statistiche ricercatore

Città	#
Singapore	168
Turin	160
Ashburn	142
Milan	99
Chandler	97
San Jose	97
Southend	75
Rome	51
Ho Chi Minh City	50
Hanoi	46
Princeton	45
Beijing	41
Zogno	41
Seoul	39
Ann Arbor	34
Santa Clara	33
Torino	33
Dublin	31
Houston	28
Orbassano	27
Berlin	25
Dallas	25
Council Bluffs	24
Boardman	22
Hefei	21
Hong Kong	21
Brussels	19
Frankfurt am Main	15
Lauterbourg	15
Amsterdam	14
Los Angeles	14
Da Nang	10
Jakarta	10
San Donato Milanese	10
Wilmington	9
Aosta	8
Cinisello Balsamo	8
Haiphong	8
Barletta	7
Lecce	7
Warsaw	7
Addis Ababa	6
Bangkok	6
Izmir	6
New York	6
Palermo	6
Sotto il Monte Giovanni XXIII	6
Sumberrejo	6
Algiers	5
Bottanuco	5
Crema	5
L’Aquila	5
Mola Di Bari	5
Moscow	5
Munich	5
Piscataway	5
Redwood City	5
The Dalles	5
Varese	5
Vienna	5
Argenteuil	4
Barcelona	4
Bari	4
Brooklyn	4
Buffalo	4
Cagliari	4
Carignano	4
Charlotte	4
Columbus	4
Helsinki	4
Manchester	4
Mumbai	4
Naples	4
Nichelino	4
Paris	4
Seattle	4
Shanghai	4
South Tangerang	4
São Paulo	4
Toronto	4
Vĩnh Tường	4
Woodbridge	4
Wuhan	4
Arlington	3
Arzano	3
Baghdad	3
Basingstoke	3
Campinas	3
Falls Church	3
Hangzhou	3
Istanbul	3
Lappeenranta	3
Mashhad	3
Massy	3
Menlo Park	3
Norwalk	3
Novara	3
Phoenix	3
Pinerolo	3
Pune	3
Totale	1.881

Nome	#
Advanced Concepts for Rocket Engine Applications	604
Dual-bell nozzle with fluidic control of transition for space launchers	328
Experimental investigation of the effects of different internal surface features on additive-manufactured resonant igniters performance	269
Simple, affordable evaporative cooler to reduce food loss in developing countries	245
Preliminary study of a resonant igniter for Rocket Engines	219
Numerical Tool Optimization for Advanced Rocket Nozzle Performance Prediction	184
Design of Interplanetary Hybrid CubeSat and SmallSat Propulsion Systems	167
CFD Simulation of Hybrid Rocket Motors for Interplanetary CubeSats	164
Numerical investigation for performance prediction of gas dynamic resonant igniters	163
Design, modeling and testing of a O2/CH4 igniter for a hybrid rocket motor	160
Thermal Analysis of a Hybrid Rocket Propulsion System for Interplanetary CubeSats	151
Dual-bell nozzle for space launchers with fluidic control of transition	148
Characterization of PolyMethylMethAcrylate as a Fuel for Hybrid Rocket Motors	139
SmallSat Hybrid Propulsion System	130
Development Testing of Hybrid Rocket Motors Using Classical Fuels for Interplanetary CubeSats	122
Totale	3.193

	Totale	Lug	Ago	Sett	Ott	Nov	Dic	Gen	Feb	Mar	Apr	Mag	Giu
2020/2021	4	0	0	0	0	0	0	0	0	0	0	0	4
2021/2022	274	10	6	3	11	3	6	17	15	47	9	84	63
2022/2023	461	31	52	13	33	30	64	42	56	52	18	52	18
2023/2024	306	26	26	18	38	33	19	7	35	25	26	38	15
2024/2025	516	35	85	54	43	27	37	24	45	42	27	44	53
2025/2026	1.169	117	44	79	84	68	82	132	108	254	129	28	44
Totale													3.193

PORTO @ Archivio Istituzionale della Ricerca