Chaos, Turbulence and its Transition Process in Marangoni Convection-Exp (Marangoni-Exp) - 09.17.14

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ISS Science for Everyone

Science Objectives for Everyone
Marangoni convection is the flow driven by the presence of a surface tension gradient which can be produced by temperature difference at a liquid/gas interface. The convection in liquid bridge of silicone oil is generated by heating the one disc higher than the other. Scientists are observing flow patterns of how fluids move to learn more about how heat is transferred in microgravity.

Science Results for Everyone

Marangoni convection, which is flow driven by a surface tension gradient produced by temperature difference at a liquid/gas interface, is helping scientists learn how heat is transferred in microgravity. This investigation provided data on transition to oscillatory flow in a hydrothermal wave and applied several flow visualization techniques to reveal three-dimensional flow patterns that appear after the transition. Researchers observed that flow patterns change at a critical temperature difference and that surface boundary conditions determine whether fluid movement is uniform or unstable. Understanding the nature of Marangoni convection will support various micro-fluid handling techniques such as DNA examination and design of high-performance heat exchangers and pipes in space and on Earth.



The following content was provided by Hiroshi Kawamura, Ph.D., Koichi Nishino, and is maintained in a database by the ISS Program Science Office.
Information provided courtesy of the Japan Aerospace and Exploration Agency (JAXA).

Experiment Details

OpNom

Principal Investigator(s)

  • Hiroshi Kawamura, Ph.D., Tokyo University of Science, Chiba, Japan
  • Koichi Nishino, Yokohama National University, Yokohama, Japan

  • Co-Investigator(s)/Collaborator(s)
  • Mitsuru Ohnishi, Innovative Technology Research Center, Tokyo, Japan
  • Masato Sakurai, Innovative Technology Research Center, Tokyo, Japan
  • Ichiro Ueno, Tokyo University of Science, Yamazaki, Japan
  • Masahiro Kawaji, University of Toronto, Toronto, Ontario, Canada

  • Developer(s)
    IHI Aerospace Company, Ltd., Tomioka, , Japan

    Japan Aerospace Exploration Agency (JAXA), Tsukuba, , Japan

    Sponsoring Space Agency
    Japan Aerospace Exploration Agency (JAXA)

    Sponsoring Organization
    Information Pending

    Research Benefits
    Information Pending

    ISS Expedition Duration
    April 2008 - September 2013

    Expeditions Assigned
    17,18,19/20,25/26,27/28,29/30,31/32,33/34,35/36

    Previous ISS Missions
    Increment 17 was the first mission for Marangoni.

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    Experiment Description

    Research Overview

    • The objective of scientific reaserch on Marangoni convection utilizing microgravity is to make clear the flow transition phenomena from steady to osicillatory, chaotic, and finally turburent flows. Therefore, it is important to understand an underlying principal of Marangoni convection. The finding and knowledge obtained through space experiment is applied to industrial processes as well as fluid physics.


    • JAXA has been carrying out four Marangoni experiments to fully understand Marangoni convection in microgravity on board the ISS. Fundamental questions regarding Marangoni Convection are as follows; (1) when and how are the onset of unsteady (or oscillatory) convection determined, (2) What are the characteristics of unsteady and three-dimensional flow, and temperature fields? (3) What are the mechanisms that are responsible for the formation of particle accumulation structures (PASs)? Answering these questions through space experiment should contribute to the better understanding of Marangoni convection. It will complete in 2015.


    • On the ground, we can see the only several millimeters liquid bridge because surface tension cannot support its self weight due to gravity. On the other hand, microgravity conditions provide us several advantages as follows; (1) Large and long liquid bridges can be formed, (2) Pure and ideal Marangoni convection can be observed. So, space experiment are expected to be solved the whole picture of Marangoni convection. This contributes to advance of basic science of a fluid physics directly. Moreover, the knowledge of Marangoni convection must be useful to improve the industrial process such as semiconductors, optical materials, bio materials, welding and micro/nano technologies and to increase the efficiency of thermal devices (i.e. heat pipe, evaporators/condensers).

