Sfoglia per Autore
LES of Supersonic Combustion with a variable Schmidt number
2008 Ingenito, Antonella; Bruno, C.
LES of a Supersonic Combustor with Variable Turbulent Prandtl and Schmidt Numbers
2008 Ingenito, Antonella; Bruno, Claudio
Turbulent Combustion Modelling In Supersonic Flows for Applications To Future RBCC Vehicles
2008 Ingenito, Antonella; Bruno, Claudio
Mixing and combustion in supersonic reactive flows
2008 Ingenito, Antonella; Bruno, Claudio
Effect of the Turbulent Schmidt Number on Supersonic Regime
2008 Ingenito, Antonella; Bruno, C.
Sizing of Scramjet Vehicles
2009 Ingenito, Antonella; Gulli, S; Bruno, C.
TBCC hypersonic performance: Effect of inlet entropy
2009 Ingenito, Antonella; S., Gulli; C., Bruno
Sizing of TBCC Hypersonic Airbreathing Vehicles
2009 Ingenito, Antonella; Gulli, S; Bruno, C.
Preliminary Sizing of Hypersonic Airbreathing Airliner
2009 Ingenito, Antonella; S., Gulli; Bruno, Claudio
Preliminary Sizing of an Hypersonic Airbreathing Airliner
2009 Ingenito, Antonella; Gulli, S; Bruno, C.
Reaction regimes in supersonic combustion
2009 Ingenito, Antonella; C., Bruno
Supersonic Mixing And Combustion: Advance In LES Modeling
2009 Ingenito, Antonella; Bruno, Claudio
ADVANCES IN LES OF THE HYSHOT II SCRAMJET COMBUSTOR
2010 Cecere, D; Ingenito, Antonella; Bruno, C; Giacomazzi, E; Donato, F.
Physics and Regimes of Supersonic Combustion
2010 Ingenito, Antonella; Claudio, Bruno
Sizing of a ramjet/scramjet powered vehicle for mars exploration
2010 Ingenito, Antonella; C., Bruno; P., Czysz
Sizing of a Ramjet Powered Vehicle for Mars Exploration
2010 Ingenito, Antonella; Bruno, C; Czysz, P.
7 seminari presso la Scuola di Ingegneria Aerospaziale: 1. Prof. Vladimir Bazarov, Moscow Aviation Institute (State Technical University), “Comparative Analysis and Selection of injector conception for spacecraft soft lunar landing descent variable Thrust Engine”; 2. Giuseppe Corrao, Eng. Technological Innovation Telespazio SpA, Finmeccanica/Thales company, “Utilizzo del tool STK per l'analisi delle missioni spaziali”; 3. Gammarota Antonio, Manager R&D and Product Policy Directorate, Thales Alenia Space, “Ricerca e Innovazione nell'industria Spaziale: "Infrastrutture e Trasporto Spaziale"; 4. Yuriy Shmaliy, Prof. Department of Electronics, FIMEE, Guanajuato University, “Optimal and Unbiased FIR Filtering of Discrete-Time State-Space Models”; 5. Antonio Accettura, Program Manager, Ariane 5 Program Department, Avio – Colleferro, “In-Situ Propulsion - technologies and perspectives” ; 6. Antonio Accettura, Program Manager, “Satellites Market Survey and Trend”; 7. Antonio Accettura, Program Manager, “Innovative Technologies to enable new missions”.
2010 Ingenito, Antonella
Shock/Boundary Layer/Heat Release Interaction inthe HyShot II Scramjet Combustor
2010 Cecere, D; Ingenito, Antonella; Romagnosi, L; Bruno, C; Giacomazzi, E.
LES of the HyShot scramjet combustor
2010 Ingenito, Antonella; C., Bruno; D., Cecere
Prediction of SCRJ flame anchoring
2010 Ingenito, Antonella; Cecere, D; Bruno, Claudio
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