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Effect of Gravity on Electrohydrodynamic Conduction Driven Liquid Film Flow Boiling

机译:重力对电液动力驱动液膜流沸腾的影响

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摘要

Liquid film flow boiling is used in many terrestrial thermal management applications as a heat transport mechanism. However, it suffers in microgravity applications such as spacecraft thermal management because the gravitational body force is not present to facilitate liquid film flow and bubble removal from the heater surface. One way of overcoming these constraints is to use an electrical field to move a liquid film in the absence as well as in the presence of gravity. In this experimental study, electrohydrodynamic conduction pumping is used to rewet the heater surface during liquid film flow boiling. The experiments are performed both terrestrially and onboard a variable-gravity parabolic flight. Terrestrial steady-state results show a maximum superheat reduction of 6 degrees C and a 62% increase in critical heat flux when the electrohydrodynamic pump is moderately activated. The parabolic flight transient results indicate that, although there was an adverse effect of electrohydrodynamic on heater surface temperature at heat flux less than 3.0 W/cm(2) (due to delayed onset of nucleate boiling), heater surface temperatures were actually lowered at higher heat flux due to activation of the electrohydrodynamic conduction pump. The microgravity results onboard the parabolic flights also pave the way for full-scale orbital testing of electrohydrodynamic-driven liquid film flow boiling onboard the International Space Station.
机译:液膜流沸腾在许多地面热管理应用中用作传热机制。但是,由于不存在重力来促进液膜流动和从加热器表面除去气泡,因此在诸如航天器热管理之类的微重力应用中会遇到麻烦。克服这些限制的一种方法是在不存在重力和存在重力的情况下使用电场来使液膜移动。在本实验研究中,在液膜流沸腾过程中,使用电动流体传导泵抽回加热器表面。实验是在地面上以及在可变重力抛物线飞行器上进行的。地面稳态结果显示,当电动液压泵被适度启动时,最大过热降低了6摄氏度,临界热通量增加了62%。抛物线飞行瞬态结果表明,尽管在热通量小于3.0 W / cm(2)时,由于电流体动力学对加热器表面温度有不利影响(由于成核沸腾的延迟发生),但加热器表面温度实际上在较高时降低了。由于电动液力传导泵的激活而产生的热通量。抛物线飞行中的微重力结果也为在国际空间站上沸腾的电动动力驱动的液膜流沸腾的全面轨道测试铺平了道路。

著录项

  • 来源
    《Journal of Thermophysics and Heat Transfer》 |2016年第2期|429-437|共9页
  • 作者单位

    Worcester Polytech Inst, Multi Scale Heat Transfer Lab, Dept Mech Engn, Worcester, MA 01609 USA;

    Worcester Polytech Inst, Dept Mech Engn, Worcester, MA 01609 USA;

    NASA, Goddard Space Flight Ctr, Thermal Technol Dev Lab, Greenbelt, MD 20771 USA;

    NASA, Goddard Space Flight Ctr, Nanotechol Facil, Greenbelt, MD 20771 USA;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);美国《生物学医学文摘》(MEDLINE);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

  • 入库时间 2022-08-18 03:01:17

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