statistiche ricercatore

Città	#
Turin	154
Singapore	137
Chandler	97
Ashburn	96
Milan	89
Southend	75
Princeton	45
Beijing	41
Rome	41
Zogno	41
Ann Arbor	34
Torino	33
Santa Clara	31
Dublin	30
Houston	28
Orbassano	27
Berlin	25
Dallas	25
Council Bluffs	24
Seoul	23
Boardman	22
Hefei	20
Brussels	19
Amsterdam	14
Frankfurt am Main	12
Jakarta	10
San Donato Milanese	10
Ho Chi Minh City	9
Wilmington	9
Aosta	8
Cinisello Balsamo	8
Los Angeles	8
Barletta	7
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
Warsaw	5
Addis Ababa	4
Argenteuil	4
Brooklyn	4
Cagliari	4
Carignano	4
Columbus	4
Hanoi	4
Helsinki	4
New York	4
Piscataway	4
Seattle	4
South Tangerang	4
São Paulo	4
Woodbridge	4
Wuhan	4
Arlington	3
Arzano	3
Campinas	3
Charlotte	3
Falls Church	3
Istanbul	3
Lappeenranta	3
Manchester	3
Mashhad	3
Massy	3
Menlo Park	3
Naples	3
Norwalk	3
Novara	3
Phoenix	3
Pinerolo	3
Redondo Beach	3
Shenzhen	3
Toronto	3
Valdagno	3
Ankara	2
Auckland	2
Balangero	2
Balıkesir	2
Bangkok	2
Barcelona	2
Bari	2
Batangas	2
Belo Horizonte	2
Buffalo	2
Castel San Lorenzo	2
Cesano Maderno	2
Cranfield	2
Cusano Milanino	2
Dearborn	2
Dong Ket	2
Totale	1.488

Nome	#
Advanced Concepts for Rocket Engine Applications	506
Dual-bell nozzle with fluidic control of transition for space launchers	253
Experimental investigation of the effects of different internal surface features on additive-manufactured resonant igniters performance	185
Preliminary study of a resonant igniter for Rocket Engines	181
Simple, affordable evaporative cooler to reduce food loss in developing countries	175
Numerical Tool Optimization for Advanced Rocket Nozzle Performance Prediction	145
CFD Simulation of Hybrid Rocket Motors for Interplanetary CubeSats	128
Numerical investigation for performance prediction of gas dynamic resonant igniters	124
Design, modeling and testing of a O2/CH4 igniter for a hybrid rocket motor	117
Thermal Analysis of a Hybrid Rocket Propulsion System for Interplanetary CubeSats	116
Design of Interplanetary Hybrid CubeSat and SmallSat Propulsion Systems	114
Characterization of PolyMethylMethAcrylate as a Fuel for Hybrid Rocket Motors	104
SmallSat Hybrid Propulsion System	94
Development Testing of Hybrid Rocket Motors Using Classical Fuels for Interplanetary CubeSats	89
Dual-bell nozzle for space launchers with fluidic control of transition	83
Totale	2.414

	Totale	Lug	Ago	Sett	Ott	Nov	Dic	Gen	Feb	Mar	Apr	Mag	Giu
2020/2021	130	0	0	0	0	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	390	117	44	79	84	66	0	0	0	0	0	0	0
Totale													2.414

PORTO @ Archivio Istituzionale della Ricerca