期刊文献+

聚乙烯在固体燃料冲压发动机中的燃速影响因素研究 被引量:5

Research on Influence of Selected Factors on Burning Rate of Polyethylene in Solid Fuel Ramjet
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摘要 针对影响聚乙烯(PE)在固体燃料冲压发动机燃烧室中的燃速因素,采用数值仿真与直连式实验相结合的方法,研究了空气质量通量和固体燃料内径对PE燃料平均燃速和当地燃速的影响,分析了无量纲回流区长度与突扩台阶高度的关系。研究表明,PE燃料平均燃速与空气质量通量呈幂函数递增关系,与固体燃料内径呈幂函数递减关系;点火过程的影响以及湍流燃烧模型对突扩台阶后回流区内传热的计算精度是引起回流区内计算结果与实验结果误差较大的重要原因;无量纲回流区长度与突扩台阶高度呈线性递增函数关系。研究结果对固体燃料冲压发动机燃烧室的设计具有一定的参考价值。 Numerical simulation and direct test methods are used to research the influence of selected factors on the burning rate of polyethylene in a solid fuel ramjet. The influences of air mass flux and fuel internal diameter on average burning rate and local average burning rate are studied. The relationship between reattachment length ratio and step height ratio is analyzed. The results show that the average burning rate of the fuel is increased by power function with the increase in air mass flux,and decreased by power function with fuel internal diameter. The difference between simulation and experimental results is caused by the ignition process and the computational accuracy of turbulent combustion model to predict the heat transfer behind a sudden expansion step. The reattachment length ratio increased by liner function with step height ratio.
出处 《兵工学报》 EI CAS CSCD 北大核心 2014年第11期1783-1789,共7页 Acta Armamentarii
基金 总装备部预先研究项目(404040301)
关键词 兵器科学与技术 固体燃料冲压发动机 聚乙烯 燃速 ordnance science and technology solid fuel ramjet polyethylene burning rate
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参考文献14

  • 1Schuhe G. Fuel regression and flame stabilization studies of solid- fuel ramjets [ J ]. Journal of Propulsion, 1986,6 (4) :301 - 304.
  • 2Amnon N, Alon G. Burning and flameholding characteristics of a miniature solid fuel ramjet combustor [ J ]. Journal of Propulsion and Power, 1991, 7(3) : 357 -363.
  • 3Elands P J M, Korting P A O G, Dijkstra F. Combustion of poly- ethylene in a solid fuel ramjet-A comparison of computational and experimental results [ C ] //AIAA/ASME/SAE/ASEE 24th Joint Propulsion Conference. Boston, Massachusetts: AIAA/ASME/ SAE/ASEE, 1988.
  • 4Elands P J M, Dijkstra F. Validation of the flow and combustion processes in a solid fuel ramjet [ C ] //AIAA/ASME/SAE/ASEE 24th Joint Propulsion Conference. Saerameto, CA: AIAA/ASME/ SAE/ASEE, 1991.
  • 5Zvuloni R, Gany A, Levy Y, et al. Geometric effects on the com- bustion in solid fuel ramjets [ J]. Journal of Propulsion, 1989, 5(1): 32-37.
  • 6谢爱元,武晓松,夏强.PMMA在固体燃料冲压发动机中燃烧特性的实验研究[J].兵工学报,2013,34(2):240-245. 被引量:5
  • 7Wilde J P. Fuel pyrolysis effects on hybrid rocket and solid fuel ramjet combustor performance [ D ]. Delft, Netherlands: Delft University of Technology, 1991.
  • 8Mawid M A, Sekar B. Kinetic modeling of ethylene oxidation in high speed reacting flows, AIAA 97-3269 [ R ]. US: AIAA, 1997.
  • 9Gobbo Ferrrira J. Performance of an experimental polyethylene solid fuel ramjet [ J ]. Acta Astronautiea, 1999, 45 ( 1 ) : 11 - 18.
  • 10Yang J T, Wu C Y Y. Controlling mechanisms of ignition of solid fuel in a sudden-expansion combustor[ J]. Journal of Propulsion and Power, 1995, 11(3) : 483 -488.

二级参考文献6

  • 1Elands P J M,Korting P,Wijchers T. Comparison of combustion experiments and theory in polyethylene solid fuel ramjets[J].Journal of Propulsion and Power,1990,(06):732-739.
  • 2Zvuloni R,Gany A,Levy Y. Geometric effects on the combustion in solid fuel ramjet[J].Journal of Propulsion and Power,1989,(01):32-37.
  • 3Gany A,Netzer A. Burning and flameholding characteristics of a miniature solid fuel ramjet combustor[J].Journal of Propulsion and Power,1991,(05):357-363.
  • 4VanderGeld C W M,Korting P,Wijcher T. Combustion of PMMA,PE and PS in a ramjet[J].Combustion and Flame,1990,(3-4):299-306.
  • 5郭KK;萨莫菲尔德M;宋兆武.固体推进剂燃烧基础(下)[M]北京:宇航出版社,1988201-204.
  • 6武晓松;陈军;王栋.固体火箭发动机原理[M]北京:兵器工业出版社,201160.

共引文献4

同被引文献53

  • 1刘巍,杨涛,程兴华,李理.固体燃料冲压发动机两种补燃室构型数值分析[J].推进技术,2009,30(6):647-650. 被引量:3
  • 2LI XinTian,TIAN Hui,CAI GuoBiao.Numerical analysis of fuel regression rate distribution characteristics in hybrid rocket motors with different fuel types[J].Science China(Technological Sciences),2013,56(7):1807-1817. 被引量:11
  • 3郭健,张为华,夏智勋.固体燃料冲压发动机飞行性能分析[J].国防科技大学学报,2007,29(2):10-14. 被引量:8
  • 4Schuhe G. Fuel regression and flame stabilization studies of solid- fuel ramjets[ J]. Journal of Propulsion, 1986,2 (4) :301 - 304.
  • 5VanderGeld C W M,Korting P A O G,Wijchers T. Combustion of PMMA, PE and PS in a ramjet [ J]. Combustion and Flame, 1990,79 (3/4) :299 - 306.
  • 6Netzer A,Gany A. Burning and flameholding characteristics of a miniature solid fuel ramjet combustor [ J ]. Journal of Propulsion and Power,1991,7(3) :357 -363.
  • 7Elands P J M,Korting P A O G, Dijkstra F. Combustion of poly- ethylene in a solid fuel ramjet-a comparison of computational and experimental results [ C ] //AIAA/ASME/SAE/ASEE 24 th Joint Propulsion Conference. Boston, MA, US: AIAA, 1988: AIAA- 88 -3043.
  • 8Roni Zvuloni, Alon Gany, Yeshavahou Levy, et al. Geometric effects on the combustion in solid fuel ramjets[ J]. Journal of Pro- pulsion, 1989,5( 1 ) :32 -37.
  • 9Gobbo-Ferrcira J,Silva M G,Carvalho J A. Performance of an ex- perimental polyethylene solid fuel ramjet [ J]. Acta Astronautica, 1999, 45(1): 11-18.
  • 10Zarzecki M, Quintiere J G, Lyon R E, et al. The effect of pressure and oxygen concentration on the combustion of PMMA[ J]. Com- bustion and Flame, 2013, 160($) : 1519 -1530.

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二级引证文献9

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