    Description
    Marangoni flow is categorized in the natural convection same as buoyancy convection caused by density difference. A trait of Marangoni convection is a surface-tension-driven flow which driving force is localized at the only surface. Surface tension is the characteristic of a liquid in which it forms a layer at its surface so that this surface covers as small an area as possible. One can see the coin floating on the water. Surface tension is the force to be keeping the heavier coin on. In general, surface tension becomes strong with decreasing temperature. When a temperature difference exists along surface, the surface is pulled toward low temperature region. The surface tension difference is also produced under existing concentration distribution. May have heard or seen "tears of wine". It can be caused by Marangoni effect under concentration difference near the meniscus. Its effect was named after Italian physicist Calro Marangoni who mainly studied surface phenomena in 19th century.

    Such a phenomenon is often observed in everyday life. For example, oil in a pan heated from center moves to peripheral side. Oil floating on water immediately moves when a surfactant (e.g. detergent) drops onto a part of the oil because of the imbalance in the surface tension. The detergent caused the center to have a lower surface tension. On the other hand, the outside has a higher surface tension, so the center and the oil were pulled out in all directions to equalize the surface tension. These phenomena are resulting from Marangoni effect.

    Moreover, Marangoni convection affects the quality of grown crystal such as semiconductors, optical materials or bio materials. Therefore, it is important to understand an underlying principal and nature of Marangoni convection. The finding and knowledge obtained through space experiment is applied to industrial progression as well as advance of fluid dynamics. A liquid bridge configuration is often employed to investigate Marangoni convection because it is simulated a floating-zone method which is one of the crystal growth technique.

    A liquid bridge (cylindrical liquid column) of silicone oil is formed into a pair of supporting solid disks. The convection is induced by imposing the temperature difference between disks, one end heating and other end cooling. Due to the convective instability, flow transits from laminar to oscillatory, chaos, and turbulence flows one by ones as the driving force increases. Scientists will observe the flow and temperature fields in each stage and investigate the flow transition conditions and processes. Fundamental questions regarding to Marangoni Convection are as follows;

    • What are the conditions that determine the onset of unsteady (or oscillatory) convection in liquid bridge?


    • What are the characteristics of unsteady, three-dimensional flow and temperature fields?


    • What are the mechanisms that are responsible for the formation of dynamic particle accumulation structures (PASs)?
    Answering these questions should contribute to the better understanding of the instability mechanisms of Marangoni convection.

    Now, why do we need to conduct Marangoni experiment on board the International Space Station (ISS)? On the ground, we can see the only several millimeters liquid bridge because surface tension cannot support its tare weight due to gravity. On the other hand, microgravity conditions provide us strong advantages as follows;
    • Large and long liquid bridges can be formed.


    • Therefore, high Marangoni numbers can be realized.


    • No density-driven convection exists.


    • No gravity-induced deformation of liquid bridge exists.


    • Very long period for experiment can be allotted utilizing the ISS.


    • Quite precise data with a wide range of parameters can be obtained by utilizing these merits in space.


    At the same time, a liquid bridge is very sensitive against even week vibration (called g-jitter) in the ISS because the liquid is not contained and is sustained by the only surface tension between supporting disks. Therefore, Marangoni Experiment is performed during a crew sleeping time (21:30-06:00 GMT) when the g-jitter becomes slightly calm.

    In Marangoni Exp, Marangoni convection occurred in a liquid bridge is observed to make clear the flow transition phenomena resulting from a fluid instability. A silicone oil with a viscosity of 10 cSt(10 mm2/s), which is about ten times higher one of water, is employed as working fluid and is suspended between a pair of solid disks (50mm in diameter). Small amount of fine particles is mixed into liquid bridge for flow visualization. One of the disks is heated and another cooled to impose temperature difference on both end of the liquid bridge. The temperature difference is gradually enlarged in order to increase the driving force of a thermocapillary flow (Marangoni flow). The flow transits from steady to oscillatory flow at the certain critical temperature difference. With increasing the temperature difference, the convection becomes more complicated toward turbulent via chaotic flows . These transition processes are observed in detail.

