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Experimental investigation on convective heat transfer of supercritical RP-3 in vertical miniature tubes with various diameters

机译:超临界RP-3在不同直径的垂直微型管中对流换热的实验研究

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摘要

This article presents convective heat transfer of hydrocarbon fuel RP-3 at supercritical pressures in vertical micro-tubes with inner diameters of 0.538 mm, 1.09 mm and 1.82 mm under heating conditions. Effects of system pressure, heat flux, mass flow rate and flow direction were experimented and analyzed with wide range of supercritical status. Also, inner diameter effect on heat transfer were compared at identical conditions. The results indicate that sharp variation of thermal properties with temperature is the key factor to influence heat transfer. Normal, deterioration and enhancement heat transfer phenomena generally occur in turn along with dimensionless position. Moreover, Nusselt number variation shows good agreement when the contrast temperature T_b/r_(pc) is lower than 0.80 and Bo~*= 1.0 × 10~(-8) could be the critical point to evaluate buoyancy influence. At last, two well-predicted empirical correlations of Nusselt number are proposed for downward and upward flow heat transfer in 1.09 mm tube.
机译:本文介绍了在加热条件下,内径分别为0.538 mm,1.09 mm和1.82 mm的垂直微管中,碳氢化合物燃料RP-3在超临界压力下的对流传热。在大范围的超临界状态下,对系统压力,热通量,质量流量和流向的影响进行了实验和分析。同样,在相同条件下比较了内径对传热的影响。结果表明,热性能随温度的急剧变化是影响传热的关键因素。通常,劣化和增强的热传递现象通常随无因次位置一起发生。此外,当对比温度T_b / r_(pc)低于0.80时,Nusselt数变化显示出良好的一致性,并且Bo〜* = 1.0×10〜(-8)可能是评估浮力影响的关键点。最后,针对1.09 mm管内的向下和向上流动传热,提出了两个可预测的Nusselt数经验相关性。

著录项

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  • 作者单位

    National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics, Collaborative Innovation Center of Advanced Aero-Engine, School of Energy and Power Engineering, Beihang University, Beijing 100191, China;

    National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics, Collaborative Innovation Center of Advanced Aero-Engine, School of Energy and Power Engineering, Beihang University, Beijing 100191, China;

    National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics, Collaborative Innovation Center of Advanced Aero-Engine, School of Energy and Power Engineering, Beihang University, Beijing 100191, China;

    National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics, Collaborative Innovation Center of Advanced Aero-Engine, School of Energy and Power Engineering, Beihang University, Beijing 100191, China;

    National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics, Collaborative Innovation Center of Advanced Aero-Engine, School of Energy and Power Engineering, Beihang University, Beijing 100191, China;

  • 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

    Convective heat transfer; Buoyancy; Vertical tube; Supercritical pressure; Various diameters;

    机译:对流换热;浮力;立管;超临界压力;各种直径;

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