摘要
基于发动机稳定性考虑,回顾了超音速战斗机进气装置的发展历程,并阐述了高性能战斗机所面临的进气装置一体化设计问题,重点分析了国外先进战斗机进气装置在布局型式、结构、附面层控制等方面的一体化设计特点及其卓越性能,最后得出一些有益于解决我国在研新机以及老机的改进改型面临的推进系统稳定性问题的结论和启示。
This paper reviews the development of air induction system of supersonic fighter,expounds some integration design problems of inlet and mainly analyzes the integration design characteristics and excellent performance of the foreign advanced active fighter's air induction system on layout style, structure and the control of boundary layer. All the analysis is based on the consideration of engine's stability. Finally, to the developing or developed fighter of our country, some useful conclusions and inspirations to resolve the stability problems of propulsion system are proposed.
出处
《空军工程大学学报（自然科学版）》
CSCD
2003年第1期4-7,共4页
Journal of Air Force Engineering University(Natural Science Edition)
