弹用航空发动机尾喷流红外抑制技术研究

A RESEARCH ON RADIATION RESTRICTION TECHNIQUE OF A NOZZLE FLOW OF AERO-ENGINE FOR MISSILE

详细介绍了弹用航空发动机红外抑制技术开展的一系列试验和数值分析。这些工作均取得了较好的结果，为今后此项技术的进一步深入研究直至工程应用打下了良好的基础。

In this paper experiments and the numerical analyses about infrared restriction technique of aero-engine is described in detail. Satisfactory results are obtained, which lay a good functionfor the future research and application.