EXP 1-4 Measurement Quantities and Techniques: Difference between revisions

From KBwiki
Jump to navigation Jump to search
No edit summary
 
(53 intermediate revisions by 2 users not shown)
Line 1: Line 1:


=Axisymmetric drop impact dynamics on a wall film of the same liquid=
=Axisymmetric drop impact dynamics on a wall film of the same liquid=
{{EXPHeaderLib
{{EXPHeader
|area=1
|area=1
|number=4
|number=4
Line 8: Line 8:


= Measurement quantities and techniques=
= Measurement quantities and techniques=
<pre style="color: red">
Describe the measurement techniques and indicate which quantities were measured and where. Describe how well conditions at boundaries of the flow such as inflow, outflow, walls, far fields, free surface are given or could be reasonably estimated to provide boundary conditions for CFD calculations.
</pre>


When carrying out the experiments, a uniform film of 500
== Experiment ==
μm thickness is prepared utilizing the film thickness sensor. In the next
step, the film thickness sensor is moved and a drop is generated. Shadowgraph
images are taken during the drop impact onto the liquid film.
A synchronized high-performance LED (Constellation 120E)
in combination with a diffuser plate provides a uniform background
illumination. Images are taken with a high-speed CMOS camera (Photron SA-X2),
recording the impact at a frame rate of 20000 fps with a magnification of
31 μm/px.


The dynamics of the drop-film interaction is characterized by the following three parameters. The crown diameter at the crown
When carrying out the experiments, a uniform film of 500 μm thickness is prepared utilizing the film thickness sensor. In the next step, the film thickness sensor is moved and a drop is generated. During the drop impact onto the liquid film shadowgraphy images are taken. A synchronized high-performance LED (Constellation 120E) in combination with a diffuser plate provides a uniform background illumination. Images are taken with a high-speed CMOS camera (Photron SA-X2), recording the impact at a frame rate of 20000 fps with a resolution of 31 μm/px.
base dCB, measured 0.13 mm above the film surface, the crown diameter
 
at the free rim dCT and the crown height hC as indicated in Fig. 3. These
The dynamics of the drop-film interaction is characterized by three parameters as indicated in Fig. 4.  
parameters are obtained from preprocessed images with the help of the
* The crown diameter at the crown base ''d''<sub>CB</sub>, measured 0.13 mm above the film surface
* The crown diameter at the free rim forming the crown top ''d''<sub>CT</sub>
* The crown height ''h''<sub>C</sub>
These parameters are obtained from preprocessed images with the help of the
MATLAB Image-Processing Toolbox. For this, a background subtraction
MATLAB Image-Processing Toolbox. For this, a background subtraction
from raw images is first performed to be able to distinguish the crown
from raw images is first performed to be able to distinguish the crown
from the background. Then the images are binarised, using a global
from the background. Then the images are binarised, using a global
thresholding method, as shown on the left side of Fig. 3. From the
thresholding method, as shown on the left side of Fig. 4. From the
evaluation of consecutive binarised images, the temporal evolution of
evaluation of consecutive binarised images, the temporal evolution of
dCB, dCT and hC can be determined. Reflections on the crown surface can
''d''<sub>CB</sub>, ''d''<sub>CT</sub> and ''h''<sub>C</sub> can be determined. Reflections on the crown surface can
lead to nonphysical interpretations of the crowns dimensions in individual
lead to nonphysical interpretations of the crowns dimensions in individual
frames. To eliminate erroneous values from the results, all values
frames. To eliminate erroneous values from the results, all values
Line 37: Line 29:
median of 20 consecutive frames are considered as outlier.
median of 20 consecutive frames are considered as outlier.


!!! Show here Fig. 3 from Bagheri et al IJHFF (2022) !!!


