Francesco Nasuti | Ricerc@Sapienza

Publications

Title	Published on	Year
Heat transfer prediction in rough cooling channels for liquid rocket engines	Proceedings of AIDAA 2021	2021
Design and evaluation of aerospike nozzles for an upper stage application.	Proceedings of the Space Propulsion Conference 2020+1	2021
Dual-bell nozzle for space launchers with fluidic control of transition	AIAA Propulsion and Energy Forum, 2021	2021
Numerical analysis of paraffin-wax/oxygen hybrid rocket engines	JOURNAL OF PROPULSION AND POWER	2020
Numerical Approach for the Estimation of Throat Heat Flux in Liquid Rocket Engines	AEROTECNICA MISSILI & SPAZIO	2020
A sensitivity study on a cfd model for paraffin-based hybrid rockets	AIAA Propulsion and Energy 2020 Forum	2020
Fluidic control of transition in a dual-bell nozzle	AIAA Propulsion and Energy 2020 Forum	2020
Analysis of thermal stratification impact on the design of cooling channels for liquid rocket engines	INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER	2019
Characterization of unsteadiness in an overexpanded planar nozzle	AIAA JOURNAL	2019
Modeling of high density polyethylene regression rate in the simulation of hybrid rocket flowfields	AEROSPACE	2019
Experimental and numerical methods for radiative wall heat flux predictions in paraffin–based hybrid rocket engines	ACTA ASTRONAUTICA	2019
A low order modeling approach to transverse combustion instability	2019 AIAA Propulsion and Energy Forum and Exposition	2019
Low-order modeling of combustion instability applied to cryogenic propellants	Proceedings of the 8th European Conference for Aeronautics and Aerospace Sciences (EUCASS)	2019
Numerical investigation on radiative heat loads in liquid rocket thrust chambers	JOURNAL OF PROPULSION AND POWER	2019
Predictive cfd model for internal ballistics of hybrid rocket engines using supercritical paraffin-wax and oxygen	AIAA Propulsion and Energy Forum and Exposition, 2019	2019
Cfd analysis of paraffin-based hybrid rockets with coupled nozzle erosion characterization	AIAA Propulsion and Energy Forum and Exposition, 2019	2019
Numerical estimations of peak heat flux at throat of liquid rocket engines	32nd International Symposium on Space Technology and Science (ISTS), & 9th Nano-Satellite Symposium (NSAT) proceedings	2019
Role of combustion modeling in the prediction of heat transfer in LRE thrust chambers	8 TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) proceedings	2019
Estimation of Throat Heat Flux in Liquid Rocket Engines	A.I.D.A.A Congress proceedings	2019
Convective and radiative wall heat transfer in liquid rocket thrust chambers	JOURNAL OF PROPULSION AND POWER	2018

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)