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CHAO Kan, NIU Nan, LU He-jian. Effect of Primary Water-to-Fuel Ratio on Specific Impulse Performance of Water Ramjet with High Metal Content Propellant[J]. Journal of Unmanned Undersea Systems, 2017, 25(创刊号): 052-56. doi: 10.11993/j.issn.2096-3920.2017.01.004
Citation: CHAO Kan, NIU Nan, LU He-jian. Effect of Primary Water-to-Fuel Ratio on Specific Impulse Performance of Water Ramjet with High Metal Content Propellant[J]. Journal of Unmanned Undersea Systems, 2017, 25(创刊号): 052-56. doi: 10.11993/j.issn.2096-3920.2017.01.004

Effect of Primary Water-to-Fuel Ratio on Specific Impulse Performance of Water Ramjet with High Metal Content Propellant

doi: 10.11993/j.issn.2096-3920.2017.01.004
  • Received Date: 2017-01-20
  • Rev Recd Date: 2017-02-16
  • Publish Date: 2017-04-20
  • To improve specific impulse performance of a water ramjet, based on eddy-dissipation combustion model, a 3D multi-phase flow non-premixed combustion reaction model was established for the water ramjet with high metal content magnesium-based propellant. Further, the effects of water-to-fuel ratio on such parameters as temperature distribution and variation of composition in afterburning chamber as well as specific impulse of the water ramjet were obtained, and the calculations are in good agreement with the experiment results. It is shown that the primary water-to-fuel ratio is more important to performance improvement of the water ramjet, and the specific impulse of the water ramjet firstly increases then decreases with the increase of primary water-to-fuel ratio, showing an optimum primary water-to-fuel ratio, at which the water ramjet gains the highest specific impulse.

     

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  • [1]
    Stinbring D R, Cook R B, Dzielski J, et al. High-Speed Supercavitating Vehicles[C]//Collection of Technical Papers-AIAA Guidance, Navigation, and Control Conference. Colorado, US: [s.n.], 2006.
    [2]
    Ko H, Park B H, Yoon W S. Evolution of Combusting Flow in Rocket-Ramjet Transition Regime[C]//41st AIAA/ ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Joint Propulsion Conferences. Tucson, Arizona: AIAA/ ASME/SAE/ASEE, 2005.
    [3]
    Risha G A, Huang Y, Yetter R A, et al. Combustion of Aluminum Particles with Steam and Liquid Water[C]//44th AIAA Aerospace Sciences Meeting and Exhibit, Ae- rospace Sciences Meetings. Reno, Nevada: AIAA, 2006.
    [4]
    Tahsini A M, Ebrahimi M. Increasing Isp by Injecting Water into Combustion Chamber of an Underwater SRM[C]//42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit Sacramento. California: AIAA/ ASME/SAE/ASEE, 2006.
    [5]
    Ermakov V A, Razdobreev A A, Skorik A I, et al. Temperature of Aluminum Particles at the Time of Ignition and Combustion. Combustion[J]. Explosion and Shock Waves, 1982, 18(2): 256-257.
    [6]
    MilIer T F, Herr J D. Green Rocket Propulsion by Reaction of Al and Mg Powders and Water[C]//40th AIAA/ ASME/SAE/ASEE Joint Propulsion Conference and Exhibit Fort Lauderdale, Florida, 2004.
    [7]
    MiIler T F, walter J L, Kiely D H. A Next-generation AUV Energy System Based on Aluminum-seawater Combustion [C]//Proceedings of the Symposium on Autonomous Underwater Vehicle Technology, [s.l.]: IEEE, 2002: 111-119.
    [8]
    Miller T F, Garza A B. Finite Rate Calculations of Magnesium Combustion in Vitiated Oxygen and Steam Atmospheres[C]//4th International Energy Conversion En-gineering Conference and Exhibit(IECEC). San Diego, California: IECEC, 2006.
    [9]
    黄利亚, 夏智勋, 胡建新, 等. 镁基水冲压发动机燃烧室长度及进水距离设计方法[J]. 航空学报, 2011, 32(1): 67-74.

    Huang Li-ya, Xia Zhi-xun, Hu Jian-xin, et al. Design Method Combustion Chamber Length and Water Intake Distance of Magnesium-basedwater Ramjets[J]. Acta Aeronautica et Astronautica Sinica, 2011, 32(1): 67-74.
    [10]
    朱千稳, 刘冰, 夏智勋, 等. 喷嘴特性对水冲压发动机性能的影响[J]. 导弹与航天运载技术, 2010(6): 10-13.

    Zhu Qian-wen, Liu Bing, Xia Zhi-xun, et al. Analysis of Nozzle Characteristic Effects on Water Ramjet Engine[J]. Missiles and Spacevehicles, 2010(6): 10-13.
    [11]
    韩超, 夏智勋, 胡建新, 等. 一次进水角度对水冲压发动机比冲性能影响研究[J]. 固体火箭技术, 2009, 32(5): 496-499.

    Han Chao, Xia Zhi-xun, Hu Jian-xin, et al. Effect of Pri-mary Water Penetration Angle on Specific Impulse of Water Ramjet[J]. Journal of Solid Rocket Technology, 2009, 32(5): 496-499.
    [12]
    韩超, 夏智勋, 胡建新, 等. 水燃比对水冲压发动机性能影响数值模拟与试验研究[J]. 国防科技大学学报, 2009, 31(4): 117-121.

    Han Chao, Xia Zhi-xun, Hu Jian-xin, et al. Numerical and Experiment Studies on Water Ramjet with Effect of Water-fuel Ratio[J]. Journal of National University of Defense Technology, 2009, 31(4): 117-121.
    [13]
    黄利亚, 夏智勋, 张为华, 等. 水冲压发动机试验水燃比选择方法[J]. 航空学报, 2010, 31(9): 1740-1745.

    Huang Li-ya, Xia Zhi-xun, Zhang Wei-hua, et al. Wa-ter/Fuel Ratio Selection Method in Water Ramjet Engine Test[J]. Acta Aeronautica et Astronautica Sinica, 2010, 31(9): 1740-1745.
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