Daniele Bianchi | Ricerc@Sapienza

Pubblicazioni

Titolo	Pubblicato in	Anno
Numerical analysis of carbon-based nozzle erosion including transient heating and shape change	Thermophysics. (2 vols) papers presented at the aiaa aviation forum 2022	2022
Numerical Simulations of Fuel Shape Change in Paraffin-Oxygen Hybrid Rocket Engines	AIAA Aviation Forum	2022
Solid Rocket Motor Internal Ballistics Simulation Using Eulerian Multiphase Models	Proceedings of 9th European Conference for Aeronautics and Space Sciences	2022
Numerical simulation of multiphase flows in solid rocket motors nozzles	AIAA AVIATION 2022 Forum	2022
Student Activities in Manufacturing and Launching Advanced Small-Scale Solid-Propellant Rockets		2022
Transient Material Response Analysis of Carbon-based Thermal Protection Systems for Rocket Nozzle Applications	2nd International Conference on Flight Vehicles, Aerothermodynamics and Re-entry Missions and Engineering (FAR)	2022
Q1D modeling of hydrodynamic instabilities in solid rocket motors	AIP Conference Proceedings	2022
Vega P80 SRM Pressure Oscillations Analysis by means of Q1D Model	AIAA AVIATION 2022 Forum	2022
Analysis of Pressure Oscillations within Vega Launchers First Stage SRMs	Proceedings of the International Astronautical Congress, IAC	2022
Q1d modeling of hydrodynamic instabilities in solid rocket motors	ADVANCES IN AIRCRAFT AND SPACECRAFT SCIENCE	2022
Thermoacoustics Q1D Modeling in Solid Rocket Motors	AIAA Propulsion and Energy 2021	2021
Analysis and Reconstruction of Zefiro 40 Solid Rocket Motor Static Firing Tests and Extrapolation to Flight	AIAA Propulsion and Energy 2021	2021
Numerical Simulation of Thermoacoustic Phenomena in Aft-Finocyl Solid Rocket Motors	AIAA Propulsion and Energy 2021	2021
Numerical Analysis and Wind Tunnel Validation of Low-Temperature Ablators undergoing Shape Change	INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER	2021
Numerical Analysis of Nozzle Transient Heating and Erosion in Hybrid Rockets burning HDPE	AIAA Propulsion and Energy Forum 2021	2021
Numerical Analysis of Nozzle Erosion in Hybrid Rockets and Comparison with Experiments	JOURNAL OF PROPULSION AND POWER	2021
Numerical simulations of the internal ballistics of paraffin–oxygen hybrid rockets at different scales	AEROSPACE	2021
Gas-Phase Reaction Effects on Nozzle Erosion in Paraffin/Oxygen Hybrid Rockets	AIAA Propulsion and Energy Forum, 2021	2021
Machine Learning Techniques for Flight Performance Prediction of Hybrid Rocket Engines	AIAA Propulsion and Energy Forum, 2021	2021
A Computational Tool for the Design of Hybrid Rockets	AEROTECNICA MISSILI & SPAZIO	2021