Volume 36 Issue 4
Oct.  2018
Turn off MathJax
Article Contents
Ni Yanjie, Xing Rongjun, Wan Gang, Jin Yong, Li Haiyuan, Yang Chunxia, Li Baoming. Porous propellant burning rate enhanced by plasma[J]. Explosion And Shock Waves, 2016, 36(4): 562-567. doi: 10.11883/1001-1455(2016)04-0562-06
Citation: Ni Yanjie, Xing Rongjun, Wan Gang, Jin Yong, Li Haiyuan, Yang Chunxia, Li Baoming. Porous propellant burning rate enhanced by plasma[J]. Explosion And Shock Waves, 2016, 36(4): 562-567. doi: 10.11883/1001-1455(2016)04-0562-06

Porous propellant burning rate enhanced by plasma

doi: 10.11883/1001-1455(2016)04-0562-06
  • Received Date: 2014-12-01
  • Rev Recd Date: 2015-01-29
  • Publish Date: 2016-07-25
  • The experimental system with a closed bomb was employed to discuss the characteristics of 4/7 high-nitrogen solid propellant burning rate enhanced by plasma. The plasma energy transferred into the closed bomb was measured by the utilization efficiency of the plasma generator electrical energy. A transient burning rate formula of propellant including the influence of pressure gradient and an enhanced gas generation rates coefficient by electrical power was presented. The enhanced gas generation rates coefficient of 4/7 high-nitrogen solid propellant is equal to 0.005 MW-1. Compared with the burning rate formula given by Woodley, the pressure curve simulated by the transient burning rate formula is in better agreement with the tests. And the transient burning rate formula can describe the combustion process of solid propellant by plasma more accurately.
  • loading
  • [1]
    Goldenberg C, Zoler D, Shafir N, et al. Plasma-propellant interaction at low plasma energies in ETC guns[J]. IEEE Transactions on Magnetics, 2003, 39(1):227-230. doi: 10.1109/TMAG.2002.805945
    [2]
    Kaste P, Birk A, Kinkennon A, et al. Analysis of burning rate phenomena and extinguished solid propellants from an interrupted closed bomb with plasma igniter[J]. IEEE Transactions on Magnetics, 2001, 37(1):173-177. doi: 10.1109/20.911815
    [3]
    Beyer R A, Brant A L. Plasma ignition in a 30-mm cannon[J]. IEEE Transactions on Magnetics, 2007, 43(1):294-298. doi: 10.1109/TMAG.2006.887689
    [4]
    Zoler D, Shafir N, Forte D, et al. Study of plasma jet capabilities to produce uniform ignition of propellants, ballistic gain, and significant decrease of the temperature gradient[J]. IEEE Transactions on Magnetics, 2007, 43(1):322-328. doi: 10.1109/TMAG.2006.887664
    [5]
    Alimi R, Bakshi L, Kot E, et al. Temperature compensation and improved ballistic performance in a solid-propellant electrothermal-chemical(SPETC) 40-mm gun[J]. IEEE Transactions on Magnetics, 2007, 43(1):289-293. doi: 10.1109/TMAG.2006.887688
    [6]
    Beckstead M W. Recent progress in modeling solid propellant combustion[J]. Combustion, Explosion, and Shock Waves, 2006, 42(6):623-641. doi: 10.1007/s10573-006-0096-5
    [7]
    Beckstead M W, Puduppakkam K, Thakre P, et al. Modeling of combustion and ignition of solid-propellant ingredients[J]. Progress in Energy and Combustion Science, 2007, 33(6):497-551. doi: 10.1016/j.pecs.2007.02.003
    [8]
    Woodley C R, Billett S J. Modeling enhanced gas generation rates in a 155 mm ETC gun[J]. IEEE Transactions on Magnetics, 2001, 37(1):207-210. doi: 10.1109/20.911822
    [9]
    Woodley C R. Comparison of 0D and 1D interior ballistics modeling of high performance direct fire guns[C]//Crewther I R. Proceedings of 19th International Symposium of Ballistics. Switzerland: International Ballistics Committe, 2001: 57-64.
    [10]
    Taylor M J, Woodley C R. Variation in enhanced gas generation rates in electrothermal-chemical closed chamber studies[C]//Crewther I R. Proceedings of 19th International Symposium of Ballistics. Switzerland: International Ballistics Committe, 2001: 179-186.
    [11]
    李海元, 栗保明, 李鸿志, 等.等离子体点火密闭爆发器中火药燃速特性的研究[J].爆炸与冲击, 2004, 24(2):145-150. doi: 10.3321/j.issn:1001-1455.2004.02.008

    Li Haiyuan, Li Baoming, Li Hongzhi, et al. Propellant burn rate characteristics in closed bomb ignited with plasma[J]. Explosion and Shock Waves, 2004, 24(2):145-150. doi: 10.3321/j.issn:1001-1455.2004.02.008
    [12]
    李海元, 栗保明, 李鸿志.等离子体点火条件下火药燃速的实验研究[J].弹道学报, 2007, 19(2):78-81. doi: 10.3969/j.issn.1004-499X.2007.02.021

    Li Haiyuan, Li Baoming, Li Hongzhi. Experimental study on propellant burning rate under the conditions of plasma ignition[J]. Journal of Ballistics, 2007, 19(2):78-81. doi: 10.3969/j.issn.1004-499X.2007.02.021
    [13]
    Brik A, Guercio M D, Kinkennon A, et al. Interrupted-burning tests of plasma-ignited JA2 and M30 grains in a closed chamber[J]. Propellants, Explosives, Pyrotechnics, 2000, 25(3):133-142. doi: 10.1002/(ISSN)1521-4087
    [14]
    翁春生, 王浩.计算内弹道学[M].北京:国防工业出版社, 2006:7-15.
    [15]
    Krier H. Solid propellant burning rate during a pressure transient[J]. Combustion Science and Technology, 1972, 5(2):69-73 doi: 10.1080/00102207208952505
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Figures(7)  / Tables(2)

    Article Metrics

    Article views (4021) PDF downloads(439) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return