This work was performed in the cooperation framework of Wetsus European Center of Excellence for Sustainable Water Technology (www.wetsus.eu) within the Applied Water Physics theme. Wetsus is cofounded by the Dutch Ministry of Economic Affairs and Ministry of Infrastructure and Environment, The Province of Friesland and the Northern Netherlands Provinces. This research has received funding from the European Union&#8217;s Horizon 2020 research and innovation program under the Marie Sklodowska-Curie grant agreement No. 665874 and the Gilbert- Armstrong lab. We highly appreciate Maarten V. van de Griend&#39;s support of this work.

1. General recommendations
<ol>
	<li>Check all the pipe connections for leaks before starting the setup.</li>
	<li>Check that the funnel lid is in place, and secure.</li>
	<li>Clean the funnel before and after each experiment with a brush and glass cleaner, as it may turn yellow due to the high concentration of iron in the groundwater.</li>
</ol>
2. Experimental setup
<ol>
	<li>Water vortex system (Figure 3)
	<ol>
		<li>Securely fix the glass funnel (Figure 4) in a vertical position on a special frame - a board with four legs and a slot in the middle, which corresponds to the diameter of the cylindrical part of the funnel and is big enough for the funnel to fit in but not too big for it to fall through. Securely fasten the frame so that it does not shake.</li>
		<li>Put a rubber gasket between the lid and the funnel to avoid leaks. Attach the funnel lid, and tighten it using the bolts.</li>
		<li>Connect the groundwater pump to the tangential inlet in the top cylindrical part of the funnel using hoses and hose connectors.</li>
		<li>Connect a special control valve to adjust the water flow rate between the pump and the funnel. Connect a water flow meter between the control valve and the funnel.</li>
		<li>Connect the outlet of the funnel to the drain with a hose. On the drainage hose, near the outlet of the funnel, install a clamp to create back pressure during the unit&#39;s operation. 
		NOTE: The clamp should be installed immediately after all the other adapters and connectors required for the experiments.</li>
	</ol>
	</li>
	<li>System for tracer experiments (Figure 3)
	<ol>
		<li>Install special adapters for installing probes near the inlet and outlet. Install pH probes in these adapters, and connect them to the data logger.</li>
		<li>Install sensors as close as possible to the funnel to reduce error in the HRT calculations.</li>
		<li>Prepare 1 mL of NaOH solution (concentration: 0.2 M) to be used as a chemical tracer that is injected into the water flow of the jet. 
		NOTE: As sodium hydroxide aqueous solution is a strong base, it is displayed as a peak-like increase in the pH30.</li>
		<li>Install an adapter with three openings for connecting the tracer-injection system, which consists of a valve and a syringe before the pH probe near the inlet.</li>
	</ol>
	</li>
	<li>System for DO experiments (Figure 3)
	<ol>
		<li>Glue two oxygen sensor spots to the inside wall of the two different glass adapters, placing them as close as possible to the inlet and outlet of the funnel and connecting them to the water pipeline. 
		NOTE: During operation, the water must completely cover the stickers.</li>
		<li>Install the glass adapter with the oxygen sensor spot near the inlet and outlet of the funnel, and fix the tip of the polymer optical fiber (which is 2 m long) over the sticker on the other side of the glass.</li>
		<li>Install the water temperature sensor near the funnel inlet in the same adapter as for the pH probe. Ensure that it is close to the fiber, since the water temperature is used to correlate the DO measurements.</li>
		<li>Connect the polymer optical fiber and temperature sensor to the fiber-optic oxygen transmitter.</li>
		<li>Connect the fiber-optic oxygen transmitter to a laptop with special software installed to display the signal from the sensor, which is related to the concentration of dissolved oxygen and the water temperature.</li>
	</ol>
	</li>
</ol>
3. Operation (medium funnel)
<ol>
	<li>Vortex regimes
	<ol>
		<li>Turn on the flow meter. Start the underground water pump, and fully open the control valve. Make sure that the water flow is significantly higher than the maximum flow required to form a water vortex (1338&#160;L/h for the medium funnel).</li>
		<li>Adjust the desired value of the water flow by turning the control valve. If necessary, squeeze the clamp near the outlet of the funnel to allow water to be blocked in the funnel, which causes the water level to rise in the upper cylindrical part of the funnel.</li>
		<li>To set different regimes, adjust the values of the water flow and the water level in the upper cylindrical part of the funnel (Table 1), sequentially in one experiment. Check the water vortex for stability for 15 min. In stable mode, the water level should not change.
		<ol>
			<li>For the twisted regime, adjust the flow rate to 1194 L/h and the water level to 2&#160;cm and the flow rate to 1218 L/h and the water level to 5 cm.</li>
			<li>For the straight regime, adjust the flow rate to 1314 L/h and water level to 11&#160;cm and the flow rate to 1338 L/h and the water level to 11.7 cm.</li>
			<li>For the restricted regime, as opposed to the twisted and straight regimes, create back pressure by squeezing the clamp near the outlet of the funnel. Set the flow rate to 882 L/h and the water level to 3&#160;cm and the flow rate to 936 L/h and the water level to 9&#160;cm.</li>
		</ol>
		</li>
	</ol>
	</li>
	<li>Tracer experiment
	<ol>
		<li>Using a data logger, calibrate the pH probes to ensure the validity and accuracy of the data obtained.
		<ol>
			<li>Prepare two standard solutions, one with a pH that is higher than the pH of the operating range (6-10), and one with a pH that is lower than the pH of the operating range. Set their values in the data logger and measure them one by one during the calibration. After that, the data logger calibrates the pH probes.</li>
			<li>Install pH probes at the inlet and outlet of the funnel, connect them to the data logger, and start the recording mode.</li>
		</ol>
		</li>
		<li>Start the setup.
		<ol>
			<li>Start the setup, and make sure that the water vortex is stable.</li>
			<li>Fill the syringe with the prepared tracer mixture of NaOH and connect it to the tracer injection line. Quickly unscrew the valve in the injection system, inject the tracer liquid, and then quickly screw the valve.</li>
		</ol>
		</li>
		<li>Perform the saving and analysis.
		<ol>
			<li>When the pH stabilizes, save the pH peaks recorded during the passage of the tracer liquid through a glass funnel.</li>
			<li>Analyze the entry and exit peaks as described in a previous work22 for HRT calculation. To do this, take the point at the beginning of the first peak for the countdown, and take the point on the second peak, which divides it into two figures of equal area, for the end of the countdown.</li>
		</ol>
		</li>
	</ol>
	</li>
	<li>DO experiment
	<ol>
		<li>Calibrate the DO sensor using software with a laptop and the fiber-optic oxygen transmitter. Use two fluids: one oxygen-free (mix 0.1 L of water and 1 g of sodium sulfite), and the other saturated with oxygen (to do this, aerate it with air for 15 min). Then, select the calibration function in the software, and measure both liquids in turn.</li>
		<li>Perform the installation and recording.
		<ol>
			<li>Install the DO sensor at the inlet and outlet of the funnel. Additionally, install the temperature sensor near the funnel inlet. Connect them to the fiber-optic oxygen transmitter, and start the recording mode.</li>
			<li>Start the setup, and make sure the water vortex is stable. Reach the mode in which the value of the concentration of DO is stable and record the data. 
			NOTE: If the readings are not stable, the data are not valid, and the experiment must be repeated.</li>
		</ol>
		</li>
	</ol>
	</li>
</ol>

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The authors declare that they have no known competing financial interests or personal relationships that could have appeared to influence the work reported in this paper.

