| A review on hydrogen industrial aerospace applications D Cecere, E Giacomazzi, A Ingenito International journal of hydrogen energy 39 (20), 10731-10747, 2014 | 310 | 2014 |
| Using aluminum for space propulsion A Ingenito, C Bruno Journal of Propulsion and Power 20 (6), 1056-1063, 2004 | 185 | 2004 |
| Hydrogen/air supersonic combustion for future hypersonic vehicles D Cecere, A Ingenito, E Giacomazzi, L Romagnosi, C Bruno International Journal of Hydrogen Energy 36 (18), 11969-11984, 2011 | 165 | 2011 |
| Physics and regimes of supersonic combustion A Ingenito, C Bruno AIAA journal 48 (3), 515-525, 2010 | 145 | 2010 |
| Experimental study of pyrolysis–combustion coupling in a regeneratively cooled combustor: system dynamics analysis L Taddeo, N Gascoin, K Chetehouna, A Ingenito, F Stella, M Bouchez, ... Aerospace Science and Technology 67, 473-483, 2017 | 35 | 2017 |
| Experimental study of pyrolysis-combustion coupling in a regeneratively cooled combustor: Heat transfer and coke formation L Taddeo, N Gascoin, K Chetehouna, A Ingenito, F Stella, M Bouchez, ... Fuel 239, 1091-1101, 2019 | 27 | 2019 |
| LES modeling of scramjet combustion A Ingenito, MG De Flora, C Bruno, E Giacomazzi, J Steelant 44th AIAA Aerospace Sciences Meeting and Exhibit, 1383, 2006 | 27 | 2006 |
| Large Eddy simulation of turbulent hydrogen-fuelled supersonic combustion in an air cross-flow A Ingenito, D Cecere, E Giacomazzi Shock Waves 23, 481-494, 2013 | 26 | 2013 |
| Theoretical investigation of air vitiation effects on hydrogen fuelled scramjet performance A Ingenito International Journal of Hydrogen Energy 40 (6), 2862-2870, 2015 | 25 | 2015 |
| LAPCAT II: conceptual design of a Mach 8 TBCC civil aircraft, enforced by full Navier-Stokes 3D nose-to-tail computation S Defoort, M Ferrier, L Serre, JL Pastre, C Paridaens, D Scherrer, ... 17th AIAA international space planes and hypersonic systems and technologies …, 2011 | 24 | 2011 |
| Preliminary Sizing of an Hypersonic Airbreathing Airliner A Ingenito, S Gulli, C Bruno Transactions of the Japan Society for Aeronautical and Space Sciences …, 2010 | 23 | 2010 |
| LES of the HyShot scramjet combustor A Ingenito, C Bruno, D Cecere 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and …, 2010 | 23 | 2010 |
| Review on the regression rate-improvement techniques and mechanical performance of hybrid rocket fuels Y Pal, SN Mahottamananda, SK Palateerdham, S Subha, A Ingenito FirePhysChem 1 (4), 272-282, 2021 | 21 | 2021 |
| NOx reduction strategies for high speed hydrogen fuelled vehicles A Ingenito, A Agresta, R Andriani, F Gamma International Journal of Hydrogen Energy 40 (15), 5186-5196, 2015 | 21 | 2015 |
| The role of the baroclinic term in supersonic fuel/air mixing enhancement L Romagnosi, A Ingenito, D Cecere, G Eugenio, C Bruno 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and …, 2011 | 16 | 2011 |
| A novel model of turbulent supersonic combustion: Development and validation A Ingenito, G De Flora, C Bruno, E Giacomazzi, J Steelant 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 4351, 2006 | 16 | 2006 |
| Mixing and combustion in supersonic reactive flows A Ingenito, C Bruno 44th AIAA/ASME/SAE/ASEE joint propulsion conference & exhibit, 4574, 2008 | 15 | 2008 |
| The implication of injection locations in an axisymmetric cavity-based scramjet combustor N Relangi, A Ingenito, S Jeyakumar Energies 14 (9), 2626, 2021 | 14 | 2021 |
| NOx reduction strategies in scramjet combustors A Ingenito Aerospace Science and Technology 59, 189-198, 2016 | 14 | 2016 |
| LES of a supersonic combustor with variable turbulent Prandtl and Schmidt numbers A Ingenito, C Bruno 46th AIAA Aerospace Sciences Meeting and Exhibit, 515, 2008 | 14 | 2008 |
