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mauro.valorani@uniroma1.it
Mauro Valorani
Professore Ordinario
Struttura:
DIPARTIMENTO DI INGEGNERIA MECCANICA E AEROSPAZIALE
E-mail:
mauro.valorani@uniroma1.it
Pagina istituzionale corsi di laurea
Curriculum Sapienza
Publications
Title
Published on
Year
Radial Mass Flow Rate Partition on LOx/GCH4 Pintle Injector Configurations
JOURNAL OF PROPULSION AND POWER
2025
Turbulence Closure Assessment in URANS of a Cold-Flow Lab-Scale Swirled Burner
AIAA SCITECH 2024 Forum
2024
Pintle Injector Performance Sensitivity to the Radial Injection Arrangement
AIAA SCITECH 2024 Forum
2024
Family of Skeletal Reaction Mechanisms for Methane–Oxygen Combustion in Rocket Propulsion
JOURNAL OF PROPULSION AND POWER
2024
Impact of chemical modeling on the numerical analysis of a LOx/GCH4 rocket engine pintle injector
ACTA ASTRONAUTICA
2024
A data-driven reduced-order model for stiff chemical kinetics using dynamics-informed training
ENERGY AND AI
2024
A Lagrangian Analysis of Combustion Regimes Using Multi-modal Turbulent Combustion Model
FLOW TURBULENCE AND COMBUSTION
2024
Anisotropy analysis of vortex breakdown states via direct numerical simulation
INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW
2024
Large Eddy Simulations of Conventional and Alternative Aviation Fuel Spray Breakup
AIAA AVIATION FORUM AND ASCEND 2024
2024
BayeSAF: A Bayesian Framework for Modeling Physicochemical Surrogates of Sustainable Alternative Fuels
9th European Congress on Computational Methods in Applied Sciences and Engineering (ECCOMAS Congress 2024)
2024
BayeSAF: A Bayesian Framework for Modeling Physicochemical Surrogates of Sustainable Alternative Fuels
SIAM Conference on Uncertainty Quantification (UQ24)
2024
A combined PCA-CSP solver for dimensionality and stiffness reduction in reacting flow simulations
PROCEEDINGS OF THE COMBUSTION INSTITUTE
2024
A thermal flash-boiling model for secondary atomization of Lagrangian droplets
AIAA SciTech Forum 2024
2024
Evaluation of Non-ideal Fluid Modeling for Droplet Evaporation in Jet-Engine-Like Conditions
FLOW TURBULENCE AND COMBUSTION
2024
CSP-driven optimization of a 16-species skeletal mechanism for methane ignition at high pressure
AIAA SCITECH Forum
2023
Uncertainty quantification analysis of RANS of spray swirling jets undergoing vortex breakdown
Mediterranean Combustion Symposium
2023
Unsteady RANS simulations with uncertainty quantification of a spray combustor under liquid rocket engine relevant conditions
AIAA Scitech 2023 Forum
2023
Heat Transfer in Rocket Combustion Chambers Firing Plates: Role of Injector Confinement
JOURNAL OF PROPULSION AND POWER
2023
Uncertainty quantification analysis of Reynolds-averaged Navier–Stokes simulation of spray swirling jets undergoing vortex breakdown
INTERNATIONAL JOURNAL OF SPRAY AND COMBUSTION DYNAMICS
2023
Anisotropy analysis of vortex breakdown states via direct numerical simulation
10th Symposium on Turbulence, Heat and Mass Transfer
2023
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ERC
PE8_1
KET
Big data & computing
Sustainable technologies & development
Interessi di ricerca
Keywords
aerospace vehicles
high-pressure combustion
MILD combustion
chemical model reduction
chemical kinetics simplification
Gas Turbine
Progetti di Ricerca
Advanced modeling of reactive flows in next generation throttleable, restartable liquid-propellant rocket engine.
Parallel computing server for numerical characterization of space transportation vehicles
Gruppi di ricerca - Responsabile
Modellistica della Combustione
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