If the groundwater pump is too powerful and the system cannot hold the pressure, an additional drain can be added before the control valve to reduce it. It is very important to calibrate the sensors for reliable results and for the tracer experiment to ensure fast probes. If the probes are slow, then this will distort the HRT measurements. Further, if the HRT is much smaller than the MRT for the straight regime, this may indicate that the tangential entrance to the funnel is significantly below the water level and that part of the tracer liquid is going down to the drain after entering the funnel, thus causing a decrease in HRT.
The water vortex in a hyperbolic Schauberger funnel is very sensitive to the water flow rate. The smaller the system, the more it depends on flow changes. If the regime is stable, then the water level in the funnel should not change with time. If this is not the case, it will rise or fall. Therefore, it is worth paying attention to the water level to avoid water overflow, cracks due to increased pressure inside the funnel, or an unwanted regime change.
To&#160;determine the regime of the vortex (protocol steps 3.1.3.1-3.1.3.3) and its stability, it is advantageous for the funnel to be transparent. For this reason, a glass funnel&#160;was used in this work. It is imperative to be very careful when transporting, handling, and installing it, and one should pay attention not to tighten the screws of the lid too much so as not to damage it (protocol step 2.1.2).
To determine the HRT, protocol steps 3.2.2-3.2.3 should be repeated as many times as possible (at least 10x) because, due to the&#160;high turbulence of the system and the presence of secondary flows (Taylor-like vortices), the tracer jet can separate and travel different ways through the funnel. For example, it was shown by Donepudi et al.24 and Mulligan et al.28 that the closer the water layer is to the glass wall, the faster it will move to the drain. The probes should always be washed with deionized water and wiped to avoid mixing the sample and the storage solution, which can spoil the data and deteriorate the quality of the electrode storage.
For the&#160;DO experiment, it is important to achieve a stable oxygen concentration value at the output of the system (protocol step 3.3.2.2). If the regime is not stable but the fluctuations in the system are not significant, then the obtained value should be averaged. It is also necessary to have a hole in the lid for ventilation to allow airflow into the system for further aeration.
Despite the high values of KLa20&#160;and energy efficiency of this system, the SOTR value is low compared to other methods26 because of the low water flow rates of the available funnels; this is currently a limitation for the industrial use of the hyperbolic funnel for water aeration. However, it has been demonstrated that high efficiency of the system can be achieved for different scales with large, medium, and small funnels. From this, we can conclude that by changing the geometry (dimensions, diameters of the inlet and outlet, curvature of the walls), it is possible to significantly increase the speed and volume of water treatment without reducing the aeration efficiency. Moreover, in Table 1, it can be seen that an increase in the funnel length by 1.1 m led to a more than 100-fold rise in the SOTR. Taking into account the fact that in some water treatment plants, the water level difference can reach several meters, (partial) aeration could be achieved at much lower costs than at present. Thus, determining how different geometric parameters of the funnel affect the water flow rate and KLa20&#160;for vortex regimes can provide a cheap and competitive technology for the aeration of groundwater. Alternatively, as shown by Schauberger31, aeration can be used to improve the quality of water reservoirs, lakes, and rivers.

