numericalsimulationofliquidspraysforjetengineapplications · 2019. 3. 15. · atomization mechanism...

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CN DAVIES AWARD PROGRESS REPORT JANUARY 2016 Numerical Simulation of Liquid Sprays for Jet Engine Applications Camille Bilger Department of Engineering, University of Cambridge Supervisor: Prof. Stewart Cant Aims and Objectives Several graphical classifications of regimes for two-phase flow dynam- ics have been reported in the literature based on experimental observations but none for prefilming liquid sheet atomization, to this date. The primary aim for 2015 has been to classify the phenomenology observed during primary breakup of a planar liquid sheet with a set of high-fidelity numerical simulations, using our novel in-house state-of-the-art numerical capa- bility for efficient modelling of multiphase flows – the Robust Conservative Level Set (RCLS). Using the results, we propose a regime mapping for prefilming liquid sheet atomization. Results Throughout the last twelve months, we have enhanced our flow parametric study to make an informed qualitative assessment on the influence of various fuel and air velocities for a fixed prefilmer geometry at ambient atmospheric conditions. This qualitative analysis now concerns four main characteristics of the atomization process: the formation of interfacial instabilities (series of longitudinal and transverse waves), the conditions required for the onset of spanwise and streamwise ligament formation disintegrating into smaller liquid structures, the ligament and drop sizes along the liquid surface, and the interaction of the two fluids at the prefilmer lip. Results show that the behaviour and development of the liquid sheet is influenced mainly by the relative inertia of the gas and the liquid. The development of surface instabilities is mainly dependent on the shearing intensity exerted by the air on the liquid sheet. Breakup does not always occur in the vicinity of the prefilmer lip, but sometimes on the plate. Furthermore, the results also indicate the importance of the interaction between the two fluids at the prefilmer lip. In consequence, the results suggest that, in some cases, the atomization mechanism is not aerodynamic tearing but vortex flapping downstream of the lip. All of these results show that phenomenological analyses are effective to help interpret and correlate the different behaviours of atomization by varying the operating conditions to map a wide range of gas and liquid velocities. Based on the observed physics, we worked towards a matrix of liquid film breakup phenomena. We have identified regimes of breakup and mapped them in velocity space. We are working towards mapping them onto a non-dimensional space and then move on to changing different sets of parameters. [a] [b] [c] Figure 0.1: Simulation of flat sheet breakup – Interface coloured by liquid velocity. [a]: U air = 20m/s, U liq = 1m/s; [b]: U air = 40m/s, U liq = 5m/s; [c]: U air = 80m/s, U liq = 2m/s. Acknowledgments This work was funded by Rolls-Royce Group plc.

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  • CN DAVIES AWARD PROGRESS REPORT – JANUARY 2016

    Numerical Simulation of Liquid Sprays for Jet Engine Applications

    Camille BilgerDepartment of Engineering, University of Cambridge

    Supervisor: Prof. Stewart Cant

    Aims and Objectives Several graphical classifications of regimes for two-phase flow dynam-ics have been reported in the literature based on experimental observations but none forprefilming liquid sheet atomization, to this date. The primary aim for 2015 has been to classifythe phenomenology observed during primary breakup of a planar liquid sheet with a set ofhigh-fidelity numerical simulations, using our novel in-house state-of-the-art numerical capa-bility for efficient modelling of multiphase flows – the Robust Conservative Level Set (RCLS).Using the results, we propose a regime mapping for prefilming liquid sheet atomization.

    Results Throughout the last twelve months, we have enhanced our flow parametric study tomake an informed qualitative assessment on the influence of various fuel and air velocities fora fixed prefilmer geometry at ambient atmospheric conditions. This qualitative analysis nowconcerns four main characteristics of the atomization process: the formation of interfacialinstabilities (series of longitudinal and transverse waves), the conditions required for the onsetof spanwise and streamwise ligament formation disintegrating into smaller liquid structures,the ligament and drop sizes along the liquid surface, and the interaction of the two fluidsat the prefilmer lip. Results show that the behaviour and development of the liquid sheet isinfluenced mainly by the relative inertia of the gas and the liquid. The development of surfaceinstabilities is mainly dependent on the shearing intensity exerted by the air on the liquidsheet. Breakup does not always occur in the vicinity of the prefilmer lip, but sometimes onthe plate. Furthermore, the results also indicate the importance of the interaction betweenthe two fluids at the prefilmer lip. In consequence, the results suggest that, in some cases, theatomization mechanism is not aerodynamic tearing but vortex flapping downstream of the lip.All of these results show that phenomenological analyses are effective to help interpret andcorrelate the different behaviours of atomization by varying the operating conditions to map awide range of gas and liquid velocities. Based on the observed physics, we worked towards amatrix of liquid film breakup phenomena. We have identified regimes of breakup and mappedthem in velocity space. We are working towards mapping them onto a non-dimensional spaceand then move on to changing different sets of parameters.

    [a] [b] [c]

    Figure 0.1: Simulation of flat sheet breakup – Interface coloured by liquid velocity. [a]: Uair =20m/s, Uliq = 1m/s; [b]: Uair = 40m/s, Uliq = 5m/s; [c]: Uair = 80m/s, Uliq = 2m/s.

    Acknowledgments This work was funded by Rolls-Royce Group plc.