Marco Fabiani | Ricerc@Sapienza

Pubblicazioni

Titolo	Pubblicato in	Anno
Radiative Wall Heat Transfer Evaluation in Hybrid Rocket Thrust Chambers	AIAA SciTech Forum 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
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 and experimental analysis of fuel regression rate in a lab-scale hybrid rocket engine with swirl injection	AEROSPACE SCIENCE AND TECHNOLOGY	2023
Modeling of swirl injection effects in a H2O2-HDPE hybrid rocket	Proceedings of the Aerospace Europe Conference 2023 - 10th EUCASS - 9th CEAS	2023
Convective and Radiative Wall Heat Transfer Evaluation in Film-Cooled Liquid Rocket Thrust Chambers	Proceedings of the International Astronautical Congress, IAC	2023
T(H)RUST: applied research activities on liquid rocket propulsion at Sapienza University of Rome	Proceedings of the International Astronautical Congress, IAC	2023
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