Francesco Nasuti | Ricerc@Sapienza

Publications

Title	Published on	Year
Quasi-1D modeling of heat release for the study of longitudinal combustion instability	AEROSPACE SCIENCE AND TECHNOLOGY	2018
A multi-dimensional approach for low order modeling of combustion instability in a rocket combustor	AIAA/SAE/ASEE joint propulsion conference 2018	2018
Driving mechanisms in low order modeling of longitudinal combustion instability	2018 AIAA/SAE/ASEE joint propulsion conference. Proceedings	2018
The accuracy of reconstruction techniques for determining hybrid rocket fuel regression rate	proceedings of AIAA 2018 Joint Propulsion Conference	2018
Modeling and simulation of paraffin–based hybrid rocket internal ballistics	2018 joint propulsion conference, AIAA propulsion and energy forum	2018
Simulation of a single-element GCH4/GOx rocket combustor using a non-adiabatic flamelet method		2018
Low-order modeling of coupling effects between propellant injection and pressure fluctuations in high frequency combustion instability	Proceedings of Space Propulsion 2018	2018
Assessment of detached eddy simulation of a separated flow in a planar nozzle	56th AIAA Aerospace Sciences Meeting 2018	2018
Systematic strategies for thermochemical model reduction in rocket propulsion applications	2018 Joint Propulsion Conference	2018
Numerical investigation on the role of thermal radiation in hybrid rocket fuel pyrolysis	2018 Joint Propulsion Conference	2018
Extraction of response function from numerical simulations and their use for longitudinal combustion intsbility modeling	Proceedings of AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting	2017
Detached-Eddy simulation of shock unsteadiness in an overexpanded planar nozzle	AIAA JOURNAL	2017
Numerical issues in modeling combustion instability by quasi-1D Euler equations	INTERNATIONAL JOURNAL OF SPRAY AND COMBUSTION DYNAMICS	2017
The shock fitting technique from Gino Moretti towards the future	30th International symposium on shock waves 1. ISSW30 - Volume 1	2017
CSP-based chemical kinetics mechanisms simplification strategy for non-premixed combustion: An application to hybrid rocket propulsion	COMBUSTION AND FLAME	2017
Simulations of paraffin-based hybrid rocket motors and comparison with experiments	53rd AIAA/SAE/ASEE Joint Propulsion Conference	2017
A methodology to study the possible occurrence of chugging in liquid rocket engines during transient start-up	ACTA ASTRONAUTICA	2017
Numerical and experimental investigation of nozzle thermochemical erosion in hybrid rockets	53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017. Proceedings	2017
Experimental and numerical evaluation of the radiative wall heat flux in the post-chamber of a paraffin-based hybrid rocket engine	7 TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS)	2017
Basic analysis of a LOX / methane expander bleed engine	7 TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS)	2017

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)