    We employ Fluid Physics Experiment Facility (FPEF) mounted in Ryutai Rack inside KIBO Pressurized Module. Experiment is conducted in combining FPEF and an experiment unique hardware which is exchangeable according to the purpose of investigation and is called "Experiment Cell". FPEF equips several cameras and Infrared Imager for flow and temperature visualizations. Three units of black and white CCD cameras are mounted near the heating disk to observe three dimensional flow pattern through the transparent sapphire disk. This system allows constructing 3-dimensional visualization of flow field using 3D Particle Tracking Velocimetry (3D-PTV) technique. A color CCD camera takes side view of liquid bridge to check the flow pattern and liquid bridge shape. An infrared imager is used to observe dynamic temperature distribution on the liquid bridge surface. Marangoni experiment also uses Image Processing Unit (IPU) and Microgravity Measurement Apparatus (MMA) with accelerometer to measure microgravity environment near the FPEF.

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    Applications

    Space Applications
    The valuable knowledge from Marangoni space experiment is also applicable to the high performance heat exchanger and heat pipe both in the space and on the earth. For future space development, it should be necessary to more efficient and compact thermal management system, no doubt to help its development.

    Earth Applications
    The obtained knowledge on the Marangoni convection is vital for the production of high-quality crystal growth such as semiconductors, optical crystal so on. Since the surface tension is dominant not only under the microgravity but also in the micro-scale, the results obtained on the nature of the Marangoni convection will significantly contribute to various micro-fluid handling techniques in micro-TAS (Micro total analysis system) such as DNA examination and clinical diagnostics.

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    Operations

    Operational Requirements


    Number of experiment: 30 runs

    Downlink of data: (Real-time)

    • Five channel video images from observation cameras


    • Telemetry concerning health & status of equipment and experimental data (e.g. temperatures, pressure)
    • (Non real time)
      • Five channel video play back


      • Acceleration data file
      Return of samples Hard disk drive units recorded high resolution video images

      Operational Protocols
      As preparation for experiment by an ISS crew, the experiment cell is assembled and installed in FPEF. The experiment is operated from Space Station Integration and Promotion Center, Tsukuba Space Center by ground staffs.

      The experiment procedure is as follows;

      (1) Preparation of experiment

    • Starting up FPEF, EC and Image Processing Unit (IPU)


    • Setting of FPEF, observation systems


    • Start of acceleration measurement
    (2) Experiment
    • Liquid bridge formation


    • Adjustment of Volume ratio of liquid bridge


    • Imposing the temperature difference between hot and cold disks to induce convection


    • Video Recording


    • Bubble removal if liquid bridge contains bubble
    (3) Post experiment operation
    • Retrieving liquid bridge


    • Video play back down link and acceleration data files transfer


    • Shut down FPEF, EC and Image Processing Unit (IPU)

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    Results/More Information

    Warmer fluids move toward a cooler, higher surface tension region driven by a process known as thermocapillary force along the free (unbound) surface. Accordingly, convection is induced in fluid, which is called Marangoni convection. Depending on boundary conditions, the flow may be steady and symmetric or become unstable and time-dependent at a certain critical point. The Chaos, Turbulence and its Transition Process in Marangoni Convection (Marangoni-Exp) is designed to identify these critical conditions. In microgravity, scientists were able to form floating silicone oil columns much larger than on Earth allowing for a highly detailed observation of flow and instability within these "liquid bridges". A series of experiments have been carried out from 2008 – 2013 in the Fluid Physics Experiment Facility (FPEF) of the “KIBO” laboratory of the ISS.

