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fulvio.stella@uniroma1.it
Fulvio Stella
Professore Ordinario
Struttura:
DIPARTIMENTO DI INGEGNERIA MECCANICA E AEROSPAZIALE
E-mail:
fulvio.stella@uniroma1.it
Pagina istituzionale corsi di laurea
Curriculum Sapienza
Pubblicazioni
Titolo
Pubblicato in
Anno
High-fidelity simulations of the aeroacoustic environment of the VEGA launch vehicle at lift-off
COMPUTERS & FLUIDS
2023
CFD Analysis of the Lateral Sloshing Phenomenon inside an Aerospace LH2 Cryogenic Tank
Aerospace Europe Conference 2023 – 10ᵀᴴ EUCASS – 9ᵀᴴ CEAS
2023
Numerical Analysis of the Free-Fall Behavior of a Space Launcher Fragment
JOURNAL OF SPACECRAFT AND ROCKETS
2022
Immersed boundary simulations of aeroacoustics phenomena in solid rocket motors
9ᵀᴴ EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
2022
Implicit Large-Eddy Simulation of Solid Rocket Motors using the Immersed Boundary Method
Solid Rockets: Modeling and Simulation Advancements
2021
Wind tunnel measurements of the surface pressure fluctuations on the new VEGA-C space launcher
AEROSPACE SCIENCE AND TECHNOLOGY
2020
Large-Eddy Simulation of Vortex Shedding and Pressure Oscillations in Solid Rocket Motors
AIAA JOURNAL
2020
Modeling and simulating distributed combustion in SRM
Proceedings of the International Astronautical Congress, IAC
2020
Experimental study of pyrolysis-combustion coupling in a regeneratively cooled combustor: heat transfer and coke formation
FUEL
2019
Enhanced delayed DES of shock wave/boundary layer interaction in a planar transonic nozzle
INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW
2019
Enhanced Delayed DES of shock wave/boundary layer interaction in a planar transonic nozzle
Proceedings of the International Symposium on Turbulence, Heat and Mass Transfer
2018
Experimental study of pyrolysis-combustion coupling in a regeneratively cooled combustor: System dynamics analysis
AEROSPACE SCIENCE AND TECHNOLOGY
2017
Experimental investigation of fuel-cooled combustor: Cooling efficiency and coke formation
21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017
2017
Assessment and development of a ROM for linearized aeroelastic analyses of aerospace vehicles
CEAS AERONAUTICAL JOURNAL
2017
A numerical approach for the heat fluxes analysis in the nearwall region
33rd UIT HEAT TRANSFER CONFERENCE
2015
Gruppi di ricerca
Aerodinamica e Fluidodinamica Sperimentale
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