Hybrid Continuum CFD/DSMC Method for Simulating High-Altitude Plume Flows Expanding into Vacuum
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Matteo Bernardini | Aggiungi Tutor di riferimento (Professore o Ricercatore afferente allo stesso Dipartimento del Proponente) |
The hybrid NS-DSMC method will be used to simulate the lateral jet interaction flow of a RACS system with the rarefied atmosphere in transitional regimes. The open-source DSMC solver under the framework of OpenFOAM, used to solve the rarefied zone of the flow field, will be coupled with an in-house, compressible, finite-volume, structured NS solver that will be used to solve the continuum regime zones of the flow field. The coupling of the two solvers will be accomplished with a state-based method, which implies an exchange of information between a continuum-molecular overlap region. The location of this region will be intercepted and tracked through the local Knudsen number based on the gradients local length (GLL). A campaign of 2D numerical simulations for a lateral Hydrazine (HZ) RACS thruster expanding at high altitude will be carried out with various molecule models (VHS and VSS) to investigate the effect of collisions between the particles and non-equilibrium effects. The results will be used to set up and initialize a campaign of 3D numerical simulations that will be used to highlight the three-dimensional effects of the phenomena under investigation, to shed some light on the complex physical mechanisms that characterize the interaction of the nozzle plume with the rarefied atmosphere, and to study the effects of chemical reactions, vibrational and electronic excitation of the air molecules in the rarefied regimes.