UniSa - IRIS Institutional Research Information System

CRICRI', Gabriele
 Distribuzione geografica
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Continente #
AS - Asia 6.322
NA - Nord America 4.867
EU - Europa 1.575
SA - Sud America 204
AF - Africa 31
Continente sconosciuto - Info sul continente non disponibili 3
OC - Oceania 2
Totale 13.004
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Nazione #
US - Stati Uniti d'America 4.830
HK - Hong Kong 4.636
SG - Singapore 750
IT - Italia 605
CN - Cina 460
UA - Ucraina 336
VN - Vietnam 203
RU - Federazione Russa 159
BR - Brasile 144
DE - Germania 114
IE - Irlanda 84
FR - Francia 74
FI - Finlandia 73
TR - Turchia 66
SE - Svezia 56
IN - India 48
KR - Corea 47
GB - Regno Unito 28
AR - Argentina 23
IQ - Iraq 21
BD - Bangladesh 20
CA - Canada 17
MX - Messico 13
CO - Colombia 11
MA - Marocco 9
NL - Olanda 9
CL - Cile 8
JP - Giappone 8
SA - Arabia Saudita 8
PL - Polonia 7
UZ - Uzbekistan 7
ZA - Sudafrica 6
EC - Ecuador 5
MY - Malesia 5
PH - Filippine 5
PK - Pakistan 5
VE - Venezuela 5
ES - Italia 4
ID - Indonesia 4
TW - Taiwan 4
AE - Emirati Arabi Uniti 3
AT - Austria 3
BE - Belgio 3
IL - Israele 3
LB - Libano 3
NP - Nepal 3
PY - Paraguay 3
TN - Tunisia 3
AL - Albania 2
BG - Bulgaria 2
EG - Egitto 2
EU - Europa 2
GR - Grecia 2
LV - Lettonia 2
LY - Libia 2
MN - Mongolia 2
NG - Nigeria 2
PE - Perù 2
PS - Palestinian Territory 2
PT - Portogallo 2
RO - Romania 2
RS - Serbia 2
SY - Repubblica araba siriana 2
UY - Uruguay 2
AU - Australia 1
AZ - Azerbaigian 1
BA - Bosnia-Erzegovina 1
BO - Bolivia 1
CI - Costa d'Avorio 1
CM - Camerun 1
CR - Costa Rica 1
DZ - Algeria 1
EE - Estonia 1
ET - Etiopia 1
IR - Iran 1
IS - Islanda 1
JM - Giamaica 1
JO - Giordania 1
KE - Kenya 1
KG - Kirghizistan 1
KN - Saint Kitts e Nevis 1
KZ - Kazakistan 1
LT - Lituania 1
MD - Moldavia 1
ME - Montenegro 1
NI - Nicaragua 1
NZ - Nuova Zelanda 1
OM - Oman 1
PA - Panama 1
SO - Somalia 1
TH - Thailandia 1
TT - Trinidad e Tobago 1
UG - Uganda 1
VG - Isole Vergini Britanniche 1
XK - ???statistics.table.value.countryCode.XK??? 1
Totale 13.004
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Città #
Hong Kong 4.634
Ann Arbor 965
Singapore 414
San Jose 411
Chandler 408
Woodbridge 397
Jacksonville 371
Dallas 315
Wilmington 291
Princeton 241
Houston 233
Ashburn 232
Milan 173
Salerno 122
Dong Ket 95
Council Bluffs 86
Dublin 80
Nanjing 78
Beijing 72
Lauterbourg 63
Andover 62
Izmir 60
Pellezzano 54
Boardman 51
The Dalles 50
Rome 43
Moscow 33
Hanoi 32
Ho Chi Minh City 31
Nanchang 30
San Mango 30
Los Angeles 28
Fairfield 24
Shenyang 23
Changsha 21
Hebei 21
Munich 21
Jiaxing 18
New York 18
Santa Clara 18
Mestre 16
Figino 15
Tianjin 15
Jinan 14
Düsseldorf 13
Norwalk 12
Pune 11
Brooklyn 10
Baghdad 9
Columbus 9
Denver 9
Orem 9
Stockholm 9
São Paulo 9
Turin 9
Boston 8
Cambridge 8
Chennai 8
Chicago 8
San Diego 8
Tokyo 8
Turku 8
Washington 8
Atlanta 7
Frankfurt am Main 7
Manchester 7
Mumbai 7
Tashkent 7
Amsterdam 6
Caserta 6
Da Nang 6
New Delhi 6
Ottawa 6
Porto Alegre 6
San Francisco 6
Seattle 6
Zhengzhou 6
Acerra 5
Buenos Aires 5
Guangzhou 5
Hefei 5
Phoenix 5
Qingdao 5
Rio de Janeiro 5
Warsaw 5
Benevento 4
Bogotá 4
Bắc Ninh 4
Dearborn 4
Helsinki 4
Johannesburg 4
Kunming 4
London 4
Modena 4
Montreal 4
Naples 4
Wuhan 4
Asunción 3
Bengaluru 3
Bologna 3
Totale 10.768
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Nome #
Indagine numerico sperimentale del comportamento post-buckling di pannelli aeronautici con e senza irrigidimenti caricati a taglio 1.282