Our lives are closely connected with spiral structures. They exist in almost everything and everywhere, including the structure of shells and ammonites and the formation of hurricanes, tornadoes, and whirlpools1,2. On a cosmological scale, galaxies form and evolve according to the principle of the logarithmic spiral3. The best-known spirals are the golden and the Fibonacci spirals4, which have many applications ranging from describing plant growth and the crystallographic structure of certain solids to developing computer database search algorithms. The Fibonacci sequence is characterized as a numerical series that starts with 0 and 1 and has subsequent numbers corresponding to the sum of the previous two. This sequence can also be found when counting the reproduction rate of rabbits. Spirals are among some of the oldest geometric shapes drawn by Homo sapiens, such as the concentric circles found in Colombia and Australia (40,000-20,000 BC1). Leonardo da Vinci5 tried to create a helicopter-shaped flying machine using a spiral blade (from the Greek word &#7957;&#955;&#953;&#958; &#960;&#964;&#949;&#961;&#972;&#957;, or helix pteron, meaning spiral wing). Following the same principle, an&#160;aircraft designer, Igor Sikorsky, constructed the first helicopter in series production 450 years later6.
Many other examples point to the fact that helical flow structures might be very efficient and expense-saving because this type of flow is preferentially seen in nature.&#160;At the beginning of the 20th century, the Austrian forester and philosopher Viktor Schauberger realized this. He said that humans should study nature and learn from it rather than trying to correct it. Based on his ideas, he built rather unusual log flumes to float timber; the flumes did not take the straightest path between two points but followed the meandering of valleys and streams. This design made the water flow by twisting in a spiral along its axis, thus forming a vortex, which thereby reduced the amount of water used and produced a transport rate that significantly exceeded what was considered normal7.
Following his father&#39;s footsteps, Viktor&#39;s son Walter developed new technologies using the water vortex8 for various purposes: the treatment of drinking water, industrial process, the restoration of ponds and water courses, the oxygenation of ponds and little lakes, and river regulation and restoration. One of these ideas has recently gained considerable interest, namely water treatment using a hyperbolic funnel8, in which a vortex is created only by the flow of water without any stirring devices. It has been proven to be a very effective method for oxidizing iron in groundwater9,10. A limitation of this technology is that it is less efficient for low-pH water11.
Large amounts of drinking water in the Netherlands are obtained from underground sources12, in which the concentration of iron can reach several tens of milligrams per liter13, whereas 0.2 mg/L is considered acceptable by the standards14. Most drinking water plants use aeration as one of the first steps to reduce the iron concentration in the water purification process. In most cases, the purpose of aeration is to increase the dissolved oxygen content, to remove gases and other related substances from the water, or both15. There are various methods by which aeration can introduce oxygen into liquid media. These methods include agitating the liquid surface using a mixer or turbine and releasing air through either macroscopic orifices or porous materials16.
The chemical process of iron oxidation was demonstrated by van de Griend17, in which an oxygen molecule takes an electron from ferrous iron and reacts with a free proton to form water, while the iron ion is oxidized (equation [1]):
<img alt="Equation 1" src="/files/ftp_upload/64516/64516eq01.jpg" style="margin: auto;" />,&#160; &#160; &#160;(1)
The iron ion then precipitates as Fe(OH)3 because of its reaction with water, which releases protons (equation [2]):
<img alt="Equation 2" src="/files/ftp_upload/64516/64516eq02.jpg" style="margin: auto;" />&#160; &#160; &#160;(2)
The total reaction is given by equation (3):
<img alt="Equation 3" src="/files/ftp_upload/64516/64516eq03.jpg" style="margin: auto;" />.&#160; &#160; &#160;(3)
In aeration, the techniques most often applied are cascades, tower, spray, and plate aeration systems18,19. The disadvantage of these technologies is that they consume from 50% to 90% of all energy20 and up to 40% of the budget for the operation and maintenance of the treatment facilities21.
Using a hyperbolic funnel for aeration can significantly decrease the costs and increase the efficiency of this process. Hyperbolic funnels are less sensitive to clogging due to their geometry and the fact that there are no moving parts, meaning the energy is spent only on pumping water. Such a system can be characterized by several parameters, such as the water flow rate of the funnel per hour (&#966;), the mean residence time (MRT), the hydraulic retention time (HRT), the oxygen volumetric mass transfer coefficient (KLa20) (corrected to a standardized temperature of 20&#176;C), the standard oxygen transfer rate (SORT), and the standard aeration efficiency (SAE). The flow rate of the funnel is needed to calculate the volume of water that can be processed in a certain time. The MRT is calculated from the ratio of the water flow rate to its volume in the funnel for a certain regime using equation (4):
<img alt="Equation 4" src="/files/ftp_upload/64516/64516eq04.jpg" style="margin: auto;" />&#160; &#160; &#160;(4)
where V represents the liquid volume in the reactor.
The HRT can be determined experimentally using tracer technologies22&#160;via its residence time distribution function. HRT provides fundamental insight into mixing processes, hold-ups, and segregation phenomena23. It was shown by Donepudi24 that the farther away the water jet is from the inlet, the faster it moves toward the outlet. At the initial moment, water is pumped tangentially to the upper cylindrical part of the funnel. Then, under the influence of gravity, together with the system&#39;s geometry, the tangential velocity decreases, and the axial velocity increases. The oxygen volumetric mass transfer coefficient, KLa20 (unit reciprocal time), indicates the capability of a system to facilitate oxygen transfer to the liquid phase10. It can be calculated25,26 according to equation (5):
<img alt="Equation 5" src="/files/ftp_upload/64516/64516eq05.jpg" style="margin: auto;" />&#160; &#160; &#160;(5)
where Cout&#160; is the dissolved oxygen (DO) concentration in the bulk liquid, Cin is the DO concentration in the feed, Cs is the DO concentration at saturation, and T is the water temperature.
The SORT value is the standard rate of oxygen transferred to the liquid phase by the system and is determined by equation (6)27:
<img alt="Equation 6" src="/files/ftp_upload/64516/64516eq06.jpg" style="margin: auto;" />&#160; &#160; &#160;(6)
where <img alt="Equation 8" src="/files/ftp_upload/64516/64516eq08.jpg" style="margin: auto;" /> is the DO at saturation for a temperature of 20 &#176;C. The SOTR value can be defined for a certain process, in which case the volume used in equation (6) is normalized by assuming 1 h of treatment time (process-specific SOTR), so that pilot scale aeration methods can be compared with real-scale systems. For the capability of a certain regime in the funnel, the system-specific SOTR must be calculated, which uses the volume of water inside the funnel for a (regime-specific) hydraulic retention time. This value is important when calculating the actual aeration capabilities of a regime in a given funnel.
The SAE is the ratio between the SOTR and the power expended for aeration. Since energy is spent only on pumping water to the top of the funnel and giving it the necessary flow to form a vortex, it is calculated as the sum of the potential energy of the volume of water pumped per hour at a height corresponding to the length of the funnel and the kinetic energy needed by the water to create a vortex27 using&#160;equation (7):
<img alt="Equation 7" src="/files/ftp_upload/64516/64516eq07.jpg" style="margin: auto;" />&#160; &#160; &#160;(7)
where Pp is the potential power (in kW) required to lift the water pumped to the height of the funnel, and Pk is kinetic power (in kW) required for the water pumped at the top of the funnel to gain enough flow to create a vortex. Normally, for equation (7), the system-specific SOTR should be used. If the process-specific SOTR is applied instead, it yields the energy consumption of a (theoretical) system with 1 h of hydraulic retention time.
These parameters are sufficient to assess the effectiveness and feasibility of using this technology but not to describe the process itself. It should be mentioned that vortices are among the least understood phenomena in fluid dynamics. Therefore, a lot of research efforts are invested in this direction. One of the main challenges in finding the general laws and rules of vortices in fluid dynamics is that there are always variations in the geometric boundary conditions, which influence the development of vortices and significantly influence their formation and dynamics. Thus, it is reasonable to assume that a free-surface vortex (FSV) cannot be considered analogously to a laboratory-type confined one. However, it was shown by Mulligan et al.28 for the Taylor-Couette flow (TCF) that if the air-core of the FSV is considered as a virtual inner cylinder rotating at the same speed as the air core, both can be treated similarly. By doing so, equations that represent the free-surface vortex flow field can be substituted with the angular velocity conditions of the virtual cylinder, resulting in equations for the TCF system. It was also demonstrated that if the rotation speed of an imaginary cylinder is increased, at some point, Taylor-like vortices28 appear as a secondary flow field and then disappear when approaching the walls.
After it was shown by Niemeijr29 that it is possible to obtain three different types of water vortices in a Schauberger funnel (twisted, straight, and restricted) (Figure 1 and Figure 2), which are characterized by other hydraulic parameters, Donepudi24 used the same approach as Mulligan et al.28 to simulate vortex regimes using computational fluid dynamics (CFD) and thereby analyze the organization of their flow field to understand the underlying physical mechanisms. The system is very turbulent, and the secondary flow field is very unstable and is characterized by the appearance of a large number of Taylor-like vortices. Gas transport from the gas phase into the liquid phase is governed by diffusion, advection, and reaction. Therefore, to increase the efficiency of this process, it is necessary either to increase the gas concentration gradient or the volumetric motion of the liquid. The latter directly depends on the turbulence of the system in the form of Taylor-like vortices, which facilitate the transport of saturated fluid elements from the interface into the bulk liquid. In another work on this topic9, the main parameters for different vortex regimes, such as the water flow rate, KLa20, and SOTR, were compared. This study showed great promise for this technology because the system enables very fast gas transfer compared to other methods that are used for water aeration.
The purpose of this article is to provide and demonstrate this method for creating different water vortex regimes in hyperbolic Schauberger funnels (small: 26 cm high and 15 cm top diameter; medium: 94 cm high and 30 cm top diameter; large: 153 cm high and 59 cm top diameter) with the goal of efficient water aeration.

