The wake-mixing layer flow developing past a splitter plate separating two parallel gas and liquid co-flowing currents is experimentally investigated in this work. Time-resolved particle image velocimetry (TR-PIV) measurements of the two-phase velocity field are simultaneously performed in gas and liquid streams, shedding light on both mean (time-averaged) and unsteady features of the flow configuration. A selected reference case is first analyzed, revealing the presence of a wake region within the flow field, right behind the splitter plate. By progressively moving downstream along the streamwise G direction, a pure mixing layer region is retrieved. The effect of two governing flow parameters, namely the gas Reynolds number '46 and the gasliquid dynamic pressure ratio ", is then investigated, focusing first on the mean flow topology. It is found that the streamwise extension of the wake GF is a monotonic decreasing function of '46, and it vanishes for the highest '46 value considered, the two-phase flow resulting in a pure mixing layer regime. The flow unsteady development is then characterized by means of the spectral analysis of normal-to-flow (i.e. along H direction) velocity fluctuating quantities E01C°, performed in both gas and liquid flows. As major results, it is found that frequency spectra are characterized by a high frequency content in the low '46 configuration, the peak frequency depending on the streamwise location G. On the other hand, by progressively increasing '46 the peak frequency shifts to lower values, and it becomes independent on the specific spatial location by increasing ". It is found that, at high '46 and " values, velocity fluctuations are characterized by low frequency temporal oscillations synchronized over a large spatial extent of the flow field. The different regimes outlined by variation of the flow governing parameters are found to be consistent with convective/absolute instability behaviors highlighted by spatiotemporal linear stability analyses of the flow recently presented in literature.

Two-phase wake-mixing layer flow past a splitter plate: An experimental investigation / Della Pia, A.; Michelis, T.; Chiatto, M.; Kotsonis, M.; De Luca, L.. - (2023). ( AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023 usa 2023) [10.2514/6.2023-3774].

Two-phase wake-mixing layer flow past a splitter plate: An experimental investigation

Della Pia A.;Chiatto M.;De Luca L.
2023

Abstract

The wake-mixing layer flow developing past a splitter plate separating two parallel gas and liquid co-flowing currents is experimentally investigated in this work. Time-resolved particle image velocimetry (TR-PIV) measurements of the two-phase velocity field are simultaneously performed in gas and liquid streams, shedding light on both mean (time-averaged) and unsteady features of the flow configuration. A selected reference case is first analyzed, revealing the presence of a wake region within the flow field, right behind the splitter plate. By progressively moving downstream along the streamwise G direction, a pure mixing layer region is retrieved. The effect of two governing flow parameters, namely the gas Reynolds number '46 and the gasliquid dynamic pressure ratio ", is then investigated, focusing first on the mean flow topology. It is found that the streamwise extension of the wake GF is a monotonic decreasing function of '46, and it vanishes for the highest '46 value considered, the two-phase flow resulting in a pure mixing layer regime. The flow unsteady development is then characterized by means of the spectral analysis of normal-to-flow (i.e. along H direction) velocity fluctuating quantities E01C°, performed in both gas and liquid flows. As major results, it is found that frequency spectra are characterized by a high frequency content in the low '46 configuration, the peak frequency depending on the streamwise location G. On the other hand, by progressively increasing '46 the peak frequency shifts to lower values, and it becomes independent on the specific spatial location by increasing ". It is found that, at high '46 and " values, velocity fluctuations are characterized by low frequency temporal oscillations synchronized over a large spatial extent of the flow field. The different regimes outlined by variation of the flow governing parameters are found to be consistent with convective/absolute instability behaviors highlighted by spatiotemporal linear stability analyses of the flow recently presented in literature.
2023
Two-phase wake-mixing layer flow past a splitter plate: An experimental investigation / Della Pia, A.; Michelis, T.; Chiatto, M.; Kotsonis, M.; De Luca, L.. - (2023). ( AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023 usa 2023) [10.2514/6.2023-3774].
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11588/992043
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