Daniele Bianchi | Ricerc@Sapienza

Pubblicazioni

Titolo	Pubblicato in	Anno
Modeling and simulation of paraffin–based hybrid rocket internal ballistics	2018 joint propulsion conference, AIAA propulsion and energy forum	2018
Systematic strategies for thermochemical model reduction in rocket propulsion applications	2018 Joint Propulsion Conference	2018
Performance reconstruction of VEGA solid rocket motors: VERTA flights experience	2018 Joint Propulsion Conference	2018
Numerical investigation on the role of thermal radiation in hybrid rocket fuel pyrolysis	2018 Joint Propulsion Conference	2018
Ablative and catalytic behavior of carbon-based porous thermal protection materials in nitrogen plasmas	CARBON	2018
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
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
Modeling of high density polyethylene regression rate in the simulation of hybrid rocket flowﬁelds	7 TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS)	2017
Chemical reaction effects on heat loads of CH4/O2 and H2/O2 rockets	AIAA JOURNAL	2016
Hybrid rockets with axial injector: port diameter effect on fuel regression rate	JOURNAL OF PROPULSION AND POWER	2016
Modeling of paraffin-based fuels in the simulation of hybrid rocket flowfields	52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016	2016
Navier–Stokes simulation of graphite nozzle erosion at different pressure conditions	AIAA JOURNAL	2015
Radius of curvature effects on throat thermochemical erosion in solid rocket motors	JOURNAL OF SPACECRAFT AND ROCKETS	2015
Simulation of gaseous oxygen/hydroxyl-terminated polybutadiene hybrid rocket flowfields and comparison with experiments	JOURNAL OF PROPULSION AND POWER	2015
Convective and radiative contributions to wall heat transfer in liquid rocket Engine thrust chambers	51st AIAA/ASME/SAE/ASEE Joint Propulsion Conference	2015
Numerical analysis of port diameter effect on hybrid rocket fuel regression rate with axial injection	51st AIAA/SAE/ASEE Joint Propulsion Conference - Proceedings	2015
Numerical simulation of chemical erosion in VEGA launcher solid-propellant rocket motor nozzles	51st AIAA/SAE/ASEE Joint propulsion conference	2015