Archivio Istituzionale della RicercaMARSILIO, Roberto
MARSILIO, Roberto
Dipartimento di Ingegneria Meccanica e Aerospaziale
001952
A 2-D Viscous Inverse Problem Method for Aerodynamics Design
2004-01-01 Ferlauto, Michele; Marsilio, Roberto
A CFD Method for Optimal Air-Intake Design
2007-01-01 Ferlauto, Michele; Marsilio, Roberto
A Computational Method for Combustion in High Speed Flows
2012-01-01 Ferrat, Christian; Marsilio, Roberto
A computational method for combustion in supersonic flows
2011-01-01 Ferrat, Christian; Marsilio, Roberto
A Computational Method for Gas Turbine Engines
2005-01-01 Marsilio, Roberto
A Methodology to Solve External Flowfields in Aero-Spike Engines
2000-01-01 Marsilio, Roberto; Pandolfi, M.
A New Set of Boundary Conditions for Aerodynamic Design
2003-01-01 Ferlauto, Michele; Iollo, Angelo; Marsilio, Roberto; Zannetti, Luca
A Numerical Method for Solving the Three-DimensionalParabolized Navier-Stokes Equations
1995-01-01 D'Ambrosio, Domenic; Marsilio, Roberto
A numerical method for solving the threedimensional Parabolized Navier-Stokes equations
1997-01-01 D'Ambrosio, Domenic; Marsilio, Roberto
A Shock-Fitting Spectral Method for the Study of Shock-Vortex Interactions
1997-01-01 Arina, Renzo; Marsilio, Roberto
A Study of the Stability of Vortical Structures in Supersonic Inlets
1993-01-01 Marsilio, Roberto
ACTIVE FLOW CONTROL OF AN OVER-EXPANDED NOZZLE BY SHOCK VECTOR CONTROL
2019-01-01 Rizzo, Simone; Ferlauto, Michele; Marsilio, Roberto
Aerodynamic Design by Inverse Method
2003-01-01 Ferlauto, Michele; Marsilio, Roberto
AI Assisted Detection of Shock Motions Inside a Transonic Duct
2022-01-01 Resta, Emanuele; Ferlauto, Michele; Marsilio, Roberto
AI Based Shock-Wave Detection by Using a Pressure Sensor Array
2021-01-01 Resta, E; Ferlauto, M; Marsilio, R
An Eulerian-Lagrangian Method for Vortical Flow Simulations
2002-01-01 Ferlauto, Michele; Marsilio, Roberto
An Upwind 3D Space-Marching Procedure
1990-01-01 Marsilio, Roberto; Pandolfi, M.
Asymmetric Vortical Solutions in Supersonic Corners:Steady 3D Space-marching Versus Time-Dependent Conical Results
1993-01-01 Degrez, G; Spazzini, Pg; Marsilio, Roberto; Pandolfi, M.
CFD-based Fluidic Thrust Vectoring model for fighter aircraft
2019-01-01 Capello, Elisa; Ferrero, Andrea; Marsilio, Roberto; Ferlauto, Michele
Cold Gas Measurement System for Linear Aerospike Nozzles
2022-01-01 Bonnet, Valentin; Ortone, Francesca; Di Cicca, Gaetano Maria; Marsilio, Roberto; Ferlauto, Michele
| Citazione | Data di pubblicazione | Autori | File |
|---|---|---|---|
| A 2-D Viscous Inverse Problem Method for Aerodynamics Design / Ferlauto, Michele; Marsilio, Roberto. - (2004). ((Intervento presentato al convegno 34th AIAA Fluid Dynamics Conference - Portland OR. USA nel 28 Jun. - 1 July 2004. | 1-gen-2004 | FERLAUTO, MicheleMARSILIO, Roberto | AIAA-2004-2326.pdf |
| A CFD Method for Optimal Air-Intake Design / Ferlauto, Michele; Marsilio, Roberto. - (2007). ((Intervento presentato al convegno 8th International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows tenutosi a Lyon nel JULY 2007. | 1-gen-2007 | FERLAUTO, MicheleMARSILIO, Roberto | 66_07-02-14_isaif-0028.pdf |
| A Computational Method for Combustion in High Speed Flows / Ferrat, Christian; Marsilio, Roberto. - In: COMPUTERS & FLUIDS. - ISSN 0045-7930. - STAMPA. - 70:(2012), pp. 44-52. [10.1016/j.compfluid.2012.09.005] | 1-gen-2012 | FERRAT, CHRISTIANMARSILIO, Roberto | 1-s2.0-S0045793012003490-main.pdf; 2502525.pdf |
| A computational method for combustion in supersonic flows / Ferrat, Christian; Marsilio, Roberto. - (2011). ((Intervento presentato al convegno 47th AIAA/ASME Joint Propulsion Conference tenutosi a San Diego (USA) nel 31/7 - 3/8 - 2011. | 1-gen-2011 | FERRAT, CHRISTIANMARSILIO, Roberto | jpp2011c.pdf |
| A Computational Method for Gas Turbine Engines / Marsilio, Roberto. - (2005). ((Intervento presentato al convegno 43rd AIAA Aerospace Sciences Meeting and Exhibit tenutosi a Reno, Nevada (USA) nel 10-13 January 2005. | 1-gen-2005 | MARSILIO, Roberto | aiaa-2005-1009.pdf |
| A Methodology to Solve External Flowfields in Aero-Spike Engines / Marsilio, Roberto; Pandolfi, M.. - (2000). ((Intervento presentato al convegno ECCOMAS 2000 nel Settembre 11-14. | 1-gen-2000 | MARSILIO, Roberto + | - |
