CINECA IRIS Institutional Research Information System

FREDIANI, ALDO
 Distribuzione geografica
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Continente #
NA - Nord America 10.698
AS - Asia 6.481
EU - Europa 6.182
SA - Sud America 821
AF - Africa 227
OC - Oceania 25
Continente sconosciuto - Info sul continente non disponibili 15
Totale 24.449
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Nazione #
US - Stati Uniti d'America 10.209
IT - Italia 2.216
CN - Cina 1.894
SG - Singapore 1.782
HK - Hong Kong 987
SE - Svezia 911
BR - Brasile 649
DE - Germania 482
BG - Bulgaria 431
VN - Vietnam 420
GB - Regno Unito 399
CA - Canada 386
KR - Corea 367
FR - Francia 329
UA - Ucraina 323
TR - Turchia 262
FI - Finlandia 257
IN - India 205
RU - Federazione Russa 204
JP - Giappone 188
CH - Svizzera 180
AT - Austria 136
NL - Olanda 100
BD - Bangladesh 85
IQ - Iraq 51
CO - Colombia 43
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
UZ - Uzbekistan 23
AU - Australia 22
JM - Giamaica 18
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
ID - Indonesia 10
AE - Emirati Arabi Uniti 9
AL - Albania 9
HU - Ungheria 9
OM - Oman 9
DZ - Algeria 8
HN - Honduras 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
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
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
PA - Panama 2
RS - Serbia 2
Totale 24.411
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Città #
Woodbridge 1.038
Ashburn 978
Singapore 972
Hong Kong 967
Ann Arbor 804
Milan 759
Chandler 701
Santa Clara 643
Houston 634
San Jose 537
Jacksonville 466
Hefei 446
Sofia 430
Fairfield 389
Beijing 348
Seoul 339
Ottawa 317
Dallas 314
New York 261
Wilmington 222
Shanghai 216
Boardman 198
Seattle 197
Los Angeles 178
Princeton 172
Nanjing 168
Tokyo 166
Serra 162
Lawrence 158
Chicago 149
Izmir 147
Lauterbourg 142
Bern 140
Cambridge 140
Rome 113
Vienna 106
Dearborn 98
Council Bluffs 96
Des Moines 91
Jüchen 89
Medford 88
Ho Chi Minh City 86
Dong Ket 74
London 68
Nanchang 65
Hanoi 63
Helsinki 63
Istanbul 56
Redwood City 56
Buffalo 55
São Paulo 51
Frankfurt am Main 47
Redondo Beach 47
Palermo 45
Delft 44
Abidjan 40
Zurich 40
Florence 39
Marseille 39
Orem 38
Shenyang 38
Dakar 37
Munich 33
Brussels 32
Boulder 31
Hebei 29
San Diego 29
Hyderabad 26
Norwalk 25
Alessandria 24
Düsseldorf 24
Kunming 24
Ankara 22
Belo Horizonte 22
Changsha 22
Chennai 22
Manchester 22
Tianjin 22
Turin 22
Brasília 21
Pune 21
Dhaka 20
Tashkent 18
Guangzhou 17
Rio de Janeiro 17
Kingston 16
Ogden 16
Turku 16
Amsterdam 15
Auburn Hills 15
Baghdad 15
Bogotá 15
Hangzhou 15
Moscow 15
Pisa 15
Riyadh 15
Cape Town 14
Livorno 14
Toronto 14
Zhengzhou 14
Totale 16.439
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Nome #
Conceptual design of PrandtlPlane civil transport aircraft 517
Conceptual design of a box-wing aircraft for the air transport of the future 334
Preliminary transonic CFD analyses of a PrandtlPlane transport aircraft 323
Progetto Idintos: rendicontazione Giugno 2012 281
Metro Taipei: equipment attachments FEA static and fatigue strenght analysis 272
Ultralight amphibious PrandtlPlane: the final design 262
The Project “Parsifal”: Prandtlplane Architecture For The Sustainable Improvement Of Future Airplanes 262
A 250 Passenger PrandtlPlane Transport Aircraft Preliminary Design 260
Metro Taipei: carbody A FEA static and fatigue analysis 260
Sul problema di Prandtl della minima resistenza indotta di un sistema portante 238
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 223
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 218
A computation of the three-dimensional J-Integral for elastic materials with a view to applications in fracture mechanics 211
Tiltrotor with double mobile wing 210
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
Design of an airfreight system based on innovative PrandtlPlane aircraft 203
Dynamic response of a ship-beam undergoing transverse shock waves using MSC MARC code 193
The PrandtlPlane Configuration: Overview on Possible Applications to Civil Aviation 192
Bioinspired mechanisms and sensorimotor schemes for flying: A preliminary study for a robotic bat 192
Fracture Mechanics 190
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
A 250 Passenger PrandtlPlane Transport Aircraft Preliminary Design 177
Advanced Design Problems in Aerospace Engineering 176
Macchina generatrice di polinomi 174
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 172
On the Crack Extension Energy Rate in Elastic-Plastic Bodies 171
A CODE FOR SHAPE GENERATION AND AERODYNAMIC DESIGN OF AIRCRAFT 170
Resarch on fuselage design, lifting system at cruise conditions and low aerodynamic design of a PrandtlPlane aircraft 168
Numerical Validation of a New Energetic Fracture Criterion in Elastic Plastic Fracture Mechanics for Aluminum Alloy 168
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
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 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. 11 164
