RUSSO, ANGELA
 Distribuzione geografica
Continente #
EU - Europa 2.120
AS - Asia 1.364
NA - Nord America 1.171
SA - Sud America 350
AF - Africa 23
OC - Oceania 5
Totale 5.033
Nazione #
RU - Federazione Russa 1.160
US - Stati Uniti d'America 1.121
SG - Singapore 413
IE - Irlanda 375
CN - Cina 326
BR - Brasile 299
HK - Hong Kong 258
IT - Italia 223
VN - Vietnam 136
DE - Germania 89
GB - Regno Unito 77
KR - Corea 65
FR - Francia 43
IN - India 42
CA - Canada 32
AR - Argentina 26
UA - Ucraina 26
FI - Finlandia 22
GR - Grecia 21
ID - Indonesia 21
SE - Svezia 19
JP - Giappone 18
TR - Turchia 16
IQ - Iraq 14
NL - Olanda 14
BD - Bangladesh 13
EC - Ecuador 12
AT - Austria 9
MX - Messico 8
RO - Romania 8
PK - Pakistan 7
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
EG - Egitto 4
PL - Polonia 4
DZ - Algeria 3
ES - Italia 3
LT - Lituania 3
MA - Marocco 3
PY - Paraguay 3
TT - Trinidad e Tobago 3
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
UY - Uruguay 2
VE - Venezuela 2
AE - Emirati Arabi Uniti 1
AL - Albania 1
AO - Angola 1
AZ - Azerbaigian 1
CL - Cile 1
CR - Costa Rica 1
ET - Etiopia 1
HN - Honduras 1
HR - Croazia 1
HU - Ungheria 1
JM - Giamaica 1
KE - Kenya 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 5.033
Città #
Moscow 385
Dublin 375
Hong Kong 257
Santa Clara 248
Singapore 150
Chandler 146
Dallas 70
Hefei 67
Jacksonville 61
Seoul 61
Beijing 58
Ho Chi Minh City 55
Munich 40
Princeton 40
Roxbury 40
Ashburn 36
Cambridge 36
Bengaluru 28
São Paulo 27
Hanoi 23
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
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
Haiphong 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
Mountain View 3
Nanjing 3
Paris 3
Phủ Lý 3
Piscataway 3
Quito 3
Totale 2.716
Nome #
A robust cumulative damage approach for the simulation of delamination under cyclic loading conditions 128
A FEASIBILITY STUDY ON ADDITIVE MANUFACTURED HYBRID METAL/COMPOSITE SHOCK ABSORBER PANELS 126
FIBREGLASS WIND TURBINE ONE SHOT BLADE®: DAMAGE TOLERANT DESIGN 110
A Computational Cost-effective numerical methodology for the simulation of the fatigue behaviour in composite materials. 110
A numerical/experimental study on the induction heating of adhesives for composite materials bonding 107
A sensitivity analysis on Fibre bridging effects in delaminated composite panels under Flexural Loading Conditions 103
A robust numerical methodology for fatigue damage evolution simulation in composites 100
On the use of Double - Double advanced materiai processing for the design of a composite fuselage barrel. 97
A Numerical Assessment of Fibre Bridging Influence on Composite Panels Skin-stringer Debonding 97
Large Notch Damage Evolution in Omega Stiffened Composite Panels 96
A numerical-analytical approach for the preliminary design of thin-walled cylindrical shell structures with elliptical cut-outs 96
A feasibility study on additive manufactured hybrid metal/composite shock absorbers 96
An Experimental Assessment on the Influence of Carbon Nanotubes Matrix Charging on the Fatigue Behavior of Composite Laminates 94
A numerical investigation of the interaction between interlaminar and intralaminar damages in a fatigued composite panel 93
Fatigue driven delamination in composite structures: Definition and assessment of a novel fracture mechanics based computational tool 93
EFFECTS OF THERMAL LOADS ON THE MECHANICAL BEHAVIOUR OF BONDED AIRCRAFT SUBCOMPONENTS. 93
Compressive Behaviour of a Damaged Omega Stiffened Panel: Damage Detection and Numerical Analysis 92
An insight on the crashworthiness behavior of a full-scale composite fuselage section at different impact angles 92
Experimental investigation on 3D printed lightweight sandwich structures for energy absorption aerospace applications 91
A Numerical Study on the Influence of Nanosilica-Reinforced Epoxy Resin on the Delamination Behavior of Composite Laminates 91
Compressive behaviour of a damaged omega stiffened panel: Damage detection and numerical analysis 91
A Numerical Study on Mode II Fatigue Delamination Growth in Composite Laminates 90
A NUMERICAL-EXPERIMENTAL STUDY ON THE IMPCAT RESPONSE OF AN ADDITIVE MANUFACTED HYBRID METAL-COMPOSITE STRURCTURE 90
Modelling the damage evolution in notched omega stiffened composite panels under compression 89
DEVELOPMENT OF A NUMERICAL METHODOLOGY FOR THE SIMULATION OF THE FATIGUE INDUCED DELAMINATION IN COMPOSITE STRUCTURES 89
Experimental investigation on the delamination onset and propagation in composite specimens subjected to compressive loads by using Digital Image Correlation 87
NUMERICAL STUDY ON INDUCTION HEATING OF ADHESIVE FOR BONDING OF COMPOSITE MATERIALS 84
A Paris Law Based Mesh Independent Numerical Methodology for the Simulation of Fatigue Driven Delamination in Composites 82
