statistiche ricercatore

Continente	#
NA - Nord America	2.268
EU - Europa	1.744
AS - Asia	1.154
SA - Sud America	101
AF - Africa	29
Continente sconosciuto - Info sul continente non disponibili	10
OC - Oceania	2
Totale	5.308

Nazione	#
US - Stati Uniti d'America	2.247
IT - Italia	379
DE - Germania	377
CN - Cina	329
SG - Singapore	309
FR - Francia	261
GB - Regno Unito	251
VN - Vietnam	200
RU - Federazione Russa	111
UA - Ucraina	95
NL - Olanda	81
BR - Brasile	70
KR - Corea	57
BD - Bangladesh	48
TR - Turchia	38
CH - Svizzera	36
HK - Hong Kong	35
IE - Irlanda	27
AT - Austria	26
SE - Svezia	26
FI - Finlandia	20
MY - Malesia	20
GR - Grecia	19
JP - Giappone	19
IN - India	17
PE - Perù	16
TW - Taiwan	16
JO - Giordania	15
CA - Canada	13
DZ - Algeria	11
TH - Thailandia	11
ES - Italia	10
AR - Argentina	8
EU - Europa	8
IQ - Iraq	8
AP - ???statistics.table.value.countryCode.AP???	6
PH - Filippine	6
IL - Israele	5
PK - Pakistan	5
DK - Danimarca	4
KE - Kenya	4
ZA - Sudafrica	4
AE - Emirati Arabi Uniti	3
BO - Bolivia	3
IR - Iran	3
SA - Arabia Saudita	3
UZ - Uzbekistan	3
AU - Australia	2
BE - Belgio	2
EG - Egitto	2
JM - Giamaica	2
MA - Marocco	2
MD - Moldavia	2
NG - Nigeria	2
PL - Polonia	2
TT - Trinidad e Tobago	2
AZ - Azerbaigian	1
BA - Bosnia-Erzegovina	1
CL - Cile	1
CO - Colombia	1
CR - Costa Rica	1
CZ - Repubblica Ceca	1
DM - Dominica	1
EC - Ecuador	1
ET - Etiopia	1
ID - Indonesia	1
LU - Lussemburgo	1
ML - Mali	1
MU - Mauritius	1
NP - Nepal	1
PR - Porto Rico	1
RO - Romania	1
SN - Senegal	1
SV - El Salvador	1
VE - Venezuela	1
Totale	5.300

Nome	#
Advanced higher-order one-dimensional models for fluid-structure interaction analysis	604
Static aeroelastic response of wing-structures accounting for in-plane cross-section deformation	558
Advanced Beam Formulations for Free Vibration Analysis of Conventional and Joined Wings	523
A refined structural model for static aeroelastic response and divergence of metallic and composite wings	473
Nonhomogeneous atherosclerotic plaque analysis via enhanced 1D structural models	407
Dynamic Response of Thin-Walled Structures by Variable Kinematic One-Dimensional Models	372
An Improved Beam Formulation for Aeroelastic Applications	365
Vortex Lattice Method Coupled with Advanced One-Dimensional Structural Models	364
Static and Dynamic Analysis of a Thin-Walled Layered Cylinder by Refined 1D Theories	330
Accurate 1D structural models for the analysis of non-homogeneous biomechanical structures	296
Refined Kinematics for Dynamic Analysis of Thin-Walled Composite Beams	263
A Refined 1D FE Model for the Application to Aeroelasticity of Composite Wings	262
Effect of Warping due to Aerodynamic Loadings in Composite Wings	259
Analysis of Stokes flows by Carrera unified formulation	232
Totale	5.308

	Totale	Lug	Ago	Sett	Ott	Nov	Dic	Gen	Feb	Mar	Apr	Mag	Giu
2021/2022	142	0	0	0	3	8	12	11	3	19	17	16	53
2022/2023	796	24	58	4	34	26	37	99	13	42	8	31	420
2023/2024	93	4	0	5	5	8	10	1	9	10	2	20	19
2024/2025	397	5	39	14	30	67	37	11	38	88	20	21	27
2025/2026	1.042	85	56	50	75	106	49	183	61	196	98	34	49
2026/2027	179	35	40	58	46	0	0	0	0	0	0	0	0
Totale													5.308

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