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

RICCI, SERGIO
 Distribuzione geografica
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Continente #
NA - Nord America 8.937
EU - Europa 5.921
AS - Asia 1.145
AF - Africa 148
SA - Sud America 26
OC - Oceania 20
Continente sconosciuto - Info sul continente non disponibili 7
Totale 16.204
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Nazione #
US - Stati Uniti d'America 8.763
IT - Italia 2.720
IE - Irlanda 645
UA - Ucraina 441
DE - Germania 403
SE - Svezia 368
VN - Vietnam 367
CN - Cina 327
GB - Regno Unito 311
AT - Austria 254
FI - Finlandia 243
CA - Canada 163
ES - Italia 156
CI - Costa d'Avorio 135
PH - Filippine 112
FR - Francia 99
NL - Olanda 98
BE - Belgio 84
JO - Giordania 66
IN - India 43
IR - Iran 36
KR - Corea 29
TR - Turchia 27
HK - Hong Kong 24
PK - Pakistan 20
PL - Polonia 20
AU - Australia 18
BR - Brasile 18
PT - Portogallo 18
CH - Svizzera 17
IL - Israele 17
JP - Giappone 17
ID - Indonesia 13
SG - Singapore 12
GR - Grecia 11
MX - Messico 11
RU - Federazione Russa 9
EU - Europa 7
MY - Malesia 7
SD - Sudan 7
TH - Thailandia 7
AE - Emirati Arabi Uniti 6
TW - Taiwan 6
MK - Macedonia 5
RO - Romania 4
AR - Argentina 3
AZ - Azerbaigian 3
CZ - Repubblica Ceca 3
MU - Mauritius 3
CL - Cile 2
DK - Danimarca 2
DZ - Algeria 2
EC - Ecuador 2
IQ - Iraq 2
NO - Norvegia 2
NZ - Nuova Zelanda 2
RS - Serbia 2
SA - Arabia Saudita 2
SI - Slovenia 2
AM - Armenia 1
BG - Bulgaria 1
CO - Colombia 1
HR - Croazia 1
KH - Cambogia 1
LT - Lituania 1
LU - Lussemburgo 1
MA - Marocco 1
Totale 16.204
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Città #
Fairfield 1.279
Milan 973
Woodbridge 961
Dublin 627
Ann Arbor 626
Houston 619
Chandler 609
Ashburn 608
Wilmington 598
Seattle 593
Cambridge 461
Jacksonville 254
Vienna 247
Dearborn 230
Dong Ket 183
Lawrence 170
Málaga 139
Abidjan 135
Medford 135
Ottawa 132
Rome 123
Davao City 108
Beijing 99
Helsinki 97
Redwood City 69
Amman 66
Des Moines 66
San Diego 64
Bovisio Masciago 58
Brussels 46
Monza 40
New York 40
Princeton 40
Auburn Hills 35
Busto Arsizio 35
Amsterdam 34
Changsha 34
Novara 34
Atvidaberg 31
Ciampino 30
Delft 30
Shanghai 29
Harbin 25
Zibido San Giacomo 25
Crema 24
Luft 22
Robbiate 22
Fremont 21
Norwalk 19
Washington 19
Gavirate 18
Gentbrugge 18
Istanbul 18
Cranfield 17
London 17
Mountain View 17
Xian 17
Edinburgh 14
Munich 14
Rho 14
Hamburg 13
Redmond 13
Turin 13
Verona 13
Braunschweig 12
Bristol 12
Hangzhou 12
Menlo Park 12
Bareggio 11
Los Angeles 11
Magdeburg 11
Paris 11
Torino 11
Isfahan 10
Montréal 10
Nanjing 10
Napoli 10
Seongnam 10
Swansea 10
Warsaw 10
Besana in Brianza 9
Boardman 9
Bresso 9
Central 9
Zhengzhou 9
Zurich 9
Bengaluru 8
Falls Church 8
Hefei 8
Krefeld 8
Madrid 8
Meda 8
Naples 8
Segrate 8
Seregno 8
Trecate 8
Varese 8
Brescia 7
Camburzano 7
Centro 7
Totale 11.516
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Nome #
Design and Wind Tunnel Test Validation of Gust Load Alleviation Systems 203
Compliant Structures-Based Wing and Wingtip Morphing Devices 196
Active Aeroelastic Control over a Multi-Surface Wing: Modelling and Wind Tunnel Testing 194
Development of a Wind Tunnel Model for Active Flutter Suppression Studies 191
Design of a Leading Edge Morphing Based on Compliant Structures for a Twin-Prop Regional Aircraft 179
Application of Active Camber Morphing Concept to a Regional Aircraft 170
Design, Manufacturing and Wind Tunnel Validation of a Morphing Compliant Wing 170
Introduction and application of PyPAD, a framework for multidisciplinary airframe design 161
PyPAD: a Multidisciplinary Framework for Preliminary Airframe Design 158
Aeroelastic Analysis of the CAWAPI F-16XL Configuration at Transonic Speeds 157
Flow Field Around the Flapping Flag 155
Structural Sizing, Aeroelastic Analysis, and Optimization in Aircraft Conceptual Design 153
Application of MDO Techniques to the Preliminary Design of Morphed Aircraft 152
Active Camber Morphing Wings Based on Compliant Structures: an Aeroelastic Assessment 152
