statistiche ricercatore

Continente	#
NA - Nord America	1.737
EU - Europa	1.314
AS - Asia	605
SA - Sud America	108
AF - Africa	40
OC - Oceania	3
Continente sconosciuto - Info sul continente non disponibili	1
Totale	3.808

Nazione	#
US - Stati Uniti d'America	1.692
RU - Federazione Russa	452
IT - Italia	423
SG - Singapore	181
CN - Cina	159
VN - Vietnam	104
BR - Brasile	91
DE - Germania	67
GB - Regno Unito	57
FR - Francia	51
AT - Austria	42
FI - Finlandia	40
UA - Ucraina	39
SE - Svezia	37
CA - Canada	35
NL - Olanda	23
KR - Corea	22
CI - Costa d'Avorio	20
JP - Giappone	20
IE - Irlanda	19
JO - Giordania	19
ES - Italia	18
IN - India	18
MA - Marocco	15
PH - Filippine	15
ID - Indonesia	14
BE - Belgio	13
HK - Hong Kong	12
CH - Svizzera	9
AR - Argentina	8
IQ - Iraq	6
TW - Taiwan	6
MX - Messico	5
PL - Polonia	5
BD - Bangladesh	4
PT - Portogallo	4
TR - Turchia	4
AE - Emirati Arabi Uniti	3
AU - Australia	3
EC - Ecuador	3
LT - Lituania	3
MY - Malesia	3
PE - Perù	3
CZ - Repubblica Ceca	2
DK - Danimarca	2
EE - Estonia	2
IR - Iran	2
KE - Kenya	2
KH - Cambogia	2
PA - Panama	2
TT - Trinidad e Tobago	2
VE - Venezuela	2
ZA - Sudafrica	2
AM - Armenia	1
AZ - Azerbaigian	1
BA - Bosnia-Erzegovina	1
CO - Colombia	1
CY - Cipro	1
EU - Europa	1
GR - Grecia	1
GT - Guatemala	1
IL - Israele	1
IM - Isola di Man	1
LB - Libano	1
LK - Sri Lanka	1
ME - Montenegro	1
OM - Oman	1
PK - Pakistan	1
RS - Serbia	1
SA - Arabia Saudita	1
SK - Slovacchia (Repubblica Slovacca)	1
TH - Thailandia	1
UZ - Uzbekistan	1
ZW - Zimbabwe	1
Totale	3.808

Nome	#
A Vision-Based Technique for in-Flight Measurement of Helicopter Blade Motion	365
ROTOR FOR A HOVER-CAPABLE AIRCRAFT AND METHOD FOR DETECTING THE ATTITUDE OF A BLADE WITH RESPECT TO A HUB OF SUCH A ROTOR	285
Contactless Rotor Flapping Sensor Design, Implementation and Testing	265
Multilevel Structural Optimization for Preliminary Wing-Box Weight Estimation	235
Application of MDO Techniques to the Preliminary Design of Morphed Aircraft	229
Aeroelastic Control of Morphing Wings	223
Viscoelastic Shear Damping Mechanism for Vibration Reduction on a Helicopter Anti-Torque Beam	221
Analytically Driven Experimental Characterisation of Damping in Viscoelastic Materials	216
Weight Prediction of the Lifting System for an Unconventional Aircraft Configuration	214
Design, Manufacturing and Preliminary Test Results of an Adaptive Wing Camber Model	210
The Lifting System of a Prandtlplane, Part 1: Design and Analysis of a Light Alloy Structural Solution	203
Improvement of Structures Vibroacoustics by Widespread Embodiment of Viscoelastic Materials	200
SMorph - Smart Aircraft Morphing Technologies Project	186
Winbox Weight Estimation for Metallic and Composite Manufacturing in a Conceptual Design Phase	176
Hexapod Mechanical Assembly Modal Survey Test	164
Coupling MDO and Principal Component Analysis Techniques for Model Updating and Damage Detection	161
Conceptual Design of an Adaptive Wing for a Three-Surfaces Airplane	151
Preliminary Design Against Flutter of a Prandtlplane Lifting System	123
Totale	3.827

	Totale	Lug	Ago	Sett	Ott	Nov	Dic	Gen	Feb	Mar	Apr	Mag	Giu
2020/2021	74	0	0	0	0	0	0	0	0	0	19	23	32
2021/2022	193	10	16	20	23	24	8	8	10	4	8	32	30
2022/2023	299	20	29	23	26	38	24	2	32	63	16	19	7
2023/2024	172	11	18	6	12	17	21	27	9	5	22	3	21
2024/2025	560	68	6	15	11	125	31	15	47	57	25	87	73
2025/2026	1.305	370	212	76	103	76	51	177	75	69	96	0	0
Totale													3.827

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