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Francesco.Nasuti@uniroma1.it
Francesco Nasuti
Professore Ordinario
Struttura:
DIPARTIMENTO DI INGEGNERIA MECCANICA E AEROSPAZIALE
E-mail:
Francesco.Nasuti@uniroma1.it
Pagina istituzionale corsi di laurea
Curriculum Sapienza
Pubblicazioni
Titolo
Pubblicato in
Anno
Modeling liquid rocket engine coolant flow and heat transfer in high roughness channels
AEROSPACE SCIENCE AND TECHNOLOGY
2022
Graphite Nozzle Erosion Trends in Paraffin/Oxygen Hybrid Rockets
JOURNAL OF PROPULSION AND POWER
2022
Modeling of Wall Heat Flux in Oxygen-Methane Liquid Rocket Thrust Chambers
AIAA aviation 2022 Forum
2022
HEM modeling for subcritical flows in liquid rocket engine cooling systems
Proceedings of the AIAA Aviation Conference 2022
2022
Numerical estimation of nozzle throat heat flux in oxygen-methane rocket engines
JOURNAL OF PROPULSION AND POWER
2022
A design strategy for water-based noise suppression systems in liquid rocket engines firing tests
CEAS SPACE JOURNAL
2022
Review and Implementation of Engineering Models of Rocket Film Cooling and Nozzle Erosion
Proceedings of EUCASS-3AF 2022
2022
A Family of Skeletal Mechanisms for Methane Oxidation at High Pressure
44th Meeting of the Italian Section of the Combustion Institute
2022
Analysis of coolant flow and heat transfer in highly rough channels for LRE
Proceedings of the 9th EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
2022
Numerical simulations of fuel shape change and swirling flows in paraffin/oxygen hybrid rocket engines
AEROTECNICA MISSILI E SPAZIO
2022
Numerical and experimental investigation of a lab-scale paraffin motor with swirled injection of gaseous oxygen
Proceedings of the 9th EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
2022
Numerical Simulations of Fuel Shape Change in Paraffin-Oxygen Hybrid Rocket Engines
AIAA Aviation Forum
2022
Low-order modeling of combustion instability using a hybrid real/ideal gas mixture model
9th european conference for aeronautics and space sciences, 2022
2022
Pseudo-boiling and heat transfer deterioration while heating supercritical liquid rocket engine propellants
THE JOURNAL OF SUPERCRITICAL FLUIDS
2021
Development of a film-cooled thrust chamber component in the ESPSS library
7th Space Propulsion conference proceedings
2021
A hybrid real/ideal gas mixture computational framework to capture wave propagation in liquid rocket combustion chamber conditions
AEROSPACE
2021
A Hybrid Real/Ideal Gas Mixture Model in the Framework of Low Order Modeling of Combustion Instability
Proceedings of AIAA Propulsion and Energy Forum 2021
2021
Film cooling modeling in liquid rocket thrust chambers
AIAA propulsion and energy forum 2021-3574
2021
Conjugate heat transfer analysis of rectangular cooling channels using modeled and direct numerical simulation of turbulence
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER
2021
Numerical simulations of the internal ballistics of paraffin–oxygen hybrid rockets at different scales
AEROSPACE
2021
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ERC
PE8_1
Progetti di Ricerca
Combined RANS/DNS analysis of conjugate heat transfer in rocket cooling channels
Gruppi di ricerca - Responsabile
T(H)RUST (THermal Rocket propUlsion: a Sapienza university research Team)
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