| A New Set of Boundary Conditions for Aerodynamic Design / Ferlauto, Michele; Iollo, Angelo; Marsilio, Roberto; Zannetti, Luca. - (2003), pp. 279-284. [10.1007/978-3-642-59334-5_40] | 1-gen-2003 | FERLAUTO, MicheleIOLLO, ANGELOMARSILIO, RobertoZANNETTI, LUCA | - |
| A Numerical Method for Solving the Three-DimensionalParabolized Navier-Stokes Equations / D'Ambrosio, Domenic; Marsilio, Roberto. - (1995). | 1-gen-1995 | D'AMBROSIO, DomenicMARSILIO, Roberto | - |
| A numerical method for solving the threedimensional Parabolized Navier-Stokes equations / D'Ambrosio, Domenic; Marsilio, Roberto. - In: COMPUTERS & FLUIDS. - ISSN 0045-7930. - 26:(1997), pp. 587-611. | 1-gen-1997 | D'AMBROSIO, DomenicMARSILIO, Roberto | dambrosiomarsilio_c&f_26(6)1997.pdf |
| A Shock-Fitting Spectral Method for the Study of Shock-Vortex Interactions / Arina, Renzo; Marsilio, Roberto. - (1997). ((Intervento presentato al convegno 28th AIAA Fluid Dynamics Conference nel June 1997. | 1-gen-1997 | ARINA, RENZOMARSILIO, Roberto | - |
| A Study of the Stability of Vortical Structures in Supersonic Inlets / Marsilio, Roberto. - 2:(1993), pp. 1051-1061. ((Intervento presentato al convegno Proceedings of XI ISABE tenutosi a Tokyo, Japan. | 1-gen-1993 | MARSILIO, Roberto | - |
| ACTIVE FLOW CONTROL OF AN OVER-EXPANDED NOZZLE BY SHOCK VECTOR CONTROL / Rizzo, Simone; FERLAUTO, MICHELE; MARSILIO, Roberto. - ELETTRONICO. - (2019), pp. 461-470. ((Intervento presentato al convegno 6th. European Conference on Computational Mechanics (Solids, Structures and Coupled Problems) ECCM 6 / 7th. European Conference on Computational Fluid Dynamics ECFD 7 tenutosi a Glasgow , UK nel Jugno 2018. | 1-gen-2019 | Michele FerlautoRoberto Marsilio + | ecfd-2018.pdf |
| Aerodynamic Design by Inverse Method / Ferlauto, Michele; Marsilio, Roberto. - (2003). ((Intervento presentato al convegno Congresso AIMETA XVI nel Settembre 2003. | 1-gen-2003 | FERLAUTO, MicheleMARSILIO, Roberto | AIMETA-2003.pdf |
| AI Assisted Detection of Shock Motions Inside a Transonic Duct / Resta, Emanuele; Ferlauto, Michele; Marsilio, Roberto. - ELETTRONICO. - 2424:(2022), p. 030005. ((Intervento presentato al convegno International Conference on Computational Intelligence and Computing Applications-21 (ICCICA-21) tenutosi a Virtual nel 18-19 June 2021 [10.1063/5.0076817]. | 1-gen-2022 | Emanuele RestaMichele FerlautoRoberto Marsilio | acceptedVersion.pdf |
| AI Based Shock-Wave Detection by Using a Pressure Sensor Array / Resta, E; Ferlauto, M; Marsilio, R. - ELETTRONICO. - (2021). ((Intervento presentato al convegno ECCOMAS CSAI - Computational Sciences and AI in Industry tenutosi a Virtual nel 7-9 June 2021. | 1-gen-2021 | E RestaM FerlautoR Marsilio | a26-1.pdf |
| An Eulerian-Lagrangian Method for Vortical Flow Simulations / Ferlauto, Michele; Marsilio, Roberto. - (2002). ((Intervento presentato al convegno GIMC2002, Third Joint Conference of GIMC and Ibero-Latin American Ass. nel Giugno. | 1-gen-2002 | FERLAUTO, MicheleMARSILIO, Roberto | - |
| An Upwind 3D Space-Marching Procedure / Marsilio, Roberto; Pandolfi, M.. - 2:(1990), pp. 715-726. ((Intervento presentato al convegno Third International Conference on Hyperbolic Problems nel June 11-15. | 1-gen-1990 | MARSILIO, Roberto + | - |
| Asymmetric Vortical Solutions in Supersonic Corners:Steady 3D Space-marching Versus Time-Dependent Conical Results / Degrez, G; Spazzini, Pg; Marsilio, Roberto; Pandolfi, M.. - AIAA Paper 93-2957:(1993). | 1-gen-1993 | MARSILIO, Roberto + | - |
| CFD-based Fluidic Thrust Vectoring model for fighter aircraft / Capello, Elisa; Ferrero, Andrea; Marsilio, Roberto; Ferlauto, Michele. - ELETTRONICO. - (2019). ((Intervento presentato al convegno AIAA Propulsion and Energy 2019 Forum tenutosi a Indianapolis, IN nel 19-22 August 2019 [10.2514/6.2019-4311]. | 1-gen-2019 | Capello, ElisaFerrero, AndreaMarsilio, RobertoFerlauto, Michele | AIAA-2019-4311.pdf |
| Cold Gas Measurement System for Linear Aerospike Nozzles / Bonnet, Valentin; Ortone, Francesca; Di Cicca, Gaetano Maria; Marsilio, Roberto; Ferlauto, Michele. - ELETTRONICO. - (2022), pp. 92-96. ((Intervento presentato al convegno 2022 IEEE INTERNATIONAL WORKSHOP ON METROLOGY FOR AEROSPACE tenutosi a Pisa, ITALY nel June 27-29, 2022. | 1-gen-2022 | Di Cicca, Gaetano MariaMarsilio, RobertoFerlauto Michele + | MetroAerospace 2022 paper #1570793785.pdf |