IRIS
RUSSO, ANGELA
 Distribuzione geografica
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Continente #
EU - Europa 3.910
AS - Asia 1.386
NA - Nord America 1.173
SA - Sud America 356
AF - Africa 26
OC - Oceania 5
Totale 6.856
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Nazione #
RU - Federazione Russa 2.948
US - Stati Uniti d'America 1.122
SG - Singapore 415
IE - Irlanda 375
CN - Cina 326
BR - Brasile 303
HK - Hong Kong 258
IT - Italia 223
VN - Vietnam 152
DE - Germania 89
GB - Regno Unito 77
KR - Corea 65
FR - Francia 43
IN - India 43
CA - Canada 32
AR - Argentina 26
UA - Ucraina 26
FI - Finlandia 22
GR - Grecia 21
ID - Indonesia 21
SE - Svezia 19
JP - Giappone 18
IQ - Iraq 16
TR - Turchia 16
NL - Olanda 14
BD - Bangladesh 13
EC - Ecuador 12
AT - Austria 9
MX - Messico 9
PK - Pakistan 8
RO - Romania 8
ZA - Sudafrica 7
IR - Iran 6
JO - Giordania 6
PT - Portogallo 6
UZ - Uzbekistan 6
AU - Australia 5
CO - Colombia 5
CZ - Repubblica Ceca 4
DZ - Algeria 4
EG - Egitto 4
PL - Polonia 4
ES - Italia 3
KE - Kenya 3
LT - Lituania 3
MA - Marocco 3
PY - Paraguay 3
TT - Trinidad e Tobago 3
UY - Uruguay 3
AL - Albania 2
AM - Armenia 2
BE - Belgio 2
CG - Congo 2
CH - Svizzera 2
DO - Repubblica Dominicana 2
EE - Estonia 2
IL - Israele 2
LK - Sri Lanka 2
PH - Filippine 2
RS - Serbia 2
SA - Arabia Saudita 2
VE - Venezuela 2
AE - Emirati Arabi Uniti 1
AO - Angola 1
AZ - Azerbaigian 1
BO - Bolivia 1
BY - Bielorussia 1
CL - Cile 1
CR - Costa Rica 1
ET - Etiopia 1
HN - Honduras 1
HR - Croazia 1
HU - Ungheria 1
JM - Giamaica 1
KZ - Kazakistan 1
LU - Lussemburgo 1
LV - Lettonia 1
MY - Malesia 1
NI - Nicaragua 1
PA - Panama 1
PS - Palestinian Territory 1
SK - Slovacchia (Repubblica Slovacca) 1
SY - Repubblica araba siriana 1
TJ - Tagikistan 1
TN - Tunisia 1
Totale 6.856
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Città #
Moscow 1.078
Dublin 375
Hong Kong 257
Santa Clara 248
Singapore 152
Chandler 146
Dallas 70
Hefei 67
Ho Chi Minh City 64
Jacksonville 61
Seoul 61
Beijing 58
Munich 40
Princeton 40
Roxbury 40
Ashburn 37
Cambridge 36
Bengaluru 28
São Paulo 27
Hanoi 26
Naples 23
Rome 20
Des Moines 17
Falkenstein 17
Los Angeles 17
New York 14
Medford 13
Seattle 13
Ann Arbor 12
Belo Horizonte 12
Montreal 11
The Dalles 11
Milan 10
Turku 10
Marigliano 9
Marseille 9
Nuremberg 9
Turin 9
Amsterdam 8
Aversa 8
Brooklyn 8
Caserta 8
Magelang 8
Cluj-Napoca 6
Columbus 6
Ottawa 6
Tashkent 6
Tokyo 6
Wilmington 6
Boardman 5
Brasília 5
Buenos Aires 5
Guayaquil 5
Ha Long 5
Haiphong 5
Helsinki 5
Kaiserslautern 5
Napoli 5
Orta di Atella 5
Pompei 5
Redwood City 5
San Francisco 5
San Jose 5
Akyazı 4
Baoding 4
Bogotá 4
Cabo Frio 4
Can Tho 4
Da Nang 4
Fortaleza 4
Istanbul 4
Juiz de Fora 4
Lappeenranta 4
Lund 4
New Delhi 4
Norwalk 4
Petrolina 4
Porto Alegre 4
Quận Bình Thạnh 4
Rio de Janeiro 4
Rockville 4
Volla 4
Warsaw 4
Woodbridge 4
Baghdad 3
Bristol 3
Cuenca 3
Guangzhou 3
Hyde 3
Hải Dương 3
Kokuryocho 3
Las Vegas 3
Manchester 3
Mexico City 3
Montevideo 3
Mountain View 3
Nanjing 3
Paris 3
Phủ Lý 3
Piscataway 3
Totale 3.425
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Nome #
A FEASIBILITY STUDY ON ADDITIVE MANUFACTURED HYBRID METAL/COMPOSITE SHOCK ABSORBER PANELS 158
A robust cumulative damage approach for the simulation of delamination under cyclic loading conditions 157
A Computational Cost-effective numerical methodology for the simulation of the fatigue behaviour in composite materials. 138
A numerical/experimental study on the induction heating of adhesives for composite materials bonding 135
A robust numerical methodology for fatigue damage evolution simulation in composites 134
A sensitivity analysis on Fibre bridging effects in delaminated composite panels under Flexural Loading Conditions 132
