弹用航空发动机尾喷流红外抑制技术研究

推进技术 ›› 1996, Vol. 17 ›› Issue (4): 17-20.

弹用航空发动机尾喷流红外抑制技术研究

翟普,隋俊友,崔杰,赵克云,孙华,徐祥春

北京机电工程研究所;北京机电工程研究所;北京机电工程研究所;北京机电工程研究所;北京机电工程研究所;北京机电工程研究所

发布日期:2021-08-15

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

Beijing Electro-Mechanical Engineering Inst., Beijing, 100074;Beijing Electro-Mechanical Engineering Inst., Beijing, 100074;Beijing Electro-Mechanical Engineering Inst., Beijing, 100074;Beijing Electro-Mechanical Engineering Inst., Beijing, 100074;Beijing Electro-Mechanical Engineering Inst., Beijing, 100074;Beijing Electro-Mechanical Engineering Inst., Beijing, 100074

Published:2021-08-15

摘要/Abstract

摘要： 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。

关键词: 航空发动机;喷管气流;红外特征;红外抑制

Abstract: 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.

Key words: Aircraft engine;Nozzle gas flow;Infrared signature;Infrared suppression

翟普,隋俊友,崔杰,赵克云,孙华,徐祥春. 弹用航空发动机尾喷流红外抑制技术研究[J]. 推进技术, 1996, 17(4): 17-20.

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

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