<table><tbody><tr><td>1-/2-channel transmitter</td><td>Endress+Hauser</td><td>CM442</td><td>Data logger</td></tr><tr><td>Control valve</td><td>+GF+</td><td>625DN20</td><td>Typ514</td></tr><tr><td>Data Logger</td><td>Endress+Hauser</td><td>CM442</td><td>Liquiline</td></tr><tr><td>Fiber Optic Oxygen Transmitter</td><td>PreSens</td><td>SACN0002000005</td><td>Fibox 3</td></tr><tr><td>Glass Elbow Connector</td><td>Custom made</td><td>-</td><td>Adapter for the pipeline</td></tr><tr><td>Groundwater pump</td><td>SAER</td><td>3637899</td><td>H/150</td></tr><tr><td>Laptop</td><td>any</td><td>any</td><td>Windows 10 or higher</td></tr><tr><td>Large glass funnel</td><td>Custom made</td><td>-</td><td>94 cm high</td></tr><tr><td>Oxygen Calculator</td><td>PreSens</td><td>v. 3.1.1</td><td>Software</td></tr><tr><td>Oxygen Sensor Spots</td><td>PreSens</td><td>NAU-D5-YOP</td><td>SP-PSt3</td></tr><tr><td>pH connector</td><td>Custom made</td><td>-</td><td>Adapter for the pH probe</td></tr><tr><td>pH sensor</td><td>Endress+Hauser</td><td>CPS11</td><td>Orbisint CPS11</td></tr><tr><td>Polymer Optical Fiber</td><td>PreSens</td><td>POF-L2.5-2SMA</td><td>OXY-1 SMA</td></tr><tr><td>Rubber gasket</td><td>ERIKS</td><td>11535207</td><td>141x197x2mm</td></tr><tr><td>Rubber gasket</td><td>ERIKS</td><td>12252766</td><td>273x340x3mm</td></tr><tr><td>Small glass funnel</td><td>Custom made</td><td>-</td><td>26 cm high</td></tr><tr><td>Water flow meter</td><td>Endress+Hauser</td><td>P7066819000</td><td>Picomag</td></tr><tr><td>Water flow meter</td><td>Kobolt</td><td>5NA15AC34P</td><td>MIK</td></tr><tr><td>Water Temperature Connector</td><td>PreSens</td><td>-</td><td>Pt100</td></tr></tbody></table>

preparation of free-surface hyperbolic water vortices

Free surface vortices are present in industry in flow regulation, energy dissipation, and energy generation. Although investigated extensively, detailed experimental data regarding free surface vortices are lacking, particularly regarding the turbulence at the interface. The present paper reports on a special type of free surface vortex first proposed by Walter Schauberger in the 1960s that has an oxygen volumetric mass transfer coefficient exceeding the value of similar systems. This special type of vortex forms in a hyperbolic funnel. Different stable regimes can be stabilized with different hydraulic characteristics. Other advantages of this technology are its energy efficiency, simple design, and scalability. The flow in this hyperbolic funnel is characterized by strong turbulence and an increased surface area of the air-water interface. The local pressure strongly varies along the surface, resulting in a pronounced wavey air-water boundary layer. Due to the helical flow, these perturbations move inward, pulling the boundary layer with them. The resultant pressure gradient draws a certain air volume into the water vortex. The construction of the basic hyperbolic funnel setup and operational examples, including high-speed visualization for three different stable regimes, are presented in this work.

