CINECA IRIS Institutional Research Information System

FREDIANI, ALDO
 Distribuzione geografica
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Continente #
NA - Nord America 10.834
AS - Asia 6.489
EU - Europa 6.226
SA - Sud America 822
Continente sconosciuto - Info sul continente non disponibili 254
AF - Africa 227
OC - Oceania 25
Totale 24.877
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Nazione #
US - Stati Uniti d'America 10.324
IT - Italia 2.237
CN - Cina 1.900
SG - Singapore 1.782
HK - Hong Kong 987
SE - Svezia 933
BR - Brasile 649
DE - Germania 482
BG - Bulgaria 431
VN - Vietnam 420
GB - Regno Unito 400
CA - Canada 393
KR - Corea 367
FR - Francia 329
UA - Ucraina 323
TR - Turchia 262
FI - Finlandia 257
IN - India 205
RU - Federazione Russa 204
JP - Giappone 189
CH - Svizzera 180
AT - Austria 136
NL - Olanda 100
BD - Bangladesh 85
IQ - Iraq 51
CO - Colombia 44
ES - Italia 43
MX - Messico 42
ZA - Sudafrica 41
CI - Costa d'Avorio 40
SA - Arabia Saudita 38
AR - Argentina 37
GR - Grecia 37
SN - Senegal 37
PK - Pakistan 35
BE - Belgio 33
VE - Venezuela 32
IE - Irlanda 26
JM - Giamaica 23
UZ - Uzbekistan 23
AU - Australia 22
PL - Polonia 17
KE - Kenya 16
MA - Marocco 16
EC - Ecuador 15
EG - Egitto 15
TN - Tunisia 15
TT - Trinidad e Tobago 15
PH - Filippine 14
BJ - Benin 13
EU - Europa 13
IL - Israele 13
AZ - Azerbaigian 12
BO - Bolivia 11
PE - Perù 11
HN - Honduras 10
ID - Indonesia 10
AE - Emirati Arabi Uniti 9
AL - Albania 9
HU - Ungheria 9
OM - Oman 9
DZ - Algeria 8
IR - Iran 8
RO - Romania 8
JO - Giordania 7
KZ - Kazakistan 7
PT - Portogallo 7
PY - Paraguay 7
UY - Uruguay 7
BH - Bahrain 6
LB - Libano 6
AM - Armenia 5
CL - Cile 5
CR - Costa Rica 5
CZ - Repubblica Ceca 5
KG - Kirghizistan 5
NP - Nepal 5
AO - Angola 4
BB - Barbados 4
CG - Congo 4
ET - Etiopia 4
GY - Guiana 4
MY - Malesia 4
PS - Palestinian Territory 4
HR - Croazia 3
NI - Nicaragua 3
TW - Taiwan 3
BA - Bosnia-Erzegovina 2
BM - Bermuda 2
BY - Bielorussia 2
CY - Cipro 2
DK - Danimarca 2
DO - Repubblica Dominicana 2
KH - Cambogia 2
KW - Kuwait 2
LK - Sri Lanka 2
LT - Lituania 2
MN - Mongolia 2
NG - Nigeria 2
NZ - Nuova Zelanda 2
Totale 24.595
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Città #
Woodbridge 1.038
Ashburn 995
Singapore 972
Hong Kong 967
Ann Arbor 804
Milan 762
Chandler 701
Santa Clara 647
Houston 635
San Jose 537
Jacksonville 467
Hefei 446
Sofia 430
Fairfield 389
Beijing 348
Seoul 339
Dallas 320
Ottawa 317
New York 263
Wilmington 222
Shanghai 217
Boardman 198
Seattle 197
Los Angeles 180
Princeton 172
Nanjing 168
Tokyo 166
Serra 162
Lawrence 158
Chicago 149
Izmir 147
Lauterbourg 142
Bern 140
Cambridge 140
Council Bluffs 135
Rome 114
Vienna 106
Dearborn 98
Des Moines 91
Jüchen 89
Medford 88
Ho Chi Minh City 86
Dong Ket 74
London 68
Nanchang 65
Hanoi 63
Helsinki 63
Buffalo 56
Istanbul 56
Redwood City 56
São Paulo 51
Frankfurt am Main 47
Redondo Beach 47
Palermo 45
Delft 44
Abidjan 40
Zurich 40
Florence 39
Marseille 39
Orem 39
Shenyang 38
Dakar 37
Munich 33
Brussels 32
Boulder 31
Hebei 29
Kunming 29
San Diego 29
Hyderabad 26
Turin 26
Norwalk 25
Alessandria 24
Düsseldorf 24
Ankara 22
Belo Horizonte 22
Changsha 22
Chennai 22
Manchester 22
Tianjin 22
Brasília 21
Pune 21
Dhaka 20
Kingston 18
Tashkent 18
Guangzhou 17
Rio de Janeiro 17
Livorno 16
Ogden 16
Turku 16
Amsterdam 15
Auburn Hills 15
Baghdad 15
Bogotá 15
Hangzhou 15
Moscow 15
Pisa 15
Riyadh 15
Toronto 15
Cape Town 14
Paris 14
Totale 16.532
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Nome #
Conceptual design of PrandtlPlane civil transport aircraft 519
Conceptual design of a box-wing aircraft for the air transport of the future 335
Preliminary transonic CFD analyses of a PrandtlPlane transport aircraft 326
Progetto Idintos: rendicontazione Giugno 2012 283
Metro Taipei: equipment attachments FEA static and fatigue strenght analysis 273
Ultralight amphibious PrandtlPlane: the final design 270
The Project “Parsifal”: Prandtlplane Architecture For The Sustainable Improvement Of Future Airplanes 263
Metro Taipei: carbody A FEA static and fatigue analysis 262
A 250 Passenger PrandtlPlane Transport Aircraft Preliminary Design 261
Sul problema di Prandtl della minima resistenza indotta di un sistema portante 239
A Model for Solar Powered Aircraft Preliminary Design 230
