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front page - tuprints - Technische Universität Darmstadt

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Experiment of drop diameter impact velocity roughness<br />

mm m/s µm<br />

Stow and Hadfield [142] 1.65 3.62 to 3.82 3 to 12<br />

Range and Feuillebois [115] 1.94 2.16 12 to 23<br />

Xu et al. [166, 167] 3.4 4.3 5 to 78<br />

Pan et al. [103] 0.5 29.6 to 32.5 0.003 to 0.2<br />

Mehdizadeh et al. [83] 0.55 30 0.03<br />

our experiment 0.2 11 to 18 0.75 to 1.25<br />

Table 6.1.: Summary of the conditions of the prompt splash.<br />

Figure 6.9.: Force field analysis on the spreading lamella.<br />

the aerodynamic force are dependent on the lamella thickness and the spreading<br />

velocity. Beside the necessity of sufficiency, the lamella thickness and the spreading<br />

velocity correlate to each other in a complementary manner that a thicker lamella<br />

requires a lower spreading velocity to create the uprising liquid film. For a certain<br />

lamella thickness, there exists a minimum spreading velocity, above which the<br />

liquid corona forms. This velocity is named as the critical spreading velocity. The<br />

viscosity does not enter this hypothesis explicitly, however it influences both the<br />

lamella thickness and the spreading velocity.<br />

Two submodels are desired for the thickness of the lamella, and the corresponding<br />

critical spreading velocity. Ruiter et al. [124] shows that the thickness of the<br />

lamella for the normal impact is multiple times thicker than the boundary layer<br />

which grows proportional to ν water t, where ν is the kinematic viscosity. Furthermore,<br />

the lamella thickness is dependent on the impact velocity. Far away from<br />

splash threshold, the lamella thickness decreased with the increasing impact velocity.<br />

While approaching the splash threshold, the lamella thickness increased, probably<br />

due to the aerodynamic pressure which stalls the spreading of the lamella.<br />

172 6. Results and Discussion

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