The water vortex in the Schauberger hyperbolic funnel is formed in different regimes (twisted, straight, and restricted) (Figure 1). As a result, the water is enriched with atmospheric oxygen, and oxidation of chemical species in the water is fostered. The system does not require energy except for pumping water into the upper part of the hyperbolic funnel.
The twisted regime has a double-helix shape and the largest interface between water and air. For its creation, it is necessary to apply an average water flow (75-78 L/h for the small funnel, 1,194-1,218 L/h for the medium funnel, and 4,834-5,032 L/h for the large funnel). Its height in the upper cylindrical part of the funnel should not be more than 2 cm for the small funnel, 7 cm for the medium funnel, and 16 cm for the large funnel.
The straight regime has a smooth straight shape and a smaller interface between water and air. This regime requires maximum water flow (93-100 L/h for the small funnel, 1,314-1,338 L/h for the medium funnel, and 5,102-5,289 L/h for the large funnel). Its height can reach the cover for all the funnels.
Depending on the water level, the restricted regime can take the form of both twisted and straight vortices. However, the peculiarity of this regime is that its length changes depending on the application of back pressure, unlike in the previous modes, for which no pressure is applied. It is also formed at the top of the funnel; however, with increasing back pressure, its tail begins to shorten, and the vortex gradually disappears from the bottom part. Its water flow is extremely small (58-70 L/h for the small funnel, 882-936 L/h for the medium funnel, and 2,351-2,634 L/h for the large funnel), and its height can be both minimal and maximal depending on the funnel geometry.
The different regimes can be stabilized and transformed into each other depending on the water flow rate, back pressure, and system geometry. Parameters such as the water flow rate, oxygen volumetric mass transfer coefficient, and standard oxygen transfer rate characterize the aeration efficiency. It can be seen that for the twisted vortex with a low water flow rate, the KLa20 was the highest (Figure 4), several times higher than the KLa20 for straight and restricted regimes and dozens of times higher than the same indicator for conventional systems, which are also used for the aeration of lakes and rivers (Air Jet, Impeller, Paddle) and are much more energy intensive. With further increases in water flow, the KLa20 gradually decreased, but the water level, that is, the volume of water in the system, increased. After some threshold value, the twisted regime switched to the straight regime. For each regime, there were stationary conditions when their volume and hydraulic parameters do not change.
However, when comparing similar regimes for small, medium, and large funnels, the differences between the systems&#39; water flow rates and volumes were significant. However, at the same time, the ratios of the KLa20 values did not change much. The maximum values of 83 h-1 for the small funnel, 60 h-1 for the medium funnel, and 79 h-1 for the large funnel were achieved in the twisted regime.
At the same time, when the KLa20 decreased with increasing water flow, the MRT increased, indicating that the water took more time to pass through the funnel, as described in detail by Donepudi24. However, as for KLa20, the value of MRT was approximately the same for the twisted and straight regimes in different funnels. The MRT varied from 10 s to 43 s for the small funnel, from 14 s to 30 s for the medium funnel, and from 24 s to 43 s for the large one (Table 1).
<img alt="Figure 1" class="xfigimg" src="/files/ftp_upload/64516/64516fig01.jpg" /> 
Figure 1: Water vortex regimes in a 26 cm high glass hyperbolic Schauberger funnel. (A) Twisted (75 L/h), (B) straight (100 L/h), (C) restricted (70 L/h). <a href="https://jove.unicartagenaproxy.elogim.com/files/ftp_upload/64516/64516fig01large.jpg" target="_blank">Please click here to view a larger version of this figure.</a>
<img alt="Figure 2" class="xfigimg" src="/files/ftp_upload/64516/64516fig02.jpg" /> 
Figure 2: Water vortex regimes in a 94 cm high glass hyperbolic Schauberger funnel. (A) Twisted (1,194 L/h), (B) straight (1,314 L/h), (C) restricted (882 L/h). <a href="https://jove.unicartagenaproxy.elogim.com/files/ftp_upload/64516/64516fig02large.jpg" target="_blank">Please click here to view a larger version of this figure.</a>
<img alt="Figure 3" class="xfigimg" src="/files/ftp_upload/64516/64516fig03.jpg" /> 
Figure 3: Sketch of the setup used for the experiments described in protocol steps 3.1-3.3. (1) Groundwater pump; (2) control valve; (3) water flow meter; (4, 5) polymer optical fibers for DO detection; (6, 7) pH probes; (8) temperature sensor; (9) syringe with tracer; (10) valve; (11) Schauberger hyperbolic funnel; (12) fiber-optic oxygen transmitter; (13) laptop; (14) data logger; (15) clamp; (16) water drain. <a href="https://jove.unicartagenaproxy.elogim.com/files/ftp_upload/64516/64516fig03large.jpg" target="_blank">Please click here to view a larger version of this figure.</a>
<img alt="Figure 4" class="xfigimg" src="/files/ftp_upload/64516/64516fig04.jpg" /> 
Figure 4: Photo of the large funnel setup. (1) Groundwater reservoir; (2) water pump; (3) water flow meter; (4) syringe with tracer; (5, 6) glass adapters with the oxygen sensor spot; (7), (8) pH probes; (9) Schauberger hyperbolic funnel; (10) water drain. <a href="https://jove.unicartagenaproxy.elogim.com/files/ftp_upload/64516/64516fig04large.jpg" target="_blank">Please click here to view a larger version of this figure.</a>
<table fo:font-size="8px">
	<tbody>
		<tr>
			<td>Funnel</td>
			<td>Regime</td>
			<td>&#966; (L/h)</td>
			<td>HRT (s)</td>
			<td>MRT (s)</td>
			<td>KLa20 (h-1)</td>
			<td>V (L)</td>
			<td>Level (cm)</td>
			<td>Cin (mg/L)</td>
			<td>Cout (mg/L)</td>
			<td>SOTR (g O2/h)</td>
			<td>SAE (g O2/kWh)</td>
		</tr>
		<tr>
			<td rowspan="6">Small</td>
			<td rowspan="2">Twisted</td>
			<td>75</td>
			<td>10</td>
			<td>15</td>
			<td>83</td>
			<td>0.2</td>
			<td>0.5</td>
			<td>0.0</td>
			<td>1.8</td>
			<td>0.2</td>
			<td>2801</td>
		</tr>
		<tr>
			<td>78</td>
			<td>20</td>
			<td>24</td>
			<td>41</td>
			<td>0.4</td>
			<td>2</td>
			<td>0.0</td>
			<td>1.9</td>
			<td>0.2</td>
			<td>2932</td>
		</tr>
		<tr>
			<td rowspan="2">Straight</td>
			<td>93</td>
			<td>31</td>
			<td>24</td>
			<td>25</td>
			<td>0.8</td>
			<td>4</td>
			<td>0.0</td>
			<td>1.8</td>
			<td>0.2</td>
			<td>2688</td>
		</tr>
		<tr>
			<td>100</td>
			<td>43</td>
			<td>32</td>
			<td>18</td>
			<td>1.2</td>
			<td>6</td>
			<td>0.0</td>
			<td>1.7</td>
			<td>0.2</td>
			<td>2635</td>
		</tr>
		<tr>
			<td rowspan="2">Restricted</td>
			<td>58</td>
			<td>18</td>
			<td>23</td>
			<td>14</td>
			<td>0.3</td>
			<td>1</td>
			<td>0.0</td>
			<td>0.6</td>
			<td>0.0</td>
			<td>872</td>
		</tr>
		<tr>
			<td>70</td>
			<td>53</td>
			<td>31</td>
			<td>2</td>
			<td>1.0</td>
			<td>5</td>
			<td>0.0</td>
			<td>0.3</td>
			<td>0.0</td>
			<td>459</td>
		</tr>
		<tr>
			<td rowspan="6">Medium</td>
			<td rowspan="2">Twisted</td>
			<td>1194</td>
			<td>14</td>
			<td>13</td>
			<td>60</td>
			<td>4.5</td>
			<td>2</td>
			<td>0.0</td>
			<td>1.8</td>
			<td>2.4</td>
			<td>784</td>
		</tr>
		<tr>
			<td>1218</td>
			<td>19</td>
			<td>19</td>
			<td>37</td>
			<td>6.3</td>
			<td>5</td>
			<td>0.0</td>
			<td>1.6</td>
			<td>2.1</td>
			<td>667</td>
		</tr>
		<tr>
			<td rowspan="2">Straight</td>
			<td>1314</td>
			<td>29</td>
			<td>29</td>
			<td>18</td>
			<td>10.7</td>
			<td>11</td>
			<td>0.0</td>
			<td>1.2</td>
			<td>1.8</td>
			<td>509</td>
		</tr>
		<tr>
			<td>1338</td>
			<td>30</td>
			<td>31</td>
			<td>18</td>
			<td>11.0</td>
			<td>11.7</td>
			<td>0.0</td>
			<td>1.2</td>
			<td>1.8</td>
			<td>500</td>
		</tr>
		<tr>
			<td rowspan="2">Restricted</td>
			<td>882</td>
			<td>21</td>
			<td>24</td>
			<td>17</td>
			<td>5.1</td>
			<td>3</td>
			<td>0.0</td>
			<td>0.9</td>
			<td>0.8</td>
			<td>348</td>
		</tr>
		<tr>
			<td>936</td>
			<td>37</td>
			<td>36</td>
			<td>5</td>
			<td>9.7</td>
			<td>9</td>
			<td>0.0</td>
			<td>0.5</td>
			<td>0.4</td>
			<td>180</td>
		</tr>
		<tr>
			<td rowspan="6">Large</td>
			<td rowspan="2">Twisted</td>
			<td>4834</td>
			<td>24</td>
			<td>23</td>
			<td>79</td>
			<td>32</td>
			<td>11</td>
			<td>0.7</td>
			<td>4.1</td>
			<td>22.9</td>
			<td>1113</td>
		</tr>
		<tr>
			<td>5032</td>
			<td>34</td>
			<td>26</td>
			<td>52</td>
			<td>48</td>
			<td>16</td>
			<td>0.6</td>
			<td>4.0</td>
			<td>22.6</td>
			<td>1054</td>
		</tr>
		<tr>
			<td rowspan="2">Straight</td>
			<td>5102</td>
			<td>38</td>
			<td>29</td>
			<td>31</td>
			<td>54</td>
			<td>19.5</td>
			<td>0.7</td>
			<td>3.0</td>
			<td>15.0</td>
			<td>690</td>
		</tr>
		<tr>
			<td>5289</td>
			<td>43</td>
			<td>30</td>
			<td>19</td>
			<td>64</td>
			<td>22.5</td>
			<td>0.6</td>
			<td>2.3</td>
			<td>10.8</td>
			<td>479</td>
		</tr>
		<tr>
			<td rowspan="2">Restricted</td>
			<td>2351</td>
			<td>58</td>
			<td>43</td>
			<td>16</td>
			<td>38</td>
			<td>7</td>
			<td>0.6</td>
			<td>2.6</td>
			<td>5.5</td>
			<td>557</td>
		</tr>
		<tr>
			<td>2634</td>
			<td>95</td>
			<td>50</td>
			<td>7</td>
			<td>70</td>
			<td>19</td>
			<td>0.6</td>
			<td>2.0</td>
			<td>4.2</td>
			<td>380</td>
		</tr>
	</tbody>
</table>
Table 1: Basic hydraulic characteristics and aeration efficiency parameters for small (Figure 1), medium (Figure 2), and large funnels.&#160;

