Volume 42 Issue 6
Jun.  2016
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WANG Yue, GUO Jun, DENG Hongwu, et al. Effects of RP-3's wall coke deposition on flow resistance under supercritical pressure[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(6): 1250-1255. doi: 10.13700/j.bh.1001-5965.2015.0403(in Chinese)
Citation: WANG Yue, GUO Jun, DENG Hongwu, et al. Effects of RP-3's wall coke deposition on flow resistance under supercritical pressure[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(6): 1250-1255. doi: 10.13700/j.bh.1001-5965.2015.0403(in Chinese)

Effects of RP-3's wall coke deposition on flow resistance under supercritical pressure

doi: 10.13700/j.bh.1001-5965.2015.0403
  • Received Date: 18 Jun 2015
  • Publish Date: 20 Jun 2016
  • The effect of the jet fuel RP-3 coking deposition in stainless micro-tube on flow resistance and heat transfer characteristics under long heating condition is analyzed based on experimental results. In the experiment, fuel flowing through miniature tube was heated from 130℃ to 450℃ under the pressure 5 MPa when dissolved oxygen in fuel saturated. The whole experiment lasted 36 h with the mass flow rate maintained at 3 g/s. The experimental results show that with the growth of time, coking amount in the tube increases along time. The results also show that the effect of coke deposition on flow resistance and heat transfer is significant. As more and more coke particles adhere, the heat transfer resistance increases rapidly in the early stage of the test and gradually stabilizes, while the flow resistance along the miniature tube increases as the experiment continues. As time grows, the flow resistance in the tube presents a "rapid growth to steady growth, then to exponential growth" process. Besides, based on the test results, an influence coefficient used as an engineering model to value the impact of the coke deposition on single tube of the heat exchanger is proposed.

     

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  • [1]
    BRUENING G B,CHANG W S.Cooled cooling air systems for turbine thermal management:ASME 1990-GT-14[R].New York:ASME, 1999.
    [2]
    SOBEL D R,SPADACCINI L J.Hydrocarbon fuel cooling technologies for advanced propulsion[J].Journal of Engineering for Gas Turbines and Power,1997,119(2):344-351.
    [3]
    EDWARDST,ZABARNICK S.Supercritical fuel deposition mechanisms[J].Industrial & Engineering Chemistry Research,1993,32(12):3117-3122.
    [4]
    GVL O,RUDNICK L R,SCHOBERT H H.Effect of the reaction temperature and fuel treatment on the deposit formation of jet fuels[J].Energy & Fuels,2007,22(1):433-439.
    [5]
    STRAWSON H,LEWIS A.Predicting fuel requirements for the concorde:SAE Paper 680734[R].Detroit:SAE,1968.
    [6]
    EDWARDS T.Cracking and deposition behavior of supercritical hydrocarbon aviation fuels[J].Combustion Science and Technology,2007,178(1):307-334.
    [7]
    SMITH J D.Fuel for the supersonic transport.Effects of deposits on heat transfer to aviation kerosine[J].Industrial & Engineering Chemistry Process Design and Development,1969,8(3):299-308.
    [8]
    SPADACCINI L J,SOBEL D R,HUANG H.Deposit formation and mitigation in aircraft fuels[J].Journal of Engineering for Gas Turbines and Power,2001,123(4):741-746.
    [9]
    HAHNE I E,NEUMANN I R T.Boiling-like phenomena in free-convection heat transfer at supercritical pressures[J].Wärme-und Stoffübertragung,1981,15(3):171-180.
    [10]
    王英杰.超临界RP-3流动换热及结焦实验研究[D].北京:北京航空航天大学,2010:86-90.WANG Y J.Experimental investigation on convection heat transfer and coke characteristics of RP-3 at supercritical pressures[D].Beijing:Beihang University,2010:86-90(in Chinese).
    [11]
    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 B,ZHANG C B,DENG H W,et al.Heat transfer characteristics of hydrocarbon fuel at supercritical pressure in vertical circulartubes[J].Journal of Aerospace Power,2012, 27(3):595-603(in Chinese).
    [12]
    ALEXANDER V,OIERRE J M,BRIAN A K.Determination of coking rate in jet fuel[J].Combustion Science and Technology,1981,26(3):171-175.
    [13]
    HENEGHAN S P.Static tests of jet fuel thermal and oxidative stability[J].Journal of Propulsion and Power,1993,9(1):5-9.
    [14]
    ORHAN A,SEMIH E.Analysis of solid deposits from thermal stressing of a JP-8 fuel on different tube surfaces in a flow reactor[J].Industrial and Engineering Chemistry Research,2001,40(2):596-603.
    [15]
    KLAVETTER E A,MARTIN S J,WESSENDORF K O.Monitoring jet fuel thermal stability using a quartz crystal microbalance[J].Energy & Fuels,1993,7(5):582-588.
    [16]
    袁立公,邓宏武,徐国强,等.超临界压力下航空煤油RP-3壁面结焦特性对换热的影响[J].航空动力学报,2013,28(4):832-837.YUAN L G,DENG H W,XU G Q,et al.Effect of RP-3's coke deposition under the condition of supercritical pressure on heat transfer[J].Journal of Aerospace Power,2013,28(4):832-837(in Chinese).
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