推进技术 ›› 1991, Vol. 12 ›› Issue (1): 57-62.

• • 上一篇    下一篇

固体推进剂喷气羽烟对微波衰减的理论模拟

彭培根,柳青   

  1. 国防科学技术大学;国防科学技术大学
  • 发布日期:2021-08-15

THEORETICAL MODEL OF MICROWAVE ATTENUATION FOR EXHAUST PLUME OF SOLID PROPELLANTS

  1. National University of Defence Technology;National University of Defence Technology
  • Published:2021-08-15

摘要: 本文根据流体力学理论和等离子体知识,建立了推进剂喷气羽烟电磁特性的理论模型,并利用非平衡化学反应模拟了二次燃烧和电子捕获剂对喷气羽烟电磁特性的影响.计算值与实验结果的一致性较好,误差的最大值约为10%.模拟计算表明:添加少量电子捕获剂和降低铝粉含量,能有效地改善喷气羽烟的微波透射性.

关键词: 排气尾迹;模拟;计算;微波衰减

Abstract: Based on the theory of fluid mechanics and the knowledge of plasma a theoretical model of electromagnetive properties of propellant exhaust plume is developed.The effect of afterburning or electron-capturing additives on electromagnetive properties of exhaust plume is modeled by application of the model together with noneqibibrium chemistry reactions. The calculation coincides with the experimental results well,the maximum error is about 10%.The calculation results showed that microwave attenuation can be reduced by additives of capturing free electron and reducing quantity of aluminium.

Key words: Exhaust trail;Simulation;Calculation;Microwave attenuation