机载高超声速飞行器中的轴对称旋成体气动布局研究综述  

Review of Aerodynamic Layout of Axisymmetric Rotating Body in Airborne Hypersonic Vehicle

作　　者：王奕权 曹军伟 袁成 Wang Yiquan;Cao Junwei;Yuan Cheng(Chinese Aeronautical Establishment,Beijing 100029,China)

机构地区：[1]中国航空研究院,北京100029

出　　处：《航空科学技术》2023年第4期11-20,共10页Aeronautical Science & Technology

摘　　要：气动布局设计是机载高超声速飞行器总体设计的必要内容之一,轴对称旋成体布局作为一种机载飞行器应用的主流布局形式之一,有着极为重要的研究价值。本文从总体和气动的视角概述了三款使用轴对称旋成体布局的机载高超声速飞行器。分析了采用此种布局的飞行器在研发过程中可能遇到的难题和阻碍,并站在工程应用的角度给出了解决这些难题和阻碍的手段。最后,展望了轴对称旋成体布局的机载高超声速飞行器在未来的发展趋势,为国内机载高超声速飞行器的研制工作提供借鉴与参考。Aerodynamic layout design is one of the essential contents of the overall design of airborne hypersonic vehicle.As one of the main layout forms of airborne vehicle application,axisymmetric rotational body layout has very important research value.In this paper,three airborne hypersonic vehicles using axisymmetric rotational body layout are summarized from the overall and aerodynamic perspectives.The problems and obstacles that may be encountered in the development of the aircraft with this layout are analyzed,and the means to solve these problems and obstacles are given from the perspective of engineering application.The future development trend of airborne hypersonic vehicle with axisymmetric rotational body layout is prospected in order to provide reference for domestic airborne hypersonic vehicle development.

关 键 词：高超声速 轴对称旋成体 机载武器 气动布局 

分 类 号：V221[航空宇航科学与技术—飞行器设计]