PORTO @ Archivio Istituzionale della Ricerca

SAPUTO, SALVATORE
 Distribuzione geografica
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Continente #
EU - Europa 385
NA - Nord America 274
AS - Asia 227
SA - Sud America 5
AF - Africa 2
Totale 893
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Nazione #
US - Stati Uniti d'America 273
BE - Belgio 172
IT - Italia 130
SG - Singapore 114
RU - Federazione Russa 38
CN - Cina 34
KR - Corea 27
ID - Indonesia 18
TR - Turchia 11
IE - Irlanda 9
IN - India 9
FI - Finlandia 8
NL - Olanda 7
DE - Germania 6
IR - Iran 5
BR - Brasile 4
BG - Bulgaria 3
FR - Francia 3
PT - Portogallo 3
TW - Taiwan 3
ES - Italia 2
GB - Regno Unito 2
JP - Giappone 2
AE - Emirati Arabi Uniti 1
AR - Argentina 1
CH - Svizzera 1
CI - Costa d'Avorio 1
DO - Repubblica Dominicana 1
HK - Hong Kong 1
JO - Giordania 1
PK - Pakistan 1
SI - Slovenia 1
ZA - Sudafrica 1
Totale 893
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Città #
Brussels 172
Singapore 89
Council Bluffs 81
Turin 48
Boardman 43
Seattle 38
Jakarta 18
Santa Clara 13
Milan 12
Naples 11
Yubileyny 11
Dublin 9
Bari 6
Genoa 6
Helsinki 6
Beijing 5
Seoul 5
Ankara 4
Arezzo 4
Cedar Knolls 4
Crispano 4
Dongguan 4
Istanbul 4
Pastorano 4
Rome 4
Stillwater 4
Tewksbury 4
Boston 3
Tehran 3
Ashburn 2
Barolo 2
Bengaluru 2
Bolzano 2
Busto Arsizio 2
Chang-hua 2
Chennai 2
Eskişehir 2
Fiume Veneto 2
Florence 2
Fronteira 2
Guangzhou 2
Lappeenranta 2
Madrid 2
Melito di Napoli 2
Palermo 2
Roorkee 2
Shijiazhuang 2
Tokyo 2
Zhengzhou 2
Zwolle 2
Abidjan 1
Abu Dhabi 1
Americana 1
Amsterdam 1
Apricena 1
Asti 1
Bahía Blanca 1
Borgosesia 1
Caselle Torinese 1
Caserta 1
Frankfurt am Main 1
Gangbuk-gu 1
Goirle 1
Imola 1
Itaguai 1
Johannesburg 1
Kowloon 1
Kunming 1
Lahore 1
Little Rock 1
London 1
Lucknow 1
Newark 1
Orta di Atella 1
Oxford 1
Paris 1
Pasadena 1
Piscataway 1
Porto 1
Porto Alegre 1
Qiqihar 1
Richmond 1
Rivoli 1
Santo Domingo 1
St Petersburg 1
São Paulo 1
Taipei 1
Talas 1
Tianjin 1
Trieste 1
Yuncheng 1
Zhongshan 1
Zurich 1
Totale 704
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Nome #
Free edge stress analysis of composite laminates subjected to low-velocity impact using higher-order layer-wise models 144
High-Fidelity Stress Fields in Contact Problems using Beam, Plates, and Shells Layer-Wise Models 84
Low-Velocity Impact Analysis of Stiffened Composite Plates Using Higher-Order Layer-Wise Models 75
BISTABLE ACTUATOR | [BISTABILER STELLANTRIEB] 29
Application of an additive manufactured hybrid metal/composite shock absorber panel to a military seat ejection system 27
A robust numerical methodology for fatigue damage evolution simulation in composites 23
2D higher-order theories for progressive damage model of composite structures based on Hashin and Puck failure criteria 22
A numerical-analytical approach for the preliminary design of thin-walled cylindrical shell structures with elliptical cut-outs 22
Dynamic Pulse Buckling of Composite Stanchions in the Sub-Cargo Floor Area of a Civil Regional Aircraft 21
Mixed-mode delamination growth prediction in stiffened CFRP panels by means of a novel fast procedure 21
Numerical methodologies for simulating bird-strike on composite wings 21
Shape memory alloy-based actuator: Experimental and modelling 21
A numerical-experimental assessment on a composite fuselage barrel vertical drop test: Induced damage onset and evolution 20
A numerical study on the impact behaviour of natural fibres made honeycomb cores 20
Modelling the damage evolution in notched omega stiffened composite panels under compression 19
A sensitivity analysis of the damage behavior of a leading-edge subject to bird strike 19
A feasibility study on additive manufactured hybrid metal/composite shock absorbers 19
A Joint Numerical-Experimental Study on Impact Induced Intra-laminar and Inter-laminar Damage in Laminated Composites 19
A user defined material model for the simulation of impact induced damage in composite 19
Numerical-Experimental Correlation of Interlaminar Damage Growth in Composite Structures: Setting Cohesive Zone Model Parameters 19
Crashworthiness of a Composite Wing Section: Numerical Investigation of the Bird Strike Phenomenon by Using a Coupled Eulerian–Lagrangian Approach 18
A brief introduction to the bird strike numerical simulation 18
Crashworthiness of a general aviation fuselage section: 3D FEM numerical modelling and validation 18
On the crashworthiness behaviour of a composite fuselage Sub-floor component 18
A numerical study on multi-terrain impacts of an aeronautical fuselage section 18
Numerical-experimental investigation into the tensile behavior of a hybrid metallic-CFRP stiffened aeronautical panel 18
Numerical simulation of the mechanical behaviour of shape memory alloys based actuators 17
Modeling the Behavior of Shape Memory Alloys and Memory Alloy-Based Devices 17
Crashworthiness of wing leading edges under bird impact event 17
A numerical assessment on the influences of material toughness on the crashworthiness of a composite fuselage barrel 17
Modeling low velocity impact phenomena on composite structures 16
On the mechanical behavior of laminated composite plates subjected to compression after impact tests 16
Numerical-experimental correlation of impact-induced damages in CFRP laminates 16
Impact behaviour of omega stiffened composite panels 15
Numerical investigation of a stiffened panel subjected to low velocity impacts 15
An insight on the crashworthiness behavior of a full-scale composite fuselage section at different impact angles 15
Stacking sequence effects on damage onset in composite laminate subjected to low velocity impact 15
Numerical investigation on the stringer termination debonding in tensile loaded hybrid metallic-CFRP stiffened aeronautical panel 15
Thermo-mechanical behaviour of a composite stiffened panel undergoing the tail-pipe fire event 14
Characterisation of the impact induced damage in composites by cross-comparison among experimental non-destructive evaluation techniques and numerical simulations 14
Parametric investigation on the damage behavior of a CFRP omega reinforced panel subjected to asymmetrical flexural load conditions 14
Fire condition effects on the mechanical behaviour of composite structures 13
Large Notch Damage Evolution in Omega Stiffened Composite Panels 13
Cross-influence between intra-laminar damages and fibre bridging at the skin-stringer interface in stiffened composite panels under compression 12
Totale 1.043
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Categoria #
all - tutte 6.339
article - articoli 3.166
book - libri 0
conference - conferenze 2.780
curatela - curatele 0
other - altro 0
patent - brevetti 153
selected - selezionate 0
volume - volumi 240
Totale 12.678
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Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2022/2023201 0 0 0 0 6 5 3 7 16 8 13 143
2023/2024534 276 31 24 15 16 15 19 49 17 6 26 40
2024/2025308 5 105 33 129 36 0 0 0 0 0 0 0
Totale 1.043