Francesco Nasuti | Ricerc@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

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)