A numerical parametric study on delamination influence on the fatigue behaviour of stiffened composite components 77
Delamination Effect on the Buckling Behaviour of Carbon–Epoxy Composite Typical Aeronautical Panels 77
On the mechanical behavior of laminated composite plates subjected to compression after impact tests 77
Unstable Delamination Growth in Stiffened Composite Panels Under Cyclic Loading Conditions 76
Influence of manufacturing defects on the mechanical behaviour of all-composite wing under service load conditions 76
Numerical Assessment on the Fatigue Behavior of Composite Open-Hole Tensile Specimens 74
Double-Double Laminate Composites for Unmanned Aerial Vehicles 74
Cross-influence between intra-laminar damages and fibre bridging at the skin-stringer interface in stiffened composite panels under compression 74
Influence of failure criteria and intralaminar damage progression numerical models on the prediction of the mechanical behavior of composite laminates 74
Fibreglass wind turbine blades: Damage tolerant design and verification 73
On The Propagation Of Fatigue Damage In An Aerospace Hybrid Shock Absorber Designed For Additive Manufacturing 71
The role of intralaminar damages on the delamination evolution in laminated composite structures 70
The peculiar SMart-Time XB approach for delamination growth prediction and its evolution towards fatigue investigations 69
Development of a Numerical Methodology Able to Simulate the Unstable Mixed Mode Delamination Growth in Stiffened Composite Panels Under Cyclic Loading Conditions 69
On the Use of Digital Image Correlation to Assess the Damage Behavior of Composite Coupons Under Compression 69
Nanofillers’ effects on fracture energy in composite aerospace structures 69
Ultrasonic damage detection of impacted long and short fibre composite specimens 65
NUMERICAL INVESTIGATION ON DELAMINATION GROWTH IN COMPOSITE PANELS INCLUDING FIBRE-BRIDGING EFFECT 64
Numerical-experimental correlation of impact-induced damages in CFRP laminates 63
Parametric Investigation of Stiffened Panel Subjected to Compressive Loads: Influence of Initial Delamination Length on Damage Behaviour 62
Hybrid Composite-Polypropylene Sandwich-based Design for the Fuselage Panel in Commercial Aircraft to Increase the Passive Safety of Passengers 62
Damage Tolerant Behaviour of Unstable Skin-Stringer Debonding Growth in Composite Stiffened Structures 62
A novel numerical methodology for the simulation of unstable debonding growth in aerospace stiffened composite panels 61
Hybrid Composite-Polypropylene Sandwich-Based Design for the Fuselage Panel in Commercial Aircraft to Increase the Passive Safety of Passengers 61
Development and application of a numerical procedure for the simulation of the “Fibre Bridging” phenomenon in composite structures 58
Design of a composite wind turbine blade manufactured with the ONE SHOT BLADE® technology 58
On the Compressive Behaviour of a Composite Stiffened Panel with Artificially Introduced Delamination 55
NUMERICAL INVESTIGATION ON DELAMINATION GROWTH IN COMPOSITE PANELS INCLUDING FIBRE-BRIDGING EFFECT 52
Experimental and numerical assessment of fibre bridging toughening effects on the compressive behaviour of delaminated composite plates 52
An Experimental Approach for Investigating Fatigue-Induced Debonding Propagation in Composite Stiffened Panels Using Thermographic Phase Mapping 51
Evolution of Unstable Skin-Stringer Debonding Propagation in Composite Aircraft Structures: Implications on Damage Tolerant Design 51
Numerical-experimental investigation into the tensile behavior of a hybrid metallic-CFRP stiffened aeronautical panel 51
Damage tolerance evaluation of a C/C-SiC composite body flap of a re-entry vehicle 50
Mixed-mode delamination growth prediction in stiffened CFRP panels by means of a novel fast procedure 45
Influence of Delamination Size and Depth on the Compression Fatigue Behaviour of a Stiffened Aerospace Composite Panel 44
Optimization of composite aeronautical components by Re-designing with double-double laminates 42
Fiber bridging induced toughening effects on the delamination behavior of composite stiffened panels under bending loading: A numerical/experimental study 42
Numerical study on the toughening effect of the fiber bridging on delaminated composite stiffened panel 40
Numerical and Experimental Investigation on Single Lap Composite Joints 39
Numerical investigation on the stringer termination debonding in tensile loaded hybrid metallic-CFRP stiffened aeronautical panel 39
Totale 5.145
Categoria #
all - tutte 21.329
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 21.329


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
2025/20262.399 161 296 364 232 423 923 0 0 0 0 0 0
Totale 5.145