EXP 1-4 Description
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Axisymmetric drop impact dynamics on a wall film of the same liquid
Description of Study Test Case
This section should: * Convey the general set-up of the test case configuration (e.g. airflow over a bump on the floor of a wind tunnel) * Describe the geometry, illustrated by a sketch * Specify the flow parameters which define the flow regime (e.g. Reynolds number, Rayleigh number, angle of incidence etc.) * give the principal quantities of interest that were measured - these should include global parameters but also mean-flow and turbulence parameters. The description can be kept fairly short if reference can be made to a publication or a link to a data base where details are given. For other cases a more detailed, self-contained description should be provided.
The liquid used in the experiments is silicone oil. Its physical properties are summarized in Table 1. The film height h = 500 μm as well as the drop diameter D = 1.5mm are kept fixed, resulting in δ = 0.33 and Oh = 0.03, respectively. The drop velocity is varied from 1 to 3 m/s. Accordingly, the Weber number is in the range 78 702 while the Reynolds number Re = We0.5/Oh is in the range 300 900, see Table 2
Impact energy | Impact velocity | Weber number | Reynolds number |
---|---|---|---|
Example | Example | Example | 300 |
Example | Example | Example | 600 |
Example | Example | Example | 900 |
Contributed by: Bastian Stumpf, Milad Bagheri, Ilia V. Roisman, Cameron Tropea, Jeanette Hussong, Martin Wörner, Holger Marschall — Technical University of Darmstadt and Karlsruhe Institute of Technology
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