    Marangoni-Exps are set up with different oil viscosity and diameter. A series of experimental runs are changed the parameters such as temperature difference between supporting disks, and length for the liquid bridges, thus giving a wide range of aspect ratio (Ar = length over diameter) and volume ration for analysis. Convective flows are observed three-dimensionally by tracking fine tracer particles dispersed in the fluid and using CCD cameras at preset angles; an infrared (IR) camera is also used to see surface temperature distributions of the liquid bridge. Results show that, when critical temperature differences exceed a certain level, a standing-wave (imagine a horizontal liquid surface in a sealed half-filled glass jar tilting very slowly end to end) oscillation appears and that the wavelength is comparable to the length of the liquid bridge. The stable two-dimensional stationary flow pattern is replaced by the standing wave which then is followed by more chaotic flows with multiple vortices traveling from the heated zone toward the cooled zone. These results indicate that perturbations in the flow and temperature field are due to the propagation of simple and complex hydrothermal waves.

    Critical temperature differences (∆Tc), resultant Marangoni number (Mac), which is required for the onset of oscillatory flow, and oscillation frequency are determined for a wide range of aspect ratio and different fluid viscosities over the course of the Marangoni-Exp investigation. As expected, the measured ∆Tc for the more viscous liquid is substantially higher than that for the less viscous one. Some of the experimental results are in good agreement with each other, while others show the similar patterns but are distinctly offset due, perhaps, to different fluid viscosity and the relative size of the liquid bridges (Yano et al., 2011, Kawamura et al., 2012).

    Studying long liquid bridges in space will help scientists to make more accurate predictions of instability onsets which can give rise to different pattern forming instabilities. The floating-zone (liquid bridge) refining technique is used extensively to produce extremely high purity crystals by the semiconductor and rare metals industries, and flow disturbance is a major cause for the deterioration of the quality of the crystal grown by this method. Understanding the rheological (deformation and flow of matter) dynamics in liquid bridges is of fundamental interest for many industrial as well as biological processes.

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    Results Publications

      Ueno I, Tanaka S, Kawamura H.  Various flow patterns in thermocapillary convection in half-zone liquid bridge of high prandtl number fluid. Advances in Space Research. 2003 July; 32(2): 143-148. DOI: 10.1016/S0273-1177(03)90244-4.

      Yano T, Nishino K, Kawamura H, Ueno I, Matsumoto S, Ohnishi M, Sakurai M.  Space Experiment on the Instability of Marangoni Convection in Large Liquid Bridge - MEIS-4: Effect of Prandtl Number -. Journal of Physics: Conference Series. 2011; 327. DOI: 10.1088/1742-6596/327/1/012029.

      Kawamura H, Nishino K, Matsumoto S, Ueno I.  Report on Microgravity Experiments of Marangoni Convection Aboard International Space Station. Journal of Heat Transfer. 2012; 134(3): 031005-1 - 031005-13. DOI: 10.1115/1.4005145.

      Yano T, Nishino K, Kawamura H, Ueno I, Matsumoto S, Ohnishi M, Yoda S.  3-D Flow Measurement of Oscillatory Thermocapillary Convection in Liquid Bridge in MEIS. Japan Society of Microgravity Application. 2011; 28(2): 126-132.

      Goto M, Sakagami K, Matsumoto S, Ohkuma H.  Entering "A NEW REALM" of KIBO Payload Operations - Continuous efforts for microgravity experiment environment and lessons learned from real time experiment operations in KIBO. Journal of Physics: Conference Series. 2011; 327(012054): 1-13. DOI: 10.1088/1742-6596/327/1/012054.

      Irikura M, Arakawa Y, Ueno I, Kawamura H.  Effect of ambient fluid flow upon onset of oscillatory thermocapillary convection in half-zone liquid bridge. Microgravity Science and Technology. 2005 March; 16(1-4): 176-180. DOI: 10.1007/BF02945971.

