RUSSO, ANGELA
 Distribuzione geografica
Continente #
EU - Europa 4.055
AS - Asia 1.793
NA - Nord America 1.524
SA - Sud America 366
AF - Africa 34
OC - Oceania 6
Totale 7.778
Nazione #
RU - Federazione Russa 3.010
US - Stati Uniti d'America 1.464
SG - Singapore 644
CN - Cina 397
IE - Irlanda 375
BR - Brasile 311
HK - Hong Kong 281
IT - Italia 255
VN - Vietnam 205
DE - Germania 94
GB - Regno Unito 85
KR - Corea 65
IN - India 52
FR - Francia 49
CA - Canada 36
NL - Olanda 30
UA - Ucraina 28
AR - Argentina 27
FI - Finlandia 26
ID - Indonesia 24
GR - Grecia 21
JP - Giappone 19
SE - Svezia 19
IQ - Iraq 18
TR - Turchia 18
BD - Bangladesh 14
EC - Ecuador 13
MX - Messico 12
AT - Austria 10
PK - Pakistan 9
RO - Romania 9
ZA - Sudafrica 7
AU - Australia 6
IR - Iran 6
JO - Giordania 6
PL - Polonia 6
PT - Portogallo 6
UZ - Uzbekistan 6
CO - Colombia 5
CZ - Repubblica Ceca 5
ES - Italia 5
SA - Arabia Saudita 5
CH - Svizzera 4
DZ - Algeria 4
EG - Egitto 4
KE - Kenya 4
MA - Marocco 4
MY - Malesia 4
TN - Tunisia 4
LT - Lituania 3
PY - Paraguay 3
TT - Trinidad e Tobago 3
UY - Uruguay 3
AL - Albania 2
AM - Armenia 2
BE - Belgio 2
BY - Bielorussia 2
CG - Congo 2
CR - Costa Rica 2
DO - Repubblica Dominicana 2
EE - Estonia 2
ET - Etiopia 2
GE - Georgia 2
IL - Israele 2
LK - Sri Lanka 2
NP - Nepal 2
PH - Filippine 2
RS - Serbia 2
VE - Venezuela 2
AE - Emirati Arabi Uniti 1
AO - Angola 1
AZ - Azerbaigian 1
BF - Burkina Faso 1
BO - Bolivia 1
CL - Cile 1
GT - Guatemala 1
HN - Honduras 1
HR - Croazia 1
HU - Ungheria 1
JM - Giamaica 1
KZ - Kazakistan 1
LB - Libano 1
LU - Lussemburgo 1
LV - Lettonia 1
NG - Nigeria 1
NI - Nicaragua 1
PA - Panama 1
PS - Palestinian Territory 1
SK - Slovacchia (Repubblica Slovacca) 1
SY - Repubblica araba siriana 1
TH - Thailandia 1
TJ - Tagikistan 1
Totale 7.778
Città #
Moscow 1.116
Dublin 375
Singapore 330
Hong Kong 279
Santa Clara 260
San Jose 165
Chandler 146
Ashburn 88
Ho Chi Minh City 82
Beijing 73
Dallas 71
Hefei 67
Jacksonville 61
Seoul 61
Hanoi 42
Munich 40
Princeton 40
Roxbury 40
Cambridge 36
Bengaluru 29
São Paulo 29
Naples 28
Rome 23
Los Angeles 20
New York 20
Amsterdam 19
Des Moines 17
Falkenstein 17
Medford 13
Seattle 13
Ann Arbor 12
Belo Horizonte 12
Nuremberg 12
Milan 11
Montreal 11
The Dalles 11
Aversa 10
Council Bluffs 10
Turku 10
Brooklyn 9
Helsinki 9
Marigliano 9
Marseille 9
Turin 9
Caserta 8
Haiphong 8
Magelang 8
Orem 8
Atlanta 7
Chennai 6
Cluj-Napoca 6
Columbus 6
Da Nang 6
Ha Long 6
Orta di Atella 6
Ottawa 6
San Francisco 6
Tashkent 6
Tokyo 6
Warsaw 6
Wilmington 6
Baghdad 5
Boardman 5
Brasília 5
Buenos Aires 5
Can Tho 5
Guayaquil 5
Kaiserslautern 5
Napoli 5
New Delhi 5
Phủ Lý 5
Pompei 5
Redwood City 5
Toronto 5
Trani 5
Akyazı 4
Baoding 4
Bogotá 4
Cabo Frio 4
Fortaleza 4
Istanbul 4
Juiz de Fora 4
Lappeenranta 4
Las Vegas 4
Lund 4
Nanjing 4
Norwalk 4
Paris 4
Petrolina 4
Piscataway 4
Porto Alegre 4
Quận Bình Thạnh 4
Rio de Janeiro 4
Rockville 4
Shanghai 4
Vienna 4
Volla 4
Woodbridge 4
Biên Hòa 3
Bristol 3
Totale 4.023
Nome #
A FEASIBILITY STUDY ON ADDITIVE MANUFACTURED HYBRID METAL/COMPOSITE SHOCK ABSORBER PANELS 190
A robust cumulative damage approach for the simulation of delamination under cyclic loading conditions 175
A Computational Cost-effective numerical methodology for the simulation of the fatigue behaviour in composite materials. 162
A robust numerical methodology for fatigue damage evolution simulation in composites 161
A sensitivity analysis on Fibre bridging effects in delaminated composite panels under Flexural Loading Conditions 152
FIBREGLASS WIND TURBINE ONE SHOT BLADE®: DAMAGE TOLERANT DESIGN 148
A Numerical Study on the Influence of Nanosilica-Reinforced Epoxy Resin on the Delamination Behavior of Composite Laminates 145
A numerical/experimental study on the induction heating of adhesives for composite materials bonding 145