FIBREGLASS WIND TURBINE ONE SHOT BLADE®: DAMAGE TOLERANT DESIGN 131
A numerical investigation of the interaction between interlaminar and intralaminar damages in a fatigued composite panel 130
A feasibility study on additive manufactured hybrid metal/composite shock absorbers 129
A Numerical Assessment of Fibre Bridging Influence on Composite Panels Skin-stringer Debonding 128
Large Notch Damage Evolution in Omega Stiffened Composite Panels 128
A Numerical Study on the Influence of Nanosilica-Reinforced Epoxy Resin on the Delamination Behavior of Composite Laminates 127
EFFECTS OF THERMAL LOADS ON THE MECHANICAL BEHAVIOUR OF BONDED AIRCRAFT SUBCOMPONENTS. 127
An Experimental Assessment on the Influence of Carbon Nanotubes Matrix Charging on the Fatigue Behavior of Composite Laminates 126
A Numerical Study on Mode II Fatigue Delamination Growth in Composite Laminates 126
A numerical-analytical approach for the preliminary design of thin-walled cylindrical shell structures with elliptical cut-outs 125
DEVELOPMENT OF A NUMERICAL METHODOLOGY FOR THE SIMULATION OF THE FATIGUE INDUCED DELAMINATION IN COMPOSITE STRUCTURES 124
Fatigue driven delamination in composite structures: Definition and assessment of a novel fracture mechanics based computational tool 123
Modelling the damage evolution in notched omega stiffened composite panels under compression 122
An insight on the crashworthiness behavior of a full-scale composite fuselage section at different impact angles 122
Compressive Behaviour of a Damaged Omega Stiffened Panel: Damage Detection and Numerical Analysis 120
A NUMERICAL-EXPERIMENTAL STUDY ON THE IMPCAT RESPONSE OF AN ADDITIVE MANUFACTED HYBRID METAL-COMPOSITE STRURCTURE 120
Experimental investigation on 3D printed lightweight sandwich structures for energy absorption aerospace applications 119
On the use of Double - Double advanced materiai processing for the design of a composite fuselage barrel. 118
A Paris Law Based Mesh Independent Numerical Methodology for the Simulation of Fatigue Driven Delamination in Composites 116
Compressive behaviour of a damaged omega stiffened panel: Damage detection and numerical analysis 115
A numerical parametric study on delamination influence on the fatigue behaviour of stiffened composite components 114
Unstable Delamination Growth in Stiffened Composite Panels Under Cyclic Loading Conditions 110
Experimental investigation on the delamination onset and propagation in composite specimens subjected to compressive loads by using Digital Image Correlation 110
Delamination Effect on the Buckling Behaviour of Carbon–Epoxy Composite Typical Aeronautical Panels 109
On the mechanical behavior of laminated composite plates subjected to compression after impact tests 104
Numerical Assessment on the Fatigue Behavior of Composite Open-Hole Tensile Specimens 103
Nanofillers’ effects on fracture energy in composite aerospace structures 103
Influence of manufacturing defects on the mechanical behaviour of all-composite wing under service load conditions 102
Development of a Numerical Methodology Able to Simulate the Unstable Mixed Mode Delamination Growth in Stiffened Composite Panels Under Cyclic Loading Conditions 101
Influence of failure criteria and intralaminar damage progression numerical models on the prediction of the mechanical behavior of composite laminates 100
On the Use of Digital Image Correlation to Assess the Damage Behavior of Composite Coupons Under Compression 99
NUMERICAL STUDY ON INDUCTION HEATING OF ADHESIVE FOR BONDING OF COMPOSITE MATERIALS 99
The role of intralaminar damages on the delamination evolution in laminated composite structures 98
The peculiar SMart-Time XB approach for delamination growth prediction and its evolution towards fatigue investigations 97
