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antonella.ingenito@uniroma1.it
Antonella Ingenito
Professore Associato
Struttura:
SCUOLA DI INGEGNERIA AEROSPAZIALE
E-mail:
antonella.ingenito@uniroma1.it
Pagina istituzionale corsi di laurea
Curriculum Sapienza
Pubblicazioni
Titolo
Pubblicato in
Anno
Combustion performance of hybrid rocket fuels loaded with MgB2 and carbon black additives
PROPULSION AND POWER RESEARCH
2022
The investigation of inclined aft wall cavities in a circular scramjet combustor
INTERNATIONAL JOURNAL OF ENGINE RESEARCH
2022
Thermal decomposition kinetics and combustion performance of paraffin-based fuel in the presence of CeO2 catalyst
FIREPHYSCHEM
2022
Some Key Issues in Hypersonic Propulsion
ENERGIES
2021
The implication of injection locations in an axisymmetric cavity-based scramjet combustor
ENERGIES
2021
Review on the Regression Rate-Improvement Techniques and Mechanical Performance of Hybrid Rocket Fuels
FIREPHYSCHEM
2021
Igniter Design Guidelines
SpringerBriefs in Applied Sciences and Technology
2021
Design of Supersonic/Hypersonic Vehicles
SpringerBriefs in Applied Sciences and Technology
2021
Ramjet Engines Performance
SpringerBriefs in Applied Sciences and Technology
2021
Flameholder Design Guidelines
SpringerBriefs in Applied Sciences and Technology
2021
Combustor Design Guidelines
SpringerBriefs in Applied Sciences and Technology
2021
Material Selection for Ramjet Engines
SpringerBriefs in Applied Sciences and Technology
2021
Injector Design Guidelines
SpringerBriefs in Applied Sciences and Technology
2021
Fundamentals of Ramjet Engines
SpringerBriefs in Applied Sciences and Technology
2021
Ramjets Fuels
SpringerBriefs in Applied Sciences and Technology
2021
Step by Step RJ Design Methodology
SpringerBriefs in Applied Sciences and Technology
2021
A hybrid propulsion solution for a microsatellite to perform a capture maneuver in a Mars orbit
AIAA Propulsion and Energy 2020 Forum
2020
Numerical simulations of axisymmetric aft wall angle cavity in supersonic combustion ramjets
AIAA Propulsion and Energy 2020 Forum
2020
Experimental and numerical investigation of a paraffin-based hybrid rocket engine to brake a 24U microsatellite in a Mars orbit
Proceedings of the International Astronautical Congress, IAC
2020
Experimental study of pyrolysis-combustion coupling in a regeneratively cooled combustor: heat transfer and coke formation
FUEL
2019
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Progetti di Ricerca
NUMERICAL INVESTIGATION OF PLASMA ASSISTED SUPERSONIC COMBUSTION
Numerical and experimental investigation of biopolymers -based hybrid propulsion
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