Francesco Nasuti | Ricerc@Sapienza

Publications

Title	Published on	Year
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
Cooling system design for an upper-stage aerospike	Proceedings of the 34th ISTS Conference	2023
Cooling system analysis of a clustered module aerospike for upper-stage applications	Proceedings of Aerospace Europe Conference 2023 – 10ᵀᴴ EUCASS – 9ᵀᴴ CEAS	2023
Direct numerical simulation of turbulent flow in pipes with realistic large roughness at the wall	JOURNAL OF FLUID MECHANICS	2023
Numerical and experimental analysis of fuel regression rate in a lab-scale hybrid rocket engine with swirl injection	AEROSPACE SCIENCE AND TECHNOLOGY	2023
CFD simulations of flow in LREs rectangular cooling channels	Proceedings of the 34th International Symposium on Space Technology and Science	2023
Modeling of swirl injection effects in a H2O2-HDPE hybrid rocket	Proceedings of the Aerospace Europe Conference 2023 - 10th EUCASS - 9th CEAS	2023
Sensitivity Study on a Low Order Model for the Analysis of Transverse Combustion Instability	Aerospace Europe Conference 2023 – 10ᵀᴴ EUCASS – 9ᵀᴴ CEAS	2023
Numerical Simulations of Fuel Shape Change in Paraffin–Oxygen Hybrid Rocket Engines	JOURNAL OF PROPULSION AND POWER	2023
Simplified Numerical Modeling of Film Cooling and Mixture Ratio Bias in Liquid Rocket Thrust Chambers	Proceedings of the Aerospace Europe Conference 2023 - 10th EUCASS - 9th CEAS	2023
Numerical and Experimental Analysis of a Paraffin-based 1000 N Thrust Class Hybrid Rocket including Nozzle Erosion	AIAA Scitech 2023 Forum	2023
Study, development, implementation and testing of a water resistojet propulsion system for CubeSats	Proceedings of the International Astronautical Congress, IAC	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
Driving mechanisms in low-order modeling of longitudinal combustion instability	JOURNAL OF PROPULSION AND POWER	2023
Conjugate heat transfer applied to transitory analysis for rocket engine cooling systems design	Materials Research Proceedings	2023
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

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)