Masciago 58
Amsterdam 49
Brussels 47
New York 41
Monza 40
Princeton 40
Auburn Hills 35
Busto Arsizio 35
Changsha 34
Novara 34
Shanghai 32
Atvidaberg 31
Ciampino 30
Delft 30
Giussano 26
Harbin 25
Zibido San Giacomo 25
Crema 24
Luft 22
Robbiate 22
Fremont 21
Washington 20
Norwalk 19
Gavirate 18
Gentbrugge 18
Istanbul 18
Cranfield 17
London 17
Mountain View 17
Xian 17
Munich 16
Braunschweig 15
Bristol 14
Edinburgh 14
Rho 14
Hamburg 13
Redmond 13
Turin 13
Verona 13
Brescia 12
Hangzhou 12
Menlo Park 12
Seregno 12
Bareggio 11
Los Angeles 11
Magdeburg 11
Paris 11
Torino 11
Boardman 10
Bogotá 10
Isfahan 10
Montréal 10
Nanjing 10
Naples 10
Napoli 10
Seongnam 10
Swansea 10
Warsaw 10
Besana in Brianza 9
Bresso 9
Central 9
Lappeenranta 9
Zhengzhou 9
Zurich 9
Bengaluru 8
Falls Church 8
Hefei 8
Krefeld 8
Madrid 8
Meda 8
Segrate 8
Totale 11.847
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Nome #
Design and Wind Tunnel Test Validation of Gust Load Alleviation Systems 205
Compliant Structures-Based Wing and Wingtip Morphing Devices 198
Active Aeroelastic Control over a Multi-Surface Wing: Modelling and Wind Tunnel Testing 195
Development of a Wind Tunnel Model for Active Flutter Suppression Studies 193
Design, Manufacturing and Wind Tunnel Validation of a Morphing Compliant Wing 183
Design of a Leading Edge Morphing Based on Compliant Structures for a Twin-Prop Regional Aircraft 181
Application of Active Camber Morphing Concept to a Regional Aircraft 171
Introduction and application of PyPAD, a framework for multidisciplinary airframe design 162
PyPAD: a Multidisciplinary Framework for Preliminary Airframe Design 160
Aeroelastic Analysis of the CAWAPI F-16XL Configuration at Transonic Speeds 159
Flow Field Around the Flapping Flag 157
Structural Sizing, Aeroelastic Analysis, and Optimization in Aircraft Conceptual Design 154
Coupling Equivalent Plate and Beam Models at Conceptual Design Level 154
Application of MDO Techniques to the Preliminary Design of Morphed Aircraft 153
Active Camber Morphing Wings Based on Compliant Structures: an Aeroelastic Assessment 153
Design, Manufacturing and Wind Tunnel Test of a Morphing Wing Based on Compliant Structures 153
Active Aeroelastic Control over a Four Control Surface Wing Model 152
Computation of aeroelastic effects on F-16XL at flight conditions FC70 and FC25 145
Optimization of compliant adaptive structures in the design of a morphing droop nose 144
Design of a wing tip device for active maneuver and gust load alleviation 143
Active Flutter Suppression Analysis and Wind Tunnel Studies of an Uncertain Commercial Transport Configuration 140
Buckling optimization of variable stiffness cylindrical shells through artificial intelligence techniques 140
Combining Density-based Approach and Optimization Refinement in the Design of Morphing Airfoil Structures 136
Freeplay-Induced Limit-Cycle Oscillations in a T-Tail: Numerical vs Experimental Validation 135
Gust Load Alleviation for a Regional Aircraft Through a Static Output Feedback 134
Estimated Performances of an Adaptive Trailing-Edge Device Aimed at Reducing Fuel Consumption on a Medium-Size Aircraft 132
Numerical and experimental investigations on active flutter suppression technologies 130
Expected Performances 129
Active Load Control of a Regional Aircraft Wing Equipped with Morphing Winglets 129
Multilevel Structural Optimization for Preliminary Wing-Box Weight Estimation 128
Adaptive Trailing Edge: Specifications, Aerodynamics, and Exploitation 128
A Two-Level Approach for the Optimal Design of Morphing Wings Based on Compliant Structures 127
Multi-scale analysis and optimisation of three-dimensional woven composite structures combining response surface method and genetic algorithms 126
Validation of Numerical Prediction of Dynamic Derivatives: the DLR-F12 and the Transcruiser Test Cases 124
Active Control of Three-Surface Aeroelastic Model 122
Wind Tunnel Evaluation of a Static Output Feedback Controller for Gust Load Alleviation on a Regional Aircraft 121
Active Aeroelastic Control over a Multisurface Wing: Modeling and Wind-Tunnel Testing 121
Aeroelastic analysis of a slender wing 121
High Order Harmonic Balance Applied to an Aeroelastic T-Tail Model with a Control Surface Freeplay 120
Design, Manufacturing and Preliminary Test Results of an Adaptive Wing Camber Model 119
Minimum-weight design for three dimensional woven composite stiffened panels using neural networks and genetic algorithms 119
NeoCASS: An integrated tool for structural sizing, aeroelastic analysis and MDO at Conceptual Design Level 118
An Optimization Procedure for the Optimal Design of Morphing Devices 118
Design of a Leading Edge Morphing Based on Compliant Structures in the Framework of the CS2-Airgreen2 Project 118
Increasing Updated FE Model Fidelity using a Generalized Delta Stick Model Approach 116
Advanced Design of a Full-Scale Active Morphing Droop Nose 116
Multi-Fidelity Design of Aeroelastic Wing Tip Devices 115
Application of the Active Camber Morphing Concept Based on Compliant Structures to a Regional Aircraft 115
