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加速度对丁羟推进剂燃速影响的研究 被引量:6

Study of the Acceleration Effects on the Burning Rate of HTPB Propellant
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摘要 通过试验研究了加速度场中丁羟推进剂的燃速的加速度敏感性。另外从加速度力作用下燃烧区压缩导致热反馈增大角度出发 ,建立了加速度条件下推进剂稳态燃烧模型 ,并编程计算、分析了影响推进剂燃速敏感性的因素 。 In the paper, the acceleration effects on the burning rate of HTPB propellant are presented. Through the experiments of motors in the acceleration field, the experimental data can be got, inclouding the effects of the acceleration level and the acceleration orientation. Then based on the phenomenological model and multi flame of BOP model, the model of the burning rate augmentation in the acceleration field has been built. The experimental data and the model data are uniform. The model can be available for reference to the qualitative analysis of the design of SRM.
作者 郭彤 侯晓
出处 《火炸药学报》 CAS CSCD 2001年第1期30-32,共3页 Chinese Journal of Explosives & Propellants
关键词 固体推进剂 丁羟推进剂 加速度 燃速 稳态燃烧模型 Solid propellant motor Acceleration Burning rate Model of burning rate augmentation
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参考文献3

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同被引文献34

  • 1方蜀州,胡克娴.固体火箭发动机三维药柱燃面推移仿真技术及燃面通用计算方法[J].固体火箭技术,1993,16(4):10-20. 被引量:4
  • 2张如洲,李葆江,郑晓平,耿青涛.含铝复合推进剂在加速度场中燃烧的试验研究[J].推进技术,1989,10(4):46-49. 被引量:5
  • 3刘世东.过载对固体火箭发动机影响的研究[J].航空兵器,2006,13(6):42-44. 被引量:7
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