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- W3185667044 abstract "Droplets exposed to a high speed velocity field are deformed, leading to changes in their drag coefficient thus influencing their trajectory. Within the context of SLD aircraft icing simulation, the droplet deformation should be considered in order to increase the precision in the computations of the collection efficiency. The accuracy in the predictions of the droplet deformation made by the existing models depends on the specific set of data to what they are applied. Recent experimental data of droplet deformation in the shoulder region of an airfoil is used to compare five droplet deformation models applied to SLD problems: the Taylor Analogy Breakup model, the Clark model, the improved Clark model, the Droplet Deformation and Breakup model and the Droplet Ratio Deformation model. Three droplets radii (500, 950 and 1250 µm), four airfoil velocities (30, 40, 50 and 60 m/s) and three different regions in the shoulder were used for the analysis. It was found that the models that better predict the droplets deformation were the DRD model, the TAB model and the improved Clark’s model, being the error on the order of 4% in the three of them." @default.
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- W3185667044 date "2021-07-28" @default.
- W3185667044 modified "2023-09-27" @default.
- W3185667044 title "Comparison of deformation models for droplets in the vicinity of an airfoil" @default.
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- W3185667044 doi "https://doi.org/10.2514/6.2021-3153" @default.
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