statistiche ricercatore

Nazione	#
US - Stati Uniti d'America	445
IT - Italia	338
SG - Singapore	228
CN - Cina	122
BR - Brasile	69
DE - Germania	56
BE - Belgio	52
KR - Corea	51
IE - Irlanda	33
GB - Regno Unito	25
VN - Vietnam	24
FR - Francia	23
RU - Federazione Russa	15
ID - Indonesia	13
SE - Svezia	10
HK - Hong Kong	9
AT - Austria	7
CA - Canada	7
IL - Israele	7
NL - Olanda	7
ES - Italia	6
JO - Giordania	5
JP - Giappone	5
MY - Malesia	5
UA - Ucraina	5
PT - Portogallo	4
AR - Argentina	3
FI - Finlandia	3
IN - India	3
TR - Turchia	3
BD - Bangladesh	2
CO - Colombia	2
CR - Costa Rica	2
EC - Ecuador	2
GH - Ghana	2
LV - Lettonia	2
MX - Messico	2
PL - Polonia	2
SK - Slovacchia (Repubblica Slovacca)	2
UZ - Uzbekistan	2
AE - Emirati Arabi Uniti	1
AL - Albania	1
AU - Australia	1
AZ - Azerbaigian	1
CH - Svizzera	1
CI - Costa d'Avorio	1
DO - Repubblica Dominicana	1
IQ - Iraq	1
LA - Repubblica Popolare Democratica del Laos	1
MA - Marocco	1
NO - Norvegia	1
NP - Nepal	1
OM - Oman	1
SA - Arabia Saudita	1
SN - Senegal	1
TN - Tunisia	1
TW - Taiwan	1
UY - Uruguay	1
VE - Venezuela	1
ZA - Sudafrica	1
Totale	1.623

Nome	#
H2020 STRATOFLY Project: from Europe to Australia in less than 3 hours	224
STRATOFLY MR3 – how to reduce the environmental impact of high-speed transportation	161
Strategies for preliminary re-design of a LH2 Mach 5 cruiser concept originally conceived for Mach 8 mission	148
Aerodynamic characterization of hypersonic transportation systems and its impact on mission analysis	137
Methodology and Tools for High-Speed Vehicles Conceptual Design to Support Environmental Regulations	133
Integration of an increasing-fidelity aerodynamic modelling approach in the conceptual design of hypersonic cruiser	130
Integrated Flight Control System Characterization Approach for Civil High-Speed Vehicles in Conceptual Design	115
Main Achievements of the H2020 STRATOFLY Project	114
Low-boom supersonic business jet: aerodynamic analysis and mission simulation towards a CO2 emission standard	113
Hypersonic aircraft and mission concept re-design to move from Mach 8 to Mach 5 operations	103
Aerodatabase Development and Integration and Mission Analysis of a Mach 2 Supersonic Civil Aircraft	100
From conceptual to preliminary design: Aerodynamic characterization of MR5 civil high-speed aircraft	83
Simplified models for the preliminary aerodynamic characterization of high-speed vehicles to support mission analysis	63
Towards a CO2 emission standard for supersonic transport: A Mach 2 concept case study	52
Totale	1.676

	Totale	Lug	Ago	Sett	Ott	Nov	Dic	Gen	Feb	Mar	Apr	Mag	Giu
2021/2022	274	0	0	0	0	10	3	9	98	21	26	76	31
2022/2023	174	13	20	9	22	11	35	6	6	20	4	17	11
2023/2024	263	30	20	15	35	43	23	10	14	13	15	8	37
2024/2025	552	17	80	39	50	55	29	45	40	74	26	38	59
2025/2026	413	61	49	88	96	64	55	0	0	0	0	0	0
Totale													1.676

PORTO @ Archivio Istituzionale della Ricerca