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高超声速再入钝头体飞行走廊等离子体化学反应分析

关山月 田正雨 谢文佳 付黔粤 褚雨航 朱家俊

航空学报2025,Vol.46Issue(18):20-34,15.
航空学报2025,Vol.46Issue(18):20-34,15.DOI:10.7527/S1000-6893.2025.31735

高超声速再入钝头体飞行走廊等离子体化学反应分析

Analysis of plasma chemical reactions of hypersonic reentry blunt in flight corridor

关山月 1田正雨 1谢文佳 1付黔粤 1褚雨航 1朱家俊2

作者信息

  • 1. 国防科技大学 空天科学学院,长沙 410073
  • 2. 湖南大学 材料科学与工程学院,长沙 410082
  • 折叠

摘要

Abstract

During hypersonic atmospheric entry,vehicles encounter the"blackout"phenomenon,which severely af-fects communications.To accurately simulate the plasma flow field,it is essential to rely on accurate chemical reaction models.However,the applicability range of existing models has not been fully defined.This study employs sensitivity analysis to analyze the stagnation line flow field of the spherical nose in the flight corridor,aiming to evaluate five ion-ization reactions.The study finds that,in the altitude range of 58-64 km and Mach number range of 11-15,only the associative ionization reaction of nitrogen(N)and oxygen(O)atoms needs to be considered.In the altitude range of 64-70 km and Mach number range of 15-19,in addition to the associative ionization reaction of N and O atoms,the associative ionization reaction of O atoms must also be considered.Furthermore,in the altitude range of 64-70 km and Mach number range of 19-22,the associative ionization reaction between N atoms also become significant.Within the flight altitude range of 60-70 km and Mach number range of 22-26,it is necessary to consider the electron-impact ionization reactions of N and O atoms.Meanwhile,all ionization reactions should be taken into account.This study provides important theoretical basis and reference for the selection and application of chemical reaction models,contributing to improving the accuracy and reliability of plasma flow field simulation for re-entry vehicles.

关键词

高超声速/黑障/等离子体流场/化学反应模型/电离反应/灵敏度分析

Key words

hypersonic/blackout/plasma flow/chemical reaction model/ionization reaction/sensitivity analysis

分类

航空航天

引用本文复制引用

关山月,田正雨,谢文佳,付黔粤,褚雨航,朱家俊..高超声速再入钝头体飞行走廊等离子体化学反应分析[J].航空学报,2025,46(18):20-34,15.

基金项目

国防基础科学研究计划(JCKY2022110C069) (JCKY2022110C069)

国家自然科学基金(12202490) (12202490)

湖南省自然科学基金(2024JJ6455,11472004) National Defense Basic Scientific Research Program of China(JCKY2022110C069) (2024JJ6455,11472004)

National Natural Science Foundation of China(12202490) (12202490)

Natural Science Foundation of Hunan Province(2024JJ6455,11472004) (2024JJ6455,11472004)

航空学报

OA北大核心

1000-6893

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