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弹道与气动力技术

弹道导弹燃气弹射技术

  • 程洪杰 ,
  • 陈力 ,
  • 林睿
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  • 火箭军工程大学兵器发射理论与技术国家重点学科实验室,西安 710025

程洪杰(1978-),男,山东定陶人,副教授,硕士生导师,博士,研究方向:导弹发射理论与技术。

收稿日期: 2016-09-11

  网络出版日期: 2025-05-28

基金资助

国家自然科学基金(51475462)

Gas Ejection Technology of Ballistic Missile

  • CHENG Hongjie ,
  • CHEN Li ,
  • LIN Rui
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  • State Key Subject Laboratory of Weapon Launching Theory and Technology, Rocket Force University of Engineering, Xi'an 710025, China

Received date: 2016-09-11

  Online published: 2025-05-28

摘要

对近年来弹道导弹燃气弹射技术的研究进展和现存问题进行了综述。简述了弹射技术的需求背景和发展历程,重点探讨了燃气弹射技术的零维内弹道模型、多维数值模拟和缩比实验等3种研究方法的进展现状,总结了结构和环境影响因素对内弹道性能的影响机理及结构设计优化方法。从多变量耦合、现代智能算法在线优选结构参数、建立一体化内弹道模型、多相流以及低燃温推进剂5个方面指出了尚存在的问题及发展趋势。

本文引用格式

程洪杰 , 陈力 , 林睿 . 弹道导弹燃气弹射技术[J]. 弹箭与制导学报, 2017 , 37(4) : 109 -112 . DOI: 10.15892/j.cnki.djzdxb.2017.04.026

Abstract

The research progress and existing problems of gas ejection technology of ballistic missile in recent years were reviewed in this article. The demand background and development process of ejection technology were introduced briefly, and the progress status of three kinds of research methods for gas ejection technology, such as zero-dimensional internal ballistic model, multi-dimensional numerical simulation and scaling experiment was discussed, and the influence mechanism of the structural and environmental factors on internal ballistic performance and optimization method of structural design were summarized. The existing problems and development trends were pointed out from five aspects, which including multivariable coupling, online optimization configuration parameters of modern intelligent algorithms, establishment of integrated internal ballistic model, multiphase flow and low burning temperature propellant.

