Volume 34 Issue 2
Feb.  2019
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0Numerical study on heat transfer deterioration of hydrocarbon fuel in transcritical process under influence of multiple influencing factors[J]. Journal of Aerospace Power, 2019, 34(2): 387-395. doi: 10.13224/j.cnki.jasp.2019.02.015
Citation: 0Numerical study on heat transfer deterioration of hydrocarbon fuel in transcritical process under influence of multiple influencing factors[J]. Journal of Aerospace Power, 2019, 34(2): 387-395. doi: 10.13224/j.cnki.jasp.2019.02.015

0Numerical study on heat transfer deterioration of hydrocarbon fuel in transcritical process under influence of multiple influencing factors

doi: 10.13224/j.cnki.jasp.2019.02.015
  • Received Date: 2018-03-03
  • Publish Date: 2019-02-28
  • In order to deeply understand the heat transfer characteristics of supercritical hydrocarbon fuel in the process of active regeneration cooling, the heat transfer characteristics of supercritical RP-3 were numerically calculated based on the open source software OpenFOAM. The SST(shear stress transport) k-ω turbulence model was used and the physical properties of aviation kerosene alternative fuels were calculated by the generalized corresponding state law. Comparative analyses between numerical and experimental results were used to evaluate the reliability of calculation method, the average error of wall temperature was less than 3% with the heat flux ranging from 300kW/m2 to 400kW/m2. The mechanism of heat transfer deterioration was analyzed, the effects of pressure, inlet temperature and the ratio of heat flux and mass flow rate on the flow and heat transfer were discussed. It indicated that the dramatic changes of hydrocarbon fuel physical properties near the pseudo critical temperature were the main cause of heat transfer deterioration under forced convection. Improving the pressure and the ratio of heat flux and mass flow rate or decreasing the inlet temperature were effective measures to avoid the heat transfer deterioration near the pseudo critical temperature. The predictive correlation formula of heat transfer deterioration had been proposed, providing a reference for the regeneration cooling technology.

     

