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Numerical investigation of heat transfer characteristics and flow resistance of kerosene RP-3 under supercritical pressure

机译:超临界压力下煤油RP-3传热特性和流动阻力的数值研究

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摘要

An in-house three-dimensional Navier-Stokes code was used to investigate the heat transfer characteristics and flow resistance of kerosene RP-3 under supercritical pressure in a tube. For the numerical simulation, the thermophysical and transport properties of the surrogate fuel, which is consist of 53% (mole fraction) n-undecane, 18% 1-butylcyclohexane and 29% 13.5-trimethyl-benzene, were calculated and verified by contrast with RP-3 experimental data. The length and diameter of the stainless tube are 300 mm, 1.8 mm respectively. The inlet temperatures varied from 370 K to 770 K, and the operation pressure were 3 MPa, 4 MPa and 5 MPa. The mass flow were 2 g/s, 3 g/s and 4 g/s, with different heat flow density 300 kW/m~2, 400 kW/m~2, 500 kW/m~2 and 550 kW/m~2. The research results show that the calculated pressure drops agreed well with the experimental data when the temperature was lower than 720 K. The discrepancy of numerical and experimental data becomes gradually distinct after the temperature is higher than 720 K. When the bulk temperature is lower than the critical temperature, the pressure drops under different operating pressures are almost the same. While the bulk temperature is higher than the critical temperature, the diversity of pressure drop under different operating pressures becomes manifest gradually. The local Nusselt number firstly increased and then suddenly decreased at a certain position. The heat transfer deterioration was caused by the intensive variations of thermo-physical properties of the fuel under supercritical pressures. Furthermore, the larger the heat flux was, the earlier the turnover position appeared.
机译:内部三维Navier-Stokes代码用于研究管中超临界压力下煤油RP-3的传热特性和流动阻力。为了进行数值模拟,计算并替代了由53%(摩尔分数)正十一烷,18%1-丁基环己烷和29%13.5-三甲基苯组成的替代燃料的热物理性质和传输性质,并与RP-3实验数据。不锈钢管的长度和直径分别为300毫米和1.8毫米。入口温度在370 K至770 K之间变化,操作压力分别为3 MPa,4 MPa和5 MPa。质量流量为2 g / s,3 g / s和4 g / s,不同的热流密度分别为300 kW / m〜2、400 kW / m〜2、500 kW / m〜2和550 kW / m〜 2。研究结果表明,当温度低于720 K时,计算出的压降与实验数据吻合较好。当温度高于720 K时,数值与实验数据的差异逐渐明显。在临界温度下,不同工作压力下的压降几乎相同。当整体温度高于临界温度时,在不同工作压力下压降的多样性逐渐显现。本地Nusselt数在某个位置先增加然后突然减少。传热恶化是由于燃料在超临界压力下热物理性质的剧烈变化而引起的。此外,热通量越大,周转位置越早出现。

著录项

  • 来源
    《International Journal of Heat and Mass Transfer》 |2015年第12期|330-341|共12页
  • 作者单位

    National Key Laboratory of Science and Technology on Aero-Engines, School of Energy and Power Engineering, Beihang University, Beijing 100190, China;

    National Key Laboratory of Science and Technology on Aero-Engines, School of Energy and Power Engineering, Beihang University, Beijing 100190, China;

    National Key Laboratory of Science and Technology on Aero-Engines, School of Energy and Power Engineering, Beihang University, Beijing 100190, China;

    Institute of Engineering Thermophysics, Chinese Academy of Science, Beijing 100190, China;

    Shenyang Aero-engine Research Institute, Aviation Industry Corporation of China, Shenyang 110015, 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

    Supercritical pressure; Kerosene RP-3; Heat transfer; Flow resistance;

    机译:超临界压力;煤油RP-3;传播热量;流动阻力;

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