statistiche ricercatore

Nazione	#
US - Stati Uniti d'America	428
RU - Federazione Russa	163
SG - Singapore	107
CN - Cina	85
IT - Italia	47
VN - Vietnam	38
BR - Brasile	35
GB - Regno Unito	28
FR - Francia	23
DE - Germania	22
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	1.161

Nome	#
Fatigue damage diagnosis and prognosis of an aeronautical structure based on surrogate modelling and particle filter	156
Qualification of distributed optical fiber sensors using probability of detection curves for delamination in composite laminates	148
Strain-based delamination prediction in fatigue loaded CFRP coupon specimens by deep learning and static loading data	137
Probability of Delamination Detection for CFRP DCB Specimens Using Rayleigh Distributed Optical Fiber Sensors	127
IMPACT DAMAGE IDENTIFICATION IN A COMPOSITE STRUCTURE BY SURROGATE MODELLING AND MARKOV-CHAIN MONTE-CARLO METHOD	124
An interactive damage progression model for cross-ply laminates subject to fatigue load cycles	124
Damage diagnosis and prognosis in a composite structure by surrogate modelling and particle filtering	122
Damage diagnosis and prognosis in composite double cantilever beam coupons by particle filtering and surrogate modelling	120
On the evaluation of a coupled sequential approach for rotorcraft landing simulation	117
Totale	1.175

	Totale	Lug	Ago	Sett	Ott	Nov	Dic	Gen	Feb	Mar	Apr	Mag	Giu
2020/2021	16	0	0	0	0	0	0	0	0	0	0	0	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	679	117	119	34	49	65	29	92	49	32	72	17	4
Totale													1.175

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