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Study of two-phase flows in reduced gravity.

机译:研究减小重力的两相流。

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摘要

Study of gas-liquid two-phase flows under reduced gravity conditions is extremely important. One of the major applications of gas-liquid two-phase flows under reduced gravity conditions is in the design of active thermal control systems for future space applications. Previous space crafts were characterized by low heat generation within the spacecraft which needed to be redistributed within the craft or rejected to space. This task could easily have been accomplished by pumped single-phase loops or passive systems such as heat pipes and so on. However with increase in heat generation within the space craft as predicted for future missions, pumped boiling two-phase flows are being considered. This is because of higher heat transfer co-efficients associated with boiling heat transfer among other advantages. Two-phase flows under reduced gravity conditions also find important applications in space propulsion as in space nuclear power reactors as well as in many other life support systems of space crafts.;Two-fluid model along with Interfacial Area Transport Equation (IATE) is a useful tool available to predict the behavior of gas-liquid two-phase flows under reduced gravity conditions. It should be noted that considerable differences exist between two-phase flows under reduced and normal gravity conditions especially for low inertia flows. This is because due to suppression of the gravity field the gas-liquid two-phase flows take a considerable time to develop under reduced gravity conditions as compared to normal gravity conditions. Hence other common methods of analysis applicable for fully developed gas-liquid two-phase flows under normal gravity conditions, like flow regimes and flow regime transition criteria, will not be applicable to gas-liquid two-phase flows under reduced gravity conditions.;However the two-fluid model and the IATE need to be evaluated first against detailed experimental data obtained under reduced gravity conditions. Although lot of studies have been done in the past to understand the global structure of gas-liquid two-phase flows under reduced gravity conditions, using experimental setups aboard drop towers or aircrafts flying parabolic flights, detailed data on local structure of such two-phase flows are extremely rare.;Hence experiments were carried out in a 304 mm inner diameter (ID) test facility on earth. Keeping in mind the detailed experimental data base that needs to be generated to evaluate two-fluid model along with IATE, ground based simulations provide the only economic path. Here the reduced gravity condition is simulated using two-liquids of similar densities (water and Therminol 59 RTM in the present case). Only adiabatic two-phase flows were concentrated on at this initial stage. Such a large diameter test section was chosen to study the development of drops to their full extent (it is to be noted that under reduced gravity conditions the stable bubble size in gas-liquid two-phase flows is much larger than that at normal gravity conditions). Twelve flow conditions were chosen around predicted bubbly flow to cap-bubbly flow transition region. Detailed local data was obtained at ten radial locations for each of three axial locations using state-of-the art multi-sensor conductivity probes. The results are presented and discussed. Also one-group as well as two-group, steady state, one-dimensional IATE was evaluated against data obtained here and by other researchers, and the results presented and discussed.
机译:在降低的重力条件下研究气液两相流非常重要。降低重力条件下气液两相流的主要应用之一是为未来太空应用设计主动式热控制系统。以前的航天器的特点是航天器内部发热低,需要在航天器中重新分配热量或将其排入太空。可以通过抽运的单相回路或无源系统(例如热管)轻松完成此任务。但是,随着航天器内部热量产生的增加(如未来的飞行任务所预测的那样),正在考虑抽水沸腾的两相流。这是因为除其他优点外,与沸腾传热相关的更高的传热系数。在重力降低的情况下,两相流在空间推进中也有重要应用,如在空间核动力反应堆以及航天器的许多其他生命支持系统中。两流体模型与界面面积传输方程(IATE)是一个可用于预测重力降低条件下气液两相流动行为的有用工具。应该注意的是,在减小重力和正常重力条件下,两相流之间存在相当大的差异,特别是对于低惯性流而言。这是因为由于重力场的抑制,与正常重力条件相比,气液两相流在降低的重力条件下花费了大量时间。因此,适用于正常重力条件下充分发展的气液两相流的其他常见分析方法(如流态和流态转换标准)将不适用于降低重力条件下的气液两相流。首先需要根据在降低的重力条件下获得的详细实验数据评估双流体模型和IATE。尽管过去已经进行了大量研究以了解重力降低条件下气液两相流的整体结构,但通过使用落塔式或抛物线飞行的飞机上的实验装置以及此类两相局部结构的详细数据流量极少发生。因此,在地球上的304毫米内径(ID)测试设备中进行了实验。考虑到需要生成详细的实验数据库来评估IID的双流体模型,基于地面的模拟提供了唯一的经济途径。在这里,使用相似密度的两种液体(在当前情况下为水和Therminol 59 RTM)模拟降低的重力条件。在此初始阶段,仅绝热的两相流集中。选择如此大直径的试验段来研究液滴的全部发展(应注意,在重力降低的情况下,气液两相流中的稳定气泡尺寸要比正常重力条件下的气泡尺寸大得多) )。在预测的气泡流量到帽泡流量过渡区域周围选择了十二个流量条件。使用最新型的多传感器电导率探头,可以在三个轴向位置的每一个的十个径向位置获得详细的本地数据。结果进行了介绍和讨论。还根据此处和其他研究人员获得的数据评估了一组以及两组的稳态一维IATE,并提出和讨论了结果。

著录项

  • 作者

    Roy, Tirthankar.;

  • 作者单位

    Purdue University.;

  • 授予单位 Purdue University.;
  • 学科 Engineering Chemical.;Engineering Mechanical.;Engineering Nuclear.
  • 学位 Ph.D.
  • 年度 2010
  • 页码 193 p.
  • 总页数 193
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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