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6 Summary and outlook

The capability to accurately predict forced wetting in shear flow is highly anticipated in industrial applications, e.g.

for the optimization of vehicle soiling early on in the design process. This thesis is motivated by the necessity of a highly accurate simulation framework to cover complex industrial cases, as well as, to provide phenomenological insight complementary to experimental and theoretical analysis. To cover multi-phase flow, wetting, and turbulent shear flow in cases motivated by industry, high-performance techniques and the ability to handle complex geometries are required. Therefore, in each of this research areas novelties have been presented in this work. They have been com-bined in one solver based on OpenFOAM, which has been extensively validated and successfully applied to relevant cases.

To efficiently discretize multiple length scales with transient transport processes, such as moving two-phase interfaces and reduce computational effort, Adaptive Mesh Refinement represents a powerful tool. The respective refinement algorithm in OpenFOAM has been enhanced, abstracting the basic 3D refinement and the underlying single criterion refinement to a versatile application in 2D, 2.5D, and 3D and a multi-criterion refinement. Thereby, severe bugs have been found and fixed to ensure accurate and stable simulations. To maintain the benefits of Adaptive Mesh Refinement on highly parallelized computations, Dynamic Load Balancing is required. An existing algorithm has been consolidated, enhanced and combined with improved Adaptive Mesh Refinement. Both, the developments in Adaptive Mesh Refinement and Dynamic Load Balancing have been published in Rettenmaier et al. (2019).

In the analyzed characteristic length scales, the surface tension plays an important role at the multi-phase interface. Using the interface capturing Volume of Fluid method, in which no explicit interface representation exists, the accurate calcu-lation of the curvature is a major challenge especially on an unstructured mesh. Inaccuracies of the curvature calcucalcu-lation affect the surface tension directly and cause parasitic currents near the interface. To reduce such currents and to increase the accuracy of the simulations, three models for improved surface tension have been implemented and validated in this study: the Continuum Surface Force model, an iso-surface reconstruction of the interface and a conservative hybrid of the Volume of Fluid and Level-Set methods called S-CLSVOF(DSB). For the applications of this study, the iso-surface reconstruction model has been found to be most suitable. The modular implementation structure allows for an easy incorporation of even better models developed in the future.

A major focus of this work are the many phenomena related to the dynamic three-phase contact line. A variety of models for the discretization of the position of the contact line, the contact line velocity, the dependence of the contact angle on the contact line velocity, the contact angle hysteresis, as well as to reduce the mesh size dependency, have been imple-mented. All these models are part of a unique contact line library which has been successfully validated.

Shear flow in industrial applications is often turbulent. For high Reynolds numbers, the small turbulent scales cannot be resolved with a reasonable computational effort, therefore, turbulence models are necessary. The combination of turbu-lence models with multi-phase flow is a field of ongoing research and requires a particular treatment at the two-phase interface. On this behalf, two models, the WALE model and theζf-VLES model have been analyzed. The results point out, that only the latter model yields satisfactory results at the interface.

Then the piecewise validated numerical framework has been applied, first on drops and rivulets on tilted plates and then for drops in laminar and turbulent shear flow. The point of incipient motion of a drop on a slowly tilting plate has been matched in 2D and 3D with theoretical and experimental results for different surfaces and drop volumes.

The accurate simulation results indicate that the adhesion force has been modeled correctly but also point out, that experimental contact angle measurements are required to be very accurate. Simulations of the continuous motion of drops sliding down a tilted plate show the characteristic cornered tail of a drop, which forms to a cusp and

eventu-ally emits droplets. These regimes are equeventu-ally found in experiments. The path of a rivulet on a tilted plate can be categorized as straight, quasi-static meandering and dynamic meandering for increasing volumetric flow and constant wetting conditions. As a novelty in literature, simulations of this study recover all three regimes. A quasi-static meander-ing path can only be achieved when accountmeander-ing for the contact angle hysteresis and the related pinnmeander-ing of the contact line.

Shear flow has been validated first on a drop impact case, for which the receding phase is in exceptional good agreement with experiments using the pinning boundary condition. Also for the incipient motion of drops in laminar conditions.