Assessment of Crack Growth from a Cold Worked Hole by Coupled FEM-DBEM Approach 995
Experimental evaluation of the long-term creep deformations of epoxy resin 732
Creep behavior of GFRP laminates and their phases: Experimental investigation and analytical modeling 474
Experimental and numerical post-buckling analysis of thin aluminium aeronautical panels under shear load 415
A novel fixture for measuring mode III toughness of bonded assemblies 358
DETERMINAZIONE SPERIMENTALE DELLA RESISTENZA DI GIUNZIONI INCOLLATE ALLA FRATTURA DI MODO III 350
Thermo-Mechanical Crack Propagation in Aircraft Engine Vane by Coupled FEM-DBEM Approach 331
Characterization and modelling of mechanical properties of polymer/clay nanocomposites by film blowing 222
Post-buckling behaviour of thin aluminium panels undergoing shear load: experimental and numerical investigation 205
A novel methodology for shear cohesive law identification of bonded reinforcements 202
Homogenised properties of composite materials in large deformations 197
A two-parameter model for crack growth simulation under variable load spectrum by combined FEM-DBEM approach 193
Honeycombs onset of failure and failure processes under in-plane loading 182
Coupled FEM-DBEM Simulation of 3D Crack Growth under Fatigue Load Spectrum 179
Crack Growth Under Fatigue Load Spectrum: Numerical Simulation By Coupled Fem-Dbem Approach 174
Honeycomb failure processes under in-plane loading 174
A two-parameter model for crack growth simulation under variable load spectrum by combined FEM-DBEM approach 172
DISPOSITIVO PER PROVE DI RESISTENZA ALLA FRATTURA IN MODO III SU GIUNZIONI INCOLLATE 170
Modelling the mechanical behaviour of metal powder during die compaction process 170
A coupled FEM-BEM approach for crack growth simulation under fatigue load spectrum 167
CHARACTERIZATION AND MODELLING OF MECHANICAL PROPERTIES OF POLYMER/CLAY NANOCOMPOSITES BY FILM BLOWING 167
An advanced creep model allowing for hardening and damage effects 167
Fuzzy evaluation of temperature distribution in laser sheet metal forming 162
Modelling micro and macro failure surfaces of media with microstructure 157
Assessment of allowable dents on aeronautic panels based on the coupled usage of FEM-DBEM methodology 154
Investigation of mode III fracture behaviour in bonded pultruded GFRP composite joints 150
A two-parameter model for crack growth simulation by combined FEM-DBEM approach 150
Three-Dimensional BEM and FEM Submodelling in a Cracked FML Full Scale Aeronautic Panel 150
A two parameter model for crack growth simulation under variable spectrum load by combined FEM/analytical approach 149
Multiple crack propagation with Dual Boundary Element Method in stiffened and reinforced full scale aeronautic panels 148
Elementi di meccanica della frattura 146
A consistent use of the Gurson-Tvergaard-Needleman damage model for the R-curve calculation 144
Stiffness constants prediction of nanocomposites using a periodic 3D-FEM model 141
Assessment of allowable dents on aeronautic panels based on the coupled usage of FEM-DBEM methodology 138
Crack growth under fatigue load spectrum: numerical simulation by coupled FEM-DBEM approach 138
DBEM Simulation of a FML Full Scale Aeronautic Panel Undergoing Biaxial Fatigue Load, 133
Consistent use of the Gurson-Tvergaard damage model for the R-curve calculation 129
Cohesive fracture in composite systems: Experimental setup and first results 125
