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固体燃料冲压增程炮弹力学分析 被引量:1

Dynamic Analysis of a Solid Fuel Ramjet Assisted Projectile
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摘要 采用有限元法对某固体燃料冲压增程炮弹及其零部件在火炮膛内的结构完整性进行了系统分析.建立了三维有限元模型,研究了高过载下各部件受轴向、径向和切向惯性力综合作用下的应力、应变分布.结果表明,中心锥支座和堵盖处应力集中严重,在初步设计时必须重点考虑;增大支柱宽度和厚度有利于降低最大应力;其他零部件的应力、应变均能满足强度要求.该研究为固体燃料冲压增程炮弹的结构设计提供了有用依据. The finite element method(FEM) was used to analyze structural integrality of solid fuel ramjet(SFRJ) extended-range projectile and its components in chamber.The three-dimension FEM models of SFRJ extended-range projectile and its components were established.The stress and strain distributions of all the components affected by axial inertial force,radial inertial force and tangential inertial force together,were investigated.Results show that the stress around bearings of central cone and port cover concentr...
出处 《弹道学报》 EI CSCD 北大核心 2010年第1期49-52,64,共5页 Journal of Ballistics
关键词 固体燃料 冲压发动机 增程炮弹 应力 应变 有限元法 solid fuel ramjet extended-range projectile stress stain finite element method
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参考文献5

  • 1崔平.现代炮弹增程技术综述[J].四川兵工学报,2006,27(3):17-19. 被引量:5
  • 2郑颖建.高过载下固体火箭发动机药柱结构的完整性分析[D]哈尔滨工程大学,哈尔滨工程大学2005.
  • 3S. Krishnan,and Philmon George.Solid Fuel Ramjet Combustor Design. Aerospace Science . 1998
  • 4Oosthuizen R,Stockenstr m A,Buisson J J.Solid fuel ramjet(SFRJ)propulsion for artillery projectile applications concept de-velopment overview. 20thInternational Symposiumon Ballis-tics . 2002
  • 5Drysdale,W. H.Design of Kinetic Energy Projectiles for Structural Integrity. AD—A 105502 .

共引文献4

同被引文献15

  • 1吴护林.炮弹增程技术的发展[J].四川兵工学报,2005,26(5):3-6. 被引量:5
  • 2向敏,张为华,王中伟.冲压增程炮弹发动机工作性能分析[J].弹箭与制导学报,2006,26(4):185-187. 被引量:4
  • 3张玲翔.美国弹用冲压发动机技术的进展[J].飞航导弹,1998,(11).
  • 4Ronalds Fry. A Century of Ramjet Propulsion Technology Evolution[J]. Journal of Propulsion and Power, 2004, 20(1): 27-58.
  • 5单益义.冲压炮弹的发展及前景.现代兵器,1987,:1-5.
  • 6杨小平.先进的间接瞄准系统(AIFS)-远程末端制导炮弹.现代兵器,1984,:34-36.
  • 7Chen Xiong, Zhou Changsheng, Zheng Ya. Influence of Cowl Leading Edge on Inlet Performance of Ramjet Assisted-Range Projectiles[R]. America: AIAA, 2005: 2005-3642.
  • 8Chen Xiong, Zheng Ya, Zhou Changsheng. Numerical Simulation on Ramjet Inlet with different Cowl Leading Edge[R]. America: AIAA, 2005: 2005-5288.
  • 9Chen Xiong, Zheng Jian, Liang Hua. Experimental and Numerical Research on Inlet of Ramjet Assisted-range Projectile[R]. America: AIAA, 2007: 2007-5010.
  • 10张磊,周长省,鞠玉涛.冲压增程炮弹发动机补燃室内流场分析[J].系统仿真学报,2008,20(20):5480-5483. 被引量:2

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