The critical shear velocity is accurately matched for different surfaces and drop volumes described in experiments in literature. A novelty of this study is the simulation of the incipient motion of drops in turbulent shear flow with the Volume of Fluid method and a Very Large Eddy Simulation modeling the turbulence. Experiments on incipient motion of drops in turbulent shear flow by Seiler et al. (2018a) have been compared with simulations with good accordance, which encouraged the expansion of a theoretical model for incipient motion in laminar shear flow to turbulent flows on the basis of simulation data. The characteristic drop oscillation, caterpillar-like motion have been compared qualitatively with experiments.

Great care has been taken to ensure the compatibility of the applied models with unstructured meshes to be able to handle complex geometries. To show the predictive capabilities of the framework even on complex geometries, a mi-crochannel has been placed perpendicular to the drop motion in turbulent channel flow. The interaction of a moving drop with a microchannel as obstacle depends on the drop velocity, the drop volume, and the microchannel width are in qualitative agreement with experimental findings.

All in all, the numerical framework including high-performance techniques, interface, and dynamic contact line handling, as well as turbulence modeling in combination with multi-phase flows has been successfully validated with experiments.

The trustworthy validation builds a water-proof step-stone for future work on drops and rivulets in turbulent shear flow and complex geometries.

There are two possible directions for future work research, the improvement of numerical models and the simulation of related application relevant cases as well as theoretical modeling. Numerical methods are being improved constantly.

Currently, Adaptive Mesh Refinement is restricted to hexahedra and prisms, therefore the next step regarding Adap-tive Mesh Refinement would be the incorporation of a polyeder (un)refinement as presented in Meredith and Vukˇcevi´c (2018). Especially the surface tension model has great potential for game-changing improvements. Second-order accu-rate geometrical Volume of Fluid methods for unstructured meshes are currently developed, among others, by Maric et al.

(2013). Handling the diffusion of the interface is an ongoing challenge with algebraic Volume of Fluid methods. An im-provement is expected by incorporating the Ghost-Fluid method by Vukˇcevi´c et al. (2017), which has yet to be combined with surface tension modeling within OpenFOAM. Besides that, an already available advection method is the so-called iso-advector, a geometrically based volume fraction transport scheme by Roenby et al. (2016). A stable combination of this model with Adaptive Mesh Refinement and Dynamic Load Balancing in OpenFOAM would be promising. Regarding the contact line velocity, the model of Afkhami et al. (2009) did not result in the expected reduction of mesh dependence for all contact line model combinations. An incorporation of the Navier-Slip model might help in that aspect.

On the application side, the complexity of cases is to be increased by simulation of rivulets in shear flow, interaction and shedding of drops and rivulets on complex geometry. A detailed analysis of merging and breakup of drops and rivulets could also give valuable insight. Moreover, the predictive capability of the presented framework with respect to the transitions between thin films, drops, and rivulets have yet to be proven. Furthermore, the influence of surface vibration on wetting as shown by Burgmann et al. (2018) should be included. Resolving large-scale industrial applications droplet by droplet might not always be practical. Therefore, further theoretical work is necessary, in particular on the interaction of the contact line with complex geometry. Such theoretical models might base on simulations using the presented well validated numerical framework.

A Test cases for the validation of the numerical framework

The test case setups for the validation of the numerical framework are given in the following to allow for a compact presentation of Chapter 3 and provide necessary details in a unified manner. A legend and the used units are given in Table A.2.

wall - slip wall - no slip axis symmetry symmetry interface

Table A.1:Legend

Unit

% kg/m3 ν m2/s σ kg/(s2m) θ

Table A.2:Units of physical quantities

A.1 Dam break with an obstacle (3D)

0.3 0.7 1.0

0.25

0.75 0.4

0.19

t0

G L

g

Figure A.1:3D dam break

L G

% 1000 1

ν 1.00×10−6 14.8×10−6 σ 0.070

θe 90.0

Table A.3:Physical quantities

A dam break with a centric obstacle in 3D with measurements in Figure A.1 is given in meters. At time t0the liquid is initialized as a square. During the simulation the liquid is forced down due to the gravitational acceleration hitting the obstacle. The domain is cubic and surrounded by walls. For a better visualization the front and left wall are not shown.