Gradient-Based Aerodynamic Optimization of an Airfoil with Morphing Leading and Trailing Edges 114
Aeroservoelastic Response of Nonlinear Wind Tunnel Model to Non-Uniform Gust Field 113
Active Flutter Suppression Techniques in Aircraft Wings 111
Coupled CSD/CFD Non-Linear Aeroelastic Trim of Free-Flying Flexible Aircraft 110
Best Achievable Modal Eigenvectors in Structural Damage Detection 108
Structural Damage Detection Using Nonlinear Vibrations 108
An Active Flutter Suppression (AFS) Project: Overview, Results and Lessons Learned 106
Knowledge-Based Shape Optimization of Morphing Wing for More Efficient Aircraft 105
Airgreen2 - Clean Sky 2 Programme: Adaptive Wing Technology Maturation, Challenges and Perspectives 105
Aeroelastic Investigation and Design Improvements on a Three Surface Transport Airplane 104
Active Control for Buffet Load Alleviation on the Fin of a High Performance Training Aircraft 103
Design of an Innovative Wing Tip Device 101
Aeroelastic Optimization of High Aspect Ratio Wings for Environmentally Friendly Aircraft 101
NeoCASS+, a Conceptual Design and Simulation Framework for Morphing Aircraft 100
Wind Tunnel Experimental Validation of Future Green Regional A/C Gust Load Alleviation Control System 100
Non-Linear Spacecraft Component Parameters Identification Based on Experimental Results and Finite Element Modelling 100
Comparison Between Density-Based And Load-Pathbased Method In Various Camber Aerofoil Design 100
A Fast Tool for Structural Sizing, Aeroelastic Analysis and Optimization in Aircraft Conceptual Design 100
A Two Levels Approach for the Optimal Design of Morphing Airfoils 99
Experimental Investigations of a Vibration Suppression System for a Three Surface Aeroelastic Model 98
Size and Topological Optimization for Crashworthiness Design of Helicopter Subfloor 98
PyPAD: a Multidisciplinary Framework for Preliminary Airframe Design 98
Design, manufacturing and validation of a gust generator for wind tunnel test of a large scale aeroelastic model 98
NeoCASS: an Integrated Tool for Structural Sizing, Aeroelastic Analysis and MDO at Conceptual Design Level 97
Wind Tunnel System for Active Flutter Suppression Research: Overview and Insights 94
Aeroelastic Analysis of a Regional Aircraft with Active Camber Morphing Device 94
Aeroelastic Testing on a Three Surface Airplane 93
Winbox Weight Estimation for Metallic and Composite Manufacturing in a Conceptual Design Phase 92
Use of MDO Techniques for the Design of Morphing Aircraft 92
Ground Modal Tests of Space-structure Components Using Boundary Masses 91
Experimental and Numerical Investigation of the Behavior of a T-Tail with Control Surface Freeplay 91
Experimental Modal Analysis of Large Structures by Substructuring 91
Aeroservoelastic Optimization of a High Aspect Transport Wing with Morphing Trailing Edge 91
Crashworthiness Optimization of Helicopter Subfloor Based on Decomposition and Global Approximation 90
Aeroelastic Multi-Surface Roll Control of a Three Surfaces Wind Tunnel Model 89
Preliminary Sizing of the Wing-Box Structure by Multi-Level Approach 88
NeoCASS+, a Conceptual Design and Simulation Framework for Morphing Aircraft 87
Hexapod Mechanical Assembly Modal Survey Test 86
Analytical and Experimental Evaluation of Multivariable Stability Margins in Active Flutter Suppression Wind Tunnel Tests 86
Design and Experimental Validation of Gust Load Alleviation Systems Based on Static Output Feedback 86
Integrated Servostructural Optimization in the Design of Aerospace Systems 85
Coupling MDO and Principal Component Analysis Techniques for Model Updating and Damage Detection 85
Rapid Prediction of Worst Case Gust Loads 85
An Italian Experience On Morphing Aircraft Systems 84
Improving Aircraft Performances Using Active Wing Camber Control: Numerical and Experimental Validation on a Multi-Control Surfaces Forward Swept Wing Model 83
Aeroelastic Analysis and Optimization at Conceptual Design Level Using Neocass Suite 83
Size and Topological Optimization for Crashworthiness Design of Helicopter Subfloor 82
A Multi-Level Approach to Preliminary Optimization of a Wing Structure 81
Active Aeroelastic Control over a Four Control Surface Wind Tunnel Wing Model 81
Wind Tunnel Testing of an Active Controlled Wing Under Gust Excitation 81
AFS-Active Flutter Suppression Project: Activities Overview and Final Results 81
Generazione delle condizioni di carico per il progetto preliminare a fatica dei velivoli 79
Totale 11.720
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Categoria #
all - tutte 44.634
article - articoli 13.335
book - libri 0
conference - conferenze 30.420
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 879
Totale 89.268
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2019/20203.231 0 201 66 278 481 414 445 306 390 189 313 148
2020/20212.392 214 154 213 121 177 151 166 248 165 200 154 429
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
2024/2025256 238 18 0 0 0 0 0 0 0 0 0 0
Totale 16.910