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参考文献

[1]
李广裕. 战略导弹弹射技术的发展[J]. 导弹与航天运载技术, 1990(7):38-49.
[2]
谭大成. 弹射内弹道学[M]. 北京: 北京理工大学出版社, 2015:2-3.
[3]
袁曾凤. 火箭导弹弹射内弹道学[M]. 北京: 北京工业学院出版社, 1987:112-432.
[4]
谢伟, 王汉平. 提拉式弹射内弹道特性的影响因素分析[J]. 固体火箭技术, 2016, 39(1):146-450.
[5]
王志健,杜佳佳.动网格在固体火箭发动机非稳态工作过程中的应用[J]. 固体火箭技术,2008,31(4):350-353.
[6]
王天辉,陈庆贵,何超. 燃气发生器内弹道设计计算[J]. 现代防御技术,2014,42(2) :56-60.
[7]
牛钰森. 自弹式发射内弹道流场特性研究[D]. 北京:北京理工大学,2016:111-114.
[8]
郝晓琴,毕世华. 高速导弹弹射内弹道优化设计研究[J]. 弹箭与制导学报,2005,25(3):520-523.
[9]
刘可平. 某型弹射器高/低温工作特性研究[D].上海:上海交通大学,2008:61-71.
[10]
EDQUIST C T. Prediction of the launch pulse for gas-generator-launched missiles[J]. Journal of Propulsion and Power,1990,6(6):705-712.
[11]
杨文,屠小昌,陈静,等. 某小型弹体发射系统低压发射室降压方案研究[J]. 火工品,2016(1) :1-5.
[12]
白鹏英,乔军. 双级气缸式弹射装置内弹道分析[J]. 现代防御技术,2007,35(4) :44-49.
[13]
惠卫华,鲍福廷,刘旸. 考虑低燃温燃气发生器试验的弹射器内弹道性能预示[J]. 固体火箭技术,2013, 36(6):715-719.
[14]
LIU Yongquan,XI Anmin,LIU Hongfei,et al. An interior ballistic simulation of the gas-steam missile ejection[C]//IEEE. 2010 Wase International Conference on Information Engineering.[S.l.]:IEEE,2010:235-237.
[15]
LIU Y Q,XI A M,LIU H F. Numerical study of interior trajectory of missile ejection based on mechanics[J]. Advanced Materials Research,2012,485:616-619.
[16]
赵雁鹏,王学智,刘少伟,等. 垂直弹射系统弹射初始阶段内流场数值分析[J]. 空军工程大学学报(自然科学版) ,2014,15(4) :5-8.
[17]
谭大成,苗佩云. 弹射器低压室二维内弹道模型及数值研究[J]. 弹箭与制导学报,2006,26 (4):224-226.
[18]
张光喜,周为民,张钢锤,等. 固体火箭发动机尾焰流场特性研究[J]. 固体火箭技术,2008,31(1):19-23.
[19]
胡晓磊,乐贵高,李仁凤,等. 燃气弹射发射筒内燃气-空气二次燃烧现象研究[J]. 弹道学报,2014,26(4):76-81.
[20]
胡晓磊,王辉,乐贵高,等. 二次燃烧对燃气弹射载荷和内弹道影响数值研究[J]. 固体火箭技术,2015,38(6):776-781.
[21]
李仁凤,乐贵高,马大为. 燃烧产物特性对燃气弹射内弹道与载荷的影响研究[J]. 兵工学报,2016,37(2):245-252.
[22]
胡晓磊,乐贵高,马大为,等. 环形腔对燃气弹射初容室二次燃烧影响数值研究[J]. 兵工学报,2015,36(6):1024-1032.
[23]
李仁凤,乐贵高,马大为,等. 壁面障碍物对燃气弹射流场和内弹道的影响[J]. 固体火箭技术,2016,39(3):444-450.
[24]
郝海鹏. 同心筒内气流特性的实验与数值研究[D]. 北京:北京理工大学,2016.
[25]
吕翔,李江,陈剑,等. 变深度水下发射系统内弹道实验研究[J]. 固体火箭技术,2012,35(1):24-28.
[26]
邵徉. 发射筒内弹道的相似准则[J]. 导弹与航天运载技术,1995(1):58-68.
[27]
CHENG C,ZHANG X. Numerical modeling and investigation of two-phase reactive flow in a high-low pressure chambers system[J]. Applied Thermal Engineering, 2016,99:244-252.
[28]
SHAFQAT W,XIE K,LIU Y. Numerical simulation of multi-phase combustion flow in solid rocket motors with metalized propellant[J]. Journal of Aerospace Power, 2009,24(7) :1654-1660.
[29]
PRICE E W,SIGMAN R K. Combusion of aluminized solid propellants[M].[S.l.]:AIAA,2000:663-687.
[30]
DRAZIN P G,REID W H. Hydrodynamic stability[M]. Cambridge:The Press Syndicate of the University Press,2004.
[31]
刘丛林,郜冶,贺征. 铝颗粒在多相流中燃烧的数值模拟[J]. 弹箭与制导学报,2012,32(3) :118-120.
[32]
RASHAD M,ZHANG X B,SADEK H E. Interior ballistics two-phase reactive flow model applied to large caliber guided projectile-gun system[J]. Advances in Mechanical Engineering,2014,2014(2):677-681.
[33]
乔应克,鲁国林. 导弹弹射用低温燃气发生剂技术研究[C]//中国宇航学会:中国宇航学会固体火箭推进 第22届年会论文集(推进剂分册). [出版地不详]:[出版者不详],2005:194-198.
[34]
秦能,贾延斌. 过渡金属催化剂对低燃温双基推进剂性能的影响[J]. 火炸药学报,2014,37(2):73-77.
[35]
吴雄岗,李笑江,宋桂贤,等. 铝粉粒径对改性双基推进剂燃烧性能的影响[J]. 火炸药学报,2010,33(3):80-83.
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