Active Aeroelastic Control over a Four Control Surface Wing Model 151
Design, Manufacturing and Wind Tunnel Test of a Morphing Wing Based on Compliant Structures 151
Coupling Equivalent Plate and Beam Models at Conceptual Design Level 150
Computation of aeroelastic effects on F-16XL at flight conditions FC70 and FC25 141
Design of a wing tip device for active maneuver and gust load alleviation 140
Active Flutter Suppression Analysis and Wind Tunnel Studies of an Uncertain Commercial Transport Configuration 138
Buckling optimization of variable stiffness cylindrical shells through artificial intelligence techniques 138
Combining Density-based Approach and Optimization Refinement in the Design of Morphing Airfoil Structures 135
Gust Load Alleviation for a Regional Aircraft Through a Static Output Feedback 134
Freeplay-Induced Limit-Cycle Oscillations in a T-Tail: Numerical vs Experimental Validation 133
Estimated Performances of an Adaptive Trailing-Edge Device Aimed at Reducing Fuel Consumption on a Medium-Size Aircraft 129
Expected Performances 128
Active Load Control of a Regional Aircraft Wing Equipped with Morphing Winglets 128
Adaptive Trailing Edge: Specifications, Aerodynamics, and Exploitation 127
A Two-Level Approach for the Optimal Design of Morphing Wings Based on Compliant Structures 126
Multilevel Structural Optimization for Preliminary Wing-Box Weight Estimation 126
Multi-scale analysis and optimisation of three-dimensional woven composite structures combining response surface method and genetic algorithms 125
Validation of Numerical Prediction of Dynamic Derivatives: the DLR-F12 and the Transcruiser Test Cases 123
Numerical and experimental investigations on active flutter suppression technologies 121
Active Control of Three-Surface Aeroelastic Model 120
High Order Harmonic Balance Applied to an Aeroelastic T-Tail Model with a Control Surface Freeplay 119
Design, Manufacturing and Preliminary Test Results of an Adaptive Wing Camber Model 118
Minimum-weight design for three dimensional woven composite stiffened panels using neural networks and genetic algorithms 118
Active Aeroelastic Control over a Multisurface Wing: Modeling and Wind-Tunnel Testing 118
NeoCASS: An integrated tool for structural sizing, aeroelastic analysis and MDO at Conceptual Design Level 117
An Optimization Procedure for the Optimal Design of Morphing Devices 117
Design of a Leading Edge Morphing Based on Compliant Structures in the Framework of the CS2-Airgreen2 Project 117
Increasing Updated FE Model Fidelity using a Generalized Delta Stick Model Approach 116
Multi-Fidelity Design of Aeroelastic Wing Tip Devices 114
Application of the Active Camber Morphing Concept Based on Compliant Structures to a Regional Aircraft 114
Aeroservoelastic Response of Nonlinear Wind Tunnel Model to Non-Uniform Gust Field 113
Aeroelastic analysis of a slender wing 111
Coupled CSD/CFD Non-Linear Aeroelastic Trim of Free-Flying Flexible Aircraft 109
Active Flutter Suppression Techniques in Aircraft Wings 109
Wind Tunnel Evaluation of a Static Output Feedback Controller for Gust Load Alleviation on a Regional Aircraft 109
Structural Damage Detection Using Nonlinear Vibrations 108
Best Achievable Modal Eigenvectors in Structural Damage Detection 107
Advanced Design of a Full-Scale Active Morphing Droop Nose 105
Gradient-Based Aerodynamic Optimization of an Airfoil with Morphing Leading and Trailing Edges 105
Knowledge-Based Shape Optimization of Morphing Wing for More Efficient Aircraft 104
An Active Flutter Suppression (AFS) Project: Overview, Results and Lessons Learned 104
Airgreen2 - Clean Sky 2 Programme: Adaptive Wing Technology Maturation, Challenges and Perspectives 104
Active Control for Buffet Load Alleviation on the Fin of a High Performance Training Aircraft 103
NeoCASS+, a Conceptual Design and Simulation Framework for Morphing Aircraft 100
Non-Linear Spacecraft Component Parameters Identification Based on Experimental Results and Finite Element Modelling 100
