statistiche ricercatore

Continente	#
AS - Asia	765
EU - Europa	655
NA - Nord America	446
SA - Sud America	68
Continente sconosciuto - Info sul continente non disponibili	63
AF - Africa	4
OC - Oceania	4
Totale	2.005

Nazione	#
US - Stati Uniti d'America	427
IT - Italia	390
VN - Vietnam	210
SG - Singapore	179
CN - Cina	154
RU - Federazione Russa	82
DE - Germania	62
BR - Brasile	51
KR - Corea	51
BD - Bangladesh	40
HK - Hong Kong	37
BE - Belgio	35
FR - Francia	26
IN - India	20
FI - Finlandia	17
GB - Regno Unito	11
PH - Filippine	11
ID - Indonesia	9
JP - Giappone	9
TH - Thailandia	9
TR - Turchia	9
AT - Austria	8
CA - Canada	8
AR - Argentina	7
MX - Messico	7
NL - Olanda	7
PK - Pakistan	6
TW - Taiwan	6
IQ - Iraq	4
PE - Perù	4
PL - Polonia	4
AE - Emirati Arabi Uniti	3
AU - Australia	3
GR - Grecia	3
CH - Svizzera	2
CZ - Repubblica Ceca	2
IE - Irlanda	2
JO - Giordania	2
MA - Marocco	2
PY - Paraguay	2
AZ - Azerbaigian	1
BB - Barbados	1
BH - Bahrain	1
BN - Brunei Darussalam	1
BW - Botswana	1
CL - Cile	1
CO - Colombia	1
CW - ???statistics.table.value.countryCode.CW???	1
DZ - Algeria	1
EC - Ecuador	1
ES - Italia	1
GT - Guatemala	1
JM - Giamaica	1
LT - Lituania	1
MY - Malesia	1
NZ - Nuova Zelanda	1
PR - Porto Rico	1
SA - Arabia Saudita	1
SI - Slovenia	1
UA - Ucraina	1
UZ - Uzbekistan	1
VE - Venezuela	1
Totale	1.943

Nome	#
Numerical Analysis of a Flow Control System for High-Pressure Turbine Vanes Subject to Highly Oscillating Inflow Conditions	278
Numerical Analysis and Design of New Exhaust Section Downstream of Constant Volume Combustor	260
Non-Reactive Experimental Analysis of an Exhaust Section downstream of a CVC	222
Development of 1D Model of Constant-Volume Combustor and Numerical Analysis of the Exhaust Nozzle	219
Development and Validation of a 0-D/1-D Model to Evaluate Pulsating Conditions from a Constant Volume Combustor	213
Experimental Inert Characterization of an Exhaust System Downstream of a CVC	209
Numerical Analysis and Design of New Exhaust Section Downstream of Constant Volume Combustor	209
Design Solutions for the Coupling of High-Pressure Turbine Vanes to Pressure-Gain Combustors	187
Numerical Analysis of a Flow Control System for High-Pressure Turbine Vanes Subject to Highly Oscillating Inflow Conditions	174
Reactive Experimental PIV Analysis of Pulsating Flow Exiting from Cyclic Deflagrative Pressure Gain Combustion	32
Aerodynamic Optimization of Transonic High-Pressure Turbine Vanes with Non-Axisymmetric Endwalls for Rotating Detonation Engines	2
Totale	2.005

	Totale	Lug	Ago	Sett	Ott	Nov	Dic	Gen	Feb	Mar	Apr	Mag	Giu
2023/2024	25	0	0	0	0	0	0	0	0	9	3	5	8
2024/2025	574	48	52	82	32	43	9	30	5	37	75	76	85
2025/2026	1.323	110	66	122	108	53	52	147	87	231	131	49	167
2026/2027	83	56	27	0	0	0	0	0	0	0	0	0	0
Totale													2.005

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