A suitable setup for CFD calculations including domain size and boundary conditions can be found in the following publication:  
[[File:TRR150-Fig-ImageProcessing.png|800px|thumb|center|Fig. 4: Montage of binarized picture on the left and a raw picture on the right. The crown diameter at the free rim ''d''<sub>CT</sub> and the crown diameter at the base ''d''<sub>CB</sub> are depicted in red. The crown height ''h''<sub>C</sub> is depicted in green. The dashed blue line indicates the film level.]]
 
 
== Numerical method and computational setup ==
 
The numerical simulations are performed with a diffuse-interface phase-field method which solves the coupled Cahn-Hilliard Navier-Stokes equations by a finite volume method using OpenFOAM (code ''phaseFieldFoam''). The computational setup is shown in Fig. 5. In OpenFOAM, axisymmetric calculations are realized by a wedge-shaped domain with small opening angle (Fig. 5 a). The domain size and the initial conditions are displayed in Fig. 5 (b). In the diffuse-interface region, the mesh is adaptive as illustrated in Fig. 5 (c) for the initial configuration. In the azimuthal direction, the wedge is discretized by one mesh cell.
 
 
[[File:TRR150-Fig-Computational-Setup.png|1200px|thumb|center|Fig. 5: Illustration of a suitable computational setup: a) Wedge-shaped domain with boundary conditions, b) Domain size and initial phase distribution, c) Typical initial configuration of the adaptive grid.]]
 
 
In the numerical simulations, two different models for the surface tension force (equilibrium/relaxation) are employed in combination with different spatial resolutions. In the phase field method, the surface tension force is related to the profile of the phase-discriminating order parameter (''C'') and depends in particular on the gradient of ''C'' within the diffuse interface region. In the standard (equilibrium) formulation, ''C'' is assumed to follow the tanh profile of the equilibrium state whereas the relaxation model accounts for the deviation of the actual profile of ''C'' from the equilibrium profile. The spatial resolution is quantified by the number of mesh cells ''N''<sub>c</sub> used to resolve the thickness of the diffuse interface at equilibrium as illustrated in Fig. 6.
 
 
[[File:TRR150-Fig-Grid-Resolution.png|850px|thumb|center|Fig. 6: Initial phase distribution with magnified views of the diffuse interface for different grid resolutions employed in numerical simulations.]]
 
 
Further details can be found in the following publication:  


M. Bagheri, B. Stumpf, I.V. Roisman, C. Tropea, J. Hussong, M. Wörner, H. Marschall, Interfacial relaxation – Crucial for phase-field methods to capture low to high energy drop-film impacts, Int. J. Heat Fluid Flow, 94 (2022) 108943, https://doi.org/10.1016/j.ijheatfluidflow.2022.108943
M. Bagheri, B. Stumpf, I.V. Roisman, C. Tropea, J. Hussong, M. Wörner, H. Marschall, ''Interfacial relaxation – Crucial for phase-field methods to capture low to high energy drop-film impacts'', Int. J. Heat Fluid Flow 94 (2022) 108943, https://doi.org/10.1016/j.ijheatfluidflow.2022.108943


<br/>
<br/>
----
----
{{ACContribs
{{ACContribs
|authors=Bastian Stumpf, Milad Bagheri, Ilia V. Roisman, Cameron Tropea, Jeanette Hussong, Martin Wörner, Holger Marschall
|authors=Milad Bagheri, Bastian Stumpf, Ilia V. Roisman, Cameron Tropea, Jeanette Hussong, Martin Wörner, Holger Marschall
|organisation=Technical University of Darmstadt and Karlsruhe Institute of Technology
|organisation=Technical University of Darmstadt and Karlsruhe Institute of Technology
}}
}}
{{EXPHeaderLib
{{EXPHeader
|area=1
|area=1
|number=4
|number=4

Latest revision as of 10:01, 17 August 2023

Axisymmetric drop impact dynamics on a wall film of the same liquid

Front Page

Introduction

Review of experimental studies

Description

Experimental Set Up

Measurement Quantities and Techniques

Data Quality and Accuracy

Measurement Data and Results


Measurement quantities and techniques

Experiment

When carrying out the experiments, a uniform film of 500 μm thickness is prepared utilizing the film thickness sensor. In the next step, the film thickness sensor is moved and a drop is generated. During the drop impact onto the liquid film shadowgraphy images are taken. A synchronized high-performance LED (Constellation 120E) in combination with a diffuser plate provides a uniform background illumination. Images are taken with a high-speed CMOS camera (Photron SA-X2), recording the impact at a frame rate of 20000 fps with a resolution of 31 μm/px.