Fibreglass wind turbine blades: Damage tolerant design and verification 97
Damage Tolerant Behaviour of Unstable Skin-Stringer Debonding Growth in Composite Stiffened Structures 96
Ultrasonic damage detection of impacted long and short fibre composite specimens 95
Hybrid Composite-Polypropylene Sandwich-Based Design for the Fuselage Panel in Commercial Aircraft to Increase the Passive Safety of Passengers 94
Hybrid Composite-Polypropylene Sandwich-based Design for the Fuselage Panel in Commercial Aircraft to Increase the Passive Safety of Passengers 94
A novel numerical methodology for the simulation of unstable debonding growth in aerospace stiffened composite panels 93
Double-Double Laminate Composites for Unmanned Aerial Vehicles 93
Cross-influence between intra-laminar damages and fibre bridging at the skin-stringer interface in stiffened composite panels under compression 92
On The Propagation Of Fatigue Damage In An Aerospace Hybrid Shock Absorber Designed For Additive Manufacturing 91
Parametric Investigation of Stiffened Panel Subjected to Compressive Loads: Influence of Initial Delamination Length on Damage Behaviour 86
An Experimental Approach for Investigating Fatigue-Induced Debonding Propagation in Composite Stiffened Panels Using Thermographic Phase Mapping 83
On the Compressive Behaviour of a Composite Stiffened Panel with Artificially Introduced Delamination 83
NUMERICAL INVESTIGATION ON DELAMINATION GROWTH IN COMPOSITE PANELS INCLUDING FIBRE-BRIDGING EFFECT 82
Evolution of Unstable Skin-Stringer Debonding Propagation in Composite Aircraft Structures: Implications on Damage Tolerant Design 78
Numerical-experimental correlation of impact-induced damages in CFRP laminates 78
Design of a composite wind turbine blade manufactured with the ONE SHOT BLADE® technology 74
Development and application of a numerical procedure for the simulation of the “Fibre Bridging” phenomenon in composite structures 73
Influence of Delamination Size and Depth on the Compression Fatigue Behaviour of a Stiffened Aerospace Composite Panel 73
Numerical-experimental investigation into the tensile behavior of a hybrid metallic-CFRP stiffened aeronautical panel 71
Damage tolerance evaluation of a C/C-SiC composite body flap of a re-entry vehicle 69
NUMERICAL INVESTIGATION ON DELAMINATION GROWTH IN COMPOSITE PANELS INCLUDING FIBRE-BRIDGING EFFECT 68
Numerical and Experimental Investigation on Single Lap Composite Joints 66
Experimental and numerical assessment of fibre bridging toughening effects on the compressive behaviour of delaminated composite plates 66
Mixed-mode delamination growth prediction in stiffened CFRP panels by means of a novel fast procedure 60
Optimization of composite aeronautical components by Re-designing with double-double laminates 59
Numerical study on the toughening effect of the fiber bridging on delaminated composite stiffened panel 59
Numerical investigation on the stringer termination debonding in tensile loaded hybrid metallic-CFRP stiffened aeronautical panel 59
Fiber bridging induced toughening effects on the delamination behavior of composite stiffened panels under bending loading: A numerical/experimental study 57
Totale 6.968
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Categoria #
all - tutte 23.776
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 23.776
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/202166 0 0 0 0 0 1 20 5 13 1 25 1
2021/2022252 4 7 0 4 71 6 5 7 20 3 21 104
2022/2023571 64 32 24 30 30 27 7 16 315 4 10 12
2023/2024390 27 20 18 40 101 21 42 6 17 10 29 59
2024/20251.226 10 34 7 22 199 169 183 110 178 118 92 104
2025/20264.222 161 296 364 232 423 2.746 0 0 0 0 0 0
Totale 6.968