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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
Publications
Title
Published on
Year
Comprehensive Analysis of the CVRC Test Case using Low-Order Modeling of Combustion Instability
AIAA SciTech Forum and Exposition, 2025
2025
Family of Skeletal Reaction Mechanisms for Methane–Oxygen Combustion in Rocket Propulsion
JOURNAL OF PROPULSION AND POWER
2024
Low-Order Modeling of Combustion Instability: A Comprehensive Analysis of the BKD Test Case
AIAA SciTech Forum 2024
2024
Modeling and Analysis of Film Cooling in Oxygen-Kerosene Rocket Thrust Chambers
AIAA SciTech Forum 2024
2024
Radiative Wall Heat Transfer Evaluation in Hybrid Rocket Thrust Chambers
AIAA SciTech Forum 2024
2024
Low-order modeling approach for the prediction of transverse combustion instabilities in multi-injector engines
CEAS SPACE JOURNAL
2024
Transient Analysis of Liquid Rocket Engine Chilldown and Startup by Conjugate Heat Transfer Approach
AIAA SciTech Forum and Exposition, 2024
2024
Computational Analysis of High-Altitude Test Facilities
Space Propulsion Conference 2024
2024
Module performance and heat transfer analysis of a clustered annular aerospike nozzle
Proceedings of the space propulsion conference 2024
2024
Modeling postcritical two-phase heat transfer in EcosimPro/ESPSS environment
Proceedings of the 9th Space Propulsion Conference
2024
Experimental Investigation of a H2O2 Hybrid Rocket with Different Swirl Injections and Fuels
APPLIED SCIENCES
2024
NUMERICAL ACTIVITIES ON THE PARAFFIN-BASED FUEL MTM IN THE FRAMEWORK OF THE PHAEDRA PROJECT
Proceedings of the 2024 Space Propulsion Conference
2024
Updating the pump and injector plate components of the ESPSS library in view of transient analysis of LOx/Methane engines
Proceedings of the 2024 Space Propulsion Conference
2024
Conjugate heat transfer numerical simulations of a methane-oxygen liquid rocket engine
Proceedings of the 2024 Space Propulsion Conference
2024
Numerical Modeling of Scale Effects in Paraffin-Hydrogen Peroxide Hybrid Rockets with Swirl Injection
Proceedings of the International Astronautical Conference
2024
Design and Evaluation of Aerospike Nozzles for an Upper-Stage Application
2024
Homogeneous Equilibrium Modeling for Subcritical Flows in Liquid Rocket Engine Cooling Systems
JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER
2024
Progresses in Applied Research on Liquid Rocket Propulsion by T(H)RUST Research Team at Sapienza University of Rome
Proceedings of the International Astronautical Congress, IAC
2024
Numerical Simulations of a Paraffin-Hydrogen Peroxide Hybrid Rocket with Swirl Injection
Proceedings of the AIAA Scitech 2023 Forum
2023
Numerical Analysis of Film Cooling and Mixture Ratio Bias in Oxygen-Methane Liquid Rocket Engines
AIAA Scitech 2023 Forum
2023
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ERC
PE8_1
KET
Sustainable technologies & development
Interessi di ricerca
Keywords
Liquid rocket engines
propulsion
rocket nozzle
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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