statistiche ricercatore

Città	#
Turin	153
Singapore	98
Chandler	97
Milan	89
Ashburn	87
Southend	75
Princeton	45
Rome	41
Zogno	41
Ann Arbor	34
Beijing	34
Torino	33
Dublin	30
Santa Clara	30
Houston	28
Orbassano	27
Berlin	25
Council Bluffs	24
Boardman	22
Seoul	22
Brussels	19
Dallas	19
Hefei	18
Amsterdam	14
Frankfurt am Main	12
Jakarta	10
San Donato Milanese	10
Wilmington	9
Aosta	8
Cinisello Balsamo	8
Barletta	7
Los Angeles	7
Ho Chi Minh City	6
Izmir	6
Palermo	6
Sotto il Monte Giovanni XXIII	6
Sumberrejo	6
Algiers	5
Bottanuco	5
Crema	5
Hong Kong	5
L’Aquila	5
Mola Di Bari	5
Munich	5
Redwood City	5
San Jose	5
Varese	5
Vienna	5
Addis Ababa	4
Argenteuil	4
Cagliari	4
Carignano	4
Columbus	4
Helsinki	4
Piscataway	4
South Tangerang	4
Woodbridge	4
Wuhan	4
Arlington	3
Arzano	3
Campinas	3
Charlotte	3
Falls Church	3
Istanbul	3
Mashhad	3
Massy	3
Menlo Park	3
Naples	3
New York	3
Norwalk	3
Novara	3
Phoenix	3
Pinerolo	3
Seattle	3
Shenzhen	3
São Paulo	3
Toronto	3
Valdagno	3
Warsaw	3
Ankara	2
Auckland	2
Balangero	2
Balıkesir	2
Bangkok	2
Barcelona	2
Bari	2
Batangas	2
Belo Horizonte	2
Brooklyn	2
Buffalo	2
Castel San Lorenzo	2
Cesano Maderno	2
Cranfield	2
Cusano Milanino	2
Dearborn	2
Dong Ket	2
Dresden	2
Fossano	2
Galati	2
Genoa	2
Totale	1.406

Nome	#
Advanced Concepts for Rocket Engine Applications	493
Dual-bell nozzle with fluidic control of transition for space launchers	232
Preliminary study of a resonant igniter for Rocket Engines	175
Experimental investigation of the effects of different internal surface features on additive-manufactured resonant igniters performance	164
Simple, affordable evaporative cooler to reduce food loss in developing countries	162
Numerical Tool Optimization for Advanced Rocket Nozzle Performance Prediction	137
CFD Simulation of Hybrid Rocket Motors for Interplanetary CubeSats	122
Numerical investigation for performance prediction of gas dynamic resonant igniters	113
Design of Interplanetary Hybrid CubeSat and SmallSat Propulsion Systems	107
Design, modeling and testing of a O2/CH4 igniter for a hybrid rocket motor	107
Thermal Analysis of a Hybrid Rocket Propulsion System for Interplanetary CubeSats	104
Characterization of PolyMethylMethAcrylate as a Fuel for Hybrid Rocket Motors	94
SmallSat Hybrid Propulsion System	85
Development Testing of Hybrid Rocket Motors Using Classical Fuels for Interplanetary CubeSats	83
Dual-bell nozzle for space launchers with fluidic control of transition	77
Totale	2.255

	Totale	Lug	Ago	Sett	Ott	Nov	Dic	Gen	Feb	Mar	Apr	Mag	Giu
2020/2021	170	0	0	6	34	2	8	8	6	67	26	9	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	231	117	44	70	0	0	0	0	0	0	0	0	0
Totale													2.255

PORTO @ Archivio Istituzionale della Ricerca