Sul progetto a fatica dei dischi di turbina dei motori aeronautici di nuova generazione 163
Full-Scale crack propagation test on spinning turbine disks using the potential drop technique 161
Analisi agli elementi finiti del sistema alare di un velivolo ultraleggero di tipo PrandtlPlane 161
Aerodynamic design of a light amphibious PrandtlPlane: wind tunnel tests and CFD validation 161
Struttura di teleferica perfezionata 161
The role of plasticity in fatigue and fracture mechanics of metallic materials 160
Dimensionamento aerodinamico preliminare di un velivolo UAV STOL elettrico in configurazione PrandtlPlane 160
Misurazione delle forze indotte da campi fluidodinamici su cilindri in galleria aerodinamica 159
Crack propagation from artificial defects in typical engine disk materials; interpretation of experimental results by means of 3D J Integral 159
Variational Analysis and Aerospace Engineering: Mathematical Challenges for Aerospace Design 159
Considerazioni sulla propagazione per fatica delle cricche nelle giunzioni saldate 158
MISSION DESIGN FOR LONG ENDURANCE FLIGHT WITH SOLAR POWERED AIRCRAFT 158
Caratterizzazione della fase di propagazione di fessure per fatica ad alta temperatura nelle superleghe a base nickel AP1 e AF115 156
BRITE EURAM BE-3379, Task 3: The Potential Drop Technique for Crack Monitoring on Rotating Disks 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
IDINTOS: the first prototype of an amphibious PrandtlPlane-shaped aircraft 155
A model for solar powered preliminary design 154
The Prandtl's best wing system 153
A mesh generation procedure for optimization in Computational Fluid Dynamics 153
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
Caratterizzazione della fase di propagazione di fessure per fatica nella lega IN100 alla temperatura di 450 °C 151
Sviluppo di materiali intelligenti per applicazioni in strutture aerospaziali 151
THE LIFTING SYSTEM OF A PRANDTLPLANE; PART 3: STRUCTURES MADE IN COMPOSITES 151
Conceptual Design of a Very Large PrandtlPlane Freighter 151
A mesh generation procedure for optimisation in Computational Fluid Dynamics 151
A personal robotic flying machine with vertical takeoff controlled by the human body movements 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 148
Turbine disks: Lifing against defects and materials development 146
Variational Analysis and Euler Equations of the Optimum Propeller Problem 146
MSD (Multibody Shape Generation)- Aerodynamic surface design and optimisation- User manual 145
A conceptual design of the CMS Tracker 145
MDO of innovative configurations - aerodynamic issue 144
Propagazione di fessure per fatica ad alta temperatura nella superlega a base nickel IN718 su provini corner crack e compact tension 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
Development of an innovative configuration for transport aircraft; a project of five Italian universities 141
THE LIFTING SYSEM OF A PRANDTLPLANE; PART 2: PRELIMINARY STUDY ON FLUTTER CHARACTERISTICS 141
A new ultralight amphibious PrandtlPlane: preliminary CFD design of the hull 141
VARIATIONAL APPROACH TO THE PROBLEM OF THE MINIMUM INDUCED DRAG OF WINGS 140
Computation of Crack Extension Energy Rate for Elastic Plastic Hardening Materials Under Variable Loading 140
Finite Element analysis of MCMV 2010 shi with underwater explosion- Contratto con Intermarine SpA 139
Caratterizzazione della fase di propagazione di fessure per fatica nella lega IN-718 alla temperatura di 450 °C 138
Development of geometric and aerodynamic grid generators for innovative aircraft configurations 138
Variational Analysis and Aerospace Engineering 137
Rilevamento in tempo reale della propagazione di una fessura in un disco di turbina durante prove di centrifugazione ciclica 135
Caratterizzazione della fase di propagazione per fatica ad alta temperatura di microfessure in alcune superleghe impiegate nei dischi di turbine per motori aeronautici 134
Centrifugal forces effects in steel chord forming: theoretical modeling and practical applications 134
Development of a PrandtlPlane aircraft configuration 133
A code for surface modeling and grid generation coupled to a panel solver 133
A Criterion for Crack Growth Based on Energy Momentum Tensor 133
Proposal for a New Large Airliner with a Non-Conventional Configuration 133
Variational Analysis and Aerospace Engineering: Mathematical Challenges for the Aerospace of the Future 133
Il risolutore universale di equazioni; da una idea matematica ad una macchina 132
The PrandtlPlane 131
Effects of centrifugal forces in producing steel ropes 130
Prove di fatica su provini in acciaio per veicoli ferroviari soggetti a profonda ossidazione superficiale 129
Totale 17.537
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Categoria #
all - tutte 62.666
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 62.666
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2021/20221.664 32 141 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
2026/202736 36 0 0 0 0 0 0 0 0 0 0 0
Totale 24.686