Mauro Valorani

Pubblicazioni

Titolo Pubblicato in Anno
Systematic strategies for thermochemical model reduction in rocket propulsion applications 2018 Joint Propulsion Conference 2018
Entropy production and timescales COMBUSTION THEORY AND MODELLING 2017
Computational characterization of ignition regimes in a syngas/air mixture with temperature fluctuations PROCEEDINGS OF THE COMBUSTION INSTITUTE 2017
Chemical model reduction under uncertainty COMBUSTION AND FLAME 2017
Detached-Eddy simulation of shock unsteadiness in an overexpanded planar nozzle AIAA JOURNAL 2017
CSP-based chemical kinetics mechanisms simplification strategy for non-premixed combustion: An application to hybrid rocket propulsion COMBUSTION AND FLAME 2017
Dynamical analysis of turbulent premixed hydrogen/air flames in the thin reaction zone regime 11th Asia-Pacific Conference on Combustion, ASPACC 2017 2017
Delayed detached eddy simulation of separated flows in a planar nozzle 7TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) 2017
Tangential stretching rate (TSR) analysis of non premixed reactive flows PROCEEDINGS OF THE COMBUSTION INSTITUTE 2016
G-scheme-based simplification and analysis methodology for hydrocarbon ignition 2016 Spring Technical Meeting of the Eastern States Section of the Combustion Institute, ESSCI 2016 2016
Dynamical system analysis of ignition phenomena using the tangential stretching rate concept COMBUSTION AND FLAME 2015
Numerical investigation of unsteady laminar methane/LOx flamelet at supercritical pressures Proceedings of the European Combustion Meeting – 2015 2015

ERC

  • PE8_1

KET

  • Big data & computing
  • Sustainable technologies & development

Interessi di ricerca

Numerical simulation of multi-dimensional, chemically reacting, unsteady compressible flows;

Numerical simulation and diagnostic techniques of reacting flow processes using asymptotic and/or vector dynamics-based computational methods;

Methods for simplification and/or reduction of chemical kinetics mechanisms;

Quantification of uncertainties in reacting flows;

Oxidation modeling of thermal protectors for re-entry aircraft;

Analysis of surrogates for aviation fuels;

Modeling of combustion in laminar and turbulent flows;

Sprays modeling;

Cavitation modeling in cryogenic flows;

Ignition in combustion chambers by "laser pulse";

Combustion modeling in super-critical reactant flows for liquid propellant (LRE) space engines;

Off-design analysis of gas turbine engines for aircraft applications.

Optimal design and verification of supersonic air intakes;

Optimal design of ship hulls;

Shape optimization of convergent/divergent nozzles;

Mission analysis for Single Stage To Orbit aircraft;

Participation to the ASI 242 program (C.Rubbia);

Keywords

aerospace vehicles
high-pressure combustion
MILD combustion
chemical model reduction
chemical kinetics simplification
Gas Turbine

Gruppi di ricerca - Responsabile

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