The Prandtl Wing 227
Flutter and Aerodynamic Phenomena Induced by Control Surfaces Freeplay for PrandtlPlane Joined-wing Configuraton 226
The solution of aeroelastic problems within the frame of tridimensional unsteady aerodynamic panel method 222
Flight dynamics model for preliminary design of PrandtlPlane wing configuration with sizing of the control surfaces 219
A computation of the three-dimensional J-Integral for elastic materials with a view to applications in fracture mechanics 214
Tiltrotor with double mobile wing 211
Design of an airfreight system based on innovative PrandtlPlane aircraft 207
BEST WING SYSTEM: AN EXACT SOLUTION OF THE PRANDTL'S PROBLEM 204
Computation of the crack extension energy rate in elasto-plastic fracture mechanics and applications in engineering 203
Dynamic response of a ship-beam undergoing transverse shock waves using MSC MARC code 193
Bioinspired mechanisms and sensorimotor schemes for flying: A preliminary study for a robotic bat 193
The PrandtlPlane Configuration: Overview on Possible Applications to Civil Aviation 192
Fracture Mechanics 191
Design of solar powered unmanned biplanes for HALE missions 187
A wind tunnel model of a ULM configuration of prandtlPlane: Design, Manufacturing and Aerodynamic testing 186
The Effects of Centrifugal Forces in Steel Cord Forming – Theoretical Modelling and Practical Applications 179
Advanced Design Problems in Aerospace Engineering 178
A 250 Passenger PrandtlPlane Transport Aircraft Preliminary Design 177
Macchina generatrice di polinomi 175
PRELIMINARY DESIGN AGAINST FLUTTER OF A PRANDTLPLANE LIFTING SYSTEM 174
A Model for Solar Powered Aircraft Preliminary Design 174
Variational approach to the problem of optimal propeller design 173
On the Crack Extension Energy Rate in Elastic-Plastic Bodies 171
A CODE FOR SHAPE GENERATION AND AERODYNAMIC DESIGN OF AIRCRAFT 170
Numerical Validation of a New Energetic Fracture Criterion in Elastic Plastic Fracture Mechanics for Aluminum Alloy 169
Resarch on fuselage design, lifting system at cruise conditions and low aerodynamic design of a PrandtlPlane aircraft 168
Applicazione dei materiali Powder Metal nella costruzione dei dischi di turbina dei motori aeronautici; stato attuale delle conoscenze e impostazione di un programma di ricerca 167
PRANDTLPLANE PROPELLED WITH LIQUID HYDROGEN. A PRELIMINARY STUDY 167
Best Wing System: an exact solution of the Prandtl's problem 166
Applicabilità dei criteri Damage Tolerance al progetto dei dischi di turbina di motori per aviazione 165
The role of plasticity in fatigue and fracture mechanics of metallic materials 165
BRITE EURAM BE-3379, Task 3: The Potential Drop Technique for Crack Monitoring on Rotating Disks: Experimental check of the Calibration Curves, Report n. 11 165
Analisi agli elementi finiti del sistema alare di un velivolo ultraleggero di tipo PrandtlPlane 164
Sul progetto a fatica dei dischi di turbina dei motori aeronautici di nuova generazione 163
Aerodynamic design of a light amphibious PrandtlPlane: wind tunnel tests and CFD validation 163
Struttura di teleferica perfezionata 163
Crack propagation from artificial defects in typical engine disk materials; interpretation of experimental results by means of 3D J Integral 162
MISSION DESIGN FOR LONG ENDURANCE FLIGHT WITH SOLAR POWERED AIRCRAFT 162
Full-Scale crack propagation test on spinning turbine disks using the potential drop technique 161
IDINTOS: the first prototype of an amphibious PrandtlPlane-shaped aircraft 161
Considerazioni sulla propagazione per fatica delle cricche nelle giunzioni saldate 160
Dimensionamento aerodinamico preliminare di un velivolo UAV STOL elettrico in configurazione PrandtlPlane 160
Variational Analysis and Aerospace Engineering: Mathematical Challenges for Aerospace Design 160
Misurazione delle forze indotte da campi fluidodinamici su cilindri in galleria aerodinamica 159
BRITE EURAM BE-3379, Task 3: The Potential Drop Technique for Crack Monitoring on Rotating Disks 159
Caratterizzazione della fase di propagazione di fessure per fatica ad alta temperatura nelle superleghe a base nickel AP1 e AF115 157
The Prandtl's best wing system 157
Caratterizzazione della fase di propagazione di fessure per fatica nella lega IN100 alla temperatura di 450 °C 156
