VENTURELLI, GIOVANNI
 Distribuzione geografica
Continente #
NA - Nord America 587
EU - Europa 110
AS - Asia 45
Totale 742
Nazione #
US - Stati Uniti d'America 580
IT - Italia 46
CN - Cina 36
DE - Germania 31
SE - Svezia 16
FI - Finlandia 8
CA - Canada 7
IN - India 4
KR - Corea 3
UA - Ucraina 3
FR - Francia 2
BD - Bangladesh 1
BE - Belgio 1
CH - Svizzera 1
JP - Giappone 1
NL - Olanda 1
NO - Norvegia 1
Totale 742
Città #
Fairfield 91
Ann Arbor 74
Ashburn 56
Woodbridge 53
Cambridge 44
Seattle 44
Wilmington 43
Chandler 38
Houston 27
Medford 17
Princeton 17
San Diego 15
Beijing 14
Padova 13
Des Moines 12
Roxbury 10
Bologna 4
Nanjing 4
Hebei 3
Helsinki 3
Munich 3
Quinto Di Treviso 3
Seoul 3
Borås 2
Hefei 2
Jacksonville 2
Jinan 2
Luft 2
Nanchang 2
Norwalk 2
Nürnberg 2
Sant'elena 2
Shenyang 2
Absecon 1
Brussels 1
Cadelbosco 1
Changsha 1
Chengdu 1
Fuzhou 1
Guangzhou 1
Gudo Visconti 1
Jiaxing 1
Lendinara 1
Linkenheim-hochstetten 1
Milan 1
Molfetta 1
New York 1
Orange 1
Ravenna 1
Selvazzano Dentro 1
Shanghai 1
Tolentino 1
Toronto 1
Trondheim 1
Wuhan 1
Totale 633
Nome #
Kriging-assisted design optimization of S-shape supersonic compressor cascades 98
Development of a Flow Control Valve for a Throttleable Hybrid Rocket Motor and Throttling Fire Tests 84
Testing of a Long-Burning-Time Paraffin-Based Hybrid Rocket Motor 79
A sounding rocket as a test bench for cost effective measurements: Development of a sounding rocket demonstrator test bench for aerospace technologies and atmospheric measurements 75
Development and Testing of a Long Burning Time Lab-scale Paraffin-Based Hybrid Rocket Motor 73
A Kriging-assisted multiobjective evolutionary algorithm 58
Helicopter fuselage aerodynamic data fitting using multivariate smoothing thin plate splines 56
Feasibility Study for a Throttleable Hybrid Rocket Motor for Soft Landing 46
Numerical Simulation of an Isochoric Combustion Chamber for Hybrid Rocket Propulsion 37
Feasibility Study for Throttleable Hybrid Rocket Motor for Soft Landing 33
Development of a Cavitating Pintle for a Throttleable Hybrid Rocket Motor 32
C/C-SiC Nozzle for a Long Burn-Time Hybrid Rocket: Design and Optimization, Manufacturing and Testing 25
Numerical Simulations of an Isochoric Hybrid Rocket Combustion Chamber and Comparison with Tests 25
Comparison between pure and surrogateassisted evolutionary algorithms for multiobjective optimization 14
Development of numerical procedures for turbomachinery optimizaion 12
Mobility Impact Assessment of Innovative Aircraft inside the European Multimodal Transport Network 9
Design evaluation and performance assessment of rotorcraft technology by 2050 7
Totale 763
Categoria #
all - tutte 1060
article - articoli 356
book - libri 0
conference - conferenze 0
curatela - curatele 0
other - altro 0
patent - brevetti 0
selected - selezionate 0
volume - volumi 0
Totale 1416


Totale Lug Ago Sett Ott Nov Dic Gen Feb Mar Apr Mag Giu
2017/201833 00114 05 20 0290
2018/201966 11522 01 33 091713
2019/2020231 1451117 2214 2232 3230293
2020/2021145 1241410 146 510 1818268
2021/2022171 427165 98 812 951454
2022/202367 323500 00 00 0000
Totale 763