Aeroelastic Investigation and Design Improvements on a Three Surface Transport Airplane 99
A Fast Tool for Structural Sizing, Aeroelastic Analysis and Optimization in Aircraft Conceptual Design 99
Size and Topological Optimization for Crashworthiness Design of Helicopter Subfloor 98
A Two Levels Approach for the Optimal Design of Morphing Airfoils 98
Aeroelastic Optimization of High Aspect Ratio Wings for Environmentally Friendly Aircraft 98
Experimental Investigations of a Vibration Suppression System for a Three Surface Aeroelastic Model 97
PyPAD: a Multidisciplinary Framework for Preliminary Airframe Design 97
Design of an Innovative Wing Tip Device 97
Comparison Between Density-Based And Load-Pathbased Method In Various Camber Aerofoil Design 97
NeoCASS: an Integrated Tool for Structural Sizing, Aeroelastic Analysis and MDO at Conceptual Design Level 96
Wind Tunnel Experimental Validation of Future Green Regional A/C Gust Load Alleviation Control System 95
Aeroelastic Analysis of a Regional Aircraft with Active Camber Morphing Device 93
Design, manufacturing and validation of a gust generator for wind tunnel test of a large scale aeroelastic model 93
Aeroelastic Testing on a Three Surface Airplane 92
Use of MDO Techniques for the Design of Morphing Aircraft 91
Ground Modal Tests of Space-structure Components Using Boundary Masses 90
Experimental and Numerical Investigation of the Behavior of a T-Tail with Control Surface Freeplay 90
Experimental Modal Analysis of Large Structures by Substructuring 90
Crashworthiness Optimization of Helicopter Subfloor Based on Decomposition and Global Approximation 89
Aeroservoelastic Optimization of a High Aspect Transport Wing with Morphing Trailing Edge 89
Aeroelastic Multi-Surface Roll Control of a Three Surfaces Wind Tunnel Model 88
Winbox Weight Estimation for Metallic and Composite Manufacturing in a Conceptual Design Phase 88
Preliminary Sizing of the Wing-Box Structure by Multi-Level Approach 86
NeoCASS+, a Conceptual Design and Simulation Framework for Morphing Aircraft 86
Hexapod Mechanical Assembly Modal Survey Test 85
Integrated Servostructural Optimization in the Design of Aerospace Systems 84
Coupling MDO and Principal Component Analysis Techniques for Model Updating and Damage Detection 84
Rapid Prediction of Worst Case Gust Loads 84
Design and Experimental Validation of Gust Load Alleviation Systems Based on Static Output Feedback 84
Improving Aircraft Performances Using Active Wing Camber Control: Numerical and Experimental Validation on a Multi-Control Surfaces Forward Swept Wing Model 83
An Italian Experience On Morphing Aircraft Systems 83
Analytical and Experimental Evaluation of Multivariable Stability Margins in Active Flutter Suppression Wind Tunnel Tests 83
Aeroelastic Analysis and Optimization at Conceptual Design Level Using Neocass Suite 82
Size and Topological Optimization for Crashworthiness Design of Helicopter Subfloor 81
Optimization of compliant adaptive structures in the design of a morphing droop nose 81
Wind Tunnel Testing of an Active Controlled Wing Under Gust Excitation 80
A Multi-Level Approach to Preliminary Optimization of a Wing Structure 79
Gust Loads Assessment: a Multi-Fidelity Approach 79
Generazione delle condizioni di carico per il progetto preliminare a fatica dei velivoli 78
Dynamic Response Analysis and Experimental Validation of the X-DIA Demonstrator Component Model 78
AFS-Active Flutter Suppression Project: Activities Overview and Final Results 78
Totale 11.436
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Categoria #
all - tutte 40.989
article - articoli 12.312
book - libri 0
conference - conferenze 27.855
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 822
Totale 81.978
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2018/2019987 0 0 0 0 0 0 0 0 0 0 543 444
2019/20203.520 289 201 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
2023/20241.387 97 206 67 154 133 145 216 64 80 217 8 0
Totale 16.383