statistiche ricercatore

Continente	#
NA - Nord America	1.828
EU - Europa	1.376
AS - Asia	609
SA - Sud America	109
AF - Africa	40
Continente sconosciuto - Info sul continente non disponibili	20
OC - Oceania	3
Totale	3.985

Nazione	#
US - Stati Uniti d'America	1.777
IT - Italia	480
RU - Federazione Russa	452
SG - Singapore	181
CN - Cina	159
VN - Vietnam	108
BR - Brasile	92
DE - Germania	67
GB - Regno Unito	57
FR - Francia	51
AT - Austria	42
FI - Finlandia	40
UA - Ucraina	39
CA - Canada	38
SE - Svezia	37
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
CH - Svizzera	14
ID - Indonesia	14
BE - Belgio	13
HK - Hong Kong	12
AR - Argentina	8
IQ - Iraq	6
MX - Messico	6
TW - Taiwan	6
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
CR - Costa Rica	1
CY - Cipro	1
EU - Europa	1
GR - Grecia	1
GT - Guatemala	1
IL - Israele	1
IM - Isola di Man	1
JM - Giamaica	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	3.966

Nome	#
A Vision-Based Technique for in-Flight Measurement of Helicopter Blade Motion	372
ROTOR FOR A HOVER-CAPABLE AIRCRAFT AND METHOD FOR DETECTING THE ATTITUDE OF A BLADE WITH RESPECT TO A HUB OF SUCH A ROTOR	294
Contactless Rotor Flapping Sensor Design, Implementation and Testing	271
Multilevel Structural Optimization for Preliminary Wing-Box Weight Estimation	257
Application of MDO Techniques to the Preliminary Design of Morphed Aircraft	233
Viscoelastic Shear Damping Mechanism for Vibration Reduction on a Helicopter Anti-Torque Beam	229
Aeroelastic Control of Morphing Wings	228
Design, Manufacturing and Preliminary Test Results of an Adaptive Wing Camber Model	226
Analytically Driven Experimental Characterisation of Damping in Viscoelastic Materials	225
Weight Prediction of the Lifting System for an Unconventional Aircraft Configuration	220
Improvement of Structures Vibroacoustics by Widespread Embodiment of Viscoelastic Materials	216
The Lifting System of a Prandtlplane, Part 1: Design and Analysis of a Light Alloy Structural Solution	213
SMorph - Smart Aircraft Morphing Technologies Project	193
Winbox Weight Estimation for Metallic and Composite Manufacturing in a Conceptual Design Phase	185
Hexapod Mechanical Assembly Modal Survey Test	168
Coupling MDO and Principal Component Analysis Techniques for Model Updating and Damage Detection	167
Conceptual Design of an Adaptive Wing for a Three-Surfaces Airplane	154
Preliminary Design Against Flutter of a Prandtlplane Lifting System	134
Totale	3.985

	Totale	Lug	Ago	Sett	Ott	Nov	Dic	Gen	Feb	Mar	Apr	Mag	Giu
2021/2022	183	0	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	1.417	370	212	76	103	76	51	177	75	69	100	23	85
2026/2027	46	28	18	0	0	0	0	0	0	0	0	0	0
Totale													3.985

RE.PUBLIC@POLIMI pubblicazioni di ricerca del Politecnico di Milano