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  • [1]
    范学军,俞刚.大庆RP-3航空煤油热物性分析[J].推进技术,2006,27(2):187-192.FAN Xuejun,YU Gang.Thermal property analysis of Daqing RP-3 aviation kerosene[J].Journal of Propulsion Technology,2006,27(2):187-192.(in Chinese)
    [2]
    SHIRALKAR B S,GRIFFITH P.Deterioration in heat transfer to fluids at supercritical pressure and high heat fluxes[J].Journal of Heat Transfer,1969,91(1):27-36.
    [3]
    BOURKE P J,PULLING D J,GILL L E,et al.Forced convective heat transfer to turbulent CO2 in the supercritical region[J].International Journal of Heat and Mass Transfer,1970,13(8):1339-1348.
    [4]
    张宇,姜培学,石润富,等.竖直圆管中超临界压力CO2在低Re下对流换热研究[J].工程热物理学报,2008,29(1):118-120.ZHANG Yu,JIANG Peixue,SHI Runfu,et al.Study on convective heat transfer of supercritical pressure CO2 in vertical tubes at low Re[J].Journal of Engineering Thermophysics,2008,29(1):118-120.(in Chinese)
    [5]
    MCELIGOT D M,COON C W,PERKINS H C.Relaminarization in tubes[J].International Journal of Heat and Mass Transfer,1970,13(2):431-433.
    [6]
    饶政华,廖胜明.超临界CO2水平细微管内层流流动与换热的数值模拟[J].热科学与技术,2005,4(2):113-117.
    RAO Zhenghua,MIU Shengming.Numerical simulation of laminar flow and heat transfer in microtubes with supercritical CO2 level[J].Journal of Thermal Science and Technology,2005,4(2):113-117.(in Chinese)
    [7]
    ZHONG Fengquan,FAN Xuejun,YU Gong,et al.Heat transfer of aviation kerosene at supercritical conditions[J].Journal of Thermophysics and Heat Transfer,2009,23(3):543-550.
    [8]
    LIU Bo,ZHU Yinhai,YAN Junjie,et al.Experimental investigation of convection heat transfer of n-decane at supercritical pressures in small vertical tubes[J].International Journal of Heat and Mass Transfer,2015,91(1):734-746.
    [9]
    JACKSON J D,COTTON M A,AXCELL B P.Studies of mixed convection in vertical tubes[J].International Journal of Heat and Fluid Flow,1989,10(1):2-15.
    [10]
    赵陈儒.超临界压力流体在圆管内流动与对流换热研究[D].北京:清华大学,2011.ZHAO Chenru.Study on flow and convection heat transfer of supercritical pressure fluid in a circular tube[D].Beijing:Tsinghua University,2011.(in Chinese)
    [11]
    DANG Guoxin,ZHONG Fengquan,CHEN Lihong,et al.Numerical investigation on flow and convective heat transfer of aviation kerosene at supercritical conditions[J].Science China Technological Sciences,2013,56(2):416-422.
    [12]
    ZHU Kun,XU Guoqiang,JIA Zhouxia,et al.Pressure effect on the heat transfer characteristics of hydrocarbon fuel in the horizontal circular tube at supercritical pressures[J].Journal of Aerospace Power,2016,31(6):1289-1296.
    [13]
    ZHOU Weixing,BAO Wen,QIN Jiang,et al.Deterioration in heat transfer of endothermal hydrocarbon fuel[J].Journal of Thermal Science,2011,20(2):173-180.
    [14]
    王彦红,李素芬,东明.浮升力对水平管内超临界航空煤油传热影响数值研究[J].大连理工大学学报,2013,53(6):816-823.WANG Yanhong,LI Sufen,DONG Ming.Numerical study on the effect of floating force on heat transfer of supercritical aviation kerosene in horizontal pipe[J].Journal of Dalian University of Technology,2013,53(6):816-823.(in Chinese)
    [15]
    ZHU Jianqin,TAO Zhi,DENG Hongwu,et al.Numerical investigation of heat transfer characteristics and flow resistance of kerosene RP-3 under supercritical pressure[J].International Journal of Heat and Mass Transfer,2015,91(1):330-341.
    [16]
    ZHAO Guozhu,SONG Wenyan ZHANG Ruoling,et al.Numerical simulation on flow and heat transfer of n-decane under supercritical pressure[J].Journal of Propulsion Technology,2014,35(4):537-543.
    [17]
    MOHSENI M,BAZARGAN M.The effect of the low Reynolds number k-ε turbulence models on simulation of the enhanced and deteriorated convective heat transfer to the supercritical fluid flows[J].Heat and Mass Transfer,2011,47(5):609-619.
    [18]
    MENTER F R.Two-equation eddy-viscosity turbulence models for engineering applications[J].AIAA Journal,1994,32(8):1598-1605.
    [19]
    ANSYS Incorporation.Fluent 14.5 user guide[M].Lebanon:Fluent Incorporation,2013.
    [20]
    程泽源,朱剑琴,金钊.吸热型碳氢燃料RP-3替代模型研究[J].航空动力学报,2016,31(2):391-398.CHENG Zeyuan,ZHU Jianqin,JIN Zhao.Study on the replacement model of endothermic hydrocarbon fuel RP-3[J].Journal of Aerospace Power,2016,31(2):391-398.(in Chinese)
    [21]
    DENG Hongwu,ZHANG Chunben,XU Guoqiang,et al.Visualization experiments of a specific fuel flow through quartz-glass tubes under both sub-and supercritical conditions[J].Chinese Journal of Aeronautics,2012,25(3):372-380.
    [22]
    张春本.超临界压力下碳氢燃料的流动与换热特性研究[D].北京:北京航空航天大学,2011.ZHANG Chunben.Study on flow and heat transfer characteristics of hydrocarbon fuel under supercritical pressure[D].Beijing:Beijing University of Aeronautics and Astronautics,2011.(in Chinese)
    [23]
    URBANO A,NASUTI F.On the onset of heat transfer deterioration in supercritical coolant flow channels[R].AIAA-2012-2880,2012.
    [24]
    张斌,张春本,邓宏武,等.超临界压力下碳氢燃料在竖直圆管内换热特性[J].航空动力学报,2012,27(3):595-603.ZHANG Bin,ZHANG Chunben,DENG Hongwu,et al.Heat transfer characteristics of hydrocarbon fuel in vertical tube under supercritical pressure[J].Journal of Aerospace Power,2012,27(3):595-603.(in Chinese)
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