保外形进气道研究及应用现状  

Research and Application Status of Conformal Inlet

作　　者：史鲲[1] 梁晓庚[1] 

机构地区：[1]西北工业大学自动化学院

出　　处：《航空制造技术》2014年第4期74-76,85,共4页Aeronautical Manufacturing Technology

摘　　要：为解决常规外露式进气道给飞行器带来的飞行阻力增大和隐身能力变差的问题,对保外形进气道的几种设计思路进行了探讨。重点综述了埋入式进气道的设计思想、研究与应用现状,分析了将保外形进气道应用在高速大机动战术导弹上的主要难点和亟待解决的问题。最后对埋入式进气道在战术导弹上的应用前景进行了展望。In order to solve the increase of re-sistance and the decrease of stealth abilities caused by the conventional exposed inlet, several design methods of the conformal inlet are discussed and compared. The design ideologies, the research and application status of sub-merged inlet are reviewed specially. The main dififculties of the application of conformal inlet on high-speed tactical missile are analyzed. Looking to the future, the application of submerged inlet has broad prospects.

关 键 词：保外形进气道 埋入式进气道 研究应用现状 战术导弹 

分 类 号：TJ760.3[兵器科学与技术—武器系统与运用工程]