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daniele.bianchi@uniroma1.it
Daniele Bianchi
Professore Associato
Struttura:
DIPARTIMENTO DI INGEGNERIA MECCANICA E AEROSPAZIALE
E-mail:
daniele.bianchi@uniroma1.it
Pagina istituzionale corsi di laurea
Curriculum Sapienza
Pubblicazioni
Titolo
Pubblicato in
Anno
Student firing tests and launches with commercial and self-made solid rocket motors
2021
Design and evaluation of aerospike nozzles for an upper stage application.
Proceedings of the Space Propulsion Conference 2020+1
2021
Modeling multiphase effects on pressure oscillations in solid propulsion
AIAA Propulsion and Energy 2020 Forum Proceedings
2020
Static firing ballistic reconstruction modelling and performance extrapolation to flight in srms
AIAA Propulsion and Energy 2020 Forum
2020
Numerical analysis of paraffin-wax/oxygen hybrid rocket engines
JOURNAL OF PROPULSION AND POWER
2020
A sensitivity study on a cfd model for paraffin-based hybrid rockets
AIAA Propulsion and Energy 2020 Forum
2020
Numerical analysis of nozzle heating and erosion in hybrid rockets and comparison with experiments
AIAA Propulsion and Energy 2020 Forum
2020
Numerical and experimental analysis of capsules ablation and shape change including heating transient effects
AIAA Propulsion and Energy 2020 Forum
2020
ASCenSIon: An innovative network to train the space access leaders of tomorrow
2020
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
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
Convective and radiative wall heat transfer in liquid rocket thrust chambers
JOURNAL OF PROPULSION AND POWER
2018
Numerical simulation of chemical erosion in Vega solid-rocket-motor nozzles
JOURNAL OF PROPULSION AND POWER
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
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
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