Mario Tindaro Migliorino

Pubblicazioni

Titolo Pubblicato in Anno
Film cooling modeling in liquid rocket thrust chambers AIAA propulsion and energy forum 2021-3574 2021
Numerical Analysis and Wind Tunnel Validation of Low-Temperature Ablators undergoing Shape Change INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER 2021
Numerical Analysis of Nozzle Transient Heating and Erosion in Hybrid Rockets burning HDPE AIAA Propulsion and Energy Forum 2021 2021
Numerical Analysis of Nozzle Erosion in Hybrid Rockets and Comparison with Experiments JOURNAL OF PROPULSION AND POWER 2021
Numerical simulations of the internal ballistics of paraffin–oxygen hybrid rockets at different scales AEROSPACE 2021
Gas-Phase Reaction Effects on Nozzle Erosion in Paraffin/Oxygen Hybrid Rockets AIAA Propulsion and Energy Forum, 2021 2021
Experimental demonstration of high-amplitude thermoacoustic instabilities under transcritical temperature conditions in a standing-wave device AIAA Scitech 2021 Forum 2021
Onset criteria for bulk-mode thermoacoustic instabilities in supercritical hydrocarbon fuels JOURNAL OF FLUIDS ENGINEERING 2021
Machine Learning Techniques for Flight Performance Prediction of Hybrid Rocket Engines AIAA Propulsion and Energy Forum, 2021 2021
A Computational Tool for the Design of Hybrid Rockets AEROTECNICA MISSILI & SPAZIO 2021
Experimental and numerical investigation of standing-wave thermoacoustic instability under transcritical temperature conditions THE JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA 2021
Student firing tests and launches with commercial and self-made solid rocket motors 2021
Numerical analysis of paraffin-wax/oxygen hybrid rocket engines JOURNAL OF PROPULSION AND POWER 2020
Numerical Approach for the Estimation of Throat Heat Flux in Liquid Rocket Engines AEROTECNICA MISSILI & SPAZIO 2020
A sensitivity study on a cfd model for paraffin-based hybrid rockets AIAA Propulsion and Energy 2020 Forum 2020
Numerical analysis of nozzle heating and erosion in hybrid rockets and comparison with experiments AIAA Propulsion and Energy 2020 Forum 2020
Numerical and experimental analysis of capsules ablation and shape change including heating transient effects AIAA Propulsion and Energy 2020 Forum 2020
Heat-induced planar shock waves in supercritical fluids SHOCK WAVES 2020
Real-fluid effects on standing-wave thermoacoustic instability JOURNAL OF FLUID MECHANICS 2020
Predictive cfd model for internal ballistics of hybrid rocket engines using supercritical paraffin-wax and oxygen AIAA Propulsion and Energy Forum and Exposition, 2019 2019

ERC

  • PE8_1

Interessi di ricerca

Hybrid Rocket Engines, Computational Fluid Dynamics, Liquid Rocket Engines, Hypersonic Reentry

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