DEVELOPMENT OF A NUMERICAL METHODOLOGY FOR THE SIMULATION OF THE FATIGUE INDUCED DELAMINATION IN COMPOSITE STRUCTURES 145
A Numerical Assessment of Fibre Bridging Influence on Composite Panels Skin-stringer Debonding 143
A feasibility study on additive manufactured hybrid metal/composite shock absorbers 143
A numerical investigation of the interaction between interlaminar and intralaminar damages in a fatigued composite panel 140
A Numerical Study on Mode II Fatigue Delamination Growth in Composite Laminates 139
Fatigue driven delamination in composite structures: Definition and assessment of a novel fracture mechanics based computational tool 138
Large Notch Damage Evolution in Omega Stiffened Composite Panels 138
An Experimental Assessment on the Influence of Carbon Nanotubes Matrix Charging on the Fatigue Behavior of Composite Laminates 137
A numerical parametric study on delamination influence on the fatigue behaviour of stiffened composite components 136
An insight on the crashworthiness behavior of a full-scale composite fuselage section at different impact angles 136
EFFECTS OF THERMAL LOADS ON THE MECHANICAL BEHAVIOUR OF BONDED AIRCRAFT SUBCOMPONENTS. 136
Modelling the damage evolution in notched omega stiffened composite panels under compression 135
A numerical-analytical approach for the preliminary design of thin-walled cylindrical shell structures with elliptical cut-outs 135
A NUMERICAL-EXPERIMENTAL STUDY ON THE IMPCAT RESPONSE OF AN ADDITIVE MANUFACTED HYBRID METAL-COMPOSITE STRURCTURE 134
Experimental investigation on 3D printed lightweight sandwich structures for energy absorption aerospace applications 133
Development of a Numerical Methodology Able to Simulate the Unstable Mixed Mode Delamination Growth in Stiffened Composite Panels Under Cyclic Loading Conditions 133
Unstable Delamination Growth in Stiffened Composite Panels Under Cyclic Loading Conditions 131
Compressive Behaviour of a Damaged Omega Stiffened Panel: Damage Detection and Numerical Analysis 130
On the use of Double - Double advanced materiai processing for the design of a composite fuselage barrel. 128
A Paris Law Based Mesh Independent Numerical Methodology for the Simulation of Fatigue Driven Delamination in Composites 127
Experimental investigation on the delamination onset and propagation in composite specimens subjected to compressive loads by using Digital Image Correlation 121
Compressive behaviour of a damaged omega stiffened panel: Damage detection and numerical analysis 120
Delamination Effect on the Buckling Behaviour of Carbon–Epoxy Composite Typical Aeronautical Panels 119
Numerical Assessment on the Fatigue Behavior of Composite Open-Hole Tensile Specimens 115
Influence of failure criteria and intralaminar damage progression numerical models on the prediction of the mechanical behavior of composite laminates 114
On the mechanical behavior of laminated composite plates subjected to compression after impact tests 113
The peculiar SMart-Time XB approach for delamination growth prediction and its evolution towards fatigue investigations 112
Damage Tolerant Behaviour of Unstable Skin-Stringer Debonding Growth in Composite Stiffened Structures 112
A novel numerical methodology for the simulation of unstable debonding growth in aerospace stiffened composite panels 110
The role of intralaminar damages on the delamination evolution in laminated composite structures 109
Hybrid Composite-Polypropylene Sandwich-based Design for the Fuselage Panel in Commercial Aircraft to Increase the Passive Safety of Passengers 109
Nanofillers’ effects on fracture energy in composite aerospace structures 109
On the Use of Digital Image Correlation to Assess the Damage Behavior of Composite Coupons Under Compression 108