Watch this Scientific Journal Video about Preparation of Free-Surface Hyperbolic Water Vortices at JoVE.com

Preparation of Free-Surface Hyperbolic Water Vortices

This paper describes how three different water vortex regimes in a hyperbolic Schauberger funnel can be created, their most important characteristics, and how associated parameters such as the oxygen transfer rates can be calculated.

Free surface vortices are present in industry in flow regulation, energy dissipation, and energy generation. Although investigated extensively, detailed ...

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2.4K Views.  Wetsus - Centre of Excellence for Sustainable Water Technology. This paper describes how three different water vortex regimes in a hyperbolic Schauberger funnel can be created, their most important characteristics, and how associated parameters such as the oxygen transfer rates can be calculated. 

Video: Preparation of Free-Surface Hyperbolic Water Vortices

High-speed Particle Image Velocimetry Near Surfaces

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Common PIV investigations measure two-component velocities in a plane at a few frames per second. However, recent developments in instrumentation have facilitated high-frame rate (&gt; 1 kHz) measurements capable of resolving transient flows with high temporal resolution. Therefore, high-frame rate measurements have enabled investigations on the evolution of the structure and dynamics of highly transient flows. These investigations play a critical role in understanding the fundamental physics of complex flows.
A detailed description for performing high-resolution, high-speed planar PIV to study a transient flow near the surface of a flat plate is presented here. Details for adjusting the parameter constraints such as image and recording properties, the laser sheet properties, and processing algorithms to adapt PIV for any flow of interest are included.

A procedure for studying transient flows near boundaries using high-resolution, high-speed particle image velocimetry (PIV) is described here. PIV is a non-intrusive measurement technique applicable to any optically accessible flow by optimizing several parameter constraints such as the image and recording properties, the laser sheet properties, and analysis algorithms.

Multi-dimensional and transient flows play a key role in many areas of science, engineering, and health sciences but are often not well understood. The ...

The Preparation of Electrohydrodynamic Bridges from Polar Dielectric Liquids

Horizontal and vertical liquid bridges are simple and powerful tools for exploring the interaction of high intensity electric fields (8-20 kV/cm) and polar dielectric liquids. These bridges are unique from capillary bridges in that they exhibit extensibility beyond a few millimeters, have complex bi-directional mass transfer patterns, and emit non-Planck infrared radiation. A number of common solvents can form such bridges as well as low conductivity solutions and colloidal suspensions. The macroscopic behavior is governed by electrohydrodynamics and provides a means of studying fluid flow phenomena without the presence of rigid walls. Prior to the onset of a liquid bridge several important phenomena can be observed including advancing meniscus height (electrowetting), bulk fluid circulation (the Sumoto effect), and the ejection of charged droplets (electrospray). The interaction between surface, polarization, and displacement forces can be directly examined by varying applied voltage and bridge length. The electric field, assisted by gravity, stabilizes the liquid bridge against Rayleigh-Plateau instabilities. Construction of basic apparatus for both vertical and horizontal orientation along with operational examples, including thermographic images, for three liquids (e.g., water, DMSO, and glycerol) is presented.

Horizontal and vertical electrohydrodynamic liquid bridges are simple and powerful tools for exploring the interaction of high intensity electric fields and polar dielectric liquids. The construction of basic apparatus and operational examples, including thermographic images, for three liquids (e.g., water, DMSO, and glycerol) is presented.

Horizontal and vertical liquid bridges are simple and powerful tools for exploring the interaction of high intensity electric fields (8-20 kV/cm) and ...

Visualization of High Speed Liquid Jet Impaction on a Moving Surface

Two apparatuses for examining liquid jet impingement on a high-speed moving surface are described: an air cannon device (for examining surface speeds between 0 and 25 m/sec) and a spinning disk device (for examining surface speeds between 15 and 100 m/sec). The air cannon linear traverse is a pneumatic energy-powered system that is designed to accelerate a metal rail surface mounted on top of a wooden projectile. A pressurized cylinder fitted with a solenoid valve rapidly releases pressurized air into the barrel, forcing the projectile down the cannon barrel. The projectile travels beneath a spray nozzle, which impinges a liquid jet onto its metal upper surface, and the projectile then hits a stopping mechanism. A camera records the jet impingement, and a pressure transducer records the spray nozzle backpressure. The spinning disk set-up consists of a steel disk that reaches speeds of 500 to 3,000 rpm via a variable frequency drive (VFD) motor. A spray system similar to that of the air cannon generates a liquid jet that impinges onto the spinning disc, and cameras placed at several optical access points record the jet impingement. Video recordings of jet impingement processes are recorded and examined to determine whether the outcome of impingement is splash, splatter, or deposition. The apparatuses are the first that involve the high speed impingement of low-Reynolds-number liquid jets on high speed moving surfaces. In addition to its rail industry applications, the described technique may be used for technical and industrial purposes such as steelmaking and may be relevant to high-speed 3D printing.

