Francesco Nasuti

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

ERC

  • PE8_1

KET

  • Sustainable technologies & development

Interessi di ricerca

Keywords

Liquid rocket engines
propulsion
rocket nozzle

Gruppi di ricerca - Responsabile

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