Analytical and FEM optimisations of twice shrink-fitted dies with inserts of different materials 122
Advantages of FEM Approach for Reliable Evaluations and Design of PM Tools 121
Micro - and Macro- failure models of heterogeneous media with micro-structure 120
DBEM and FEM Analysis of an Extrusion Press Fatigue Failure 116
MODE II FRACTURE BEHAVIOUR OF ADHESIVELY BONDED REINFORCEMENTS 115
Identification of mode-I cohesive parameters for bonded interfaces based on DCB test 114
Influence of operating temperature on the shrink-fitting pressure of PM dies 113
Comparison of DBEM and FEM Crack Path Predictions in a notched Shaft under Torsion 111
Compacting dies with rectangular profile: FEM evaluation of profile deformation on compaction 107
Compacting dies with rectangular profile: FEM analysis of stress states for different geometries 106
Numerical solution techniques for structural instability problems 106
Compaction dies for spur gears: FEM analysis to assess the influence of some design parameters on stress state [Matrici di pressatura di ingranaggi cilindrici a denti diritti: Analisi numerica FEM sull'influenza del modulo e del numero di denti sugli stati tensionali] 105
FEM analysis of stress and deformation states of shelf dies for metal powder compaction 104
Doubly shrink fitted dies: optimisation by analytical and FEM calculations 104
Fatigue crack-growth behaviour and life prediction for small crack in aluminium alloy 100
Compaction dies for spur gears: FEM analysis to assess the influence of design parameters on stress state 100
Metal Powder Compacting Dies: Numerical Optimization of the Design 99
MODELLAZIONE DEL COMPORTAMENTO DI POLVERIMETALLICHE DURANTE LA PRESSATURA 98
Numerical solution techniques for structural instability problems 97
Warm compaction: FEM analysis of stress and deformation states of compacting dies with rectangular profile of various aspect ratio 97
Structural Response of DEMO Divertor Under Electromagnetic Loading 92
Compaction Shelf Dies with Conical Shrink-fitting Surface: FEM Analysis of Stress and Deformation Behaviour 91
FEM optimisation of twice shrink-fitted dies in plane stress conditions 89
SIMULAZIONE FEM DELLA PIEGATURA LASER CON L’USO DI UNA MESH MOBILE 86
UN NUOVO APPROCCIO ALLA SOLUZIONE DI PROBLEMI LINEARI MULTISCALA 84
Short dies and thin-walled insert for room temperature or warm compaction - numerical determination of design features 81
Deformation states of dies for powder compacting. Comparison between analytical and FEM calculation 81
On the equivalent rigidity of Dies for Metal Powder Compaction 76
Optimised design parameters for twice shrink-fitted dies in plane stress conditions 74
Valutazione dello stato tensionale nello strato isolante di un magnete superconduttore. 72
Assessment of dynamic response of a DEMO divertor under electromagnetic impact loads. Part 1: A computational methodology for a cost-effective analysis 71
Metal powder compacting dies: optimised design by analytical or numerical methods 71
Totale 13.115
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Categoria #
all - tutte 31.704
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 31.704
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2021/2022462 7 7 3 5 8 14 6 29 68 65 65 185
2022/2023831 72 64 15 132 117 166 2 92 120 2 31 18
2023/2024334 29 52 19 14 24 63 11 45 1 12 15 49
2024/2025730 31 21 10 21 35 77 126 90 86 31 91 111
2025/20267.174 2.084 1.985 1.025 61 357 173 467 87 249 350 49 287
2026/20272 2 0 0 0 0 0 0 0 0 0 0 0
Totale 13.115