Numerical Analysis of Two-Phase Pipe Flow of Liquid Helium Using Multi-Fluid Model

Author:

Ishimoto Jun1,Oike Mamoru2,Kamijo Kenjiro2

Affiliation:

1. Department of Intelligent Machines and System Engineering, Hirosaki University, 3, Bunkyo-cho, Hirosaki 036-8561 Japan

2. Institute of Fluid Science, Tohoku University, 2-1-1, Katahira, Aoba-ku, Sendai 980-8577 Japan

Abstract

The two-dimensional characteristics of the vapor-liquid two-phase flow of liquid helium in a pipe are numerically investigated to realize the further development and high performance of new cryogenic engineering applications. First, the governing equations of the two-phase flow of liquid helium based on the unsteady thermal nonequilibrium multi-fluid model are presented and several flow characteristics are numerically calculated, taking into account the effect of superfluidity. Based on the numerical results, the two-dimensional structure of the two-phase flow of liquid helium is shown in detail, and it is also found that the phase transition of the normal fluid to the superfluid and the generation of superfluid counterflow against normal fluid flow are conspicuous in the large gas phase volume fraction region where the liquid to gas phase change actively occurs. Furthermore, it is clarified that the mechanism of the He I to He II phase transition caused by the temperature decrease is due to the deprivation of latent heat for vaporization from the liquid phase. According to these theoretical results, the fundamental characteristics of the cryogenic two-phase flow are predicted. The numerical results obtained should contribute to the realization of advanced cryogenic industrial applications.

Publisher

ASME International

Subject

Mechanical Engineering

Reference39 articles.

1. Filina, N. N., and Weisend, J. G., 1996, Cryogenic Two-Phase Flow, Cambridge University Press, New York, NY, pp. 20–76.

2. Van Sciver, S. W., 1996, Helium Cryogenics, Plenum Press, New York, N.Y., pp. 77–130.

3. Cheremisinoff, N. P., 1989, Encyclopedia of Fluid Mechanics Volume 8, Aerodynamics and Compressible Flows, Gulf Publishing Corp., Houston, Texas, pp. 1039–1061.

4. Kamijo, K., Yoshida, M., and Tsujimoto, Y., 1993, “Hydraulic and Mechanical Performance of LE-7 LOX Pump Inducer,” J. Propul. Power, 9, No. 6, pp. 819–826.

5. King, J. A. , 1972, “Design of Inducers for Two-Phase Operation Final Report,” NASA CR-123555, pp. 1–96.

Cited by 7 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3