The dynamics of the drop-film interaction is characterized by three parameters as indicated in Fig. 4.

  • The crown diameter at the crown base dCB, measured 0.13 mm above the film surface
  • The crown diameter at the free rim forming the crown top dCT
  • The crown height hC

These parameters are obtained from preprocessed images with the help of the MATLAB Image-Processing Toolbox. For this, a background subtraction from raw images is first performed to be able to distinguish the crown from the background. Then the images are binarised, using a global thresholding method, as shown on the left side of Fig. 4. From the evaluation of consecutive binarised images, the temporal evolution of dCB, dCT and hC can be determined. Reflections on the crown surface can lead to nonphysical interpretations of the crowns dimensions in individual frames. To eliminate erroneous values from the results, all values with a deviation of more than three standard deviations from a running median of 20 consecutive frames are considered as outlier.


Fig. 4: Montage of binarized picture on the left and a raw picture on the right. The crown diameter at the free rim dCT and the crown diameter at the base dCB are depicted in red. The crown height hC is depicted in green. The dashed blue line indicates the film level.


Numerical method and computational setup

The numerical simulations are performed with a diffuse-interface phase-field method which solves the coupled Cahn-Hilliard Navier-Stokes equations by a finite volume method using OpenFOAM (code phaseFieldFoam). The computational setup is shown in Fig. 5. In OpenFOAM, axisymmetric calculations are realized by a wedge-shaped domain with small opening angle (Fig. 5 a). The domain size and the initial conditions are displayed in Fig. 5 (b). In the diffuse-interface region, the mesh is adaptive as illustrated in Fig. 5 (c) for the initial configuration. In the azimuthal direction, the wedge is discretized by one mesh cell.


Fig. 5: Illustration of a suitable computational setup: a) Wedge-shaped domain with boundary conditions, b) Domain size and initial phase distribution, c) Typical initial configuration of the adaptive grid.


In the numerical simulations, two different models for the surface tension force (equilibrium/relaxation) are employed in combination with different spatial resolutions. In the phase field method, the surface tension force is related to the profile of the phase-discriminating order parameter (C) and depends in particular on the gradient of C within the diffuse interface region. In the standard (equilibrium) formulation, C is assumed to follow the tanh profile of the equilibrium state whereas the relaxation model accounts for the deviation of the actual profile of C from the equilibrium profile. The spatial resolution is quantified by the number of mesh cells Nc used to resolve the thickness of the diffuse interface at equilibrium as illustrated in Fig. 6.


Fig. 6: Initial phase distribution with magnified views of the diffuse interface for different grid resolutions employed in numerical simulations.


Further details can be found in the following publication:

M. Bagheri, B. Stumpf, I.V. Roisman, C. Tropea, J. Hussong, M. Wörner, H. Marschall, Interfacial relaxation – Crucial for phase-field methods to capture low to high energy drop-film impacts, Int. J. Heat Fluid Flow 94 (2022) 108943, https://doi.org/10.1016/j.ijheatfluidflow.2022.108943




Contributed by: Milad Bagheri, Bastian Stumpf, Ilia V. Roisman, Cameron Tropea, Jeanette Hussong, Martin Wörner, Holger Marschall — Technical University of Darmstadt and Karlsruhe Institute of Technology

Front Page

Introduction

Review of experimental studies

Description

Experimental Set Up

Measurement Quantities and Techniques

Data Quality and Accuracy

Measurement Data and Results


© copyright ERCOFTAC 2024