首页> 外文期刊>International Journal of Heat and Mass Transfer >An experimental study on terrestrial cryogenic tube chilldown Ⅱ. Effect of flow direction with respect to gravity and new correlation set
【24h】

An experimental study on terrestrial cryogenic tube chilldown Ⅱ. Effect of flow direction with respect to gravity and new correlation set

机译:地面低温管冷却的实验研究Ⅱ。流向对重力的影响和新的相关集

获取原文
获取原文并翻译 | 示例
       

摘要

This is the second of a two-part series of papers which presents the experimental results of a parametric series of liquid nitrogen chilldown tests of a stainless steel tube. Whereas the first paper in this series focused on the effect of mass flux, inlet subcooling, equilibrium quality, pressure, and axial distance from the inlet on two-phase convection heat flux for vertical upward flow only, this paper focuses on the effect of flow direction with respect to gravity. Nine different flow directions were examined, including horizontal, 30° inclined and declined, 45° inclined and declined, 60° inclined and declined, and vertical upward and downward. The experimental data covers liquid Reynolds numbers ranging from 800 to 230,000 and local pressures ranging from 150 to 725 kPa. Analysis is presented on the effect of flow direction on the measured film, transition, and nucleate boiling heat transfer coefficients as well as the critical heat flux. Finally, new heat transfer correlations to predict the data are presented for film boiling, nucleate boiling, and transition boiling. These correlations can be used for numerical simulations of cryogenic chilldown to help predict the chilldown time and propellant consumption for different system variables.
机译:这是由两部分组成的系列文章中的第二篇,该系列文章介绍了不锈钢管液氮冷却试验的参数系列实验结果。尽管该系列的第一篇论文仅关注质量通量,入口过冷,平衡质量,压力和距入口的轴向距离对垂直向上流动的两相对流热通量的影响,但本文重点研究了流动的影响。相对于重力的方向。检查了9个不同的流向,包括水平,倾斜30°倾斜,倾斜45°,倾斜60°,垂直向上和向下。实验数据涵盖了液体雷诺数,范围从800到230,000,局部压力范围从150到725 kPa。分析了流动方向对被测膜,转变和成核沸腾传热系数以及临界热通量的影响。最后,提出了新的传热相关性以预测膜沸腾,核沸腾和过渡沸腾的数据。这些相关性可用于低温冷却的数值模拟,以帮助预测不同系统变量的冷却时间和推进剂消耗。

著录项

  • 来源
    《International Journal of Heat and Mass Transfer》 |2016年第12期|1243-1260|共18页
  • 作者单位

    Cryogenics Heat Transfer Laboratory, Department of Mechanical and Aerospace Engineering, University of Florida, Gainesville, FL 32611 -6300, USA;

    Cryogenics Heat Transfer Laboratory, Department of Mechanical and Aerospace Engineering, University of Florida, Gainesville, FL 32611 -6300, USA;

    Cryogenics Heat Transfer Laboratory, Department of Mechanical and Aerospace Engineering, University of Florida, Gainesville, FL 32611 -6300, USA;

    NASA Glenn Research Center, Cleveland, OH 44135, USA;

    NASA Marshall Spaceflight Center, Huntsville, AL 35811, USA;

    NASA Marshall Spaceflight Center, Huntsville, AL 35811, USA;

    Cryogenics Heat Transfer Laboratory, Department of Mechanical and Aerospace Engineering, University of Florida, Gainesville, FL 32611 -6300, USA;

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

    Cryogenics; Two-phase flow; Line chilldown; Liquid nitrogen; Quenching curve; Flow direction effects;

    机译:低温;两相流;生产线冷却;液氮;淬火曲线;流向效应;

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号