statistiche ricercatore

Nazione	#
US - Stati Uniti d'America	407
RU - Federazione Russa	163
SG - Singapore	107
CN - Cina	85
IT - Italia	47
VN - Vietnam	38
BR - Brasile	35
GB - Regno Unito	28
DE - Germania	22
FR - Francia	21
KR - Corea	20
NL - Olanda	17
AU - Australia	16
HK - Hong Kong	16
JP - Giappone	10
CA - Canada	8
FI - Finlandia	6
BD - Bangladesh	5
MX - Messico	5
UA - Ucraina	5
ES - Italia	4
ZA - Sudafrica	4
AR - Argentina	3
TR - Turchia	3
AT - Austria	2
BY - Bielorussia	2
CI - Costa d'Avorio	2
GR - Grecia	2
ID - Indonesia	2
IE - Irlanda	2
IQ - Iraq	2
IR - Iran	2
JM - Giamaica	2
KG - Kirghizistan	2
PK - Pakistan	2
PL - Polonia	2
SE - Svezia	2
AE - Emirati Arabi Uniti	1
AL - Albania	1
AZ - Azerbaigian	1
BA - Bosnia-Erzegovina	1
BO - Bolivia	1
BZ - Belize	1
CL - Cile	1
CO - Colombia	1
CR - Costa Rica	1
DK - Danimarca	1
DO - Repubblica Dominicana	1
DZ - Algeria	1
EC - Ecuador	1
EE - Estonia	1
EG - Egitto	1
GA - Gabon	1
GE - Georgia	1
IL - Israele	1
IN - India	1
JO - Giordania	1
KH - Cambogia	1
LA - Repubblica Popolare Democratica del Laos	1
LT - Lituania	1
LV - Lettonia	1
MA - Marocco	1
MD - Moldavia	1
NG - Nigeria	1
OM - Oman	1
PE - Perù	1
PH - Filippine	1
PY - Paraguay	1
RO - Romania	1
SA - Arabia Saudita	1
TW - Taiwan	1
UY - Uruguay	1
UZ - Uzbekistan	1
VE - Venezuela	1
Totale	1.138

Nome	#
Fatigue damage diagnosis and prognosis of an aeronautical structure based on surrogate modelling and particle filter	153
Qualification of distributed optical fiber sensors using probability of detection curves for delamination in composite laminates	144
Strain-based delamination prediction in fatigue loaded CFRP coupon specimens by deep learning and static loading data	136
IMPACT DAMAGE IDENTIFICATION IN A COMPOSITE STRUCTURE BY SURROGATE MODELLING AND MARKOV-CHAIN MONTE-CARLO METHOD	124
Probability of Delamination Detection for CFRP DCB Specimens Using Rayleigh Distributed Optical Fiber Sensors	122
Damage diagnosis and prognosis in a composite structure by surrogate modelling and particle filtering	122
An interactive damage progression model for cross-ply laminates subject to fatigue load cycles	118
Damage diagnosis and prognosis in composite double cantilever beam coupons by particle filtering and surrogate modelling	118
On the evaluation of a coupled sequential approach for rotorcraft landing simulation	115
Totale	1.152

	Totale	Lug	Ago	Sett	Ott	Nov	Dic	Gen	Feb	Mar	Apr	Mag	Giu
2020/2021	33	0	0	0	0	0	0	0	0	0	6	11	16
2021/2022	52	4	2	7	3	1	4	5	4	4	4	8	6
2022/2023	58	6	9	2	1	2	6	1	6	12	2	10	1
2023/2024	59	3	8	5	8	3	2	5	0	1	11	3	10
2024/2025	240	1	3	2	0	41	20	2	25	45	15	47	39
2025/2026	656	117	119	34	49	65	29	92	49	32	70	0	0
Totale													1.152

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