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吸气式超声速巡航导弹进气道现状及发展趋势

evelopment of the Ramjet Inlet for Air-breathing Supersonic Cruise Missile

中文摘要英文摘要

吸气式超声速巡航导弹是未来导弹发展的一个重要方向。本文针对吸气式超声速巡航导弹的研究现状归纳了其采用的进气道型式。结合吸气式超声速巡航导弹的发展趋势来看,进气道将向与弹体一体化设计的方向发展,并满足导弹的远射程、隐身性、宽工作范围、高机动和多用途等的发展需求。其进气道设计的关键技术是高性能定几何混压式进气道设计技术、非常规外形参数下的常规进气道设计技术、定几何混压式进气道的自起动/再起动问题、变几何进气道的设计技术以及多模块进气道的耦合影响问题等。根据目前国内的研究现状,建议进气道的基础研究工作是建立进气道及其布局型式的气动性能数据库,开展简单流场控制方法研究和变几何进气道设计并结合某些导弹的特殊作战任务要求进行非常规进气道设计。

ir-breathing supersonic cruise missile is one importance part of missile in the future. The inlet types and layout on missile is reviewed in this paper. Combined with air-breathing supersonic cruise missile development, designed Ramjet inlet will be incorporated in missile, at the same time, meet with long-rang, stealth, wide flight range, maneuverability and all-purpose missile. Designed high performance inlet with fixed-geometry, designed conventional inlet based on unconventional shape, selfstarted/restarted technology of inlet with fixed-geometry, designed variable geometry inlet and coupled poly-inlets etc. are the key issues of ramjet inlet. Based on current position of our country, the advice of inlet foundation research are bring forward which include establishing database of the inlet performance, investigating realizable flow control, designing variable geometry inlet and unconventional inlet.

谢旅荣、郭荣伟

军用火箭、导弹技术航空航天技术

航空、航天推进系统超声速巡航导弹进气道设计发展趋势关键技术

aerospace propulsion systemsupersonic cruise missileinlet designdevelopmentthe key issue

谢旅荣,郭荣伟.吸气式超声速巡航导弹进气道现状及发展趋势[EB/OL].(2012-02-07)[2025-08-21].http://www.paper.edu.cn/releasepaper/content/201202-56.点此复制

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