Hybrid Composite-Polypropylene Sandwich-Based Design for the Fuselage Panel in Commercial Aircraft to Increase the Passive Safety of Passengers 107
Influence of manufacturing defects on the mechanical behaviour of all-composite wing under service load conditions 106
Fibreglass wind turbine blades: Damage tolerant design and verification 106
Ultrasonic damage detection of impacted long and short fibre composite specimens 103
NUMERICAL STUDY ON INDUCTION HEATING OF ADHESIVE FOR BONDING OF COMPOSITE MATERIALS 102
On The Propagation Of Fatigue Damage In An Aerospace Hybrid Shock Absorber Designed For Additive Manufacturing 101
Double-Double Laminate Composites for Unmanned Aerial Vehicles 101
On the Compressive Behaviour of a Composite Stiffened Panel with Artificially Introduced Delamination 100
Cross-influence between intra-laminar damages and fibre bridging at the skin-stringer interface in stiffened composite panels under compression 99
Parametric Investigation of Stiffened Panel Subjected to Compressive Loads: Influence of Initial Delamination Length on Damage Behaviour 94
Evolution of Unstable Skin-Stringer Debonding Propagation in Composite Aircraft Structures: Implications on Damage Tolerant Design 94
An Experimental Approach for Investigating Fatigue-Induced Debonding Propagation in Composite Stiffened Panels Using Thermographic Phase Mapping 92
NUMERICAL INVESTIGATION ON DELAMINATION GROWTH IN COMPOSITE PANELS INCLUDING FIBRE-BRIDGING EFFECT 89
Numerical and Experimental Investigation on Single Lap Composite Joints 83
Influence of Delamination Size and Depth on the Compression Fatigue Behaviour of a Stiffened Aerospace Composite Panel 83
Numerical-experimental correlation of impact-induced damages in CFRP laminates 82
Optimization of composite aeronautical components by Re-designing with double-double laminates 81
Damage tolerance evaluation of a C/C-SiC composite body flap of a re-entry vehicle 80
Development and application of a numerical procedure for the simulation of the “Fibre Bridging” phenomenon in composite structures 79
Design of a composite wind turbine blade manufactured with the ONE SHOT BLADE® technology 79
Numerical-experimental investigation into the tensile behavior of a hybrid metallic-CFRP stiffened aeronautical panel 76
NUMERICAL INVESTIGATION ON DELAMINATION GROWTH IN COMPOSITE PANELS INCLUDING FIBRE-BRIDGING EFFECT 74
Experimental and numerical assessment of fibre bridging toughening effects on the compressive behaviour of delaminated composite plates 73
Numerical investigation on the stringer termination debonding in tensile loaded hybrid metallic-CFRP stiffened aeronautical panel 68
Mixed-mode delamination growth prediction in stiffened CFRP panels by means of a novel fast procedure 64
Fiber bridging induced toughening effects on the delamination behavior of composite stiffened panels under bending loading: A numerical/experimental study 64
Numerical study on the toughening effect of the fiber bridging on delaminated composite stiffened panel 63
Instability of delamination growth in buckled stiffened composite panels 23
Sustainable Design of Palm- Inspired Urban Lighting System Using Hybrid Materials and 3D Printing 21
Unveiling the role of peak load in the stability and growth of interlaminar fatigue damage in composite structures 21
A local load ratio approach to fatigue delamination growth simulation in CFRP aeronautical subcomponent 13
Mimicking Alveolar Lung Structures with Lattice Designs 8
Totale 7.895
Categoria #
all - tutte 27.057
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 27.057


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2020/20211 0 0 0 0 0 0 0 0 0 0 0 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
2025/20265.149 161 296 364 232 423 2.761 273 124 196 164 101 54
Totale 7.895