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超临界压力下航空煤油RP-3在水平细圆管内对流换热特性实验研究

贾洲侠 付衍琛 孔凡金 刘宝瑞 吴振强

航天器环境工程2018,Vol.35Issue(3):233-240,8.
航天器环境工程2018,Vol.35Issue(3):233-240,8.DOI:10.3969/j.issn.1673-1379.2018.03.006

超临界压力下航空煤油RP-3在水平细圆管内对流换热特性实验研究

Experimental study of convective heat transfer of aviation kerosene RP-3 in horizontal tube under supercritical pressures

贾洲侠 1付衍琛 2孔凡金 1刘宝瑞 1吴振强1

作者信息

  • 1. 北京强度环境研究所 可靠性与环境工程技术重点实验室,北京 100076
  • 2. 北京航空航天大学 能源与动力工程学院,北京 100191
  • 折叠

摘要

Abstract

To better understand the convective heat transfer of the hydrocarbon fuel in horizontal tubes under supercritical pressures, an experimental study is carried out for the convective heat transfer of the aviation kerosene RP-3 in a horizontal miniature round tube. Under the working conditions of the air-kerosene heat exchanger, the aviation kerosene is heated up to the supercritical regime. The influences of the heat flux, the fluid inlet temperature, and the buoyancy on the heat transfer of the RP-3 are analyzed. It is found that the heat transfer coefficients decrease with the increase of the heat flux, and the buoyancy causes a large temperature difference of 50 K between the top and the bottom surfaces of the test tube under high heat flux conditions, which can be predicted by the non-dimensional parameter Grq/Grth. The effects of the buoyancy on the heat transfer can be suppressed by increasing the mass flux. The results may provide a technological basis for the active thermal protection of the flight vehicles to be cooled by hydrocarbon fuels.

关键词

主动热防护/航空煤油/水平流动/对流换热/超临界压力/雷诺数/浮升力

Key words

active thermal protection/aviation kerosene/horizontal flow/convective heat transfer/supercritical pressure/Reynolds number/buoyancy

分类

航空航天

引用本文复制引用

贾洲侠,付衍琛,孔凡金,刘宝瑞,吴振强..超临界压力下航空煤油RP-3在水平细圆管内对流换热特性实验研究[J].航天器环境工程,2018,35(3):233-240,8.

基金项目

国家自然科学基金项目(编号:11502023 ()

11502024 ()

11402028) ()

航天器环境工程

OACSTPCD

1673-1379

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