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吸气式高超声速机动飞行样式及其关键技术分析

段鹏飞 高书亮 王恩亮 王瀚

航空兵器2024,Vol.31Issue(2):99-105,7.
航空兵器2024,Vol.31Issue(2):99-105,7.DOI:10.12132/ISSN.1673-5048.2024.0028

吸气式高超声速机动飞行样式及其关键技术分析

Analysis of Air-Breathing Hypersonic Maneuver Flight Styles and Key Technologies

段鹏飞 1高书亮 2王恩亮 2王瀚2

作者信息

  • 1. 航空工业未来机载武器技术协同创新中心,北京 100029||中国航空研究院,北京 100029||中国空空导弹研究院,河南 洛阳 471009||北京航空航天大学,北京 100191
  • 2. 航空工业未来机载武器技术协同创新中心,北京 100029||中国航空研究院,北京 100029
  • 折叠

摘要

Abstract

The maneuver flight performance is one of the key capabilities to ensure the implementation of various applications for air-breathing hypersonic aircraft.This article focuses on the study of the maneuverability characteristics of air-breathing hypersonic aircraft.Firstly,the development trend of foreign air-breathing hyper-sonic aircraft is analyzed,and a preliminary analysis is conducted on their typical maneuverability levels and maneuverability styles.Taking the current typical hypersonic missile project in the United States as an example,the typical maneuverability application patterns of air-breathing hypersonic aircraft are summarized.On this ba-sis,key supporting technologies for ensuring and improving the maneuverability of air-breathing hypersonic air-craft are analyzed from the aspects of overall design,aerodynamic shape,flight engine integration,guidance control,and multi-field coupling.

关键词

高超声速飞行器/吸气式/机动能力/气动外形/飞发一体/制导控制/多场耦合

Key words

hypersonic vehicle/air-breathing/maneuverability/aerodynamic shape/flight engine integra-tion/guidance control/multi-field coupling

分类

军事科技

引用本文复制引用

段鹏飞,高书亮,王恩亮,王瀚..吸气式高超声速机动飞行样式及其关键技术分析[J].航空兵器,2024,31(2):99-105,7.

基金项目

省部级基金项目(2022-JCJX-JJ-1X40) (2022-JCJX-JJ-1X40)

航空兵器

OA北大核心CSTPCD

1673-5048

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