BRITE EURAM BE-3379, Task 3: The Potential Drop Technique for Crack Monitoring on Rotating Disks: Experimental Results of the Spinning Test, Report n. 19 155
A model for solar powered preliminary design 155
Conceptual Design of a Very Large PrandtlPlane Freighter 155
A mesh generation procedure for optimization in Computational Fluid Dynamics 154
Caratterizzazione della fase di propagazione di fessure per fatica ad alta temperatura in presenza di carichi ad ampiezza costante e ad ampiezza variabile sulla superlega Waspalloy 152
THE LIFTING SYSTEM OF A PRANDTLPLANE; PART 3: STRUCTURES MADE IN COMPOSITES 152
A personal robotic flying machine with vertical takeoff controlled by the human body movements 152
Sviluppo di materiali intelligenti per applicazioni in strutture aerospaziali 151
A mesh generation procedure for optimisation in Computational Fluid Dynamics 151
Electromecanical Characterization and Discrete Modelling of Conducting Polymer Actuators 150
The development of a PrandtlPlane aircraft configuration 149
A PROPOSAL OF A CRITERION FOR DUCTILE CRACK GROWTH 149
Variational Analysis and Euler Equations of the Optimum Propeller Problem 149
Propagazione di fessure per fatica ad alta temperatura nella superlega a base nickel IN718 su provini corner crack e compact tension 146
Turbine disks: Lifing against defects and materials development 146
A conceptual design of the CMS Tracker 146
MSD (Multibody Shape Generation)- Aerodynamic surface design and optimisation- User manual 145
MDO of innovative configurations - aerodynamic issue 144
A new ultralight amphibious PrandtlPlane: preliminary CFD design of the hull 144
Development of an innovative configuration for transport aircraft; a project of five Italian universities 143
Aerodynamics for MDO of an innovative configuration 143
THE LIFTING SYSTEM OF A PRANDTLPALNE ; PART 1: DESIGN AND ANALYSIS OF A LIGHT ALLOY STRUCTURAL SOLUTION 143
Caratterizzazione della fase di propagazione di fessure per fatica nella lega IN-718 alla temperatura di 450 °C 142
THE LIFTING SYSEM OF A PRANDTLPLANE; PART 2: PRELIMINARY STUDY ON FLUTTER CHARACTERISTICS 141
Computation of Crack Extension Energy Rate for Elastic Plastic Hardening Materials Under Variable Loading 141
VARIATIONAL APPROACH TO THE PROBLEM OF THE MINIMUM INDUCED DRAG OF WINGS 140
Finite Element analysis of MCMV 2010 shi with underwater explosion- Contratto con Intermarine SpA 139
Development of geometric and aerodynamic grid generators for innovative aircraft configurations 138
Variational Analysis and Aerospace Engineering: Mathematical Challenges for the Aerospace of the Future 138
A Criterion for Crack Growth Based on Energy Momentum Tensor 137
Variational Analysis and Aerospace Engineering 137
Caratterizzazione della fase di propagazione per fatica ad alta temperatura di microfessure in alcune superleghe impiegate nei dischi di turbine per motori aeronautici 135
Rilevamento in tempo reale della propagazione di una fessura in un disco di turbina durante prove di centrifugazione ciclica 135
Centrifugal forces effects in steel chord forming: theoretical modeling and practical applications 134
Development of a PrandtlPlane aircraft configuration 134
Il risolutore universale di equazioni; da una idea matematica ad una macchina 133
A code for surface modeling and grid generation coupled to a panel solver 133
Proposal for a New Large Airliner with a Non-Conventional Configuration 133
Determinazione sperimentale della resistenza a frattura ad alta temperatura per la superlega a base nickel IN718 131
The PrandtlPlane 131
Effects of centrifugal forces in producing steel ropes 131
Totale 17.663
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Categoria #
all - tutte 64.430
article - articoli 0
book - libri 0
conference - conferenze 0
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 0
Totale 64.430
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2021/20221.632 0 141 51 92 390 233 25 78 77 31 120 394
2022/20232.134 301 253 163 192 237 315 41 157 341 8 99 27
2023/20242.327 384 284 340 178 335 303 44 46 24 74 21 294
2024/20255.470 80 201 79 192 449 520 310 259 447 637 606 1.690
2025/20264.691 341 805 418 277 423 521 833 249 263 370 143 48
2026/2027227 129 98 0 0 0 0 0 0 0 0 0 0
Totale 24.877