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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
Large-Eddy Simulations of a Hypersonic Re-entry Capsule Coupled With the Supersonic Disk-Gap-Band Parachute
AEROSPACE
2024
Full helicon thruster modeling
IEPC 2024
2024
A Rational Design Method for the Nagoya Type-III Antenna
AEROSPACE
2024
Theoretical nderstanding of the effects of high-density energetic particles on the ramjet performance
Journal of Propulsion and Energy
2024
Numerical Study of Hydrogen Injection to initiate Oblique Detonation Wave
3rd International Conference on High-Speed Vehicle Science and Technology
2024
Investigation of mixing and Combustion in supersonic flows
3rd International Conference on High-Speed Vehicle Science and Technology
2024
TSTO Launcher for small Satellites
3rd International Conference on High-Speed Vehicle Science and Technology
2024
Knowledge Discovery on Cavity-Based Scramjet Combustor Design via Stochastic-Surrogate-Assisted Multi-Objective Optimization
3rd International Conference on High-Speed Vehicle Science and Technology
2024
Numerical Investigation Of Non-Premixed Oblique Detonation Operations In Scramjet Combustor
8th edition of the International Conference on Jets, Wakes and Separated Flows
2024
A hybrid propulsion-based mission architecture for the removal of debris from low-earth orbit
MPDI - Engineering Proceedings Journal
2024
Array of carbon black-based microthrusters for CubeSat applications
FIREPHYSCHEM
2023
A new indirect measurement method of the electron temperature for the Proto-sphera's pinch plasma
JOURNAL OF INSTRUMENTATION
2023
Oxidation reaction kinetics of HTPB-boron carbide/polytetrafluoroethylene formulations as a solid fuel
FUEL
2023
Mars One-Year Mission Craft
AEROSPACE
2023
Influence of cavity floor injection strategy on mixing improvement study of a splitter plate-assisted supersonic combustor
ENGINEERING ANALYSIS WITH BOUNDARY ELEMENTS
2023
Understanding the total pressure losses nature in a Scramjet Combustor
International Space Planes and Hypersonic Systems and Technologies Conference
2023
Numerical investigation of the impact of injectors location on fuel mixing in the HIFiRE 2 Scramjet combustor
Aerospace Europe Conference 2023 – 10ᵀᴴ EUCASS – 9ᵀᴴ CEAS
2023
3D Printed Miniaturized Micro Thrusters for Cubesat Applications
74th International Astronautical Congress 2023
2023
SHAR for a TSTO launcher
American Institute of Aeronautics and Astronautics
2023
Beeswax–EVA/Activated-Charcoal-Based Fuels for Hybrid Rockets: Thermal and Ballistic Evaluation
ENERGIES
2022
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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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