首页 | 本学科首页   官方微博 | 高级检索  
     

固体推进剂非线性压强耦合响应特性实验研究
引用本文:金秉宁,刘佩进,魏少娟.固体推进剂非线性压强耦合响应特性实验研究[J].含能材料,2019,27(4):290-296.
作者姓名:金秉宁  刘佩进  魏少娟
作者单位:西北工业大学 燃烧热结构与内流场重点实验室,陕西 西安 710072;西北工业大学 燃烧热结构与内流场重点实验室,陕西 西安 710072;西北工业大学 燃烧热结构与内流场重点实验室,陕西 西安 710072
基金项目:国家自然科学基金51706186国家自然科学基金(51706186)
摘    要:为获得固体推进剂非线性压强耦合响应特性,建立了一种非线性压强耦合响应函数的实验测量方法,分别对三种含铝复合推进剂开展了非线性压强耦合响应函数(Rp)的实验研究,获得了推进剂非线性压强耦合响应特性,深入分析了非线性压强耦合响应的影响因素。结果表明,提高触发激励压强以及改变触发激励方式,可以在T型燃烧器中模拟与实际发动机非线性燃烧不稳定相类似的非线性压强振荡特性,从而获得固体推进剂非线性压强耦合响应特性。非线性压强耦合响应函数对轴向各阶频率振荡幅值的变化较为敏感,峰值频率附近的响应值对振荡幅值的变化最为敏感,响应值变化最大,其中响应函数峰值从0.4增大到1.12。中间位置触发激励产生的二阶频率响应值与线性法长度减半对应的一阶频率响应值有明显的不同,进一步验证了线性法和非线性测量结果本质区别。

关 键 词:固体发动机  非线性燃烧不稳定  固体推进剂  压强耦合响应  实验测量
收稿时间:2018/12/17 0:00:00
修稿时间:2019/2/28 0:00:00

Experiments on the Characteristic of the Nonlinear Combustion Response Functions of Solid Propellants
JIN Bing-ning,LIU Pei-jin and WEI Shao-juan.Experiments on the Characteristic of the Nonlinear Combustion Response Functions of Solid Propellants[J].Chinese Journal of Energetic Materials,2019,27(4):290-296.
Authors:JIN Bing-ning  LIU Pei-jin and WEI Shao-juan
Abstract:In order to obtain the characteristics of nonlinear pressure coupling response of solid propellants, a method for measurement of the nonlinear pressure coupling response function of solid propellants was established. The nonlinear pressure coupling response functions of three formulations of aluminum propellants were obtained. The characteristics of the nonlinear pressure coupling response of propellants were also analyzed in detail. It indicates that with increase of the trigger pressure, higher-order frequency oscillations can be excited and the amplitude of nonlinear oscillation could be larged as well. By triggering at the both ends of the chamber, the oscillation is dominated by the longitudinal first-order frequency, but when triggering in the chamber middle, the oscillation is dominated by the longitudinal second-order frequency.The nonlinear pressure coupling response function is sensitive to the amplitude of the oscillation, whereas the response value near the peak frequency is the most sensitive to the change of the amplitude of the oscillation. The response value is significantly different between the second-order frequency by triggering in the chamber and the first-order frequency by triggering at end of the half-length chamber. This result just verifies the method of the linear and nonlinear methods are different.
Keywords:solid rocket motor  nonlinear combustion instability  solid propellant  combustion response  T-burner experimental measurement
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《含能材料》浏览原始摘要信息
点击此处可从《含能材料》下载全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号