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固体推进剂裂纹扩展研究综述
引用本文:胡松启,周宴星,刘迎吉,陈静.固体推进剂裂纹扩展研究综述[J].火箭推进,2012,38(5):86-92.
作者姓名:胡松启  周宴星  刘迎吉  陈静
作者单位:1. 西北工业大学,陕西西安,710072
2. 中国人民解放军第二炮兵部队,内蒙古自治区呼和浩特,010010
摘    要:介绍国内外关于固体推进剂裂纹扩展的研究现状,总结固体推进剂裂纹扩展的试验研究和理论分析方法,归纳影响固体推进剂裂纹扩展的各种因素。分析认为:采用拉伸装置研究有裂纹推进剂力学性能和利用高速摄影系统研究裂纹燃烧和扩展情况是当前主要的研究手段;发动机燃烧室内压力、升压速率、裂纹形状尺寸和推进剂燃速是装药裂纹扩展的重要因素;必须进一步开展各因素和裂纹扩展的定量关系研究。

关 键 词:固体推进剂  裂纹扩展  增压速率  对流燃烧  断裂韧性

Studies on crack extension in solid propellant
HU Song-qi,ZHOU Yan-xing,LIU Ying-ji,CHEN Jing.Studies on crack extension in solid propellant[J].Journal of Rocket Propulsion,2012,38(5):86-92.
Authors:HU Song-qi  ZHOU Yan-xing  LIU Ying-ji  CHEN Jing
Institution:1. Northwestern Polytechnical University, Xi' an 710072, China; 2. Second Artillery Forces of PLA, Huhhot 010010, China)
Abstract:The research status of the crack extension in solid propellant at home and abroad are introduced. Experimental study and theoretical analysis of the crack extension in solid propellant are summarized. The advantages and disadvantages of such study are analyzed. The influences of various factors on crack extension in solid propellant are generalized. The results show that the tension ma- chine and high-speed photography are main means for studying the mechanics characteristic of pro- pellant with crack, and the combustion property of propellant and the extension of crack; the working pressure in combustion chamber, pressure boost rate, style and size of crack, and burning rate of pro- pellant arc the important factors for the crack extension in solid propellant. It is pointed out that it is necessary to research the quantitative relationship between various factors and crack extension.
Keywords:solid propellant  crack extension  pressure boost rate  convective combustion  fracture toughness
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