The effects of different vortex breakdown states on the evaporation process characterizing air-acetone vapor swirling jets laden with liquid acetone droplets in the dilute regime are discussed based on results provided by direct numerical simulations. Adopting the point-droplet approximation, the carrier phase is solved using an Eulerian framework, whereas a Lagrangian tracking of the dispersed phase is used. Three test cases are investigated: one with fully-turbulent pipe inflow conditions and two with a laminar Maxworthy velocity profile at different swirl rates. Consequently, turbulent, bubble-type, and regular conical vortex breakdown states are established. Following phenomenological and statistical analyses of both phases, a significant enhancement of the overall droplet evaporation process due to the onset of the conical vortex breakdown is observed due to the strongest centrifugal forces driving the entire liquid drops towards the low-saturation mixing layer of the jet. The effects of droplet inertia on evaporation are isolated through an additional set of simulations where liquid droplets are treated as Lagrangian tracers. While it is found that inertial effects contribute to enhanced vaporization near the mixing layer under bubble vortex breakdown conditions, droplet inertia plays a secondary role under both turbulent and conical vortex breakdown due to intense turbulent mixing and high centrifugal forces, respectively.

Direct numerical simulation of vortex breakdown in evaporating dilute sprays / Liberatori, Jacopo; Battista, Francesco; Dalla Barba, Federico; Ciottoli, Pietro Paolo. - In: FLOW TURBULENCE AND COMBUSTION. - ISSN 1386-6184. - 112:(2024), pp. 643-667. [10.1007/s10494-023-00521-3]

Direct numerical simulation of vortex breakdown in evaporating dilute sprays

Jacopo Liberatori
Primo
;
Francesco Battista
Secondo
;
Pietro Paolo Ciottoli
Ultimo
2024

Abstract

The effects of different vortex breakdown states on the evaporation process characterizing air-acetone vapor swirling jets laden with liquid acetone droplets in the dilute regime are discussed based on results provided by direct numerical simulations. Adopting the point-droplet approximation, the carrier phase is solved using an Eulerian framework, whereas a Lagrangian tracking of the dispersed phase is used. Three test cases are investigated: one with fully-turbulent pipe inflow conditions and two with a laminar Maxworthy velocity profile at different swirl rates. Consequently, turbulent, bubble-type, and regular conical vortex breakdown states are established. Following phenomenological and statistical analyses of both phases, a significant enhancement of the overall droplet evaporation process due to the onset of the conical vortex breakdown is observed due to the strongest centrifugal forces driving the entire liquid drops towards the low-saturation mixing layer of the jet. The effects of droplet inertia on evaporation are isolated through an additional set of simulations where liquid droplets are treated as Lagrangian tracers. While it is found that inertial effects contribute to enhanced vaporization near the mixing layer under bubble vortex breakdown conditions, droplet inertia plays a secondary role under both turbulent and conical vortex breakdown due to intense turbulent mixing and high centrifugal forces, respectively.
2024
aerospace propulsion; multiphase flows; dns; eulerian-lagrangian approach; swirl; vortex breakdown
01 Pubblicazione su rivista::01a Articolo in rivista
Direct numerical simulation of vortex breakdown in evaporating dilute sprays / Liberatori, Jacopo; Battista, Francesco; Dalla Barba, Federico; Ciottoli, Pietro Paolo. - In: FLOW TURBULENCE AND COMBUSTION. - ISSN 1386-6184. - 112:(2024), pp. 643-667. [10.1007/s10494-023-00521-3]
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11573/1698851
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