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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 被引量:1

Analysis of Air-Breathing Hypersonic Maneuver Flight Styles and Key Technologies
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摘要 机动飞行性能是确保吸气式高超声速飞行器实现多种应用的关键能力之一,本文重点对吸气式高超声速飞行器机动能力特点进行研究。首先分析了国外吸气式高超声速飞行器的发展趋势,就其典型机动能力水平和机动样式进行了初步分析,以美国当前典型高超声速导弹项目为例,梳理了吸气式高超声速飞行器的典型机动应用样式。在此基础上,从总体设计、气动外形、飞发一体、制导控制、多场耦合等方面,梳理分析了确保和提升吸气式高超声速飞行器机动能力的关键支撑性技术。 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 hypersonic 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 basis,key supporting technologies for ensuring and improving the maneuverability of air-breathing hypersonic aircraft are analyzed from the aspects of overall design,aerodynamic shape,flight engine integration,guidance control,and multi-field coupling.
作者 段鹏飞 高书亮 王恩亮 王瀚 Duan Pengfei;Gao Shuliang;Wang Enliang;Wang Han(Collaborative Innovation Center for Future Airborne Weapon Technology,AVIC,Beijing 100029,China;Chinese Aeronautical Establishment,Beijing 100029,China;China Airborne Missile Academy,Luoyang 471009,China;Beihang University,Beijing 100191,China)
出处 《航空兵器》 CSCD 北大核心 2024年第2期99-105,共7页 Aero Weaponry
基金 省部级基金项目(2022-JCJX-JJ-1X40)。
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 hypersonic vehicle air-breathing maneuverability aerodynamic shape flight engine integration guidance control multi-field coupling
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