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Mario Tindaro Migliorino
Mario Tindaro Migliorino
Verified email at uniroma1.it
Title
Cited by
Cited by
Year
Real-fluid effects on standing-wave thermoacoustic instability
MT Migliorino, C Scalo
Journal of Fluid Mechanics 883, A23, 2020
302020
Numerical analysis of paraffin-wax/oxygen hybrid rocket engines
MT Migliorino, D Bianchi, F Nasuti
Journal of Propulsion and Power 36 (6), 806-819, 2020
282020
Numerical analysis of nozzle erosion in hybrid rockets and comparison with experiments
D Bianchi, MT Migliorino, M Rotondi, L Kamps, H Nagata
Journal of Propulsion and Power 38 (3), 389-409, 2022
182022
Numerical analysis and wind tunnel validation of low-temperature ablators undergoing shape change
D Bianchi, MT Migliorino, M Rotondi, A Turchi
International Journal of Heat and Mass Transfer 177, 121430, 2021
182021
Heat-induced planar shock waves in supercritical fluids
MT Migliorino, C Scalo
Shock Waves 30 (2), 153-167, 2020
142020
CFD Analysis of Paraffin-Based Hybrid Rockets with Coupled Nozzle Erosion Characterization
D Bianchi, MT Migliorino, F Nasuti, M Onofri
AIAA Propulsion and Energy 2019 Forum, 4263, 2019
142019
Numerical and experimental analysis of a transcritical thermoacoustic prototype
D Alexander, MT Migliorino, S Heister, C Scalo
2018 Fluid Dynamics Conference, 3536, 2018
142018
Graphite Nozzle Erosion Trends in Paraffin/Oxygen Hybrid Rockets
MT Migliorino, D Bianchi, F Nasuti
Journal of Propulsion and Power 38 (4), 508-522, 2022
112022
Numerical simulations of the internal ballistics of paraffin–oxygen hybrid rockets at different scales
MT Migliorino, D Bianchi, F Nasuti
Aerospace 8 (8), 213, 2021
112021
Numerical Simulations of Fuel Shape Change in Paraffin–Oxygen Hybrid Rocket Engines
MT Migliorino, G Gubernari, D Bianchi, F Nasuti, D Cardillo, F Battista
Journal of Propulsion and Power 39 (6), 785-799, 2023
82023
Numerical assessment of camphor ablation flight relevance in hypersonic wind-tunnel testing
M Rotondi, MT Migliorino, D Bianchi, P Pagani, A Turchi
Journal of Spacecraft and Rockets 59 (5), 1574-1591, 2022
62022
Experimental and numerical investigation of standing-wave thermoacoustic instability under transcritical temperature conditions
A Martinez, MT Migliorino, C Scalo, SD Heister
The Journal of the Acoustical Society of America 150 (4), 2900-2911, 2021
62021
Numerical analysis of nozzle heating and erosion in hybrid rockets and comparison with experiments
D Bianchi, MT Migliorino, M Rotondi, LT Kamps, H Nagata
AIAA Propulsion and Energy 2020 Forum, 3767, 2020
62020
Predictive CFD Model for Internal Ballistics of Hybrid Rocket Engines using Supercritical Paraffin-wax and Oxygen
MT Migliorino, D Bianchi, F Nasuti
AIAA Propulsion and Energy 2019 Forum, 4261, 2019
62019
Numerical Simulations of Fuel Shape Change and Swirling Flows in Paraffin/Oxygen Hybrid Rocket Engines
M Fabiani, G Gubernari, MT Migliorino, D Bianchi, F Nasuti
Aerotecnica Missili & Spazio 102 (1), 91-102, 2023
52023
A Computational Tool for the Design of Hybrid Rockets
PM Zolla, MT Migliorino, D Bianchi, F Nasuti, RC Pellegrini, E Cavallini
Aerotecnica Missili & Spazio 100 (3), 253-262, 2021
52021
Onset criteria for bulk-mode thermoacoustic instabilities in supercritical hydrocarbon fuels
SA Hunt, MT Migliorino, C Scalo, SD Heister
J. Fluids Eng. 143 (4), 040901, 2021
52021
Assessment of spurious numerical oscillations in high-order spectral difference solvers for supercritical flows
MT Migliorino, JB Chapelier, C Scalo, G Lodato
2018 Fluid Dynamics Conference, 4273, 2018
52018
Numerical and experimental analysis of fuel regression rate in a lab-scale hybrid rocket engine with swirl injection
MT Migliorino, M Fabiani, C Paravan, D Bianchi, F Nasuti, L Galfetti, ...
Aerospace Science and Technology 140, 108467, 2023
42023
System and method for stabilizing transcritical air-to-fuel heat exchange
PC Sweeney, SD Heister, SA Hunt, C Scalo, MT Migliorino
US Patent 10,890,114, 2021
42021
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Articles 1–20