VIGLIETTI, ANDREA
 Distribuzione geografica
Continente #
NA - Nord America 179
EU - Europa 153
AS - Asia 61
SA - Sud America 6
AF - Africa 3
OC - Oceania 1
Totale 403
Nazione #
US - Stati Uniti d'America 159
IT - Italia 109
CN - Cina 15
IN - India 12
MX - Messico 11
CA - Canada 9
FR - Francia 9
VN - Vietnam 9
DE - Germania 8
PH - Filippine 6
IR - Iran 5
JO - Giordania 5
PE - Perù 5
GB - Regno Unito 4
NL - Olanda 3
PT - Portogallo 3
TR - Turchia 3
UA - Ucraina 3
DZ - Algeria 2
ES - Italia 2
JP - Giappone 2
PK - Pakistan 2
PL - Polonia 2
RO - Romania 2
RU - Federazione Russa 2
AR - Argentina 1
AT - Austria 1
AU - Australia 1
BG - Bulgaria 1
DK - Danimarca 1
KR - Corea 1
LV - Lettonia 1
NO - Norvegia 1
SE - Svezia 1
TH - Thailandia 1
ZA - Sudafrica 1
Totale 403
Città #
Torino 49
Ann Arbor 18
Fairfield 18
San Donato Milanese 17
Houston 14
University Park 11
Monterrey 10
Seattle 10
Dong Ket 9
Napoli 9
Santa Cruz 8
Ashburn 7
Andover 6
Basking Ridge 6
Buffalo 6
Wilmington 6
Woodbridge 6
Beijing 5
Las Vegas 5
Lima 5
Québec 5
Cambridge 4
Esfahan 4
Lisbon 3
Palo Alto 3
Rotterdam 3
Toronto 3
Varese 3
Bengaluru 2
Hanover 2
Lentini 2
Mumbai 2
Nanchang 2
San Diego 2
Shanghai 2
Trumbull 2
Vaprio D'adda 2
Ankara 1
Auburn 1
Bangkok 1
Blacksburg 1
Boardman 1
Borso del Grappa 1
Changsha 1
Chaville 1
Chicago 1
Clayton 1
Falls Church 1
Fujisawa 1
Guangzhou 1
Haibowan 1
Hangzhou 1
Kocaeli 1
Konya 1
Koszalin 1
Lake Forest 1
Laurel 1
Lincolnshire 1
Los Angeles 1
Menlo Park 1
Mexico 1
Montréal 1
Muizenberg 1
Munich 1
Munro 1
Namakkal 1
Nanjing 1
Noicattaro 1
Oak Lawn 1
Orbassano 1
Phoenix 1
Pusan 1
Rome 1
Saint Louis 1
San Jose 1
Santiago De Compostela 1
Stavanger 1
Stuttgart 1
Tempe 1
Valdagno 1
Vienna 1
Wuhan 1
Totale 316
Nome #
Analysis of tapered composite structures using a refined beam theory, file e384c42f-d4a2-d4b2-e053-9f05fe0a1d67 172
ADVANCED NUMERICAL METHODS FOR FAILURE ANALYSIS OF METALLIC AND COMPOSITE AEROSPACE STRUCTURES, file e384c42f-dc17-d4b2-e053-9f05fe0a1d67 107
EFFECT OF FIBER ORIENTATION PATH ON THE BUCKLING, FREE VIBRATION, AND STATIC ANALYSES OF VARIABLE ANGLE TOW PANELS, file e384c432-5eac-d4b2-e053-9f05fe0a1d67 32
Numerical models for the design of variable angle tow piezo-composite structures, file e384c430-7f8b-d4b2-e053-9f05fe0a1d67 21
High-fidelity vibration analysis of tapered swept tailored composite wing boxes, file e384c431-050d-d4b2-e053-9f05fe0a1d67 15
Technical report: Finite element static response analysis of the composite fuselage of Leonardo F48 UAV, file e384c430-1865-d4b2-e053-9f05fe0a1d67 11
Preliminary technical report: Finite element structural analyses of the main landing gear of Leonardo F48 UAV, file e384c430-19a6-d4b2-e053-9f05fe0a1d67 9
Technical report: Finite element structural analyses of the nose landing gear of Leonardo F48 UAV, file e384c430-1cef-d4b2-e053-9f05fe0a1d67 9
Free vibration analysis of locally damaged aerospace tapered composite structures using component-wise models, file e384c430-027a-d4b2-e053-9f05fe0a1d67 8
Preliminary technical report: Finite element structural analyses of the nose landing gear of Leonardo F48 UAV, file e384c430-1a28-d4b2-e053-9f05fe0a1d67 8
Analyses of VAT composite structures using a layer-wise 1-D model, file e384c430-9825-d4b2-e053-9f05fe0a1d67 8
High-Fidelity modeling and dynamic analysis of damaged tapered composite structures, file e384c430-05c7-d4b2-e053-9f05fe0a1d67 7
Technical report: Finite element structural analyses of the main landing gear of Leonardo F48 UAV, file e384c430-19a7-d4b2-e053-9f05fe0a1d67 7
Preliminary technical report: Finite element static response analysis of the composite fuselage of Leonardo F48 UAV, file e384c430-1ab3-d4b2-e053-9f05fe0a1d67 7
Preliminary technical report: Finite element free vibration and buckling analyses of the composite fuselage of Leonardo F48 UAV, file e384c430-1a0b-d4b2-e053-9f05fe0a1d67 6
Technical report: Finite element free vibration analysis of the composite fuselage of Leonardo F48 UAV, file e384c430-201d-d4b2-e053-9f05fe0a1d67 6
Analysis of variable angle tow composites structures using variable kinematic models, file e384c430-d89b-d4b2-e053-9f05fe0a1d67 6
Analysis of laminate boxes made of vat composites by higher-order CUF models, file e384c430-9fa0-d4b2-e053-9f05fe0a1d67 5
Free vibration analysis of variable angle-tow composite wing structures, file e384c433-27a3-d4b2-e053-9f05fe0a1d67 5
Technical note: Critical analysis of three different layouts of the composite fuselage of Leonardo F48 UAV, file e384c430-1ab4-d4b2-e053-9f05fe0a1d67 4
The analysis of tapered structures using a component-wise approach based on refined one-dimensional models, file e384c42f-6f3e-d4b2-e053-9f05fe0a1d67 1
A Componet-Wise Approach for the Failure of Complex Aeronautical Structures, file e384c42f-d7ea-d4b2-e053-9f05fe0a1d67 1
Low Fidelity and High Fidelity Structural Models for Hybrid Composite Aircraft Structures, file e384c430-2ddc-d4b2-e053-9f05fe0a1d67 1
Totale 456
Categoria #
all - tutte 676
article - articoli 334
book - libri 0
conference - conferenze 204
curatela - curatele 0
other - altro 137
patent - brevetti 0
selected - selezionate 0
volume - volumi 0
Totale 1351


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2017/201827 0000 00 00 201411
2018/201950 3222 22 70 4989
2019/2020131 472668 57 84 6635
2020/202197 221532 133 36 6699
2021/2022118 111424 2410 151 141310
2022/202332 17654 00 00 0000
Totale 456