Investigation on Enhancement of AP/HTPB/Al Composite Solid Propellant Combustion Characteristics via DC Electric Field

被引:0
|
作者
Huang, Xing [1 ]
Gan, Yunhua [1 ]
Ao, Wen [2 ]
Chen, Ningguang [1 ]
Luo, Yanlai [1 ]
Jiang, Zhengwei [1 ]
机构
[1] South China Univ Technol, Sch Elect Power Engn, Wushan Rd, Guangzhou 510640, Peoples R China
[2] Northwestern Polytech Univ, Internal Flow & Thermostructure Lab, Sci & Technol Combust, Xian, Peoples R China
基金
中国国家自然科学基金;
关键词
Solid propellant; DC electric field; burning rates; sandwich model; combustion mechanism; ROCKET-MOTOR; COUPLED SIMULATION; IGNITION TRANSIENT; VARIABLE-THRUST; MODEL; ALUMINUM;
D O I
10.1080/00102202.2024.2393670
中图分类号
O414.1 [热力学];
学科分类号
摘要
To investigate the influence mechanisms of DC electric fields on the combustion of solid propellants, a numerical model for the combustion characteristics of AP/HTPB/Al composite solid propellant under the DC electric field is established. Effects of the applied electric field on combustion flame structure, combustion surface temperature distribution, and mixing fraction distribution are analyzed. The results indicate that the applied electric field enhances the mixing effect of the propellant gas phase decomposition products, thereby altering the flame structure and bringing it closer to the combustion surface. The application of the electric field leads to an increase in the combustion surface temperature by 20-70 K. The effect of the negative electric field on the combustion surface temperature and burning rate is more significant compared to that of the positive electric field. The results provide valuable theoretical guidance in the field of solid engine combustion control. [GRAPHICS]
引用
收藏
页数:20
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