      Nishimura M, Nishimura M, Ueno I, Nishino K, Kawamura H.  3D PTV measurement of oscillatory thermocapillary convection in half-zone liquid bridge. Experiments in Fluids. 2005 January 13; 38(3): 285-290. DOI: 10.1007/s00348-004-0885-0.

      Sato F, Ueno I, Kawamura H, Nishino K, Matsumoto S, Ohnishi M, Sakurai M.  Hydrothermal wave instability in a high-aspect-ratio liquid bridge of Pr >  200. Microgravity Science and Technology. 2013; 25(1): 43-58. DOI: 10.1007/s12217-012-9332-7.

      Abe Y, Ueno I, Kawamura H.  Effect of shape of HZ liquid bridge on particle accumulation structure (PAS). Microgravity Science and Technology. 2007 October; 19(3/4): 84-86. DOI: 10.1007/BF02915760.

      Ueno I, Abe Y, Noguchi K, Kawamura H.  Dynamic particle accumulation structure (PAS) in half-zone liquid bridge – Reconstruction of particle motion by 3-D PTV. Advances in Space Research. 2008 January; 41(12): 2145-2149. DOI: 10.1016/j.asr.2007.08.039.

      Abe Y, Ueno I, Kawamura H.  Dynamic particle accumulation structure due to thermocapillary effect in noncylindrical half-zone liquid bridge. Annals of the New York Academy of Sciences. 2009 April; 1161(1): 240-245. DOI: 10.1111/j.1749-6632.2008.04073.x.

      Ueno I, Kawazoe A, Enomoto H.  Effect of ambient-gas forced flow on oscillatory thermocapillary convection of half-zone liquid bridge. FDMP. 2010; 6(1): 99-108. DOI: 10.3970/fdmp.2010.006.099.

      Yano T, Nishino K, Kawamura H, Ueno I, Matsumoto S, Ohnishi M, Sakurai M.  3-D PTV Measurement of Marangoni Convection in Liquid Bridge in Space Experiment. Experiments in Fluids. 2011; 53(1): 9-20. DOI: 10.1007/s00348-011-1136-9.

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    Ground Based Results Publications

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    ISS Patents

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    Related Publications

      Kudo M, Shiomi J, Ueno I, Amberg G, Kawamura H.  Experiment on multimode feedback control of non-linear thermocapillary convection in a half-zone liquid bridge. Advances in Space Research. 2005; 36(1): 57-63. DOI: 10.1016/j.asr.2005.05.046.

      Ueno I, Tanaka S, Kawamura H.  Oscillatory and Chaotic Thermocapillary Convection in a Half-Zone Liquid Bridge. Physics of Fluids. 2003; 15(2): 408-416. DOI: 10.1063/1.1531993.

      Tanaka S, Kawamura H, Ueno I, Schwabe D.  Flow structure and dynamic particle accumulation in thermocapillary convection in a liquid bridge. Physics of Fluids. 2006; 18(6): 067103-1 - 067103-11. DOI: 10.1063/1.2208289.

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    Related Websites
    The information on this web page was duplicated from the JAXA Experiment Database. The "Brief Research Summary (PAO)" and "Research Summary" are provided by the Office of the ISS Program Scientist.
    Fluid Science Under Microgravity

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    Imagery

    image Fig. 1 Largest liquid bridge of silicone oil formed in Kibo. Image courtesy of JAXA.
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    image Fig.2 Observation method of Marangoni convection (UVP: Ultrasonic Velocity Profiler). Image courtesy of JAXA.
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    image NASA Image: ISS020E048792 - Canadian Space Agency astronaut Robert Thirsk, Expedition 20/21 flight engineer, holds Fluid Physics Experiment Facility/Marangoni Surface (FPEF MS) Core hardware in the Kibo laboratory of the International Space Station.
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    image Nasa Image: ISS018E012248 Sandra Magnus works with the Marangoni experiment mounted to a Maintenance work area (MWS) on Expedition 18.
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