Two experimental devices for examining liquid jet impingement on a high-speed moving surface are described: an air cannon device and a spinning disk device. The apparatuses are used to determine optimal approaches to the application of liquid friction modifier (LFM) onto rail tracks for top-of-rail friction control.

Two apparatuses for examining liquid jet impingement on a high-speed moving surface are described: an air cannon device (for examining surface speeds ...

Investigating the Three-dimensional Flow Separation Induced by a Model Vocal Fold Polyp

The fluid-structure energy exchange process for normal speech has been studied extensively, but it is not well understood for pathological conditions. Polyps and nodules, which are geometric abnormalities that form on the medial surface of the vocal folds, can disrupt vocal fold dynamics and thus can have devastating consequences on a patient&#39;s ability to communicate. Our laboratory has reported particle image velocimetry (PIV) measurements, within an investigation of a model polyp located on the medial surface of an in&#160;vitro driven vocal fold model, which show that such a geometric abnormality considerably disrupts the glottal jet behavior. This flow field adjustment is a likely reason for the severe degradation of the vocal quality in patients with polyps. A more complete understanding of the formation and propagation of vortical structures from a geometric protuberance, such as a vocal fold polyp, and the resulting influence on the aerodynamic loadings that drive the vocal fold dynamics, is necessary for advancing the treatment of this pathological condition. The present investigation concerns the three-dimensional flow separation induced by a wall-mounted prolate hemispheroid with a 2:1 aspect ratio in cross flow, i.e. a model vocal fold polyp, using an oil-film visualization technique. Unsteady, three-dimensional flow separation and its impact of the wall pressure loading are examined using skin friction line visualization and wall pressure measurements.

Vocal fold polyps can disrupt vocal fold dynamics and thus can have devastating consequences on a patient&#39;s ability to communicate. Three-dimensional flow separation induced by a wall-mounted model polyp and its impact on the wall pressure loading are examined using particle image velocimetry, skin friction line visualization, and wall pressure measurements.

The fluid-structure energy exchange process for normal speech has been studied extensively, but it is not well understood for pathological conditions. ...

Bioengineering

Experimental Investigation of Secondary Flow Structures Downstream of a Model Type IV Stent Failure in a 180&#176; Curved Artery Test Section

The arterial network in the human vasculature comprises of ubiquitously present blood vessels with complex geometries (branches, curvatures and tortuosity). Secondary flow structures are vortical flow patterns that occur in curved arteries due to the combined action of centrifugal forces, adverse pressure gradients and inflow characteristics. Such flow morphologies are greatly affected by pulsatility and multiple harmonics of physiological inflow conditions and vary greatly in size-strength-shape characteristics compared to non-physiological (steady and oscillatory) flows 1 - 7.
Secondary flow structures may ultimately influence the wall shear stress and exposure time of blood-borne particles toward progression of atherosclerosis, restenosis, sensitization of platelets and thrombosis 4 - 6, 8 - 13. Therefore, the ability to detect and characterize these structures under laboratory-controlled conditions is precursor to further clinical investigations.
A common surgical treatment to atherosclerosis is stent implantation, to open up stenosed arteries for unobstructed blood flow. But the concomitant flow perturbations due to stent installations result in multi-scale secondary flow morphologies 4 - 6. Progressively higher order complexities such as asymmetry and loss in coherence can be induced by ensuing stent failures vis-&#224;-vis those under unperturbed flows 5. These stent failures have been classified as &#34;Types I-to-IV&#34; based on failure considerations and clinical severity 14.
This study presents a protocol for the experimental investigation of the complex secondary flow structures due to complete transverse stent fracture and linear displacement of fractured parts (&#34;Type IV&#34;) in a curved artery model. The experimental method involves the implementation of particle image velocimetry (2C-2D PIV) techniques with an archetypal carotid artery inflow waveform, a refractive index matched blood-analog working fluid for phase-averaged measurements 15 - 18. Quantitative identification of secondary flow structures was achieved using concepts of flow physics, critical point theory and a novel wavelet transform algorithm applied to experimental PIV data 5, 6, 19 - 26.

Stent implants in stenosed arterial curvatures are prone to "Type IV" failures involving the complete transverse fracture of stents and linear displacement of the fractured parts. We present a protocol for detection of secondary flow (vortical) structures in a curved artery model, downstream of clinically relevant "Type IV" stent failures.

The arterial network in the human vasculature comprises of ubiquitously present blood vessels with complex geometries (branches, curvatures and ...

Visualization of Flow Field Around a Vibrating Pipeline Within an Equilibrium Scour Hole

An experimental method is presented in this paper to facilitate visualization of the detailed flow fields and determination of the near-boundary shear and normal stresses within an equilibrium scour hole induced by a vibrating pipeline. This method involves the implementation of a pipeline vibration system in a straight flume, a time-resolved particle image velocimetry (PIV) system for pipeline displacement tracking and flow fields measurements. The displacement time-series of the vibrating pipeline are obtained by using the cross-correlation algorithms. The steps for processing raw particle laden images obtained by using the time-resolved PIV are described. The detailed instantaneous flow fields around the vibrating pipeline at different vibrating phases are calculated by using a multiple-time-interval cross-correlation algorithm to avoid displacement bias error in the flow regions with a large velocity gradient. By applying the wavelet transform technique, the captured images that have the same vibrating phase are accurately cataloged before the phase-averaged velocity fields are obtained. The key advantages of the flow measurement technique described in this paper are that it has a very high temporal and spatial resolution and can be simultaneously used to obtain the pipeline dynamics, flow fields, and near-boundary flow stresses. By using this technique, more in-depth studies of the 2-dimensional flow field in a complex environment, such as that around a vibrating pipeline, can be conducted to better understand the associated sophisticated scour mechanism.

The goal of the protocol is to enable visualization of the detailed flow fields and determination of the near-boundary shear and normal stresses within an equilibrium scour hole induced by a vibrating pipeline.

An experimental method is presented in this paper to facilitate visualization of the detailed flow fields and determination of the near-boundary shear and ...

