期刊文献+

过载环境下1.002mm管内流动沸腾传热的实验 被引量:1

Experiment on flow boiling heat transfer in 1.002 mm tube under hypergravity
原文传递
导出
摘要 通过地面离心转台模拟过载,对R134a在内径为1.002mm管内的沸腾流动传热进行了实验研究。结果表明:管内流动沸腾传热特性随着重力的变化而变化;在重力为3.16g(g=9.8m/s^2)时,过载下的传热系数比常重力下的大;随着过载的增加,大多数情况下传热系数先增大后减小,转折点在1.1g^1.4g;在3.16g时,部分传热系数开始出现低于1g时的情况;干度对传热系数的影响特性因重力不同而不同。研究了常重力下流动沸腾预测模型对过载环境的适应性,鉴别出了对过载数据预测较好的公式。 An experiment investigation of R134 aflow boiling heat transfer in a 1.002 inner diameter mini-tube under hypergravity was carried out,with the hypergravity environment being achieved using a centrifugal acceleration machine.Results showed that a remarkable difference existed in flow boiling heat transfer between hypergravity and normal gravity.The heat transfer under hypergravity was stronger than that under normal gravity in the gravity of 3.16 g(g=9.8 m/s^2).With the increase of gravity,heat transfer coefficients increased at first and then decreased.The transition took place around 1.1 g-1.4 g.At3.16 g,some heat transfer coefficients became smaller than those at normal gravity.The effects of vapor quality on the heat transfer varied with gravity.The applicability of correlations for flow boiling heat transfer under normal gravity to hypergravity was also evaluated,and those having good prediction performances for hypergravity were identified.
作者 方贤德 李国华 袁宇良 李定坤 郑玲 FANG Xiande;LI Guohua;YUAN Yuliang;LI Dingkun;ZHENG Ling(Key Laboratory of Aircraft Environment Control and Life Support,Ministry of Industry and Information Technolgy,College of Aerospace Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China)
出处 《航空动力学报》 EI CAS CSCD 北大核心 2019年第8期1644-1651,共8页 Journal of Aerospace Power
基金 国家自然科学基金(51576099,51176074) 江苏高校优势学科建设工程资助项目
关键词 过载 气液两相流 流动沸腾 传热 细小通道 hypergravity gas-liquid two-phase flow flow boiling heat transfer mini-channel
  • 相关文献

参考文献2

二级参考文献22

  • 1甘云华,徐进良,周继军,陈勇.微尺度相变传热的关键问题[J].力学进展,2004,34(3):399-407. 被引量:16
  • 2赵鹏飞,毕勤成,杨朝初,陈听宽.微小圆通道内流动沸腾换热特性的研究[J].工程热物理学报,2005,26(5):802-804. 被引量:6
  • 3Kim J, Benton J, Mcquillen J, et al. Subcooled pool boiling heat transfer in microgravity and hi-g[J]. Journal of Heat Transfer, 2001, 123(1) :620.
  • 4Chen R T N. Flight dynamics of rotorcraft in steep high-g turns[R]. AIAA Paper 82-1345, 1982.
  • 5Curreri P, Downey J P, Ramachandran N, et al. Experimental results and numerical modeling of solidification during aircraft high-g arcs [R]. AIAA Paper 92- 0843, 1992.
  • 6Naoumov V, Parang M, Shough C, et al, Droplet entrainment in two phase flow under reduced gravity[R]. AIAA Paper 2007 743, 2007.
  • 7Barry J, Crowley C. Simulation of two-phase systems in variable gravity[R]. AIAA Paper 2001-0929, 2001.
  • 8刘艺涛.动载作用下水平和直角弯管内两相流动的数值模拟[D].南京:南京航空航天大学,2005.
  • 9中国工程热物理学会.中国科学技术协会.工程热物理学科发展报告[M].北京:中国科学技术出版社,2007-2008.
  • 10Pettersen J. Flow vaporization of CO2 in microchannel tubes[J]. Experimental Thermal and Fluid Science,2004, 28(2-3) : 111-121.

共引文献2

引证文献1

二级引证文献1

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部