Environment

Experimental Investigation of the Flow Structure over a Delta Wing Via Flow Visualization Methods

It is well known that the flow field over a delta wing is dominated by a pair of counter rotating leading edge vortices (LEV). However, their mechanism is not well understood. The flow visualization technique is a promising non-intrusive method to illustrate the complex flow field spatially and temporally. A basic flow visualization setup consists of a high-powered laser and optic lenses to generate the laser sheet, a camera, a tracer particle generator, and a data processor. The wind tunnel setup, the specifications of devices involved, and the corresponding parameter settings are dependent on the flow features to be obtained.
Normal smoke wire flow visualization uses a smoke wire to demonstrate the flow streaklines. However, the performance of this method is limited by poor spatial resolution when it is conducted in a complex flow field. Therefore, an improved smoke flow visualization technique has been developed. This technique illustrates the large-scale global LEV flow field and the small-scale shear layer flow structure at the same time, providing a valuable reference for later detailed particle image velocimetry (PIV) measurement.
In this paper, the application of the improved smoke flow visualization and PIV measurement to study the unsteady flow phenomena over a delta wing is demonstrated. The procedure and cautions for conducting the experiment are listed, including wind tunnel setup, data acquisition, and data processing. The representative results show that these two flow visualization methods are effective techniques for investigating the three-dimensional flow field qualitatively and quantitatively.

Here, we present a protocol to observe unsteady vortical flows over a delta wing using a modified smoke flow visualization technique and investigate the mechanism responsible for the oscillations of the leading-edge vortex breakdown locations.

It is well known that the flow field over a delta wing is dominated by a pair of counter rotating leading edge vortices (LEV). However, their mechanism is ...

Impacts of Free-falling Spheres on a Deep Liquid Pool with Altered Fluid and Impactor Surface Conditions

Vertical impacts of spheres on clean water have been the subject of numerous water entry investigations characterizing cavity formation, splash crown ascension and Worthington jet stability. Here, we establish experimental protocols for examining splash dynamics when smooth free-falling spheres of varying wettability, mass, and diameter impact the free surface of a deep liquid pool modified by thin penetrable fabrics and liquid surfactants. Water entry investigations provide accessible, easily assembled and executed experiments for studying complex fluid mechanics. We present herein a tunable protocol for characterizing splash height, flow separation metrics, and impactor kinematics, and representative results which might be acquired if reproducing our approach. The methods are applicable when characteristic splash dimensions remain below approximately 0.5 m. However, this protocol may be adapted for greater impactor release heights and impact velocities, which augurs well for translating results to naval and industry applications.

This protocol demonstrates the basic experimental configuration for water entry experiments with free-falling spheres. Methods for the alteration of liquid surface with penetrable fabrics, the preparation of chemically non-wetting spheres, and steps for splash visualization and data extraction are discussed.

Vertical impacts of spheres on clean water have been the subject of numerous water entry investigations characterizing cavity formation, splash crown ...

Flow Visualization in a Water Tunnel: Observing the Leading-edge Vortex Over a Delta Wing

Source: Jose Roberto Moreto, Gustaaf Jacobs and Xiaofeng Liu, Department of Aerospace Engineering, San Diego State University, San Diego, California
The delta wing, shown in Figure 1D, is a popular design in high-speed airplanes due to its superb performance in transonic and supersonic flight regimes. This type of wing has a small aspect ratio and high sweep angle, which reduces drag at high subsonic, transonic and supersonic flight regimes. The aspect ratio is defined as the wing span divided by the average chord <img align="middle" src="/files/ftp_upload/10459/10459eq1a.jpg" />.
An important advantage of the delta wing is its high stall angle. The stall of a delta wing is delayed compared to the stall of a high aspect ratio wing. This is because the lift of a delta wing is enhanced by the leading-edge vortex over the wing.
An effective way to observe this vortex flow phenomenon and study the vortex breakdown in a delta wing is by visualizing the flow in a water tunnel. By injecting dye in the flow surrounding a model from dye ports on the leading-edge, the vortex development and breakdown can be observed and its position measured. The data can also be used to estimate the stall angle.
<img src="/files/ftp_upload/10459/10459fig1.jpg" />
Figure 1. Typical wing planform shapes: A) Rectangular, with constant chord along span, B) elliptical, C) tapered, with variable chord along the span, and D) delta wing, an aft-swept wing with zero taper ratio.

Flow in a Water Tunnel: Leading-edge Vortex over a Delta Wing

Source: Jose Roberto Moreto, Gustaaf Jacobs and Xiaofeng Liu, Department of Aerospace Engineering, San Diego State University, San Diego, California
The ...

JoVE Science Education

Aeronautical Engineering

Visualization of Flow Past a Bluff Body

Source: Ricardo Mejia-Alvarez, Hussam Hikmat Jabbar and Mahmoud N. Abdullatif, Department of Mechanical Engineering, Michigan State University, East Lansing, MI
Owing to the non-linear nature of its governing laws, fluid motion induces complicated flow patterns. Understanding the nature of these patterns has been the subject of intense scrutiny for centuries. Although personal computers and supercomputers are extensively used to deduce fluid flow patterns, their capabilities are still insufficient to determine the exact flow behavior for complex geometries or highly inertial flows (e.g. when momentum dominates over viscous resistance). With this in mind, a multitude of experimental techniques to make flow patterns evident have been developed that can reach flow regimes and geometries inaccessible to theoretical and computational tools.
This demonstration will investigate fluid flow around a bluff body. A bluff body is an object that, due to its shape, causes separated flow over most of its surface. This is in contrast to a streamlined body, like an airfoil, which is aligned in the stream and causes less flow separation. The purpose of this study is to use hydrogen bubbles as a method of visualizing flow patterns. The hydrogen bubbles are produced via electrolysis using a DC power source by submerging its electrodes in the water. Hydrogen bubbles are formed in the negative electrode, which needs to be a very fine wire to ensure that the bubbles remain small and track fluid motion more effectively. This method is suitable for steady and unsteady laminar flows, and is based on the basic flow lines that describe the nature of the flow around objects. [1-3]
This paper focuses on describing the implementation of the technique, including details about the equipment and its installation. Then, the technique is used to demonstrate the use of two of the basics flow lines to characterize the flow around a circular cylinder. These flow lines are used to estimate some important flow parameters like flow velocity and the Reynolds number, and to determine flow patterns.

Flow Around a Bluff Body, Bubbles and Von Karman Vortex Street

Source: Ricardo Mejia-Alvarez, Hussam Hikmat Jabbar and Mahmoud N. Abdullatif, Department of Mechanical Engineering, Michigan State University, East ...